A B C D E F G H I J K L M N O P Q R S T U V W X Y Z 
All Classes All Packages

A

a - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
final semi major axis.
a - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
final semi major axis.
A - org.orekit.gnss.SignalCode
Galileo A PRS / IRNSS A SPS / GLONASS L1OCd and L2CSI / Beidou B1A and B3A codes.
A - Static variable in enum org.orekit.orbits.OrbitType
Name for semi major axis.
A_SBAS - org.orekit.files.rinex.navigation.SbasId
African Satellite-Based Augmentation System (ASECNA).
a0dp - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
original recovered semi major axis.
a0dp - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
original recovered semi major axis.
A2B - Static variable in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints
Constant for A → B diraction.
A3OVK2 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
A3OVK2.
AberrationModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical angular measurement with (the inverse of) stellar aberration.
AberrationModifier() - Constructor for class org.orekit.estimation.measurements.modifiers.AberrationModifier
Empty constructor.
AberrationModifier(DataContext) - Constructor for class org.orekit.estimation.measurements.modifiers.AberrationModifier
Constructor.
AbsoluteDate - Class in org.orekit.time
This class represents a specific instant in time.
AbsoluteDate() - Constructor for class org.orekit.time.AbsoluteDate
Create an instance with a default value (AbsoluteDate.J2000_EPOCH).
AbsoluteDate(int, int, int, int, int, double, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsoluteDate(int, int, int, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsoluteDate(int, Month, int, int, int, double, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsoluteDate(int, Month, int, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsoluteDate(String, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location (parsed from a string) in a time scale.
AbsoluteDate(Instant) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from an instant in utc time scale.
AbsoluteDate(Instant, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
AbsoluteDate(Instant, UTCScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from an instant in the time scale.
AbsoluteDate(Date, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsoluteDate(AbsoluteDate, double) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from an elapsed duration since to another instant.
AbsoluteDate(AbsoluteDate, double, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from an apparent clock offset with respect to another instant in the perspective of a specific time scale.
AbsoluteDate(AbsoluteDate, long, TimeUnit) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from an elapsed duration since to another instant.
AbsoluteDate(DateComponents, TimeComponents, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsoluteDate(DateComponents, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsoluteDate(DateTimeComponents, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsolutePVCoordinates - Class in org.orekit.utils
Position - Velocity - Acceleration linked to a date and a frame.
AbsolutePVCoordinates(Frame, AbsoluteDate, FieldVector3D<U>) - Constructor for class org.orekit.utils.AbsolutePVCoordinates
Builds a AbsolutePVCoordinates triplet from a FieldVector3D<Derivative>.
AbsolutePVCoordinates(Frame, AbsoluteDate, Vector3D, Vector3D) - Constructor for class org.orekit.utils.AbsolutePVCoordinates
Build from position and velocity.
AbsolutePVCoordinates(Frame, AbsoluteDate, Vector3D, Vector3D, Vector3D) - Constructor for class org.orekit.utils.AbsolutePVCoordinates
Build from position, velocity, acceleration.
AbsolutePVCoordinates(Frame, AbsoluteDate, PVCoordinates) - Constructor for class org.orekit.utils.AbsolutePVCoordinates
Build from frame, date and PVA coordinates.
AbsolutePVCoordinates(Frame, TimeStampedPVCoordinates) - Constructor for class org.orekit.utils.AbsolutePVCoordinates
Build from frame and TimeStampedPVCoordinates.
AbsolutePVCoordinates(AbsoluteDate, double, AbsolutePVCoordinates) - Constructor for class org.orekit.utils.AbsolutePVCoordinates
Multiplicative constructor
AbsolutePVCoordinates(AbsoluteDate, double, AbsolutePVCoordinates, double, AbsolutePVCoordinates) - Constructor for class org.orekit.utils.AbsolutePVCoordinates
Linear constructor
AbsolutePVCoordinates(AbsoluteDate, double, AbsolutePVCoordinates, double, AbsolutePVCoordinates, double, AbsolutePVCoordinates) - Constructor for class org.orekit.utils.AbsolutePVCoordinates
Linear constructor
AbsolutePVCoordinates(AbsoluteDate, double, AbsolutePVCoordinates, double, AbsolutePVCoordinates, double, AbsolutePVCoordinates, double, AbsolutePVCoordinates) - Constructor for class org.orekit.utils.AbsolutePVCoordinates
Linear constructor
AbsolutePVCoordinates(AbsoluteDate, AbsolutePVCoordinates, AbsolutePVCoordinates) - Constructor for class org.orekit.utils.AbsolutePVCoordinates
Subtractive constructor
AbsolutePVCoordinatesHermiteInterpolator - Class in org.orekit.utils
Class using a Hermite interpolator to interpolate absolute position-velocity-acceleration coordinates.
AbsolutePVCoordinatesHermiteInterpolator(int, double, Frame, CartesianDerivativesFilter) - Constructor for class org.orekit.utils.AbsolutePVCoordinatesHermiteInterpolator
Constructor.
AbsolutePVCoordinatesHermiteInterpolator(int, Frame) - Constructor for class org.orekit.utils.AbsolutePVCoordinatesHermiteInterpolator
Constructor with : Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of position and two time derivatives during interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).
AbsolutePVCoordinatesHermiteInterpolator(int, Frame, CartesianDerivativesFilter) - Constructor for class org.orekit.utils.AbsolutePVCoordinatesHermiteInterpolator
Constructor with default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s).
AbsolutePVCoordinatesHermiteInterpolator(Frame) - Constructor for class org.orekit.utils.AbsolutePVCoordinatesHermiteInterpolator
Constructor with : Default number of interpolation points of DEFAULT_INTERPOLATION_POINTS Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of position and two time derivatives during interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).
ABSORPTION_COEFFICIENT - Static variable in interface org.orekit.forces.radiation.RadiationSensitive
Parameter name for absorption coefficient.
AbstractAlfriend1999 - Class in org.orekit.ssa.collision.shorttermencounter.probability.twod
Abstract class for Alfriend1999 normal and maximised methods as they share lots of similarities.
AbstractAlfriend1999(String) - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractAlfriend1999
Default constructor.
AbstractAlmanac - Class in org.orekit.propagation.analytical.gnss.data
Base class for GNSS almanacs.
AbstractAlmanac(double, double, int) - Constructor for class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac
Constructor.
AbstractAmbiguityModifier - Class in org.orekit.estimation.measurements.modifiers
Deprecated.
as of 12.1 ambiguity is managed directly by raw measurements Phase, OneWayGNSSPhase and InterSatellitesPhase
AbstractAmbiguityModifier(int, double) - Constructor for class org.orekit.estimation.measurements.modifiers.AbstractAmbiguityModifier
Deprecated.
Constructor.
AbstractAnalyticalGradientConverter - Class in org.orekit.propagation.analytical
Converter for analytical orbit propagator.
AbstractAnalyticalGradientConverter(AbstractAnalyticalPropagator, double, int) - Constructor for class org.orekit.propagation.analytical.AbstractAnalyticalGradientConverter
Constructor.
AbstractAnalyticalMatricesHarvester - Class in org.orekit.propagation.analytical
Base class harvester between two-dimensional Jacobian matrices and analytical orbit propagator.
AbstractAnalyticalMatricesHarvester(AbstractAnalyticalPropagator, String, RealMatrix, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester
Simple constructor.
AbstractAnalyticalPropagator - Class in org.orekit.propagation.analytical
Common handling of Propagator methods for analytical propagators.
AbstractAnalyticalPropagator(AttitudeProvider) - Constructor for class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Build a new instance.
AbstractAnalyticalPropagatorBuilder - Class in org.orekit.propagation.conversion
Abstract class for propagator builders of analytical models (except for ephemeris i.e.
AbstractAnalyticalPropagatorBuilder(Orbit, PositionAngleType, double, boolean, AttitudeProvider, double) - Constructor for class org.orekit.propagation.conversion.AbstractAnalyticalPropagatorBuilder
Build a new instance.
AbstractAveragedOrbitalState - Class in org.orekit.propagation.conversion.averaging
Abstract class representing averaged orbital state.
AbstractAveragedOrbitalState(AbsoluteDate, Frame) - Constructor for class org.orekit.propagation.conversion.averaging.AbstractAveragedOrbitalState
Protected constructor.
AbstractBatchLSModel - Class in org.orekit.estimation.leastsquares
AbstractBatchLSModel(PropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Constructor for class org.orekit.estimation.leastsquares.AbstractBatchLSModel
Constructor.
AbstractBodyAttraction - Class in org.orekit.forces.gravity
Abstract class for non-central body attraction force model.
AbstractBodyAttraction(CelestialBody) - Constructor for class org.orekit.forces.gravity.AbstractBodyAttraction
Simple constructor.
AbstractBuilder<T extends AbstractBuilder<T>> - Class in org.orekit.files.ccsds.ndm
Abstract builder for all CCSDS Message files parsers/writers.
AbstractBuilder(IERSConventions, double, double, DataContext, AbsoluteDate, RangeUnitsConverter) - Constructor for class org.orekit.files.ccsds.ndm.AbstractBuilder
Complete constructor.
AbstractCartesianAdjointDerivativesProvider - Class in org.orekit.control.indirect.adjoint
Abstract class defining common things for Cartesian adjoint dynamics between standard and Field versions.
AbstractCartesianAdjointDerivativesProvider(CartesianCost) - Constructor for class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointDerivativesProvider
Constructor.
AbstractCartesianAdjointEquationTerm - Class in org.orekit.control.indirect.adjoint
Abstract class to define terms in the adjoint equations and Hamiltonian for Cartesian coordinates.
AbstractCartesianAdjointEquationTerm() - Constructor for class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointEquationTerm
 
AbstractCartesianAdjointGravitationalTerm - Class in org.orekit.control.indirect.adjoint
Abstract class for common computations regarding adjoint dynamics and gravity for Cartesian coordinates.
AbstractCartesianAdjointGravitationalTerm(double) - Constructor for class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointGravitationalTerm
Constructor.
AbstractCartesianAdjointNewtonianTerm - Class in org.orekit.control.indirect.adjoint
Abstract class for common computations regarding adjoint dynamics and Newtonian gravity for Cartesian coordinates.
AbstractCartesianAdjointNewtonianTerm(double) - Constructor for class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointNewtonianTerm
Constructor.
AbstractCartesianAdjointNonCentralBodyTerm - Class in org.orekit.control.indirect.adjoint
Abstract class defining the contributions of a point-mass, single body gravity in the adjoint equations for Cartesian coordinates.
AbstractCartesianAdjointNonCentralBodyTerm(double, ExtendedPositionProvider) - Constructor for class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointNonCentralBodyTerm
Constructor.
AbstractCartesianEnergy - Class in org.orekit.control.indirect.adjoint.cost
Abstract class for energy cost with Cartesian coordinates.
AbstractCartesianEnergy(String, double) - Constructor for class org.orekit.control.indirect.adjoint.cost.AbstractCartesianEnergy
Constructor.
AbstractChaoMappingFunction - Class in org.orekit.models.earth.troposphere
Chao mapping function for radio wavelengths.
AbstractChaoMappingFunction(double, double, double, double) - Constructor for class org.orekit.models.earth.troposphere.AbstractChaoMappingFunction
Builds a new instance.
AbstractConstantThrustPropulsionModel - Class in org.orekit.forces.maneuvers.propulsion
This abstract class simply serve as a container for a constant thrust maneuver.
AbstractConstantThrustPropulsionModel(double, double, Vector3D, String) - Constructor for class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Constructor with default control cost type.
AbstractConstantThrustPropulsionModel(double, double, Vector3D, Control3DVectorCostType, String) - Constructor for class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Generic constructor.
AbstractConstituentParser<H extends Header,​T extends NdmConstituent<H,​?>,​P extends AbstractConstituentParser<H,​T,​?>> - Class in org.orekit.files.ccsds.utils.parsing
Parser for CCSDS messages.
AbstractConstituentParser(String, String, IERSConventions, boolean, DataContext, ParsedUnitsBehavior, Function<ParseToken, List<ParseToken>>[]) - Constructor for class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser
Complete constructor.
AbstractCovarianceMatrixProvider - Class in org.orekit.estimation.sequential
Abstract provider handling a predefined initial covariance matrix.
AbstractCovarianceMatrixProvider(RealMatrix) - Constructor for class org.orekit.estimation.sequential.AbstractCovarianceMatrixProvider
Simple constructor.
AbstractCycleSlipDetector - Class in org.orekit.estimation.measurements.gnss
Base class for cycle-slip detectors.
AbstractDetector<T extends AbstractDetector<T>> - Class in org.orekit.propagation.events
Common parts shared by several orbital events finders.
AbstractDetector(double, double, int, EventHandler) - Constructor for class org.orekit.propagation.events.AbstractDetector
Build a new instance.
AbstractDetector(AdaptableInterval, double, int, EventHandler) - Constructor for class org.orekit.propagation.events.AbstractDetector
Deprecated.
as of 12.2
AbstractDetector(EventDetectionSettings, EventHandler) - Constructor for class org.orekit.propagation.events.AbstractDetector
Build a new instance.
AbstractDragForceModel - Class in org.orekit.forces.drag
Base class for drag force models.
AbstractDragForceModel(Atmosphere) - Constructor for class org.orekit.forces.drag.AbstractDragForceModel
Constructor with default value for finite differences flag.
AbstractDragForceModel(Atmosphere, boolean) - Constructor for class org.orekit.forces.drag.AbstractDragForceModel
Constructor.
AbstractDualFrequencyCombination - Class in org.orekit.estimation.measurements.gnss
Base class for dual frequency combination of measurements.
AbstractDualFrequencyCombination(CombinationType, SatelliteSystem) - Constructor for class org.orekit.estimation.measurements.gnss.AbstractDualFrequencyCombination
Constructor.
AbstractEncodedMessage - Class in org.orekit.gnss.metric.parser
Encoded messages as a sequence of bytes.
AbstractEncodedMessage() - Constructor for class org.orekit.gnss.metric.parser.AbstractEncodedMessage
Empty constructor.
AbstractEncounterLOF - Class in org.orekit.frames.encounter
Abstract class for encounter frame between two objects.
AbstractEncounterLOF(FieldPVCoordinates<T>) - Constructor for class org.orekit.frames.encounter.AbstractEncounterLOF
Constructor with FieldPVCoordinates.
AbstractEncounterLOF(PVCoordinates) - Constructor for class org.orekit.frames.encounter.AbstractEncounterLOF
Constructor with PVCoordinates.
AbstractEopLoader - Class in org.orekit.frames
Base class for EOP loaders.
AbstractEopLoader(String, DataProvidersManager, Supplier<TimeScale>) - Constructor for class org.orekit.frames.AbstractEopLoader
Simple constructor.
AbstractEphemerisMessage - Class in org.orekit.propagation.analytical.gnss.data
Base class for ephemeris-based navigation messages.
AbstractEphemerisMessage() - Constructor for class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Constructor.
AbstractFieldIntegratorBuilder<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.conversion
Abstract class for FieldODEIntegratorBuilder.
AbstractFieldIntegratorBuilder() - Constructor for class org.orekit.propagation.conversion.AbstractFieldIntegratorBuilder
Empty constructor.
AbstractFieldOfView - Class in org.orekit.geometry.fov
Abstract class representing a spacecraft sensor Field Of View.
AbstractFieldOfView(double) - Constructor for class org.orekit.geometry.fov.AbstractFieldOfView
Build a new instance.
AbstractFieldOrbitInterpolator<KK extends CalculusFieldElement<KK>> - Class in org.orekit.orbits
Abstract class for orbit interpolator.
AbstractFieldOrbitInterpolator(int, double, Frame) - Constructor for class org.orekit.orbits.AbstractFieldOrbitInterpolator
Constructor.
AbstractFieldTimeInterpolator<T extends FieldTimeStamped<KK>,​KK extends CalculusFieldElement<KK>> - Class in org.orekit.time
Abstract class for time interpolator.
AbstractFieldTimeInterpolator(int, double) - Constructor for class org.orekit.time.AbstractFieldTimeInterpolator
Constructor.
AbstractFieldTimeInterpolator.InterpolationData - Class in org.orekit.time
Nested class used to store interpolation data.
AbstractFixedBoundaryCartesianSingleShooting - Class in org.orekit.control.indirect.shooting
Abstract class for indirect single shooting methods with Cartesian coordinates for fixed time fixed boundary.
AbstractFixedBoundaryCartesianSingleShooting(ShootingPropagationSettings, FixedTimeBoundaryOrbits, CartesianBoundaryConditionChecker) - Constructor for class org.orekit.control.indirect.shooting.AbstractFixedBoundaryCartesianSingleShooting
Constructor with boundary conditions as orbits.
AbstractFixedBoundaryCartesianSingleShooting(ShootingPropagationSettings, FixedTimeCartesianBoundaryStates, CartesianBoundaryConditionChecker) - Constructor for class org.orekit.control.indirect.shooting.AbstractFixedBoundaryCartesianSingleShooting
Constructor with boundary conditions as orbits.
AbstractFixedStepFieldIntegratorBuilder<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.conversion
Abstract class for integrator builder using fixed step size.
AbstractFrames - Class in org.orekit.frames
This class is an implementation of Frames that creates frames when they are first used and uses synchronization to ensure that each frame is only created once.
AbstractFrames(TimeScales, Supplier<Frame>) - Constructor for class org.orekit.frames.AbstractFrames
Simple constructor.
AbstractGaussianContribution - Class in org.orekit.propagation.semianalytical.dsst.forces
Common handling of DSSTForceModel methods for Gaussian contributions to DSST propagation.
AbstractGaussianContribution(String, double, ForceModel, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Build a new instance.
AbstractGaussianContribution.FieldFourierCjSjCoefficients<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.forces
Compute the Cij and the Sij coefficients with field elements.
AbstractGaussianContribution.FieldGaussianShortPeriodicCoefficients<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.forces
This class handles the short periodic coefficients described in Danielson 2.5.3-26.
AbstractGaussianContribution.FieldIntegrableFunction<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.forces
Internal class for numerical quadrature.
AbstractGaussianContribution.FieldSlot<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.forces
Coefficients valid for one time slot.
AbstractGaussianContribution.FieldUijVijCoefficients<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.forces
The Uij and Vij coefficients described by equations 2.5.3-(21) and 2.5.3-(22) from Danielson.
AbstractGaussianContribution.FourierCjSjCoefficients - Class in org.orekit.propagation.semianalytical.dsst.forces
Compute the Cij and the Sij coefficients.
AbstractGaussianContribution.GaussianShortPeriodicCoefficients - Class in org.orekit.propagation.semianalytical.dsst.forces
This class handles the short periodic coefficients described in Danielson 2.5.3-26.
AbstractGaussianContribution.GaussQuadrature - Class in org.orekit.propagation.semianalytical.dsst.forces
Class used to integrate a function of the orbital elements using the Gaussian quadrature rule to get the acceleration.
AbstractGaussianContribution.IntegrableFunction - Class in org.orekit.propagation.semianalytical.dsst.forces
Internal class for numerical quadrature.
AbstractGaussianContribution.Slot - Class in org.orekit.propagation.semianalytical.dsst.forces
Coefficients valid for one time slot.
AbstractGaussianContribution.UijVijCoefficients - Class in org.orekit.propagation.semianalytical.dsst.forces
The Uij and Vij coefficients described by equations 2.5.3-(21) and 2.5.3-(22) from Danielson.
AbstractGaussianContributionContext - Class in org.orekit.propagation.semianalytical.dsst.forces
This class is a container for the common parameters used in AbstractGaussianContribution.
AbstractGenerator - Class in org.orekit.files.ccsds.utils.generation
Base class for both Key-Value Notation and eXtended Markup Language generators for CCSDS messages.
AbstractGenerator(Appendable, String, double, boolean) - Constructor for class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Simple constructor.
AbstractGlobalPressureTemperature - Class in org.orekit.models.earth.weather
Base class for Global Pressure and Temperature 2, 2w and 3 models.
AbstractGlobalPressureTemperature(DataSource, TimeScale, SeasonalModelType...) - Constructor for class org.orekit.models.earth.weather.AbstractGlobalPressureTemperature
Constructor with source of GPTn auxiliary data given by user.
AbstractGlobalPressureTemperature(Grid, TimeScale) - Constructor for class org.orekit.models.earth.weather.AbstractGlobalPressureTemperature
Deprecated.
as of 12.1 used only by GlobalPressureTemperature2Model
AbstractGradientConverter - Class in org.orekit.propagation.integration
Converter for states and parameters arrays.
AbstractGradientConverter(int) - Constructor for class org.orekit.propagation.integration.AbstractGradientConverter
Simple constructor.
AbstractIndirectShooting - Class in org.orekit.control.indirect.shooting
Abstract class for indirect shooting methods with numerical propagation.
AbstractIndirectShooting(ShootingPropagationSettings) - Constructor for class org.orekit.control.indirect.shooting.AbstractIndirectShooting
Constructor.
AbstractIntegratedPropagator - Class in org.orekit.propagation.integration
Common handling of Propagator methods for both numerical and semi-analytical propagators.
AbstractIntegratedPropagator(ODEIntegrator, PropagationType) - Constructor for class org.orekit.propagation.integration.AbstractIntegratedPropagator
Build a new instance.
AbstractIntegratedPropagator.MainStateEquations - Interface in org.orekit.propagation.integration
Differential equations for the main state (orbit, attitude and mass).
AbstractInterSatellitesMeasurement<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.gnss
Base class for measurement between two satellites that are both estimated.
AbstractInterSatellitesMeasurement(AbsoluteDate, double, double, double, ObservableSatellite, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.gnss.AbstractInterSatellitesMeasurement
Constructor.
AbstractKalmanEstimator - Class in org.orekit.estimation.sequential
Base class for Kalman estimators.
AbstractKalmanEstimator(List<? extends PropagatorBuilder>) - Constructor for class org.orekit.estimation.sequential.AbstractKalmanEstimator
Constructor.
AbstractLambdaMethod - Class in org.orekit.estimation.measurements.gnss
Base class for decorrelation/reduction engine for LAMBDA type methods.
AbstractLambdaMethod() - Constructor for class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Constructor.
AbstractLightFluxModel - Class in org.orekit.forces.radiation
Abstract class for light flux models.
AbstractLightFluxModel(ExtendedPositionProvider) - Constructor for class org.orekit.forces.radiation.AbstractLightFluxModel
Constructor.
AbstractLimitedVariableStepFieldIntegratorBuilder<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.conversion
Abstract class for integrator using a limited number of variable steps.
AbstractListCrawler<T> - Class in org.orekit.data
Provider for data files defined in a list.
AbstractListCrawler(T...) - Constructor for class org.orekit.data.AbstractListCrawler
Build a data classpath crawler.
AbstractManeuverTriggers - Class in org.orekit.forces.maneuvers.trigger
Base class for triggers.
AbstractManeuverTriggers() - Constructor for class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers
Simple constructor.
AbstractMatricesHarvester - Class in org.orekit.propagation
Base harvester between two-dimensional Jacobian matrices and one-dimensional additional state arrays.
AbstractMatricesHarvester(String, RealMatrix, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.AbstractMatricesHarvester
Simple constructor.
AbstractMeasurement<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements
Abstract class handling measurements boilerplate.
AbstractMeasurement(AbsoluteDate, double[], double[], double[], List<ObservableSatellite>) - Constructor for class org.orekit.estimation.measurements.AbstractMeasurement
Simple constructor, for multi-dimensional measurements.
AbstractMeasurement(AbsoluteDate, double, double, double, List<ObservableSatellite>) - Constructor for class org.orekit.estimation.measurements.AbstractMeasurement
Simple constructor for mono-dimensional measurements.
AbstractMeasurementBuilder<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.generation
Base class for measurements builders.
AbstractMeasurementBuilder(CorrelatedRandomVectorGenerator, double[], double[], ObservableSatellite...) - Constructor for class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
Simple constructor.
AbstractMeasurementBuilder(CorrelatedRandomVectorGenerator, double, double, ObservableSatellite...) - Constructor for class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
Simple constructor.
AbstractMessageParser<T> - Class in org.orekit.files.ccsds.utils.parsing
Parser for CCSDS messages.
AbstractMessageParser(String, String, Function<ParseToken, List<ParseToken>>[]) - Constructor for class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser
Simple constructor.
AbstractMessageWriter<H extends Header,​S extends Segment<?,​?>,​F extends NdmConstituent<H,​S>> - Class in org.orekit.files.ccsds.utils.generation
Base class for Navigation Data Message (NDM) files.
AbstractMessageWriter(String, String, double, ContextBinding) - Constructor for class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter
Constructor used to create a new NDM writer configured with the necessary parameters to successfully fill in all required fields that aren't part of a standard object.
AbstractMultipleShooting - Class in org.orekit.utils
Multiple shooting method using only constraints on state vectors of patch points (and possibly on epoch and integration time).
AbstractMultipleShooting(List<SpacecraftState>, List<NumericalPropagator>, double, int, boolean, String) - Constructor for class org.orekit.utils.AbstractMultipleShooting
Simple Constructor.
AbstractNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data
Base class for GNSS navigation messages.
AbstractNavigationMessage(double, double, int) - Constructor for class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Constructor.
AbstractOnBoardMeasurement<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.gnss
Base class modeling a measurement where receiver is a satellite.
AbstractOnBoardMeasurement(AbsoluteDate, double, double, double, List<ObservableSatellite>) - Constructor for class org.orekit.estimation.measurements.gnss.AbstractOnBoardMeasurement
Constructor.
AbstractOneWayGNSSMeasurement<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.gnss
Base class for one-way GNSS measurement.
AbstractOneWayGNSSMeasurement(PVCoordinatesProvider, QuadraticClockModel, AbsoluteDate, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.gnss.AbstractOneWayGNSSMeasurement
Simple constructor.
AbstractOrbitInterpolator - Class in org.orekit.orbits
Abstract class for orbit interpolator.
AbstractOrbitInterpolator(int, double, Frame) - Constructor for class org.orekit.orbits.AbstractOrbitInterpolator
Constructor.
AbstractPropagator - Class in org.orekit.propagation
Common handling of Propagator methods for analytical propagators.
AbstractPropagator() - Constructor for class org.orekit.propagation.AbstractPropagator
Build a new instance.
AbstractPropagatorBuilder - Class in org.orekit.propagation.conversion
Base class for propagator builders.
AbstractPropagatorBuilder(Orbit, PositionAngleType, double, boolean) - Constructor for class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Build a new instance.
AbstractPropagatorBuilder(Orbit, PositionAngleType, double, boolean, AttitudeProvider) - Constructor for class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Build a new instance.
AbstractPropagatorBuilder(Orbit, PositionAngleType, double, boolean, AttitudeProvider, double) - Constructor for class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Build a new instance.
AbstractPropagatorConverter - Class in org.orekit.propagation.conversion
Common handling of PropagatorConverter methods for propagators conversions.
AbstractPropagatorConverter(PropagatorBuilder, double, int) - Constructor for class org.orekit.propagation.conversion.AbstractPropagatorConverter
Build a new instance.
AbstractRadiationForceModel - Class in org.orekit.forces.radiation
Base class for radiation force models.
AbstractRadiationForceModel(ExtendedPVCoordinatesProvider, OneAxisEllipsoid) - Constructor for class org.orekit.forces.radiation.AbstractRadiationForceModel
Default constructor.
AbstractRelativisticClockModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical measurements with relativistic clock correction.
AbstractRelativisticClockModifier() - Constructor for class org.orekit.estimation.measurements.modifiers.AbstractRelativisticClockModifier
Simple constructor.
AbstractRelativisticClockOnBoardRangeRateModifier<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical range-rate measurement with relativistic frequency deviation.
AbstractRelativisticClockOnBoardRangeRateModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.AbstractRelativisticClockOnBoardRangeRateModifier
Simple constructor.
AbstractRelativisticJ2ClockModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical measurements with relativistic J2 clock correction.
AbstractRelativisticJ2ClockModifier(double, double, double) - Constructor for class org.orekit.estimation.measurements.modifiers.AbstractRelativisticJ2ClockModifier
Constructor for the Relativistic J2 Clock modifier.
AbstractScheduler<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.generation
Base implementation of Scheduler managing dates selection.
AbstractScheduler(MeasurementBuilder<T>, DatesSelector) - Constructor for class org.orekit.estimation.measurements.generation.AbstractScheduler
Simple constructor.
AbstractSelfFeedingLoader - Class in org.orekit.data
Abstract class that combines a DataProvidersManager with a supported names regular expression for DataProvidersManager.feed(String, DataLoader).
AbstractSelfFeedingLoader(String, DataProvidersManager) - Constructor for class org.orekit.data.AbstractSelfFeedingLoader
Create an abstract data loader that can feed itself.
AbstractShapiroBaseModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical range measurement with Shapiro time delay.
AbstractShapiroBaseModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.AbstractShapiroBaseModifier
Simple constructor.
AbstractShortTermEncounter1DNumerical2DPOCMethod - Class in org.orekit.ssa.collision.shorttermencounter.probability.twod
This abstract class serves as a foundation to create 1D numerical 2D probability of collision computing method.
AbstractShortTermEncounter1DNumerical2DPOCMethod(String, UnivariateIntegrator, int) - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter1DNumerical2DPOCMethod
Customizable constructor.
AbstractShortTermEncounter2DPOCMethod - Class in org.orekit.ssa.collision.shorttermencounter.probability.twod
This abstract class serves as a foundation to create 2D probability of collision computing method assuming a short term encounter model.
AbstractShortTermEncounter2DPOCMethod(String) - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter2DPOCMethod
Constructor.
AbstractSingleFrequencyCombination - Class in org.orekit.estimation.measurements.gnss
Base class for single frequency combination of measurements.
AbstractSingleFrequencyCombination(CombinationType, SatelliteSystem) - Constructor for class org.orekit.estimation.measurements.gnss.AbstractSingleFrequencyCombination
Constructor.
AbstractSolarActivityData<L extends AbstractSolarActivityDataLoader.LineParameters,​D extends AbstractSolarActivityDataLoader<L>> - Class in org.orekit.models.earth.atmosphere.data
Abstract class for solar activity data.
AbstractSolarActivityData(String, D, DataProvidersManager, TimeScale, int, double, double, double) - Constructor for class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData
 
AbstractSolarActivityData(DataSource, D, TimeScale, int, double, double, double) - Constructor for class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData
Simple constructor.
AbstractSolarActivityData.LocalSolarActivity - Class in org.orekit.models.earth.atmosphere.data
Container for weather parameters around current date.
AbstractSolarActivityData.SolarActivityGenerator - Class in org.orekit.models.earth.atmosphere.data
Generator used in the weather data cache.
AbstractSolarActivityDataLoader<L extends AbstractSolarActivityDataLoader.LineParameters> - Class in org.orekit.models.earth.atmosphere.data
Abstract class for solar activity data loader.
AbstractSolarActivityDataLoader(TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityDataLoader
Constructor.
AbstractSolarActivityDataLoader.LineParameters - Class in org.orekit.models.earth.atmosphere.data
Container class for Solar activity indexes.
AbstractSolarLightFluxModel - Class in org.orekit.forces.radiation
Abstract class for the definition of the solar flux model with a single occulting body of spherical shape.
AbstractSolarLightFluxModel(double, ExtendedPositionProvider, double, EventDetectionSettings) - Constructor for class org.orekit.forces.radiation.AbstractSolarLightFluxModel
Constructor.
AbstractSolarLightFluxModel(ExtendedPositionProvider, double, EventDetectionSettings) - Constructor for class org.orekit.forces.radiation.AbstractSolarLightFluxModel
Constructor with default value for reference flux.
AbstractStateCovarianceInterpolator - Class in org.orekit.propagation
Abstract class for orbit and state covariance interpolator.
AbstractStateCovarianceInterpolator(int, double, TimeInterpolator<Orbit>, Frame, OrbitType, PositionAngleType) - Constructor for class org.orekit.propagation.AbstractStateCovarianceInterpolator
Constructor.
AbstractStateCovarianceInterpolator(int, double, TimeInterpolator<Orbit>, LOFType) - Constructor for class org.orekit.propagation.AbstractStateCovarianceInterpolator
Constructor.
AbstractStateModifier - Class in org.orekit.propagation
Abstract base class for modifying state during propagation.
AbstractStateModifier() - Constructor for class org.orekit.propagation.AbstractStateModifier
 
AbstractTimeInterpolator<T extends TimeStamped> - Class in org.orekit.time
Abstract class for time interpolator.
AbstractTimeInterpolator(int, double) - Constructor for class org.orekit.time.AbstractTimeInterpolator
Constructor.
AbstractTimeInterpolator.InterpolationData - Class in org.orekit.time
Nested class used to store interpolation data.
AbstractTimeScales - Class in org.orekit.time
Abstract base class for TimeScales that implements some common functionality.
AbstractTimeScales() - Constructor for class org.orekit.time.AbstractTimeScales
Simple constructor.
AbstractVariableStepFieldIntegratorBuilder<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.conversion
Abstract class for integrator builder using variable step size.
AbstractVariableStepIntegratorBuilder - Class in org.orekit.propagation.conversion
Abstract class for integrator builder using variable step size.
AbstractVariableStepIntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.AbstractVariableStepIntegratorBuilder
Constructor.
AbstractVariableStepIntegratorBuilder(double, double, double, double) - Constructor for class org.orekit.propagation.conversion.AbstractVariableStepIntegratorBuilder
Constructor with expected velocity error.
AbstractVienna - Class in org.orekit.models.earth.troposphere
The Vienna tropospheric delay model for radio techniques.
AbstractVienna(ViennaAProvider, AzimuthalGradientProvider, TroposphericModel, TimeScale) - Constructor for class org.orekit.models.earth.troposphere.AbstractVienna
Build a new instance.
AbstractWindUp<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.gnss
Base class for wind-up effect computation.
AbstractWindUp(Dipole, Dipole) - Constructor for class org.orekit.estimation.measurements.gnss.AbstractWindUp
Simple constructor.
AbstractWriter - Class in org.orekit.files.ccsds.section
Top level class for writing CCSDS message sections.
AbstractWriter(String, String) - Constructor for class org.orekit.files.ccsds.section.AbstractWriter
Simple constructor.
ACC - org.orekit.files.ccsds.definitions.SpacecraftBodyFrame.BaseEquipment
Accelerometer.
ACC_DIR_SIGMA - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
One σ off-nominal acceleration direction.
ACC_INTERP - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
Interpolation mode between current and next acceleration line.
ACC_MAG_SIGMA - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
One σ percent error on acceleration magnitude.
ACC_X - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
Acceleration along X axis.
ACC_Y - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
Acceleration along Y axis.
ACC_Z - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
Acceleration along Z axis.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.drag.DragForce
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.drag.TimeSpanDragForce
Deprecated.
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.empirical.ParametricAcceleration
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.forces.ForceModel
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.DeSitterRelativity
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.J2OnlyPerturbation
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.LenseThirringRelativity
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.NewtonianAttraction
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.OceanTides
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.Relativity
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.SingleBodyAbsoluteAttraction
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.SingleBodyRelativeAttraction
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.SolidTides
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.ThirdBodyAttraction
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.inertia.InertialForces
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.maneuvers.Maneuver
 
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.radiation.ECOM2
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.radiation.RadiationPressureModel
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.drag.DragForce
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.drag.TimeSpanDragForce
Deprecated.
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.empirical.ParametricAcceleration
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in interface org.orekit.forces.ForceModel
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.DeSitterRelativity
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.J2OnlyPerturbation
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.LenseThirringRelativity
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.NewtonianAttraction
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.OceanTides
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.Relativity
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.SingleBodyAbsoluteAttraction
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.SingleBodyRelativeAttraction
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.SolidTides
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.ThirdBodyAttraction
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.inertia.InertialForces
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.maneuvers.Maneuver
 
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.radiation.ECOM2
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.radiation.RadiationPressureModel
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel
Compute acceleration.
ACCELERATION_SUFFIX - Static variable in class org.orekit.estimation.measurements.GroundStation
Suffix for ground clock drift parameters name.
AccelerationModel - Interface in org.orekit.forces.empirical
Acceleration model used by empirical force.
accept(boolean) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.BooleanConsumer
Consume a boolean.
accept(char) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.CharConsumer
Consume a character.
accept(char, double) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.LabeledDoubleConsumer
Consume an indexed double.
accept(double) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.DoubleConsumer
Consume a double.
accept(double[]) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.DoubleArrayConsumer
Consume an array of doubles.
accept(int) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.IntConsumer
Consume an integer.
accept(int[]) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.IntegerArrayConsumer
Consume an array of integers.
accept(int, double) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.IndexedDoubleConsumer
Consume an indexed double.
accept(int, double[]) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.IndexedDoubleArrayConsumer
Consume an indexed double array.
accept(int, int) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.IndexedIntConsumer
Consume an integer.
accept(int, int, double) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.DoublyIndexedDoubleConsumer
Consume a doubly indexed double.
accept(int, String) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.IndexedStringConsumer
Consume an indexed string.
accept(String) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.StringConsumer
Consume a string.
accept(List<String>) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.StringListConsumer
Consume a list of strings.
accept(List<BodyFacade>) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.CenterListConsumer
Consume a body center.
accept(List<Unit>) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.UnitListConsumer
Consume a list of units.
accept(List<T>) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.EnumListConsumer
Consume an enum.
accept(RotationOrder) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.RotationOrderConsumer
Consume a data.
accept(Vector3D) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.VectorConsumer
Consume a vector.
accept(IntegerLeastSquareSolution[]) - Method in interface org.orekit.estimation.measurements.gnss.AmbiguityAcceptance
Check if one of the candidate solutions can be accepted.
accept(IntegerLeastSquareSolution[]) - Method in class org.orekit.estimation.measurements.gnss.SimpleRatioAmbiguityAcceptance
Check if one of the candidate solutions can be accepted.
accept(BodyFacade) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.CenterConsumer
Consume a body center.
accept(FrameFacade) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.FrameConsumer
Consume a frame.
accept(TimeSystem) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.TimeSystemConsumer
Consume a time system.
accept(Maneuvrable) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.ManeuvrableConsumer
Consume a Maneuvrable.
accept(MessageParser<T>) - Method in class org.orekit.files.ccsds.utils.lexical.KvnLexicalAnalyzer
Parse a CCSDS Message.
accept(MessageParser<T>) - Method in interface org.orekit.files.ccsds.utils.lexical.LexicalAnalyzer
Parse a CCSDS Message.
accept(MessageParser<T>) - Method in class org.orekit.files.ccsds.utils.lexical.XmlLexicalAnalyzer
Parse a CCSDS Message.
accept(AbsoluteDate) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.DateConsumer
Consume a date.
accept(T) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.EnumConsumer
Consume an enum.
acceptComments() - Method in class org.orekit.files.ccsds.section.CommentsContainer
Check if container is still accepting comments.
acceptStep(FieldAbstractAnalyticalPropagator.FieldBasicStepInterpolator, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Accept a step, triggering events and step handlers.
acceptStep(OrekitStepInterpolator, AbsoluteDate) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Accept a step, triggering events and step handlers.
AccuracyProvider - Interface in org.orekit.gnss.metric.messages.common
This interface represents an accuracy providerused to validate RTCM ephemeris messages.
AccurateFormatter - Class in org.orekit.utils
Formatter used to produce strings from data with high accuracy.
Acm - Class in org.orekit.files.ccsds.ndm.adm.acm
This class gathers the informations present in the Attitude Comprehensive Message (ACM).
Acm(AdmHeader, List<Segment<AcmMetadata, AcmData>>, IERSConventions, DataContext) - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.Acm
Simple constructor.
ACM_DATA_ELEMENTS - org.orekit.files.ccsds.ndm.adm.acm.AcmMetadataKey
List of elements of information data blocks included in this message.
AcmData - Class in org.orekit.files.ccsds.ndm.adm.acm
Data container for Attitude Comprehensive Messages.
AcmData(List<AttitudeStateHistory>, AttitudePhysicalProperties, List<AttitudeCovarianceHistory>, List<AttitudeManeuver>, AttitudeDetermination, UserDefined) - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AcmData
Simple constructor.
AcmDataSubStructureKey - Enum in org.orekit.files.ccsds.ndm.adm.acm
Keywords for ACM data sub-structure.
AcmElements - Enum in org.orekit.files.ccsds.ndm.adm.acm
Data elements types used in CCSDS Attitude Comprehensive Messages.
AcmMetadata - Class in org.orekit.files.ccsds.ndm.adm.acm
AcmMetadata(DataContext) - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata
Create a new meta-data.
AcmMetadataKey - Enum in org.orekit.files.ccsds.ndm.adm.acm
Keys for ACM container entries.
AcmParser - Class in org.orekit.files.ccsds.ndm.adm.acm
A parser for the CCSDS ACM (Attitude Comprehensive Message).
AcmParser(IERSConventions, boolean, DataContext, ParsedUnitsBehavior, Function<ParseToken, List<ParseToken>>[]) - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AcmParser
Complete constructor.
AcmSatelliteEphemeris - Class in org.orekit.files.ccsds.ndm.adm.acm
ACM ephemeris blocks for a single satellite.
AcmSatelliteEphemeris(String, List<AttitudeStateHistory>) - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AcmSatelliteEphemeris
Create a container for the set of ephemeris blocks in the file that pertain to a single satellite.
AcmWriter - Class in org.orekit.files.ccsds.ndm.adm.acm
Writer for CCSDS Attitude Comprehensive Message.
AcmWriter(IERSConventions, DataContext) - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AcmWriter
Complete constructor.
ACTUAL_OD_SPAN - org.orekit.files.ccsds.ndm.cdm.ODParametersKey
Based on the observations available and the RECOMMENDED_OD_SPAN, the actual time span used for the OD of the object.
ACTUAL_OD_SPAN - org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey
Actual time span used for the OD of the object.
ACTUATOR - org.orekit.files.ccsds.definitions.SpacecraftBodyFrame.BaseEquipment
Actuator: could denote reaction wheels, solar arrays, thrusters, etc..
ACTUATOR_USED - org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuverKey
Actuator used.
ad - org.orekit.files.ccsds.ndm.adm.acm.AcmDataSubStructureKey
Orbit determination section.
AD - org.orekit.files.ccsds.ndm.adm.acm.AcmDataSubStructureKey
Attitude determination section.
AD - org.orekit.files.ccsds.ndm.adm.acm.AcmElements
Attitude determination.
AD_ID - org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationKey
Identification number.
AD_METHOD - org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationKey
Attitude determination method.
AD_PREV_ID - org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationKey
Identification of previous attitude determination.
AdamsBashforthFieldIntegratorBuilder<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.conversion
Builder for AdamsBashforthFieldIntegrator.
AdamsBashforthFieldIntegratorBuilder(int, double, double, double) - Constructor for class org.orekit.propagation.conversion.AdamsBashforthFieldIntegratorBuilder
Build a new instance.
AdamsBashforthFieldIntegratorBuilder(int, double, double, double, double) - Constructor for class org.orekit.propagation.conversion.AdamsBashforthFieldIntegratorBuilder
Build a new instance.
AdamsBashforthIntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for AdamsBashforthIntegrator.
AdamsBashforthIntegratorBuilder(int, double, double, double) - Constructor for class org.orekit.propagation.conversion.AdamsBashforthIntegratorBuilder
Build a new instance.
AdamsBashforthIntegratorBuilder(int, double, double, double, double) - Constructor for class org.orekit.propagation.conversion.AdamsBashforthIntegratorBuilder
Build a new instance.
AdamsMoultonFieldIntegratorBuilder<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.conversion
Builder for AdamsMoultonFieldIntegrator.
AdamsMoultonFieldIntegratorBuilder(int, double, double, double) - Constructor for class org.orekit.propagation.conversion.AdamsMoultonFieldIntegratorBuilder
Build a new instance.
AdamsMoultonFieldIntegratorBuilder(int, double, double, double, double) - Constructor for class org.orekit.propagation.conversion.AdamsMoultonFieldIntegratorBuilder
Build a new instance.
AdamsMoultonIntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for AdamsMoultonIntegrator.
AdamsMoultonIntegratorBuilder(int, double, double, double) - Constructor for class org.orekit.propagation.conversion.AdamsMoultonIntegratorBuilder
Build a new instance.
AdamsMoultonIntegratorBuilder(int, double, double, double, double) - Constructor for class org.orekit.propagation.conversion.AdamsMoultonIntegratorBuilder
Build a new instance.
AdaptableInterval - Interface in org.orekit.propagation.events
This interface represents an event checking interval that depends on state.
AdapterDetector - Class in org.orekit.propagation.events
Base class for adapting an existing detector.
AdapterDetector(EventDetector) - Constructor for class org.orekit.propagation.events.AdapterDetector
Build an adaptor wrapping an existing detector.
AdapterPropagator - Class in org.orekit.propagation.analytical
Orbit propagator that adapts an underlying propagator, adding differential effects.
AdapterPropagator(Propagator) - Constructor for class org.orekit.propagation.analytical.AdapterPropagator
Build a propagator from an underlying reference propagator.
AdapterPropagator.DifferentialEffect - Interface in org.orekit.propagation.analytical
Interface for orbit differential effects.
ADBARV - org.orekit.files.ccsds.ndm.odm.ocm.OrbitElementsType
Spherical 6-element set (α,δ,β,A,r,v).
add(double, OrekitFixedStepHandler) - Method in class org.orekit.propagation.sampling.StepHandlerMultiplexer
Add a handler for fixed size step.
add(FieldOrekitStepHandler<T>) - Method in class org.orekit.propagation.sampling.FieldStepHandlerMultiplexer
Add a handler for variable size step.
add(OrekitStepHandler) - Method in class org.orekit.propagation.sampling.StepHandlerMultiplexer
Add a handler for variable size step.
add(PolynomialFunctionMatrix) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix
Add the argument matrix with the current matrix.
add(ParameterDriver) - Method in class org.orekit.utils.ParameterDriversList
Add a driver.
add(T, FieldOrekitFixedStepHandler<T>) - Method in class org.orekit.propagation.sampling.FieldStepHandlerMultiplexer
Add a handler for fixed size step.
addAccelerationModelValidAfter(AccelerationModel, AbsoluteDate) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
Add a AccelerationModel entry valid after a limit date.
addAccelerationModelValidBefore(AccelerationModel, AbsoluteDate) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
Add an AccelerationModel entry valid before a limit date.
addAdditionalDerivativesProvider(AdditionalDerivativesProvider) - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Add a set of user-specified equations to be integrated along with the orbit propagation (author Shiva Iyer).
addAdditionalDerivativesProvider(AdditionalDerivativesProvider) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Add a provider for user-specified state derivatives to be integrated along with the orbit propagation.
addAdditionalDerivativesProvider(FieldAdditionalDerivativesProvider<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Add a provider for user-specified state derivatives to be integrated along with the orbit propagation.
addAdditionalState(String, double...) - Method in class org.orekit.propagation.SpacecraftState
Add an additional state.
addAdditionalState(String, T...) - Method in class org.orekit.propagation.FieldSpacecraftState
Add an additional state.
addAdditionalStateDerivative(String, double...) - Method in class org.orekit.propagation.SpacecraftState
Add an additional state derivative.
addAdditionalStateDerivative(String, T...) - Method in class org.orekit.propagation.FieldSpacecraftState
Add an additional state derivative.
addAdditionalStateProvider(AdditionalStateProvider) - Method in class org.orekit.propagation.AbstractPropagator
Add a set of user-specified state parameters to be computed along with the orbit propagation.
addAdditionalStateProvider(AdditionalStateProvider) - Method in interface org.orekit.propagation.Propagator
Add a set of user-specified state parameters to be computed along with the orbit propagation.
addAdditionalStateProvider(FieldAdditionalStateProvider<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator
Add a set of user-specified state parameters to be computed along with the orbit propagation.
addAdditionalStateProvider(FieldAdditionalStateProvider<T>) - Method in interface org.orekit.propagation.FieldPropagator
Add a set of user-specified state parameters to be computed along with the orbit propagation.
addAnglesData(CRD.AnglesMeasurement) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
Add an entry to the list of angles data.
addAntennaTypeValidAfter(String, AbsoluteDate) - Method in class org.orekit.files.sinex.Station
Add a antenna type entry valid after a limit date.
Using addAntennaTypeValidAfter(entry, t) will make entry valid in [t, +∞[ (note the closed bracket).
addAntennaTypeValidBefore(String, AbsoluteDate) - Method in class org.orekit.files.sinex.Station
Add a antenna type entry valid before a limit date.
Using addAntennaTypeValidBefore(entry, t) will make entry valid in ]-∞, t[ (note the open bracket).
addAppliedDCBS(AppliedDCBS) - Method in class org.orekit.files.rinex.clock.RinexClock
Add an applied differencial code bias corrections.
addAppliedDCBS(AppliedDCBS) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Add applied differential code bias corrections.
addAppliedPCVS(AppliedPCVS) - Method in class org.orekit.files.rinex.clock.RinexClock
Add an applied phase center variations.
addAppliedPCVS(AppliedPCVS) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Add antenna center variation corrections.
addBDGIMMessage(IonosphereBDGIMMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Add an ionosphere BDGIM message.
addBeidouCivilianNavigationMessage(BeidouCivilianNavigationMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Add a Beidou navigation message to the list.
addBeidouLegacyNavigationMessage(BeidouLegacyNavigationMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Add a Beidou navigation message to the list.
addCalibrationData(CRD.Calibration) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
Add an entry to the list of calibration data.
addCalibrationDetailData(CRD.CalibrationDetail) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
Add an entry to the list of calibration detail data.
addCelestialBodyLoader(String, CelestialBodyLoader) - Static method in class org.orekit.bodies.CelestialBodyFactory
Add a loader for celestial bodies.
addCelestialBodyLoader(String, CelestialBodyLoader) - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
Add a loader for celestial bodies.
addChild(OrphanFrame, Transform, boolean) - Method in class org.orekit.frames.OrphanFrame
Add a child.
addChild(OrphanFrame, TransformProvider, boolean) - Method in class org.orekit.frames.OrphanFrame
Add a child.
addClockData(String, RinexClock.ClockDataLine) - Method in class org.orekit.files.rinex.clock.RinexClock
Add a clock data line to a specified receiver/satellite.
addClockDataType(RinexClock.ClockDataType) - Method in class org.orekit.files.rinex.clock.RinexClock
Add a clock data types.
addCodeBias(CodeBias) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm05Data
Add a code bias value for the current satellite.
addComment(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set comment for relative metadata.
addComment(String) - Method in class org.orekit.files.ccsds.ndm.NdmParser
Add comment.
addComment(String) - Method in class org.orekit.files.ccsds.section.CommentsContainer
Add comment.
addComment(String) - Method in class org.orekit.files.rinex.clock.RinexClock
Add a comment line.
addComment(String) - Method in class org.orekit.files.sp3.SP3Header
Add a comment.
addComment(RinexComment) - Method in class org.orekit.files.rinex.RinexFile
Add a comment.
addConfigurationRecord(CRDConfiguration.BaseConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration
Add a configuration record, such as SystemConfiguation, LaserConfiguration, DetectorConfiguration, etc.
addConstraint(int, int, double) - Method in class org.orekit.utils.AbstractMultipleShooting
Add a constraint on one component of one patch point.
addContribution(BodiesElements, double[][], double[][]) - Method in class org.orekit.forces.gravity.potential.OceanTidesWave
Add the contribution of the wave to Stokes coefficients.
addContribution(FieldSpacecraftState<T>, FieldTimeDerivativesEquations<T>) - Method in interface org.orekit.forces.ForceModel
Compute the contribution of the force model to the perturbing acceleration.
addContribution(FieldSpacecraftState<T>, FieldTimeDerivativesEquations<T>) - Method in class org.orekit.forces.gravity.NewtonianAttraction
Compute the contribution of the force model to the perturbing acceleration.
addContribution(FieldSpacecraftState<T>, FieldTimeDerivativesEquations<T>) - Method in class org.orekit.forces.maneuvers.Maneuver
Compute the contribution of the force model to the perturbing acceleration.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in interface org.orekit.forces.ForceModel
Compute the contribution of the force model to the perturbing acceleration.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.gravity.NewtonianAttraction
Compute the contribution of the force model to the perturbing acceleration.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.maneuvers.Maneuver
Compute the contribution of the force model to the perturbing acceleration.
addCoordinate(SP3Coordinate) - Method in class org.orekit.files.sp3.SP3Segment
Adds a new P/V coordinate.
addCoordinate(SP3Coordinate, double) - Method in class org.orekit.files.sp3.SP3Ephemeris
Adds a new P/V coordinate.
addCovarianceMatrix(CartesianCovariance) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemData
Add a covariance matrix.
addData(TimeStampedAngularCoordinates) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemData
Add a data point.
addData(TimeStampedPVCoordinates, boolean) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemData
Add a data point.
addDataBlock(CRD.CRDDataBlock) - Method in class org.orekit.files.ilrs.CRD
Add a data block to the current list of data blocks.
addDcb(SatelliteSystem, Dcb) - Method in class org.orekit.files.sinex.DcbStation
Add the DCB data corresponding to a satellite system.
addDcbLine(String, String, AbsoluteDate, AbsoluteDate, double) - Method in class org.orekit.files.sinex.Dcb
Add the content of a DCB line to the DCBSatellite object.
addDefaultCelestialBodyLoader(String) - Static method in class org.orekit.bodies.CelestialBodyFactory
Add the default loaders for all predefined celestial bodies.
addDefaultCelestialBodyLoader(String) - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
Add the default loaders for all predefined celestial bodies.
addDefaultCelestialBodyLoader(String, String) - Static method in class org.orekit.bodies.CelestialBodyFactory
Add the default loaders for celestial bodies.
addDefaultCelestialBodyLoader(String, String) - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
Add the default loaders for celestial bodies.
addDefaultEOP1980HistoryLoaders(String, String, String, String, String, String) - Static method in class org.orekit.frames.FramesFactory
Add the default loaders EOP history (IAU 1980 precession/nutation).
addDefaultEOP1980HistoryLoaders(String, String, String, String, String, String) - Method in class org.orekit.frames.LazyLoadedFrames
Add the default loaders EOP history (IAU 1980 precession/nutation).
addDefaultEOP1980HistoryLoaders(String, String, String, String, String, String, Supplier<TimeScale>) - Method in class org.orekit.frames.LazyLoadedEop
Add the default loaders EOP history (IAU 1980 precession/nutation).
addDefaultEOP2000HistoryLoaders(String, String, String, String, String, String) - Static method in class org.orekit.frames.FramesFactory
Add the default loaders for EOP history (IAU 2000/2006 precession/nutation).
addDefaultEOP2000HistoryLoaders(String, String, String, String, String, String) - Method in class org.orekit.frames.LazyLoadedFrames
Add the default loaders for EOP history (IAU 2000/2006 precession/nutation).
addDefaultEOP2000HistoryLoaders(String, String, String, String, String, String, Supplier<TimeScale>) - Method in class org.orekit.frames.LazyLoadedEop
Add the default loaders for EOP history (IAU 2000/2006 precession/nutation).
addDefaultOceanTidesReaders() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Add the default READERS for ocean tides.
addDefaultOceanTidesReaders() - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
Add the default readers for ocean tides.
addDefaultPotentialCoefficientsReaders() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Add the default readers for gravity fields.
addDefaultPotentialCoefficientsReaders() - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
Add the default readers for gravity fields.
addDefaultProviders() - Method in class org.orekit.data.DataProvidersManager
Add the default providers configuration.
addDefaultUTCTAIOffsetsLoaders() - Method in class org.orekit.time.LazyLoadedTimeScales
Add the default loaders for UTC-TAI offsets history files (both IERS and USNO).
addDefaultUTCTAIOffsetsLoaders() - Static method in class org.orekit.time.TimeScalesFactory
Add the default loaders for UTC-TAI offsets history files (both IERS and USNO).
addDragSensitiveValidAfter(DragSensitive, AbsoluteDate) - Method in class org.orekit.forces.drag.TimeSpanDragForce
Deprecated.
Add a DragSensitive entry valid after a limit date.
Using addDragSensitiveValidAfter(entry, t) will make entry valid in [t, +∞[ (note the closed bracket).
addDragSensitiveValidBefore(DragSensitive, AbsoluteDate) - Method in class org.orekit.forces.drag.TimeSpanDragForce
Deprecated.
Add a DragSensitive entry valid before a limit date.
Using addDragSensitiveValidBefore(entry, t) will make entry valid in ]-∞, t[ (note the open bracket).
addEarthOrientationParameter(EarthOrientationParameterMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Add an Earth orientation parameter.
addEffect(AdapterPropagator.DifferentialEffect) - Method in class org.orekit.propagation.analytical.AdapterPropagator
Add a differential effect.
addEntry(String, String) - Method in class org.orekit.files.ccsds.ndm.odm.UserDefined
Add a key/value entry.
addEOPHistoryLoader(IERSConventions, EopHistoryLoader) - Static method in class org.orekit.frames.FramesFactory
Add a loader for Earth Orientation Parameters history.
addEOPHistoryLoader(IERSConventions, EopHistoryLoader) - Method in class org.orekit.frames.LazyLoadedEop
Add a loader for Earth Orientation Parameters history.
addEOPHistoryLoader(IERSConventions, EopHistoryLoader) - Method in class org.orekit.frames.LazyLoadedFrames
Add a loader for Earth Orientation Parameters history.
addEphemerisName(int, String) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Adds an ephemeris name to the list.
addEventDate(AbsoluteDate) - Method in class org.orekit.propagation.events.DateDetector
Add an event date.
addEventDate(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.events.FieldDateDetector
Add an event date.
addEventDetector(D) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Add an event detector.
addEventDetector(D) - Method in interface org.orekit.propagation.FieldPropagator
Add an event detector.
addEventDetector(D) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Add an event detector.
addEventDetector(EventDetector) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Add an event detector.
addEventDetector(T) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Add an event detector.
addEventDetector(T) - Method in interface org.orekit.propagation.Propagator
Add an event detector.
addFilter(DataFilter) - Method in class org.orekit.data.FiltersManager
Add a data filter.
addForceModel(ForceModel) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
Add a force model to the global perturbation model.
addForceModel(ForceModel) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Add a force model to the global perturbation model.
addForceModel(ForceModel) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Add a force model.
addForceModel(DSSTForceModel) - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder
Add a force model to the global perturbation model.
addForceModel(DSSTForceModel) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Add a force model to the global perturbation model.
addForceModel(DSSTForceModel) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Add a force model to the global perturbation model.
addGalileoNavigationMessage(GalileoNavigationMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Add a Galileo navigation message to the list.
addGlonassChannel(GlonassSatelliteChannel) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Add GLONASS satellite/channel association.
addGlonassNavigationMessage(GLONASSNavigationMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Add a Glonass navigation message to the list.
addGPSLegacyNavigationMessage(GPSCivilianNavigationMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Add a GPS civilian navigation message to the list.
addGPSLegacyNavigationMessage(GPSLegacyNavigationMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Add a GPS legacy navigation message to the list.
addGridPoint(AbsoluteDate, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.ShortPeriodicsInterpolatedCoefficient
Add a point to the interpolation grid.
addGridPoint(FieldAbsoluteDate<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldShortPeriodicsInterpolatedCoefficient
Add a point to the interpolation grid.
addHandler(EventHandler) - Method in class org.orekit.propagation.events.handlers.EventMultipleHandler
Add one handler to the managed handlers list.
addHandlers(EventHandler...) - Method in class org.orekit.propagation.events.handlers.EventMultipleHandler
Add several handlers to the managed handlers list.
addImpulseManeuver(ImpulseManeuver) - Method in class org.orekit.propagation.conversion.AbstractAnalyticalPropagatorBuilder
Add impulse maneuver.
addImpulseManeuver(ImpulseManeuver) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
Add impulse maneuver.
addInput(T) - Method in class org.orekit.data.AbstractListCrawler
Add an input to the supported list.
addIRNSSNavigationMessage(IRNSSNavigationMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Add a IRNSS navigation message to the list.
ADDITIONAL_STATE_NAME_ALREADY_IN_USE - org.orekit.errors.OrekitMessages
ADDITIONAL_STATE_NAME_ALREADY_IN_USE.
AdditionalCovarianceMetadata - Class in org.orekit.files.ccsds.ndm.cdm
Container for the additional covariance metadata (optional).
AdditionalCovarianceMetadata() - Constructor for class org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadata
Simple constructor.
AdditionalCovarianceMetadataKey - Enum in org.orekit.files.ccsds.ndm.cdm
Keys for covariance metadatail y a entries.
AdditionalDerivativesProvider - Interface in org.orekit.propagation.integration
Provider for additional derivatives.
additionalParameters - org.orekit.files.ccsds.ndm.cdm.XmlSubStructureKey
Additional Parameter section.
AdditionalParameters - Class in org.orekit.files.ccsds.ndm.cdm
Container for additional parameters data block.
AdditionalParameters() - Constructor for class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Simple constructor.
AdditionalParametersKey - Enum in org.orekit.files.ccsds.ndm.cdm
Keys for CDM additional parameters entries.
AdditionalParametersWriter - Class in org.orekit.files.ccsds.ndm.cdm
Writer for additional parameters data block for CCSDS Conjunction Data Messages.
AdditionalStateProvider - Interface in org.orekit.propagation
This interface allows to modify SpacecraftState and set up additional state data.
addKeplerContribution(double) - Method in interface org.orekit.propagation.numerical.TimeDerivativesEquations
Add the contribution of the Kepler evolution.
addKeplerContribution(PositionAngleType, double, double[]) - Method in class org.orekit.orbits.CartesianOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngleType, double, double[]) - Method in class org.orekit.orbits.CircularOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngleType, double, double[]) - Method in class org.orekit.orbits.EquinoctialOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngleType, double, double[]) - Method in class org.orekit.orbits.KeplerianOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngleType, double, double[]) - Method in class org.orekit.orbits.Orbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngleType, T, T[]) - Method in class org.orekit.orbits.FieldCartesianOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngleType, T, T[]) - Method in class org.orekit.orbits.FieldCircularOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngleType, T, T[]) - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngleType, T, T[]) - Method in class org.orekit.orbits.FieldKeplerianOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngleType, T, T[]) - Method in class org.orekit.orbits.FieldOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(T) - Method in interface org.orekit.propagation.numerical.FieldTimeDerivativesEquations
Add the contribution of the Kepler evolution.
addKlobucharMessage(IonosphereKlobucharMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Add an ionosphere Klobuchar message.
addManeuver(Maneuver) - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData
Add a maneuver.
addMassDerivative(double) - Method in interface org.orekit.propagation.numerical.TimeDerivativesEquations
Add the contribution of the flow rate (dm/dt).
addMassDerivative(T) - Method in interface org.orekit.propagation.numerical.FieldTimeDerivativesEquations
Add the contribution of the flow rate (dm/dt).
addMeasurement(ObservedMeasurement<?>) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Add a measurement.
addMeteoData(CRD.MeteorologicalMeasurement) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
Add an entry to the list of meteorological data.
addModifier(EstimationModifier<MultiplexedMeasurement>) - Method in class org.orekit.estimation.measurements.generation.MultiplexedMeasurementBuilder
Add a modifier.
addModifier(EstimationModifier<T>) - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Add a modifier.
addModifier(EstimationModifier<T>) - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
Add a modifier.
addModifier(EstimationModifier<T>) - Method in interface org.orekit.estimation.measurements.generation.MeasurementBuilder
Add a modifier.
addModifier(EstimationModifier<T>) - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
Add a modifier.
addNequickGMessage(IonosphereNequickGMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Add an ionosphere Nequick-G message.
addNewSegment(List<SpacecraftState>) - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
Injects pre-computed satellite states into this ephemeris file object, returning the generated OrekitEphemerisFile.OrekitEphemerisSegment that has been stored internally.
addNewSegment(List<SpacecraftState>, int) - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
Injects pre-computed satellite states into this ephemeris file object, returning the generated OrekitEphemerisFile.OrekitEphemerisSegment that has been stored internally.
addNewSegment(List<SpacecraftState>, String, int, AngularDerivativesFilter) - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitSatelliteAttitudeEphemeris
Injects pre-computed satellite states into this attitude ephemeris file object, returning the generated OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment that has been stored internally.
addNewSegment(List<SpacecraftState>, CelestialBody, int) - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
Injects pre-computed satellite states into this ephemeris file object, returning the generated OrekitEphemerisFile.OrekitEphemerisSegment that has been stored internally.
addNewSegment(List<SpacecraftState>, CelestialBody, int, TimeScale) - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
Injects pre-computed satellite states into this ephemeris file object, returning the generated OrekitEphemerisFile.OrekitEphemerisSegment that has been stored internally.
addNonKeplerianAcceleration(FieldVector3D<T>) - Method in interface org.orekit.propagation.numerical.FieldTimeDerivativesEquations
Add the contribution of an acceleration expressed in some inertial frame.
addNonKeplerianAcceleration(Vector3D) - Method in interface org.orekit.propagation.numerical.TimeDerivativesEquations
Add the contribution of a non-Keplerian acceleration.
addObservation(Observation) - Method in class org.orekit.files.ccsds.ndm.tdm.ObservationsBlock
Adds an observation data line.
addObservation(ObservationType, AbsoluteDate, double) - Method in class org.orekit.files.ccsds.ndm.tdm.ObservationsBlock
Adds an observation data line.
addObservationDataSet(ObservationDataSet) - Method in class org.orekit.files.rinex.observation.RinexObservation
Add an observations data set.
addObserver(int, String, MessageObserver) - Method in class org.orekit.gnss.metric.ntrip.NtripClient
Add an observer for an encoded messages.
addObserver(int, MessageObserver) - Method in class org.orekit.gnss.metric.ntrip.StreamMonitor
Add an observer for encoded messages.
addObserver(ParameterObserver) - Method in class org.orekit.utils.ParameterDriver
Add an observer for this driver.
addOccultingBody(OneAxisEllipsoid) - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel
Add a new occulting body.
addOccultingBody(ExtendedPVCoordinatesProvider, double) - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel
Add a new occulting body.
addOceanTidesReader(OceanTidesReader) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Add a reader for ocean tides.
addOceanTidesReader(OceanTidesReader) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
Add a reader for ocean tides.
addOffset(AngularCoordinates) - Method in class org.orekit.utils.AngularCoordinates
Add an offset from the instance.
addOffset(AngularCoordinates) - Method in class org.orekit.utils.TimeStampedAngularCoordinates
Add an offset from the instance.
addOffset(FieldAngularCoordinates<T>) - Method in class org.orekit.utils.FieldAngularCoordinates
Add an offset from the instance.
addOffset(FieldAngularCoordinates<T>) - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates
Add an offset from the instance.
addOptionalSubInterpolatorIfDefined(FieldTimeInterpolator<? extends FieldTimeStamped<S>, S>, List<FieldTimeInterpolator<? extends FieldTimeStamped<S>, S>>) - Method in class org.orekit.time.AbstractFieldTimeInterpolator
Add all lowest level sub interpolators to the sub interpolator list.
addOptionalSubInterpolatorIfDefined(TimeInterpolator<? extends TimeStamped>, List<TimeInterpolator<? extends TimeStamped>>) - Method in class org.orekit.time.AbstractTimeInterpolator
Add all lowest level sub interpolators to the sub interpolator list.
addParameterDriver(ParameterDriver) - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Add a parameter driver.
addParticipant(int, String) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Adds a participant to the list.
addPhaseBias(PhaseBias) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data
Add a phase bias value for the current satellite.
addPhaseShiftCorrection(PhaseShiftCorrection) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Add phase shift correction used to generate phases consistent w/r to cycle shifts.
addPoint(AbsoluteDate, double) - Method in class org.orekit.utils.SecularAndHarmonic
Add a fitting point.
addPotentialCoefficientsReader(PotentialCoefficientsReader) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Add a reader for gravity fields.
addPotentialCoefficientsReader(PotentialCoefficientsReader) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
Add a reader for gravity fields.
addPropagationConfiguration(DSSTPropagatorBuilder, CovarianceMatrixProvider) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimatorBuilder
Add a propagation configuration.
addPropagationConfiguration(DSSTPropagatorBuilder, CovarianceMatrixProvider) - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanEstimatorBuilder
Add a propagation configuration.
addPropagationConfiguration(PropagatorBuilder, CovarianceMatrixProvider) - Method in class org.orekit.estimation.sequential.KalmanEstimatorBuilder
Add a propagation configuration.
addPropagationConfiguration(PropagatorBuilder, CovarianceMatrixProvider) - Method in class org.orekit.estimation.sequential.UnscentedKalmanEstimatorBuilder
Add a propagation configuration.
addPropagator(Propagator) - Method in class org.orekit.estimation.measurements.generation.Generator
Add a propagator.
addProvider(DataProvider) - Method in class org.orekit.data.DataProvidersManager
Add a data provider to the supported list.
addPsdCorrectionValidAfter(PsdCorrection, AbsoluteDate) - Method in class org.orekit.files.sinex.Station
Add a Post-Seismic Deformation entry valid after a limit date.
Using addPsdCorrectionValidAfter(entry, t) will make entry valid in [t, +∞[ (note the closed bracket).
addPVProviderAfter(AbsoluteDate, PVCoordinatesProvider, boolean) - Method in class org.orekit.utils.AggregatedPVCoordinatesProvider.Builder
Add a PVCoordinatesProvider to the collection.
addPVProviderBefore(AbsoluteDate, PVCoordinatesProvider, boolean) - Method in class org.orekit.utils.AggregatedPVCoordinatesProvider.Builder
Add a PVCoordinatesProvider to the collection.
addQZSSCivilianNavigationMessage(QZSSCivilianNavigationMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Add a QZSS navigation message to the list.
addQZSSLegacyNavigationMessage(QZSSLegacyNavigationMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Add a QZSS navigation message to the list.
addRangeData(CRD.RangeMeasurement) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
Add an entry to the list of range data.
addRangeSupplementData(CRD.RangeSupplement) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
Add an entry to the list of range supplement data.
addReceiveDelay(int, double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Adds a receive delay to the list.
addReceiver(RinexClock.Receiver) - Method in class org.orekit.files.rinex.clock.RinexClock
Add a new receiver to the list of stored receivers.
addReferenceClockList(List<RinexClock.ReferenceClock>, AbsoluteDate) - Method in class org.orekit.files.rinex.clock.RinexClock
Add a list of reference clocks which will be used after a specified date.
addResetter(Field<T>, FieldManeuverTriggersResetter<T>) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers
Add a resetter.
addResetter(Field<T>, FieldManeuverTriggersResetter<T>) - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggers
Add a resetter.
addResetter(ManeuverTriggersResetter) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers
Add a resetter.
addResetter(ManeuverTriggersResetter) - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggers
Add a resetter.
addSatellite(String) - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile
Adds a new satellite to this object.
addSatellite(String) - Method in class org.orekit.files.general.OrekitEphemerisFile
Adds a new satellite to this object.
addSatellite(String) - Method in class org.orekit.files.rinex.clock.RinexClock
Add a new satellite with a given identifier to the list of stored satellites.
addSatellite(String) - Method in class org.orekit.files.sp3.SP3
Add a new satellite with a given identifier to the list of stored satellites.
addSatelliteCoordinate(String, CPF.CPFCoordinate) - Method in class org.orekit.files.ilrs.CPF
Add a new P/V coordinates to the satellite.
addSatelliteCoordinates(String, List<CPF.CPFCoordinate>) - Method in class org.orekit.files.ilrs.CPF
Adds a set of P/V coordinates to the satellite.
addSatelliteVelocityToCPFCoordinate(String, Vector3D) - Method in class org.orekit.files.ilrs.CPF
Add the velocity to the last CPF coordinate entry.
addSatId(String) - Method in class org.orekit.files.sp3.SP3Header
Add a satellite identifier.
addSBASNavigationMessage(SBASNavigationMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Add a SBAS navigation message to the list.
addScaleFactorCorrection(SatelliteSystem, ScaleFactorCorrection) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Add scale factor correction.
addScheduler(Scheduler<T>) - Method in class org.orekit.estimation.measurements.generation.Generator
Add a sequences generator for a specific measurement type.
addSensor(AttitudeDeterminationSensor) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination
Add a sensor used.
addSessionStatisticsData(CRD.SessionStatistics) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
Add an entry to the list of session statistics data.
addSolution(long[], double) - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Add a new solution.
addSpanAtDate(AbsoluteDate) - Method in class org.orekit.utils.ParameterDriver
Create a new span in values and names time span map given a start date.
addSpans(AbsoluteDate, AbsoluteDate, double) - Method in class org.orekit.utils.ParameterDriver
Cut values and names time span map given orbit determination start and end and driver periodicity.
addStationEccentricitiesValidAfter(Vector3D, AbsoluteDate) - Method in class org.orekit.files.sinex.Station
Add a station eccentricity vector entry valid after a limit date.
Using addStationEccentricitiesValidAfter(entry, t) will make entry valid in [t, +∞[ (note the closed bracket).
addStationEccentricitiesValidBefore(Vector3D, AbsoluteDate) - Method in class org.orekit.files.sinex.Station
Add a station eccentricity vector entry valid before a limit date.
Using addStationEccentricitiesValidBefore(entry, t) will make entry valid in ]-∞, t[ (note the open bracket).
addSubscriber(GeneratedMeasurementSubscriber) - Method in class org.orekit.estimation.measurements.generation.Generator
Add a subscriber.
addSupportedParameters(List<ParameterDriver>) - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Add supported parameters.
addSwitchingCondition(AttitudeProvider, AttitudeProvider, T, boolean, boolean, double, AngularDerivativesFilter, AttitudesSequence.SwitchHandler) - Method in class org.orekit.attitudes.AttitudesSequence
Add a switching condition between two attitude providers.
addSystemObservationType(SatelliteSystem, ObservationType) - Method in class org.orekit.files.rinex.clock.RinexClock
Add an observation type for a specified satellite system.
addSystemTimeOffset(SystemTimeOffsetMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Add a system time offset.
addTimeSystemCorrections(TimeSystemCorrection) - Method in class org.orekit.files.rinex.navigation.RinexNavigationHeader
Add a time system correction to the list.
addTransmitDelay(int, double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Adds a transmit delay to the list.
addTroposphericModelValidAfter(EstimatedModel, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedModel
Add a EstimatedTroposphericModel entry valid after a limit date.
Using addTroposphericModelValidAfter(entry, t) will make entry valid in [t, +∞[ (note the closed bracket).
addTroposphericModelValidAfter(EstimatedTroposphericModel, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
Deprecated.
Add a EstimatedTroposphericModel entry valid after a limit date.
Using addTroposphericModelValidAfter(entry, t) will make entry valid in [t, +∞[ (note the closed bracket).
addTroposphericModelValidBefore(EstimatedModel, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedModel
Add an EstimatedTroposphericModel entry valid before a limit date.
Using addTroposphericValidBefore(entry, t) will make entry valid in ]-∞, t[ (note the open bracket).
addTroposphericModelValidBefore(EstimatedTroposphericModel, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
Deprecated.
Add an EstimatedTroposphericModel entry valid before a limit date.
Using addTroposphericValidBefore(entry, t) will make entry valid in ]-∞, t[ (note the open bracket).
addUTCTAIOffsetsLoader(UTCTAIOffsetsLoader) - Method in class org.orekit.time.LazyLoadedTimeScales
Add a loader for UTC-TAI offsets history files.
addUTCTAIOffsetsLoader(UTCTAIOffsetsLoader) - Static method in class org.orekit.time.TimeScalesFactory
Add a loader for UTC-TAI offsets history files.
addValidAfter(T, AbsoluteDate, boolean) - Method in class org.orekit.utils.TimeSpanMap
Add an entry valid after a limit date.
addValidAfter(T, FieldAbsoluteDate<D>) - Method in class org.orekit.utils.FieldTimeSpanMap
Add an entry valid after a limit date.
addValidBefore(T, AbsoluteDate, boolean) - Method in class org.orekit.utils.TimeSpanMap
Add an entry valid before a limit date.
addValidBefore(T, FieldAbsoluteDate<D>) - Method in class org.orekit.utils.FieldTimeSpanMap
Add an entry valid before a limit date.
addValidBetween(T, AbsoluteDate, AbsoluteDate) - Method in class org.orekit.utils.TimeSpanMap
Add an entry valid between two limit dates.
addWaveCoefficients(int, int, int, double, double, double, double, int, String) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Add parsed coefficients.
addWaypoint(GeodeticPoint, AbsoluteDate) - Method in class org.orekit.utils.WaypointPVBuilder
Add a waypoint.
addWeightedPoint(AbsoluteDate, double, double) - Method in class org.orekit.utils.SecularAndHarmonic
Add a weighted fitting point.
AdjointDynamicsProvider - Interface in org.orekit.control.indirect.shooting.propagation
Interface for adjoint derivatives provider (both standard and Field).
ADM_MSG_LINK - org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey
Unique identifier of Attitude Data Message(s) that are linked (relevant) to this Conjunction Data Message.
ADM_MSG_LINK - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Unique identifier of Attitude Data Message linked to this Orbit Data Message.
AdmCommonMetadataKey - Enum in org.orekit.files.ccsds.ndm.adm
Keys for APM and AEM entries.
AdmCommonMetadataWriter - Class in org.orekit.files.ccsds.ndm.adm
Writer for Common metadata for CCSDS Attitude Parameter/Ephemeris Messages.
AdmCommonMetadataWriter(AdmMetadata) - Constructor for class org.orekit.files.ccsds.ndm.adm.AdmCommonMetadataWriter
Simple constructor.
AdMethodType - Enum in org.orekit.files.ccsds.definitions
Type of attitude determination method used in CCSDS Attitude Comprehensive Messages.
AdmHeader - Class in org.orekit.files.ccsds.ndm.adm
Header of a CCSDS Attitude Data Message.
AdmHeader() - Constructor for class org.orekit.files.ccsds.ndm.adm.AdmHeader
Constructor.
AdmMetadata - Class in org.orekit.files.ccsds.ndm.adm
This class gathers the meta-data present in the Attitude Data Message (ADM).
AdmMetadata() - Constructor for class org.orekit.files.ccsds.ndm.adm.AdmMetadata
Simple constructor.
AdmMetadataKey - Enum in org.orekit.files.ccsds.ndm.adm
Keys for ADM container entries.
AdmParser<T extends NdmConstituent<AdmHeader,​?>,​P extends AbstractConstituentParser<AdmHeader,​T,​?>> - Class in org.orekit.files.ccsds.ndm.adm
Base class for Attitude Data Message parsers.
AdmParser(String, String, IERSConventions, boolean, DataContext, AbsoluteDate, ParsedUnitsBehavior, Function<ParseToken, List<ParseToken>>[]) - Constructor for class org.orekit.files.ccsds.ndm.adm.AdmParser
Complete constructor.
Aem - Class in org.orekit.files.ccsds.ndm.adm.aem
This class stores all the information of the Attitude Ephemeris Message (AEM) File parsed by AEMParser.
Aem(AdmHeader, List<AemSegment>, IERSConventions, DataContext) - Constructor for class org.orekit.files.ccsds.ndm.adm.aem.Aem
Simple constructor.
AemData - Class in org.orekit.files.ccsds.ndm.adm.aem
The Attitude Ephemerides data blocks class contain list of attitude data points.
AemData() - Constructor for class org.orekit.files.ccsds.ndm.adm.aem.AemData
Constructor.
AemMetadata - Class in org.orekit.files.ccsds.ndm.adm.aem
This class gathers the meta-data present in the Attitude Data Message (ADM).
AemMetadata(int) - Constructor for class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Simple constructor.
AemMetadataKey - Enum in org.orekit.files.ccsds.ndm.adm.aem
Keys for AEM container entries.
AemParser - Class in org.orekit.files.ccsds.ndm.adm.aem
A parser for the CCSDS AEM (Attitude Ephemeris Message).
AemParser(IERSConventions, boolean, DataContext, AbsoluteDate, int, ParsedUnitsBehavior, Function<ParseToken, List<ParseToken>>[]) - Constructor for class org.orekit.files.ccsds.ndm.adm.aem.AemParser
Complete constructor.
AemSatelliteEphemeris - Class in org.orekit.files.ccsds.ndm.adm.aem
AEM ephemeris blocks for a single satellite.
AemSatelliteEphemeris(String, List<AemSegment>) - Constructor for class org.orekit.files.ccsds.ndm.adm.aem.AemSatelliteEphemeris
Create a container for the set of ephemeris blocks in the file that pertain to a single satellite.
AemSegment - Class in org.orekit.files.ccsds.ndm.adm.aem
This class stores the metadata and data for one attitude segment.
AemSegment(AemMetadata, AemData) - Constructor for class org.orekit.files.ccsds.ndm.adm.aem.AemSegment
Simple constructor.
AemWriter - Class in org.orekit.files.ccsds.ndm.adm.aem
A writer for Attitude Ephemeris Messsage (AEM) files.
AemWriter(IERSConventions, DataContext, AbsoluteDate) - Constructor for class org.orekit.files.ccsds.ndm.adm.aem.AemWriter
Constructor used to create a new AEM writer configured with the necessary parameters to successfully fill in all required fields that aren't part of a standard object.
afterIntegration() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Method called just after integration.
afterIntegration() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Method called just after integration.
afterIntegration() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Method called just after integration.
afterIntegration() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Method called just after integration.
AggregateBoundedAttitudeProvider - Class in org.orekit.attitudes
A BoundedAttitudeProvider that covers a larger time span from several constituent attitude providers that cover shorter time spans.
AggregateBoundedAttitudeProvider(Collection<? extends BoundedAttitudeProvider>) - Constructor for class org.orekit.attitudes.AggregateBoundedAttitudeProvider
Constructor.
AggregateBoundedPropagator - Class in org.orekit.propagation.analytical
A BoundedPropagator that covers a larger time span from several constituent propagators that cover shorter time spans.
AggregateBoundedPropagator(Collection<? extends BoundedPropagator>) - Constructor for class org.orekit.propagation.analytical.AggregateBoundedPropagator
Create a propagator by concatenating several BoundedPropagators.
AggregateBoundedPropagator(NavigableMap<AbsoluteDate, ? extends BoundedPropagator>, AbsoluteDate, AbsoluteDate) - Constructor for class org.orekit.propagation.analytical.AggregateBoundedPropagator
Create a propagator from several constituent propagators.
AggregatedClockModel - Class in org.orekit.time
Offset clock model aggregating several other clock models.
AggregatedClockModel(TimeSpanMap<ClockModel>) - Constructor for class org.orekit.time.AggregatedClockModel
Simple constructor.
AggregatedPVCoordinatesProvider - Class in org.orekit.utils
Aggreate multiple PVCoordinatesProvider instances together This can be used to describe an aircraft or surface vehicle.
AggregatedPVCoordinatesProvider(TimeSpanMap<PVCoordinatesProvider>) - Constructor for class org.orekit.utils.AggregatedPVCoordinatesProvider
Class constructor.
AggregatedPVCoordinatesProvider(TimeSpanMap<PVCoordinatesProvider>, AbsoluteDate, AbsoluteDate) - Constructor for class org.orekit.utils.AggregatedPVCoordinatesProvider
Class constructor.
AggregatedPVCoordinatesProvider.Builder - Class in org.orekit.utils
AggregatedPVCoordinatesProvider.InvalidPVProvider - Class in org.orekit.utils
Implementation of PVCoordinatesProvider that throws an illegal state exception.
AGILeapSecondFilesLoader - Class in org.orekit.time
Loader for UTC-TAI extracted from LeapSecond file from AGI.
AGILeapSecondFilesLoader(String) - Constructor for class org.orekit.time.AGILeapSecondFilesLoader
Build a loader for LeapSecond.dat file from AGI.
AGILeapSecondFilesLoader(String, DataProvidersManager) - Constructor for class org.orekit.time.AGILeapSecondFilesLoader
Build a loader for LeapSecond.dat file from AGI.
AGILeapSecondFilesLoader.Parser - Class in org.orekit.time
Internal class performing the parsing.
AGOM - org.orekit.files.ccsds.ndm.odm.omm.OmmTleKey
SGP4-XP solar radiation pressure-like coefficient.
AKELLAALFRIEND_2000 - org.orekit.files.ccsds.definitions.PocMethodType
Akella and Alfriend - 2000 method.
ALBEDO_GRID_SIZE - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey
Albedo grid size.
ALBEDO_MODEL - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey
Albedo model.
ALFANO_2005 - org.orekit.files.ccsds.definitions.PocMethodType
Alfano 2005 method.
ALFANO_2005 - org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethodType
Probability of collision computing method described in :"S.
ALFANO_MAX_PROBABILITY - org.orekit.files.ccsds.definitions.PocMethodType
Maximum conjunction probability method from Alfano.
ALFANO_PARAL_2007 - org.orekit.files.ccsds.definitions.PocMethodType
Adjoining parallelepipeds method from Alfano.
ALFANO_TUBES_2007 - org.orekit.files.ccsds.definitions.PocMethodType
Adjoining tubes method from Alfano.
ALFANO_VOXELS_2006 - org.orekit.files.ccsds.definitions.PocMethodType
Voxels method from Alfano.
Alfano2005 - Class in org.orekit.ssa.collision.shorttermencounter.probability.twod
Compute the probability of collision using the method described in :"S.
Alfano2005() - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.Alfano2005
Empty constructor.
ALFRIEND_1999 - org.orekit.files.ccsds.definitions.PocMethodType
Alfriend 1999 method.
ALFRIEND_1999 - org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethodType
Probability of collision computing method described in :"Kyle Alfriend, Maruthi Akella, Joseph Frisbee, James Foster, Deok-Jin Lee, and Matthew Wilkins.
ALFRIEND_1999_MAX - org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethodType
Probability of collision computing method described in :"Kyle Alfriend, Maruthi Akella, Joseph Frisbee, James Foster, Deok-Jin Lee, and Matthew Wilkins.
Alfriend1999 - Class in org.orekit.ssa.collision.shorttermencounter.probability.twod
Compute the probability of collision using the method described in : "Kyle Alfriend, Maruthi Akella, Joseph Frisbee, James Foster, Deok-Jin Lee, and Matthew Wilkins.
Alfriend1999() - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.Alfriend1999
Empty constructor.
Alfriend1999Max - Class in org.orekit.ssa.collision.shorttermencounter.probability.twod
Compute the probability of collision assuming the worst case described in : "Kyle Alfriend, Maruthi Akella, Joseph Frisbee, James Foster, Deok-Jin Lee, and Matthew Wilkins.
Alfriend1999Max() - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.Alfriend1999Max
Empty constructor.
alias(String) - Method in class org.orekit.utils.units.Unit
Create an alias for a unit.
AlignedAndConstrained - Class in org.orekit.attitudes
Attitude provider with one satellite vector aligned and another one constrained to two targets.
AlignedAndConstrained(Vector3D, TargetProvider, Vector3D, TargetProvider, ExtendedPositionProvider, OneAxisEllipsoid) - Constructor for class org.orekit.attitudes.AlignedAndConstrained
Simple constructor.
AlignmentDetector - Class in org.orekit.propagation.events
Finder for satellite/body alignment events in orbital plane.
AlignmentDetector(double, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AlignmentDetector
Build a new alignment detector.
AlignmentDetector(double, Orbit, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AlignmentDetector
Build a new alignment detector.
AlignmentDetector(Orbit, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AlignmentDetector
Build a new alignment detector.
AlignmentDetector(AdaptableInterval, double, int, EventHandler, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AlignmentDetector
Protected constructor with full parameters.
ALMOST_CRITICALLY_INCLINED_ORBIT - org.orekit.errors.OrekitMessages
ALMOST_CRITICALLY_INCLINED_ORBIT.
ALMOST_EQUATORIAL_ORBIT - org.orekit.errors.OrekitMessages
ALMOST_EQUATORIAL_ORBIT.
alongTileDirection(Vector3D, GeodeticPoint) - Method in class org.orekit.models.earth.tessellation.AlongTrackAiming
Find the along tile direction for tessellation at specified point.
alongTileDirection(Vector3D, GeodeticPoint) - Method in class org.orekit.models.earth.tessellation.ConstantAzimuthAiming
Find the along tile direction for tessellation at specified point.
alongTileDirection(Vector3D, GeodeticPoint) - Method in class org.orekit.models.earth.tessellation.DivertedSingularityAiming
Find the along tile direction for tessellation at specified point.
alongTileDirection(Vector3D, GeodeticPoint) - Method in interface org.orekit.models.earth.tessellation.TileAiming
Find the along tile direction for tessellation at specified point.
AlongTrackAiming - Class in org.orekit.models.earth.tessellation
Class used to orient tiles along an orbit track.
AlongTrackAiming(OneAxisEllipsoid, Orbit, boolean) - Constructor for class org.orekit.models.earth.tessellation.AlongTrackAiming
Simple constructor.
ALT_COV_REF_FRAME - org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey
Name of the reference frame in which the alternate covariance data are given.
ALT_COV_TYPE - org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey
Flag indicating the type of alternate covariance information provided.
AltCovarianceType - Enum in org.orekit.files.ccsds.ndm.cdm
Flag indicating the type of alternate covariance information provided.
ALTERNATE_NAMES - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Alternate names fir this space object.
ALTITUDE_BELOW_ALLOWED_THRESHOLD - org.orekit.errors.OrekitMessages
ALTITUDE_BELOW_ALLOWED_THRESHOLD.
AltitudeDetector - Class in org.orekit.propagation.events
Finder for satellite altitude crossing events.
AltitudeDetector(double, double, double, BodyShape) - Constructor for class org.orekit.propagation.events.AltitudeDetector
Build a new altitude detector.
AltitudeDetector(double, double, BodyShape) - Constructor for class org.orekit.propagation.events.AltitudeDetector
Build a new altitude detector.
AltitudeDetector(double, BodyShape) - Constructor for class org.orekit.propagation.events.AltitudeDetector
Build a new altitude detector.
AltitudeDetector(AdaptableInterval, double, int, EventHandler, double, BodyShape) - Constructor for class org.orekit.propagation.events.AltitudeDetector
Protected constructor with full parameters.
AMBIGUITY_NAME - Static variable in class org.orekit.estimation.measurements.gnss.InterSatellitesPhase
Deprecated.
as of 12.1 not used anymore
AMBIGUITY_NAME - Static variable in class org.orekit.estimation.measurements.gnss.OneWayGNSSPhase
Deprecated.
as of 12.1 not used anymore
AMBIGUITY_NAME - Static variable in class org.orekit.estimation.measurements.gnss.Phase
Deprecated.
as of 12.1 not used anymore
AmbiguityAcceptance - Interface in org.orekit.estimation.measurements.gnss
Interface defining ambiguity acceptance tests.
AmbiguityCache - Class in org.orekit.estimation.measurements.gnss
Cache for AmbiguityDriver.
AmbiguityCache() - Constructor for class org.orekit.estimation.measurements.gnss.AmbiguityCache
Simple constructor.
AmbiguityDriver - Class in org.orekit.estimation.measurements.gnss
Specialized ParameterDriver for ambiguity.
AmbiguityDriver(String, String, double) - Constructor for class org.orekit.estimation.measurements.gnss.AmbiguityDriver
Simple constructor.
AmbiguitySolver - Class in org.orekit.estimation.measurements.gnss
Class for solving integer ambiguity problems.
AmbiguitySolver(List<ParameterDriver>, IntegerLeastSquareSolver, AmbiguityAcceptance) - Constructor for class org.orekit.estimation.measurements.gnss.AmbiguitySolver
Simple constructor.
AMPERE - Static variable in class org.orekit.utils.units.Unit
Ampere unit.
AnalyticalSolarPositionProvider - Class in org.orekit.bodies
Class computing low-fidelity positions for the Sun.
AnalyticalSolarPositionProvider() - Constructor for class org.orekit.bodies.AnalyticalSolarPositionProvider
Constructor with default data context.
AnalyticalSolarPositionProvider(DataContext) - Constructor for class org.orekit.bodies.AnalyticalSolarPositionProvider
Constructor.
andCombine(Collection<? extends EventDetector>) - Static method in class org.orekit.propagation.events.BooleanDetector
Create a new event detector that is the logical AND of the given event detectors.
andCombine(Collection<? extends FieldEventDetector<T>>) - Static method in class org.orekit.propagation.events.FieldBooleanDetector
Create a new event detector that is the logical AND of the given event detectors.
andCombine(EventDetector...) - Static method in class org.orekit.propagation.events.BooleanDetector
Create a new event detector that is the logical AND of the given event detectors.
andCombine(FieldEventDetector<T>...) - Static method in class org.orekit.propagation.events.FieldBooleanDetector
Create a new event detector that is the logical AND of the given event detectors.
ANGLE - org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceType
Angles.
ANGLE_1 - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Rotation about first axis.
ANGLE_1 - org.orekit.files.ccsds.ndm.adm.apm.EulerKey
First body rotation angle entry.
ANGLE_1 - org.orekit.files.ccsds.ndm.tdm.ObservationType
Data: ANGLE_1 in degrees and in [-180, +360[ [deg].
ANGLE_1_DOT - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Rotation about first axis.
ANGLE_1_DOT - org.orekit.files.ccsds.ndm.adm.apm.EulerKey
First body rotation rate entry.
ANGLE_2 - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Rotation about second axis.
ANGLE_2 - org.orekit.files.ccsds.ndm.adm.apm.EulerKey
Second body rotation angle entry.
ANGLE_2 - org.orekit.files.ccsds.ndm.tdm.ObservationType
Data: ANGLE_2 in degrees and in [-180, +360[ [deg].
ANGLE_2_DOT - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Rotation about second axis.
ANGLE_2_DOT - org.orekit.files.ccsds.ndm.adm.apm.EulerKey
Second body rotation rate entry.
ANGLE_3 - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Rotation about third axis.
ANGLE_3 - org.orekit.files.ccsds.ndm.adm.apm.EulerKey
Third body rotation angle entry.
ANGLE_3_DOT - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Rotation about third axis.
ANGLE_3_DOT - org.orekit.files.ccsds.ndm.adm.apm.EulerKey
Third body rotation rate entry.
ANGLE_ANGVEL - org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceType
Angles and angular velocities.
ANGLE_GYROBIAS - org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceType
Angles and gyro biases.
ANGLE_TYPE - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Angle type entry.
ANGLE_TYPE_NOT_SUPPORTED - org.orekit.errors.OrekitMessages
ANGLE_TYPE_NOT_SUPPORTED.
angles(FieldSpacecraftState<T>) - Method in class org.orekit.utils.OccultationEngine
Compute the occultation angles as seen from a spacecraft.
angles(SpacecraftState) - Method in class org.orekit.utils.OccultationEngine
Compute the occultation angles as seen from a spacecraft.
AnglesMeasurement(AbsoluteDate, double, double, int, int, boolean, double, double) - Constructor for class org.orekit.files.ilrs.CRD.AnglesMeasurement
Constructor.
AngleType - Enum in org.orekit.files.ccsds.ndm.tdm
Antenna geometry represented in the angle date.
AngularAzEl - Class in org.orekit.estimation.measurements
Class modeling an Azimuth-Elevation measurement from a ground station.
AngularAzEl(GroundStation, AbsoluteDate, double[], double[], double[], ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.AngularAzEl
Simple constructor.
AngularAzElBuilder - Class in org.orekit.estimation.measurements.generation
Builder for AngularAzEl measurements.
AngularAzElBuilder(CorrelatedRandomVectorGenerator, GroundStation, double[], double[], ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.AngularAzElBuilder
Simple constructor.
AngularCoordinates - Class in org.orekit.utils
Simple container for rotation/rotation rate/rotation acceleration triplets.
AngularCoordinates() - Constructor for class org.orekit.utils.AngularCoordinates
Simple constructor.
AngularCoordinates(FieldRotation<U>) - Constructor for class org.orekit.utils.AngularCoordinates
Builds a AngularCoordinates from a FieldRotation<Derivative>.
AngularCoordinates(Rotation) - Constructor for class org.orekit.utils.AngularCoordinates
Builds angular coordinates with the given rotation, zero angular velocity, and zero angular acceleration.
AngularCoordinates(Rotation, Vector3D) - Constructor for class org.orekit.utils.AngularCoordinates
Builds a rotation/rotation rate pair.
AngularCoordinates(Rotation, Vector3D, Vector3D) - Constructor for class org.orekit.utils.AngularCoordinates
Builds a rotation/rotation rate/rotation acceleration triplet.
AngularCoordinates(PVCoordinates, PVCoordinates) - Constructor for class org.orekit.utils.AngularCoordinates
Build one of the rotations that transform one pv coordinates into another one.
AngularCoordinates(PVCoordinates, PVCoordinates, PVCoordinates, PVCoordinates, double) - Constructor for class org.orekit.utils.AngularCoordinates
Build the rotation that transforms a pair of pv coordinates into another one.
AngularDerivativesFilter - Enum in org.orekit.utils
Enumerate for selecting which derivatives to use in TimeStampedAngularCoordinates and TimeStampedFieldAngularCoordinates interpolation.
AngularIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical angular measurement with ionospheric delay.
AngularIonosphericDelayModifier(IonosphericModel, double) - Constructor for class org.orekit.estimation.measurements.modifiers.AngularIonosphericDelayModifier
Constructor.
AngularRaDec - Class in org.orekit.estimation.measurements
Class modeling a Right Ascension - Declination measurement from a ground point (station, telescope).
AngularRaDec(GroundStation, Frame, AbsoluteDate, double[], double[], double[], ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.AngularRaDec
Simple constructor.
AngularRaDecBuilder - Class in org.orekit.estimation.measurements.generation
Builder for AngularRaDec measurements.
AngularRaDecBuilder(CorrelatedRandomVectorGenerator, GroundStation, Frame, double[], double[], ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.AngularRaDecBuilder
Simple constructor.
AngularRadioRefractionModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical angular measurement with tropospheric radio refractive index.
AngularRadioRefractionModifier(AtmosphericRefractionModel) - Constructor for class org.orekit.estimation.measurements.modifiers.AngularRadioRefractionModifier
Constructor.
AngularSeparationDetector - Class in org.orekit.propagation.events
Detects when spacecraft comes close to a moving beacon, as seen from a moving observer.
AngularSeparationDetector(AdaptableInterval, double, int, EventHandler, PVCoordinatesProvider, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AngularSeparationDetector
Protected constructor with full parameters.
AngularSeparationDetector(PVCoordinatesProvider, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AngularSeparationDetector
Build a new angular separation detector.
AngularSeparationFromSatelliteDetector - Class in org.orekit.propagation.events
Detects when two moving objects come close to each other, as seen from spacecraft.
AngularSeparationFromSatelliteDetector(AdaptableInterval, double, int, EventHandler, PVCoordinatesProvider, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AngularSeparationFromSatelliteDetector
Protected constructor with full parameters.
AngularSeparationFromSatelliteDetector(PVCoordinatesProvider, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AngularSeparationFromSatelliteDetector
Build a new angular detachment detector.
AngularTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Deprecated.
as of 12.1, AngularRadioRefractionModifier shall be used to handle tropospheric effect on angular measurements
AngularTroposphericDelayModifier(DiscreteTroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.AngularTroposphericDelayModifier
Deprecated.
as of 12.1, AngularRadioRefractionModifier shall be used to handle tropospheric effect on angular measurements
AngularTroposphericDelayModifier(TroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.AngularTroposphericDelayModifier
Deprecated.
as of 12.1, AngularRadioRefractionModifier shall be used to handle tropospheric effect on angular measurements
AngularVelocity - Class in org.orekit.files.ccsds.ndm.adm.apm
Container for Attitude Parameter Message data lines.
AngularVelocity() - Constructor for class org.orekit.files.ccsds.ndm.adm.apm.AngularVelocity
Simple constructor.
AngularVelocityKey - Enum in org.orekit.files.ccsds.ndm.adm.apm
Keys for APM angular velocity entries.
angVel - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Angular velocity sub-sub-section.
ANGVEL - org.orekit.files.ccsds.ndm.adm.acm.RateElementsType
Angular velocity.
ANGVEL_FRAME - org.orekit.files.ccsds.ndm.adm.aem.AemMetadataKey
Reference frame for angular velocities.
ANGVEL_FRAME - org.orekit.files.ccsds.ndm.adm.apm.AngularVelocityKey
Frame in which angular velocity is defined.
ANGVEL_X - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Angular velocity about X axis.
ANGVEL_X - org.orekit.files.ccsds.ndm.adm.apm.AngularVelocityKey
Angular velocity around X axis.
ANGVEL_Y - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Angular velocity about Y axis.
ANGVEL_Y - org.orekit.files.ccsds.ndm.adm.apm.AngularVelocityKey
Angular velocity around Y axis.
ANGVEL_Z - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Angular velocity about Z axis.
ANGVEL_Z - org.orekit.files.ccsds.ndm.adm.apm.AngularVelocityKey
Angular velocity around Z axis.
ANT_NB_TYPE - org.orekit.files.rinex.section.RinexLabels
Antenna number and type.
Antenna - Class in org.orekit.gnss.antenna
GNSS antenna model.
Antenna(String, String, Map<Frequency, FrequencyPattern>) - Constructor for class org.orekit.gnss.antenna.Antenna
Simple constructor.
ANTENNA_B_SIGHT_XYZ - org.orekit.files.rinex.section.RinexLabels
Antenna bore sight.
ANTENNA_DELTA_H_E_N - org.orekit.files.rinex.section.RinexLabels
Antenna reference point.
ANTENNA_DELTA_X_Y_Z - org.orekit.files.rinex.section.RinexLabels
Antenna reference point.
ANTENNA_PHASE_CENTER - org.orekit.files.rinex.section.RinexLabels
Antenna phase center.
ANTENNA_ZERODIR_AZI - org.orekit.files.rinex.section.RinexLabels
Antenna zero direction.
ANTENNA_ZERODIR_XYZ - org.orekit.files.rinex.section.RinexLabels
Antenna zero direction.
AntexLoader - Class in org.orekit.gnss.antenna
Factory for GNSS antennas (both receiver and satellite).
AntexLoader(String) - Constructor for class org.orekit.gnss.antenna.AntexLoader
Simple constructor.
AntexLoader(String, DataProvidersManager, TimeScale) - Constructor for class org.orekit.gnss.antenna.AntexLoader
Construct a loader by specifying a DataProvidersManager.
AntexLoader(DataSource, TimeScale) - Constructor for class org.orekit.gnss.antenna.AntexLoader
Construct a loader by specifying the source of ANTEX auxiliary data files.
ANTICIPATED - org.orekit.files.ccsds.ndm.odm.ocm.ManBasis
Non-cooperative future maneuver that is anticipated (i.e.
anticipateNext(ProcessingState) - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser
Anticipate what next processing state should be.
Apm - Class in org.orekit.files.ccsds.ndm.adm.apm
This class stores all the information of the Attitude Parameter Message (APM) File parsed by APMParser.
Apm(AdmHeader, List<Segment<AdmMetadata, ApmData>>, IERSConventions, DataContext) - Constructor for class org.orekit.files.ccsds.ndm.adm.apm.Apm
Simple constructor.
ApmData - Class in org.orekit.files.ccsds.ndm.adm.apm
Container for Attitude Parameter Message data.
ApmData(CommentsContainer, AbsoluteDate, ApmQuaternion, Euler, AngularVelocity, SpinStabilized, Inertia) - Constructor for class org.orekit.files.ccsds.ndm.adm.apm.ApmData
Simple constructor.
ApmParser - Class in org.orekit.files.ccsds.ndm.adm.apm
A parser for the CCSDS APM (Attitude Parameter Message).
ApmParser(IERSConventions, boolean, DataContext, AbsoluteDate, ParsedUnitsBehavior, Function<ParseToken, List<ParseToken>>[]) - Constructor for class org.orekit.files.ccsds.ndm.adm.apm.ApmParser
Complete constructor.
ApmQuaternion - Class in org.orekit.files.ccsds.ndm.adm.apm
Container for Attitude Parameter Message quaternion logical block.
ApmQuaternion() - Constructor for class org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternion
Simple constructor.
ApmQuaternionKey - Enum in org.orekit.files.ccsds.ndm.adm.apm
Keys for APM quaternion entries.
ApmWriter - Class in org.orekit.files.ccsds.ndm.adm.apm
Writer for CCSDS Orbit Parameter Message.
ApmWriter(IERSConventions, DataContext, AbsoluteDate) - Constructor for class org.orekit.files.ccsds.ndm.adm.apm.ApmWriter
Complete constructor.
APOAPSIS_ALTITUDE - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
The distance of the furthest point in the objects orbit above the equatorial radius of the central body.
AppliedDCBS - Class in org.orekit.files.rinex
Corrections of Differential Code Biases (DCBs) applied.
AppliedDCBS(SatelliteSystem, String, String) - Constructor for class org.orekit.files.rinex.AppliedDCBS
Simple constructor.
AppliedPCVS - Class in org.orekit.files.rinex
Corrections of antenna phase center variations (PCVs) applied.
AppliedPCVS(SatelliteSystem, String, String) - Constructor for class org.orekit.files.rinex.AppliedPCVS
Simple constructor.
appliesTo(String) - Method in class org.orekit.frames.ITRFVersionLoader.ITRFVersionConfiguration
Check if this entry applies to a file name.
apply(Orbit) - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
Compute the effect of the maneuver on an orbit.
apply(Orbit) - Method in class org.orekit.propagation.analytical.J2DifferentialEffect
Compute the effect of the maneuver on an orbit.
apply(SpacecraftState) - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
Compute the effect of the maneuver on a spacecraft state.
apply(SpacecraftState) - Method in interface org.orekit.propagation.analytical.AdapterPropagator.DifferentialEffect
Apply the effect to a spacecraft state.
apply(SpacecraftState) - Method in class org.orekit.propagation.analytical.J2DifferentialEffect
Apply the effect to a spacecraft state.
applyCorrectionOnPV(CR3BPDifferentialCorrection) - Method in class org.orekit.orbits.HaloOrbit
Apply the differential correction to compute more accurate initial PV.
applyCorrectionOnPV(CR3BPDifferentialCorrection) - Method in class org.orekit.orbits.LibrationOrbit
Apply the differential correction to compute more accurate initial PV.
applyCorrectionOnPV(CR3BPDifferentialCorrection) - Method in class org.orekit.orbits.LyapunovOrbit
Apply the differential correction to compute more accurate initial PV.
applyDifferentialCorrection() - Method in class org.orekit.orbits.LibrationOrbit
Apply differential correction.
applyDynamicOutlierFilter(EstimatedMeasurement<T>, RealMatrix) - Static method in class org.orekit.estimation.sequential.KalmanEstimatorUtil
Set and apply a dynamic outlier filter on a measurement.
applyRelevantFilters(DataSource) - Method in class org.orekit.data.FiltersManager
Apply all the relevant data filters, taking care of layers.
applyResetters(FieldSpacecraftState<T>) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers
Apply resetters.
applyResetters(SpacecraftState) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers
Apply resetters.
applyTo(FieldPVCoordinates<T>) - Method in class org.orekit.utils.AngularCoordinates
Apply the rotation to a pv coordinates.
applyTo(FieldPVCoordinates<T>) - Method in class org.orekit.utils.FieldAngularCoordinates
Apply the rotation to a pv coordinates.
applyTo(PVCoordinates) - Method in class org.orekit.utils.AngularCoordinates
Apply the rotation to a pv coordinates.
applyTo(PVCoordinates) - Method in class org.orekit.utils.FieldAngularCoordinates
Apply the rotation to a pv coordinates.
applyTo(TimeStampedFieldPVCoordinates<T>) - Method in class org.orekit.utils.AngularCoordinates
Apply the rotation to a pv coordinates.
applyTo(TimeStampedFieldPVCoordinates<T>) - Method in class org.orekit.utils.FieldAngularCoordinates
Apply the rotation to a pv coordinates.
applyTo(TimeStampedPVCoordinates) - Method in class org.orekit.utils.AngularCoordinates
Apply the rotation to a pv coordinates.
applyTo(TimeStampedPVCoordinates) - Method in class org.orekit.utils.FieldAngularCoordinates
Apply the rotation to a pv coordinates.
APPROACH_ANGLE - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
The approach angle computed between Objects 1 and 2 in the RTN coordinate frame relative to object 1.
APPROX_POSITION_XYZ - org.orekit.files.rinex.section.RinexLabels
Approximative position.
approximateAsPolynomialOnly(int, AbsoluteDate, int, int, AbsoluteDate, AbsoluteDate, double) - Method in class org.orekit.utils.SecularAndHarmonic
Approximate an already fitted model to polynomial only terms.
APRIL - org.orekit.time.Month
April.
ApsideDetectionAdaptableIntervalFactory - Class in org.orekit.propagation.events.intervals
Factory class for AdaptableInterval suitable for apside detection on eccentric orbits.
ApsideDetector - Class in org.orekit.propagation.events
Finder for apside crossing events.
ApsideDetector(double) - Constructor for class org.orekit.propagation.events.ApsideDetector
Build a new instance.
ApsideDetector(double, Orbit) - Constructor for class org.orekit.propagation.events.ApsideDetector
Build a new instance.
ApsideDetector(Orbit) - Constructor for class org.orekit.propagation.events.ApsideDetector
Build a new instance.
ApsideDetector(AdaptableInterval, double, int, EventHandler) - Constructor for class org.orekit.propagation.events.ApsideDetector
Public constructor with full parameters.
AR - org.orekit.files.rinex.clock.RinexClock.ClockDataType
Data analysis for receiver clocks.
ARBITRARY_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
An arbitrary finite date.
ARC_MINUTE - Static variable in class org.orekit.utils.units.Unit
Arc minute unit.
ARC_SECOND - Static variable in class org.orekit.utils.units.Unit
Arc second unit.
ARC_SECONDS - org.orekit.data.PolynomialParser.Unit
Arc-seconds angles.
ARC_SECONDS_TO_RADIANS - Static variable in interface org.orekit.utils.Constants
Conversion factor from arc seconds to radians: 2*PI/(360*60*60).
ARC_SECONDS_TO_RADIANS - Static variable in class org.orekit.utils.units.UnitsConverter
Arcseconds to radians converter.
AREA_ALONG_OEB_INT - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
Cross-sectional area of Optimally Enclosing Box when viewed along the intermediate OEB direction.
AREA_ALONG_OEB_INT - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Cross-sectional area of Optimally Enclosing Box along Y-OEB.
AREA_ALONG_OEB_MAX - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
Cross-sectional area of Optimally Enclosing Box when viewed along the maximum OEB direction.
AREA_ALONG_OEB_MAX - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Cross-sectional area of Optimally Enclosing Box along X-OEB.
AREA_ALONG_OEB_MIN - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
Cross-sectional area of Optimally Enclosing Box when viewed along the minimum OEB direction.
AREA_ALONG_OEB_MIN - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Cross-sectional area of Optimally Enclosing Box along Z-OEB.
AREA_DRG - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
The effective area of the object exposed to atmospheric drag.
AREA_MAX_FOR_PC - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Maximum cross-sectional area for collision probability estimation purposes.
AREA_MIN_FOR_PC - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Minimum cross-sectional area for collision probability estimation purposes.
AREA_PC - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
The actual area of the object.
AREA_PC_MAX - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
Maximum area (or cross-section) of the object to be used in the calculation of the probability of collision.
AREA_PC_MIN - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
Minimum area (or cross-section) of the object to be used in the calculation of the probability of collision.
AREA_SRP - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
The effective area of the object exposed to solar radiation pressure.
AREA_TYP_FOR_PC - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Typical (50th percentile) cross-sectional area for collision probability estimation purposes.
areAdditionalDataAvailable() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the flag indicating if additional parameters are in the message.
areFeesRequired() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
Check if fees are required.
areFeesRequired() - Method in class org.orekit.gnss.metric.ntrip.NetworkRecord
Check if fees are required.
ARG_OF_PERICENTER - org.orekit.files.ccsds.ndm.odm.KeplerianElementsKey
Orbit argument of pericenter.
AS - org.orekit.files.rinex.clock.RinexClock.ClockDataType
Data analysis for satellite clocks.
asCelestialBodyFrame() - Method in class org.orekit.files.ccsds.definitions.FrameFacade
Get the associated celestial body frame.
asFrame() - Method in class org.orekit.files.ccsds.definitions.FrameFacade
Get the associated frame tree node.
AskneNordiusModel - Class in org.orekit.models.earth.troposphere
The Askne Nordius model.
AskneNordiusModel(TroposphereMappingFunction) - Constructor for class org.orekit.models.earth.troposphere.AskneNordiusModel
Create a new Askne Nordius model.
asOrbitRelativeFrame() - Method in class org.orekit.files.ccsds.definitions.FrameFacade
Get the associated orbit relative frame.
asSpacecraftBodyFrame() - Method in class org.orekit.files.ccsds.definitions.FrameFacade
Get the associated spacecraft body frame.
AST - org.orekit.files.ccsds.definitions.SpacecraftBodyFrame.BaseEquipment
Autonomous Star Tracker.
ASTRONOMICAL_DAWN_DUSK_ELEVATION - Static variable in class org.orekit.propagation.events.GroundAtNightDetector
Sun elevation at astronomical dawn/dusk (18° below horizon).
AstronomicalAmplitudeReader - Class in org.orekit.forces.gravity.potential
Parser for tides astronomical amplitude Hf.
AstronomicalAmplitudeReader(String, int, int, int, double) - Constructor for class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader
Simple constructor.
Atmosphere - Interface in org.orekit.models.earth.atmosphere
Interface for atmospheric models.
ATMOSPHERIC_MODEL - org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey
Name of atmospheric model.
ATMOSPHERIC_MODEL - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey
Name of atmospheric model.
AtmosphericRefractionModel - Interface in org.orekit.models
Defines an refraction model that can be used to correct for the apparent position of an object due to atmospheric effects.
att - org.orekit.files.ccsds.ndm.adm.acm.AcmDataSubStructureKey
Trajectory state time history section.
ATT - org.orekit.files.ccsds.ndm.adm.acm.AcmDataSubStructureKey
Attitude state time history section.
ATT - org.orekit.files.ccsds.ndm.adm.acm.AcmElements
Attitude state time history.
ATT_ACTUATOR_TYPE - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Type of actuator for attitude control.
ATT_BASIS - org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadataKey
Basis of this attitude state time history data.
ATT_BASIS_ID - org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadataKey
Identification number of the attitude determination or simulation upon which this attitude is based.
ATT_CONTROL - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Accuracy of attitude control.
ATT_CONTROL_MODE - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Attitude control mode.
ATT_ID - org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadataKey
Attitude identification number.
ATT_KNOWLEDGE - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Accuracy of attitude knowledge.
ATT_LINE - Static variable in class org.orekit.files.ccsds.ndm.adm.acm.Acm
Attitude line element for XML messages.
ATT_POINTING - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Overall accuracy of spacecraft to maintain attitude.
ATT_PREV_ID - org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadataKey
Identification number of previous attitude.
ATT_TYPE - org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadataKey
Attitude element set type.
attachTo(Frame, Transform, boolean) - Method in class org.orekit.frames.OrphanFrame
Attach the instance (and all its children down to leafs) to the main tree.
attachTo(Frame, TransformProvider, boolean) - Method in class org.orekit.frames.OrphanFrame
Attach the instance (and all its children down to leafs) to the main tree.
ATTEMPT_TO_GENERATE_MALFORMED_FILE - org.orekit.errors.OrekitMessages
ATTEMPT_TO_GENERATE_MALFORMED_FILE.
Attitude - Class in org.orekit.attitudes
This class handles attitude definition at a given date.
Attitude(Frame, TimeStampedAngularCoordinates) - Constructor for class org.orekit.attitudes.Attitude
Creates a new instance.
Attitude(AbsoluteDate, Frame, Rotation, Vector3D, Vector3D) - Constructor for class org.orekit.attitudes.Attitude
Creates a new instance.
Attitude(AbsoluteDate, Frame, AngularCoordinates) - Constructor for class org.orekit.attitudes.Attitude
Creates a new instance.
ATTITUDE_DIR - org.orekit.files.ccsds.ndm.adm.aem.AemMetadataKey
Rotation direction entry.
ATTITUDE_POINTING_LAW_DOES_NOT_POINT_TO_GROUND - org.orekit.errors.OrekitMessages
ATTITUDE_POINTING_LAW_DOES_NOT_POINT_TO_GROUND.
ATTITUDE_SOURCE - org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationKey
Source of attitude estimate.
ATTITUDE_STATES - org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationKey
Attitude states.
ATTITUDE_TYPE - org.orekit.files.ccsds.ndm.adm.aem.AemMetadataKey
Format of the data line entry.
AttitudeBuilder - Interface in org.orekit.attitudes
This interface represents a builder for attitude.
AttitudeCovariance - Class in org.orekit.files.ccsds.ndm.adm.acm
Covariance entry.
AttitudeCovariance(AttitudeCovarianceType, AbsoluteDate, String[], int) - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovariance
Simple constructor.
AttitudeCovarianceHistory - Class in org.orekit.files.ccsds.ndm.adm.acm
Covariance history.
AttitudeCovarianceHistory(AttitudeCovarianceHistoryMetadata, List<AttitudeCovariance>) - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistory
Simple constructor.
AttitudeCovarianceHistoryMetadata - Class in org.orekit.files.ccsds.ndm.adm.acm
Metadata for covariance history.
AttitudeCovarianceHistoryMetadata() - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadata
Empty constructor.
AttitudeCovarianceHistoryMetadataKey - Enum in org.orekit.files.ccsds.ndm.adm.acm
AttitudeCovarianceType - Enum in org.orekit.files.ccsds.ndm.adm.acm
Attitude covariance set type used in CCSDS Attitude Comprehensive Messages.
AttitudeDetermination - Class in org.orekit.files.ccsds.ndm.adm.acm
Attitude determination data.
AttitudeDetermination() - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination
Simple constructor.
AttitudeDeterminationKey - Enum in org.orekit.files.ccsds.ndm.adm.acm
Keys for attitude determination data entries.
AttitudeDeterminationSensor - Class in org.orekit.files.ccsds.ndm.adm.acm
Attitude determination sensor data.
AttitudeDeterminationSensor() - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationSensor
Simple constructor.
AttitudeDeterminationSensorKey - Enum in org.orekit.files.ccsds.ndm.adm.acm
Keys for attitude determination data sensor entries.
AttitudeElementsType - Enum in org.orekit.files.ccsds.ndm.adm.acm
Attitude element set type used in CCSDS Attitude Comprehensive Messages.
AttitudeEndpoints - Class in org.orekit.files.ccsds.ndm.adm
Endpoints for attitude definition.
AttitudeEndpoints() - Constructor for class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints
Empty constructor.
AttitudeEntryKey - Enum in org.orekit.files.ccsds.ndm.adm.aem
Keys for attitude entries in XML messages.
AttitudeEphemerisFile<C extends TimeStampedAngularCoordinates,​S extends AttitudeEphemerisFile.AttitudeEphemerisSegment<C>> - Interface in org.orekit.files.general
An interface for accessing the data stored in an attitude ephemeris file.
AttitudeEphemerisFile.AttitudeEphemerisSegment<C extends TimeStampedAngularCoordinates> - Interface in org.orekit.files.general
A segment of an attitude ephemeris for a satellite.
AttitudeEphemerisFile.SatelliteAttitudeEphemeris<C extends TimeStampedAngularCoordinates,​S extends AttitudeEphemerisFile.AttitudeEphemerisSegment<C>> - Interface in org.orekit.files.general
Contains the information about a single satellite from an AttitudeEphemerisFile.
AttitudeEphemerisFileParser<T extends AttitudeEphemerisFile<?,​?>> - Interface in org.orekit.files.general
Parse an ephemeris file.
AttitudeEphemerisFileWriter - Interface in org.orekit.files.general
An interface for writing out ephemeris files to disk.
AttitudeInterpolator - Class in org.orekit.attitudes
Class for attitude interpolation.
AttitudeInterpolator(Frame, TimeInterpolator<TimeStampedAngularCoordinates>) - Constructor for class org.orekit.attitudes.AttitudeInterpolator
Constructor.
AttitudeManeuver - Class in org.orekit.files.ccsds.ndm.adm.acm
Maneuver entry.
AttitudeManeuver() - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver
Build an uninitialized maneuver.
AttitudeManeuverKey - Enum in org.orekit.files.ccsds.ndm.adm.acm
Keys for attitude maneuver entries.
AttitudePhysicalProperties - Class in org.orekit.files.ccsds.ndm.adm.acm
Spacecraft physical properties.
AttitudePhysicalProperties(AbsoluteDate) - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalProperties
Simple constructor.
AttitudePhysicalPropertiesKey - Enum in org.orekit.files.ccsds.ndm.adm.acm
Keys for physical properties data entries.
attitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagatorBuilder
Sets the attitude provider.
attitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagatorBuilder
Sets the attitude provider.
attitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagatorBuilder
Sets the attitude provider.
attitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.numerical.GLONASSNumericalPropagatorBuilder
Sets the attitude provider.
AttitudeProvider - Interface in org.orekit.attitudes
This interface represents an attitude provider model set.
AttitudeProviderModifier - Interface in org.orekit.attitudes
This interface represents an attitude provider that modifies/wraps another underlying provider.
AttitudesSequence - Class in org.orekit.attitudes
This classes manages a sequence of different attitude providers that are activated in turn according to switching events.
AttitudesSequence() - Constructor for class org.orekit.attitudes.AttitudesSequence
Constructor for an initially empty sequence.
AttitudesSequence.Switch - Class in org.orekit.attitudes
Switch specification.
AttitudesSequence.SwitchHandler - Interface in org.orekit.attitudes
Interface for attitude switch notifications.
AttitudeState - Class in org.orekit.files.ccsds.ndm.adm.acm
Attitude state entry.
AttitudeState(AttitudeElementsType, RateElementsType, AbsoluteDate, String[], int) - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AttitudeState
Simple constructor.
AttitudeStateHistory - Class in org.orekit.files.ccsds.ndm.adm.acm
Attitude state history.
AttitudeStateHistory(AttitudeStateHistoryMetadata, List<AttitudeState>) - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistory
Simple constructor.
AttitudeStateHistoryMetadata - Class in org.orekit.files.ccsds.ndm.adm.acm
Metadata for attitude state history.
AttitudeStateHistoryMetadata() - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata
Simple constructor.
AttitudeStateHistoryMetadataKey - Enum in org.orekit.files.ccsds.ndm.adm.acm
AttitudeType - Enum in org.orekit.files.ccsds.ndm.adm
Enumerate for ADM attitude type.
AttitudeWriter - Class in org.orekit.files.ccsds.ndm.adm.aem
An AttitudeEphemerisFileWriter generating AEM files.
AttitudeWriter(AemWriter, AdmHeader, AemMetadata, FileFormat, String, double, int) - Constructor for class org.orekit.files.ccsds.ndm.adm.aem.AttitudeWriter
Constructor used to create a new AEM writer configured with the necessary parameters to successfully fill in all required fields that aren't part of a standard object.
ATTRACTION_COEFFICIENT - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Name of the single parameter of this model: the attraction coefficient.
ATTRACTION_COEFFICIENT_SUFFIX - Static variable in class org.orekit.forces.gravity.AbstractBodyAttraction
Suffix for parameter name for attraction coefficient enabling Jacobian processing.
ATTRACTION_COEFFICIENT_SUFFIX - Static variable in class org.orekit.forces.gravity.DeSitterRelativity
Suffix for parameter name for attraction coefficient enabling Jacobian processing.
AUGUST - org.orekit.time.Month
August.
Authentication - Enum in org.orekit.gnss.metric.ntrip
Enumerate for authentication method in DataStreamRecord.
AuxiliaryElements - Class in org.orekit.propagation.semianalytical.dsst.utilities
Container class for common parameters used by all DSST forces.
AuxiliaryElements(Orbit, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Simple constructor.
AVERAGE - org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation.StrengthLevel
Average level of activity.
AveragedCircularWithMeanAngle - Class in org.orekit.propagation.conversion.averaging.elements
Immutable class containing values of averaged circular elements from any applicable theory (with MEAN as PositionAngleType).
AveragedCircularWithMeanAngle(double, double, double, double, double, double) - Constructor for class org.orekit.propagation.conversion.averaging.elements.AveragedCircularWithMeanAngle
Constructor.
AveragedEquinoctialWithMeanAngle - Class in org.orekit.propagation.conversion.averaging.elements
Immutable class containing values of averaged equinoctial elements from any applicable theory (with MEAN as PositionAngleType).
AveragedEquinoctialWithMeanAngle(double, double, double, double, double, double) - Constructor for class org.orekit.propagation.conversion.averaging.elements.AveragedEquinoctialWithMeanAngle
Constructor.
AveragedKeplerianWithMeanAngle - Class in org.orekit.propagation.conversion.averaging.elements
Immutable class containing values of averaged Keplerian elements from any applicable theory (with MEAN as PositionAngleType).
AveragedKeplerianWithMeanAngle(double, double, double, double, double, double) - Constructor for class org.orekit.propagation.conversion.averaging.elements.AveragedKeplerianWithMeanAngle
Constructor.
AveragedOrbitalElements - Interface in org.orekit.propagation.conversion.averaging.elements
Interface for storing averaged orbital elements.
AveragedOrbitalState - Interface in org.orekit.propagation.conversion.averaging
Interface representing averaged orbital elements at a specific instant.
AVG_MANEUVER_FREQ - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Average number of orbit or attitude maneuvers per year.
AZEL - org.orekit.files.ccsds.ndm.tdm.AngleType
Azimuth, elevation.
AzimuthalGradientCoefficients - Class in org.orekit.models.earth.troposphere
Container for the azimuthal gradient coefficients gnh, geh, gnw and gew.
AzimuthalGradientCoefficients(double, double, double, double) - Constructor for class org.orekit.models.earth.troposphere.AzimuthalGradientCoefficients
Simple constructor.
AzimuthalGradientProvider - Interface in org.orekit.models.earth.troposphere
azimuthBetweenPoints(FieldGeodeticPoint<T>, FieldGeodeticPoint<T>) - Method in class org.orekit.bodies.OneAxisEllipsoid
Compute the azimuth angle from local north between the two points.
azimuthBetweenPoints(GeodeticPoint, GeodeticPoint) - Method in class org.orekit.bodies.OneAxisEllipsoid
Compute the azimuth angle from local north between the two points.

B

B - org.orekit.gnss.SignalCode
Galileo B I/NAV and B C/NAV / IRNSS B RS / GLONASS L1OCp and LO2Cp codes.
B_STAR - Static variable in class org.orekit.propagation.analytical.tle.FieldTLE
Parameter name for B* coefficient.
B_STAR - Static variable in class org.orekit.propagation.analytical.tle.TLE
Parameter name for B* coefficient.
B01 - org.orekit.gnss.Frequency
Beidou B1 (1561.098 MHz).
B02 - org.orekit.gnss.Frequency
Beidou B2 (1207.14 MHz).
B03 - org.orekit.gnss.Frequency
Beidou B3 (1268.52 MHz).
B08 - org.orekit.gnss.Frequency
Beidou B2 (B2a + B2b) (1191.795MHz).
B1A - org.orekit.gnss.Frequency
Beidou B1A (1575.42 MHz).
B1C - org.orekit.gnss.Frequency
Beidou B1C (1575.42 MHz).
B2A - org.orekit.gnss.Frequency
Beidou B2a (1176.45 MHz).
B2A - Static variable in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints
Constant for A ← B direction.
B2B - org.orekit.gnss.Frequency
Beidou B2b (1207.14 MHz).
B3A - org.orekit.gnss.Frequency
Beidou B3A (1268.52 MHz).
BACKUP - org.orekit.files.ccsds.ndm.odm.ocm.OpsStatus
Backup object.
BAR - Static variable in class org.orekit.utils.units.Unit
Bar unit.
BaseConfiguration() - Constructor for class org.orekit.files.ilrs.CRDConfiguration.BaseConfiguration
Empty constructor.
BaseRangeIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Base class modifying theoretical range measurement with ionospheric delay.
BaseRangeIonosphericDelayModifier(IonosphericModel, double) - Constructor for class org.orekit.estimation.measurements.modifiers.BaseRangeIonosphericDelayModifier
Constructor.
BaseRangeRateIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Base class modifying theoretical range-rate measurement with ionospheric delay.
BaseRangeRateIonosphericDelayModifier(IonosphericModel, double) - Constructor for class org.orekit.estimation.measurements.modifiers.BaseRangeRateIonosphericDelayModifier
Constructor.
BaseRangeRateTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Baselass modifying theoretical range-rate measurements with tropospheric delay.
BaseRangeRateTroposphericDelayModifier(DiscreteTroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.BaseRangeRateTroposphericDelayModifier
BaseRangeRateTroposphericDelayModifier(TroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.BaseRangeRateTroposphericDelayModifier
Constructor.
BaseRangeTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Base class modifying theoretical range measurements with tropospheric delay.
BaseRangeTroposphericDelayModifier(DiscreteTroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.BaseRangeTroposphericDelayModifier
Deprecated.
BaseRangeTroposphericDelayModifier(TroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.BaseRangeTroposphericDelayModifier
Constructor.
BASIC - org.orekit.gnss.metric.ntrip.Authentication
Basic.
BasicConstantThrustPropulsionModel - Class in org.orekit.forces.maneuvers.propulsion
Constant thrust propulsion model with: - Constant thrust direction in spacecraft frame - Parameter drivers (for estimation) for the thrust norm or the flow rate.
BasicConstantThrustPropulsionModel(double, double, Vector3D, String) - Constructor for class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
Simple constructor.
BasicConstantThrustPropulsionModel(double, double, Vector3D, Control3DVectorCostType, String) - Constructor for class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
Generic constructor.
basicPropagate(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Propagate an orbit without any fancy features.
basicPropagate(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AdapterPropagator
Propagate an orbit without any fancy features.
basicPropagate(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
 
basicPropagate(AbsoluteDate) - Method in class org.orekit.propagation.analytical.Ephemeris
Propagate an orbit without any fancy features.
basicPropagate(AbsoluteDate) - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Propagate an orbit without any fancy features.
basicPropagate(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Propagate an orbit without any fancy features.
basicPropagate(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
Propagate an orbit without any fancy features.
BATCH - org.orekit.files.ccsds.definitions.AdMethodType
Batch least squares.
BatchLSEstimator - Class in org.orekit.estimation.leastsquares
Least squares estimator for orbit determination.
BatchLSEstimator(LeastSquaresOptimizer, PropagatorBuilder...) - Constructor for class org.orekit.estimation.leastsquares.BatchLSEstimator
Simple constructor.
BatchLSModel - Class in org.orekit.estimation.leastsquares
BatchLSModel(PropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Constructor for class org.orekit.estimation.leastsquares.BatchLSModel
Simple constructor.
BatchLSObserver - Interface in org.orekit.estimation.leastsquares
Observer for batch least squares estimator iterations.
BCT - org.orekit.files.sp3.SP3OrbitType
broadcast.
BDS - org.orekit.files.rinex.navigation.IonosphericCorrectionType
Beidou α/β.
BDS - org.orekit.gnss.metric.ntrip.NavigationSystem
Beidou.
BDSBAS - org.orekit.files.rinex.navigation.SbasId
BeiDou Satellite-based Augmentation System.
BDT - org.orekit.gnss.ObservationTimeScale
Beidou time scale.
BDTScale - Class in org.orekit.time
Beidou system time scale.
beforeIntegration(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Method called just before integration.
beforeIntegration(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Method called just before integration.
beforeIntegration(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Method called just before integration.
beforeIntegration(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Method called just before integration.
beforeIntegration(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Method called just before integration.
BEIDOU - org.orekit.gnss.SatelliteSystem
Beidou system.
BEIDOU - org.orekit.gnss.TimeSystem
Beidou.
BEIDOU_2G - org.orekit.gnss.antenna.SatelliteType
BeiDou-2 GEO.
BEIDOU_2I - org.orekit.gnss.antenna.SatelliteType
BeiDou-2 IGSO.
BEIDOU_2M - org.orekit.gnss.antenna.SatelliteType
BeiDou-2 MEO.
BEIDOU_3G_CAST - org.orekit.gnss.antenna.SatelliteType
BeiDou-3.
BEIDOU_3I - org.orekit.gnss.antenna.SatelliteType
BeiDou-3 IGSO.
BEIDOU_3M_CAST - org.orekit.gnss.antenna.SatelliteType
BeiDou-3.
BEIDOU_3M_SECM - org.orekit.gnss.antenna.SatelliteType
BeiDou-3.
BEIDOU_3SI_CAST - org.orekit.gnss.antenna.SatelliteType
BeiDou-3.
BEIDOU_3SI_SECM - org.orekit.gnss.antenna.SatelliteType
BeiDou-3.
BEIDOU_3SM_CAST - org.orekit.gnss.antenna.SatelliteType
BeiDou-3.
BEIDOU_AV - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
Value of the earth's rotation rate in rad/s for Beidou user.
BEIDOU_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Reference epoch for BeiDou weeks: 2006-01-01T00:00:00 UTC.
BEIDOU_EPOCH - Static variable in class org.orekit.time.DateComponents
Reference epoch for BeiDou weeks: 2006-01-01.
BEIDOU_MU - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
Earth's universal gravitational parameter for Beidou user in m³/s².
BEIDOU_WEEK_NB - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
Number of weeks in the Beidou cycle.
BeidouAlmanac - Class in org.orekit.propagation.analytical.gnss.data
Class for BeiDou almanac.
BeidouAlmanac() - Constructor for class org.orekit.propagation.analytical.gnss.data.BeidouAlmanac
Build a new almanac.
BeidouCivilianNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data
Container for data contained in a Beidou civilian navigation message.
BeidouCivilianNavigationMessage(Frequency) - Constructor for class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage
Constructor.
BeidouGeo - Class in org.orekit.gnss.attitude
Attitude providers for Beidou geostationary orbit navigation satellites.
BeidouGeo(AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.BeidouGeo
Simple constructor.
BeidouIGSO - Class in org.orekit.gnss.attitude
Attitude providers for Beidou inclined geosynchronous orbit navigation satellites.
BeidouIGSO(AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.BeidouIGSO
Simple constructor.
BeidouLegacyNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data
Container for data contained in a BeiDou navigation message.
BeidouLegacyNavigationMessage() - Constructor for class org.orekit.propagation.analytical.gnss.data.BeidouLegacyNavigationMessage
Constructor.
BeidouMeo - Class in org.orekit.gnss.attitude
Attitude providers for Beidou Medium Earth Orbit navigation satellites.
BeidouMeo(AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.BeidouMeo
Simple constructor.
BeidouSatelliteType - Enum in org.orekit.propagation.analytical.gnss.data
Enumerate for Beidou satellite type.
BESSELIAN_YEAR - Static variable in interface org.orekit.utils.Constants
Duration of a Besselian year: 365.242198781 Constants.JULIAN_DAY.
beta0 - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
sqrt (1 - e2).
beta0 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
sqrt (1 - e2).
beta02 - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
1 - e2.
beta02 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
1 - e2.
BetaAngleDetector - Class in org.orekit.propagation.events
Finder for beta angle crossing events.
BetaAngleDetector(double) - Constructor for class org.orekit.propagation.events.BetaAngleDetector
Solar beta angle constructor.
BetaAngleDetector(double, PVCoordinatesProvider, Frame) - Constructor for class org.orekit.propagation.events.BetaAngleDetector
Class constructor.
BetaAngleDetector(AdaptableInterval, double, int, EventHandler, double, PVCoordinatesProvider, Frame) - Constructor for class org.orekit.propagation.events.BetaAngleDetector
Protected constructor with full parameters.
Bias<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.modifiers
Class modeling a measurement bias.
Bias(String[], double[], double[], double[], double[]) - Constructor for class org.orekit.estimation.measurements.modifiers.Bias
Simple constructor.
BIG_TRUNCATION_TOLERANCE - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Truncation tolerance for big, eccentric orbits.
BINEX - org.orekit.gnss.metric.ntrip.DataFormat
BINEX.
BistaticRange - Class in org.orekit.estimation.measurements
Class modeling a bistatic range measurement using an emitter ground station and a receiver ground station.
BistaticRange(GroundStation, GroundStation, AbsoluteDate, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.BistaticRange
Simple constructor.
BistaticRangeBuilder - Class in org.orekit.estimation.measurements.generation
Builder for BistaticRange measurements.
BistaticRangeBuilder(CorrelatedRandomVectorGenerator, GroundStation, GroundStation, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.BistaticRangeBuilder
Simple constructor.
BistaticRangeIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical bistatic range measurement with ionospheric delay.
BistaticRangeIonosphericDelayModifier(IonosphericModel, double) - Constructor for class org.orekit.estimation.measurements.modifiers.BistaticRangeIonosphericDelayModifier
Constructor.
BistaticRangeRate - Class in org.orekit.estimation.measurements
Class modeling a bistatic range rate measurement using an emitter ground station and a receiver ground station.
BistaticRangeRate(GroundStation, GroundStation, AbsoluteDate, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.BistaticRangeRate
Simple constructor.
BistaticRangeRateBuilder - Class in org.orekit.estimation.measurements.generation
Builder for BistaticRangeRate measurements.
BistaticRangeRateBuilder(CorrelatedRandomVectorGenerator, GroundStation, GroundStation, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.BistaticRangeRateBuilder
Simple constructor.
BistaticRangeRateIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical bistatic range-rate measurement with ionospheric delay.
BistaticRangeRateIonosphericDelayModifier(IonosphericModel, double) - Constructor for class org.orekit.estimation.measurements.modifiers.BistaticRangeRateIonosphericDelayModifier
Constructor.
BistaticRangeRateTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical bistatic range-rate measurements with tropospheric delay.
BistaticRangeRateTroposphericDelayModifier(DiscreteTroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.BistaticRangeRateTroposphericDelayModifier
BistaticRangeRateTroposphericDelayModifier(TroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.BistaticRangeRateTroposphericDelayModifier
Constructor.
BistaticRangeTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical bistatic range measurement with tropospheric delay.
BistaticRangeTroposphericDelayModifier(DiscreteTroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.BistaticRangeTroposphericDelayModifier
BistaticRangeTroposphericDelayModifier(TroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.BistaticRangeTroposphericDelayModifier
Constructor.
BIT_1 - org.orekit.gnss.metric.parser.DataType
1 bit.
BIT_10 - org.orekit.gnss.metric.parser.DataType
10 bits.
BIT_12 - org.orekit.gnss.metric.parser.DataType
12 bits.
BIT_2 - org.orekit.gnss.metric.parser.DataType
2 bits.
BIT_24 - org.orekit.gnss.metric.parser.DataType
24 bits.
BIT_3 - org.orekit.gnss.metric.parser.DataType
3 bits.
BIT_32 - org.orekit.gnss.metric.parser.DataType
32 bits.
BIT_4 - org.orekit.gnss.metric.parser.DataType
4 bits.
BIT_6 - org.orekit.gnss.metric.parser.DataType
6 bits.
BIT_7 - org.orekit.gnss.metric.parser.DataType
7 bits.
BIT_8 - org.orekit.gnss.metric.parser.DataType
8 bits.
blendArithmeticallyWith(FieldPVCoordinates<T>, T) - Method in class org.orekit.utils.FieldPVCoordinates
blendArithmeticallyWith(PVCoordinates, double) - Method in class org.orekit.utils.PVCoordinates
BLOCK_I - org.orekit.gnss.antenna.SatelliteType
GPS Block I : SVN 01-11.
BLOCK_II - org.orekit.gnss.antenna.SatelliteType
GPS Block II : SVN 13-21.
BLOCK_IIA - org.orekit.gnss.antenna.SatelliteType
GPS Block IIA : SVN 22-40.
BLOCK_IIF - org.orekit.gnss.antenna.SatelliteType
GPS Block IIF : SVN 62-73.
BLOCK_IIIA - org.orekit.gnss.antenna.SatelliteType
GPS Block IIIA : SVN 74-81.
BLOCK_IIR_A - org.orekit.gnss.antenna.SatelliteType
GPS Block IIR : SVN 41, 43-46, 51, 54, 56.
BLOCK_IIR_B - org.orekit.gnss.antenna.SatelliteType
GPS Block IIR : SVN 47, 59-61.
BLOCK_IIR_M - org.orekit.gnss.antenna.SatelliteType
GPS Block IIR-M : SVN 48-50, 52-53, 55, 57-58.
BlockWriter() - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.StreamingOcmWriter.BlockWriter
Empty constructor.
BodiesElements - Class in org.orekit.data
Elements of the bodies having an effect on nutation.
BodiesElements(AbsoluteDate, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.data.BodiesElements
Simple constructor.
body - org.orekit.files.ccsds.section.XmlStructureKey
Body structure.
BodyCenterPointing - Class in org.orekit.attitudes
This class handles body center pointing attitude provider.
BodyCenterPointing(Frame, Ellipsoid) - Constructor for class org.orekit.attitudes.BodyCenterPointing
Creates new instance.
BodyFacade - Class in org.orekit.files.ccsds.definitions
Facade in front of several center bodies in CCSDS messages.
BodyFacade(String, CelestialBody) - Constructor for class org.orekit.files.ccsds.definitions.BodyFacade
Simple constructor.
BodyShape - Interface in org.orekit.bodies
Interface representing the rigid surface shape of a natural body.
BooleanDetector - Class in org.orekit.propagation.events
This class provides AND and OR operations for event detectors.
BooleanDetector(List<EventDetector>, BooleanDetector.Operator, AdaptableInterval, double, int, EventHandler) - Constructor for class org.orekit.propagation.events.BooleanDetector
Private constructor with all the parameters.
booleanValue(EncodedMessage) - Method in interface org.orekit.gnss.metric.parser.DataField
Get the value of the field as a boolean.
BoundedAttitudeProvider - Interface in org.orekit.attitudes
This interface is intended for attitude ephemerides valid only during a time range.
BoundedCartesianEnergy - Class in org.orekit.control.indirect.adjoint.cost
Class for bounded energy cost with Cartesian coordinates.
BoundedCartesianEnergy(String, double, double) - Constructor for class org.orekit.control.indirect.adjoint.cost.BoundedCartesianEnergy
Constructor.
BoundedCartesianEnergy(String, double, double, EventDetectionSettings) - Constructor for class org.orekit.control.indirect.adjoint.cost.BoundedCartesianEnergy
Constructor.
BoundedPropagator - Interface in org.orekit.propagation
This interface is intended for ephemerides valid only during a time range.
BOX - org.orekit.files.ccsds.ndm.cdm.ScreenVolumeShape
Box.
BoxAndSolarArraySpacecraft - Class in org.orekit.forces
Class representing the features of a classical satellite with a convex body shape.
BoxAndSolarArraySpacecraft(double, double, double, ExtendedPVCoordinatesProvider, double, Vector3D, double, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft
Build a spacecraft model with best lighting of solar array.
BoxAndSolarArraySpacecraft(List<Panel>) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft
Build a spacecraft model.
BrouwerLyddaneOrbitalState - Class in org.orekit.propagation.conversion.averaging
Class representing an averaged orbital state as in the Brouwer-Lyddane theory.
BrouwerLyddaneOrbitalState(AbsoluteDate, AveragedKeplerianWithMeanAngle, Frame, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.conversion.averaging.BrouwerLyddaneOrbitalState
Constructor.
BrouwerLyddanePropagator - Class in org.orekit.propagation.analytical
This class propagates a SpacecraftState using the analytical Brouwer-Lyddane model (from J2 to J5 zonal harmonics).
BrouwerLyddanePropagator(Orbit, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Build a propagator from orbit and potential.
BrouwerLyddanePropagator(Orbit, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Build a propagator from orbit, mass and potential.
BrouwerLyddanePropagator(Orbit, double, UnnormalizedSphericalHarmonicsProvider, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Build a propagator from orbit, mass and potential provider.
BrouwerLyddanePropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Build a propagator from orbit, attitude provider and potential.
BrouwerLyddanePropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Build a propagator from orbit, attitude provider, mass and potential.
BrouwerLyddanePropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double, PropagationType, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Build a propagator from orbit, attitude provider, mass and potential.
BrouwerLyddanePropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double, PropagationType, double, double, int) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Build a propagator from orbit, attitude provider, mass and potential.
BrouwerLyddanePropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Build a propagator from orbit, attitude provider, mass and potential provider.
BrouwerLyddanePropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Private helper constructor.
BrouwerLyddanePropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, PropagationType, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Private helper constructor.
BrouwerLyddanePropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider, PropagationType, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Build a propagator from orbit, attitude provider, mass and potential provider.
BrouwerLyddanePropagator(Orbit, AttitudeProvider, UnnormalizedSphericalHarmonicsProvider, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Build a propagator from orbit, attitude provider and potential provider.
BrouwerLyddanePropagator(Orbit, UnnormalizedSphericalHarmonicsProvider, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Build a propagator from orbit and potential provider.
BrouwerLyddanePropagator(Orbit, UnnormalizedSphericalHarmonicsProvider, PropagationType, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Build a propagator from orbit and potential provider.
BrouwerLyddanePropagatorBuilder - Class in org.orekit.propagation.conversion
Builder for Brouwer-Lyddane propagator.
BrouwerLyddanePropagatorBuilder(Orbit, double, double, TideSystem, double, double, double, double, OrbitType, PositionAngleType, double, double) - Constructor for class org.orekit.propagation.conversion.BrouwerLyddanePropagatorBuilder
Build a new instance.
BrouwerLyddanePropagatorBuilder(Orbit, UnnormalizedSphericalHarmonicsProvider, PositionAngleType, double, double) - Constructor for class org.orekit.propagation.conversion.BrouwerLyddanePropagatorBuilder
Build a new instance.
BrouwerLyddanePropagatorBuilder(Orbit, UnnormalizedSphericalHarmonicsProvider, PositionAngleType, double, AttitudeProvider, double) - Constructor for class org.orekit.propagation.conversion.BrouwerLyddanePropagatorBuilder
Build a new instance.
BSTAR - org.orekit.files.ccsds.ndm.odm.omm.OmmTleKey
SGP/SGP4 drag-like coefficient.
BTERM - org.orekit.files.ccsds.ndm.odm.omm.OmmTleKey
SGP4-XP drag-like coefficient.
build() - Method in class org.orekit.estimation.sequential.KalmanEstimatorBuilder
Construct a KalmanEstimator from the data in this builder.
build() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimatorBuilder
Construct a KalmanEstimator from the data in this builder.
build() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanEstimatorBuilder
Construct a SemiAnalyticalUnscentedKalmanEstimator from the data in this builder.
build() - Method in class org.orekit.estimation.sequential.UnscentedKalmanEstimatorBuilder
Construct a UnscentedKalmanEstimator from the data in this builder.
build() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmParser
Build the file from parsed entries.
build() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser
Build the file from parsed entries.
build() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser
Build the file from parsed entries.
build() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmParser
Build the file from parsed entries.
build() - Method in class org.orekit.files.ccsds.ndm.NdmParser
Build the file from parsed entries.
build() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser
Build the file from parsed entries.
build() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser
Build the file from parsed entries.
build() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser
Build the file from parsed entries.
build() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser
Build the file from parsed entries.
build() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser
Build the file from parsed entries.
build() - Method in interface org.orekit.files.ccsds.utils.lexical.MessageParser
Build the file from parsed entries.
build() - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagatorBuilder
Finalizes the build.
build() - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagatorBuilder
Finalizes the build.
build() - Method in class org.orekit.propagation.analytical.gnss.SBASPropagatorBuilder
Finalizes the build.
build() - Method in class org.orekit.propagation.numerical.GLONASSNumericalPropagatorBuilder
Finalizes the build.
build() - Method in class org.orekit.utils.AggregatedPVCoordinatesProvider.Builder
Build the aggregated PVCoordinatesProvider.
build() - Method in class org.orekit.utils.WaypointPVBuilder
Build a PVCoordinatesProvider from the waypoints added to this builder.
build(boolean, boolean, RotationOrder, boolean, AbsoluteDate, double...) - Method in enum org.orekit.files.ccsds.ndm.adm.AttitudeType
Get the angular coordinates corresponding to the attitude data.
build(Frame, FieldPVCoordinatesProvider<T>, TimeStampedFieldAngularCoordinates<T>) - Method in interface org.orekit.attitudes.AttitudeBuilder
Build a filtered attitude.
build(Frame, FieldPVCoordinatesProvider<T>, TimeStampedFieldAngularCoordinates<T>) - Method in class org.orekit.attitudes.FixedFrameBuilder
Build a filtered attitude.
build(Frame, FieldPVCoordinatesProvider<T>, TimeStampedFieldAngularCoordinates<T>) - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints
Build a filtered attitude.
build(Frame, PVCoordinatesProvider, TimeStampedAngularCoordinates) - Method in interface org.orekit.attitudes.AttitudeBuilder
Build a filtered attitude.
build(Frame, PVCoordinatesProvider, TimeStampedAngularCoordinates) - Method in class org.orekit.attitudes.FixedFrameBuilder
Build a filtered attitude.
build(Frame, PVCoordinatesProvider, TimeStampedAngularCoordinates) - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints
Build a filtered attitude.
build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.AngularAzElBuilder
Generate a single measurement.
build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.AngularRaDecBuilder
Generate a single measurement.
build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.BistaticRangeBuilder
Generate a single measurement.
build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.BistaticRangeRateBuilder
Generate a single measurement.
build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.FDOABuilder
Generate a single measurement.
build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.InterSatellitesOneWayRangeRateBuilder
Generate a single measurement.
build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.InterSatellitesPhaseBuilder
Generate a single measurement.
build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.InterSatellitesRangeBuilder
Generate a single measurement.
build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in interface org.orekit.estimation.measurements.generation.MeasurementBuilder
Generate a single measurement.
build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.MultiplexedMeasurementBuilder
Generate a single measurement.
build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.OneWayGNSSPhaseBuilder
Generate a single measurement.
build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.OneWayGNSSRangeBuilder
Generate a single measurement.
build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.OneWayGNSSRangeRateBuilder
Generate a single measurement.
build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.PositionBuilder
Generate a single measurement.
build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.PVBuilder
Generate a single measurement.
build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.RangeBuilder
Generate a single measurement.
build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.RangeRateBuilder
Generate a single measurement.
build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.TDOABuilder
Generate a single measurement.
build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.TurnAroundRangeBuilder
Generate a single measurement.
build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.gnss.PhaseBuilder
Generate a single measurement.
build(AbsoluteDate, SpacecraftState[]) - Method in interface org.orekit.estimation.measurements.generation.MeasurementBuilder
Generate a single measurement.
buildAcmParser() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
buildAcmWriter() - Method in class org.orekit.files.ccsds.ndm.WriterBuilder
buildAdditionalDerivativesProvider() - Method in interface org.orekit.control.indirect.shooting.propagation.AdjointDynamicsProvider
Builds adjoint derivatives provider.
buildAdditionalDerivativesProvider() - Method in class org.orekit.control.indirect.shooting.propagation.CartesianAdjointDynamicsProvider
Builds adjoint derivatives provider.
buildAemParser() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Build a parser for Attitude Ephemeris Messages.
buildAemWriter() - Method in class org.orekit.files.ccsds.ndm.WriterBuilder
Build a writer for Attitude Ephemeris Messages.
buildApmParser() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Build a parser for Attitude Parameters Messages.
buildApmWriter() - Method in class org.orekit.files.ccsds.ndm.WriterBuilder
Build a writer for Attitude Parameters Messages.
buildAttitudeProvider(AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame, int) - Method in enum org.orekit.gnss.antenna.SatelliteType
Build an attitude provider suitable for this satellite type.
buildBasicGradientSpacecraftState(SpacecraftState, int, AttitudeProvider) - Static method in class org.orekit.propagation.integration.AbstractGradientConverter
Process a state into a Gradient version without force model parameter.
buildBox(double, double, double, double, double, double, double) - Static method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Build the panels of a simple parallelepipedic box.
buildCdmParser() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Build a parser for Conjunction Data Messages.
buildCdmWriter() - Method in class org.orekit.files.ccsds.ndm.WriterBuilder
Build a writer for Conjunction Data Messages.
Builder() - Constructor for class org.orekit.utils.AggregatedPVCoordinatesProvider.Builder
Create a builder using the AggregatedPVCoordinatesProvider.InvalidPVProvider as the initial provider.
Builder(PVCoordinatesProvider) - Constructor for class org.orekit.utils.AggregatedPVCoordinatesProvider.Builder
Create a builder using the provided initial provider.
buildFieldAdditionalDerivativesProvider(Field<T>) - Method in interface org.orekit.control.indirect.shooting.propagation.AdjointDynamicsProvider
Builds Field adjoint derivatives provider.
buildFieldAdditionalDerivativesProvider(Field<T>) - Method in class org.orekit.control.indirect.shooting.propagation.CartesianAdjointDynamicsProvider
Builds Field adjoint derivatives provider.
buildFieldGradientCartesianVector(T[]) - Static method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointEquationTerm
Build a Cartesian vector whose components are independent variables for automatic differentiation at order 1.
buildFieldPropagator(FieldSpacecraftState<Gradient>) - Method in class org.orekit.control.indirect.shooting.AbstractFixedBoundaryCartesianSingleShooting
Create Gradient numerical propagator.
buildFieldPropagator(FieldSpacecraftState<Gradient>) - Method in class org.orekit.control.indirect.shooting.AbstractIndirectShooting
Create Gradient numerical propagator.
buildFlatArray(Flattener, double) - Static method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Build a coefficients array in flat form.
buildFromCustomAttitude(AttitudeProvider, Vector3D) - Static method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider
Build a ThrustDirectionAndAttitudeProvider where the attitude is provided by an external.
buildFromDirectionInFrame(Frame, ThrustDirectionProvider, Vector3D) - Static method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider
Build a ThrustDirectionAndAttitudeProvider by a variable direction in a custom frame.
buildFromDirectionInLOF(LOF, ThrustDirectionProvider, Vector3D) - Static method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider
Build a ThrustDirectionAndAttitudeProvider by a variable direction in a Local Orbital Frame.
buildFromFixedDirectionInSatelliteFrame(Vector3D) - Static method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider
Build a ThrustDirectionAndAttitudeProvider from a fixed direction in the satellite frame.
buildGradientCartesianVector(double[]) - Static method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointEquationTerm
Build a Cartesian vector whose components are independent variables for automatic differentiation at order 1.
buildIdentityMatrix2() - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities
Build the identity matrix of order 2.
buildIdentityMatrix4() - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities
Build the identity matrix of order 4.
buildIntegrator(Field<T>, Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.AdamsBashforthFieldIntegratorBuilder
Build a first order integrator.
buildIntegrator(Field<T>, Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.AdamsMoultonFieldIntegratorBuilder
Build a first order integrator.
buildIntegrator(Field<T>, Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.ClassicalRungeKuttaFieldIntegratorBuilder
Build a first order integrator.
buildIntegrator(Field<T>, Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.DormandPrince54FieldIntegratorBuilder
Build a first order integrator.
buildIntegrator(Field<T>, Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.DormandPrince853FieldIntegratorBuilder
Build a first order integrator.
buildIntegrator(Field<T>, Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.EulerFieldIntegratorBuilder
Build a first order integrator.
buildIntegrator(Field<T>, Orbit, OrbitType) - Method in interface org.orekit.propagation.conversion.FieldODEIntegratorBuilder
Build a first order integrator.
buildIntegrator(Field<T>, Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.GillFieldIntegratorBuilder
Build a first order integrator.
buildIntegrator(Field<T>, Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.HighamHall54FieldIntegratorBuilder
Build a first order integrator.
buildIntegrator(Field<T>, Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.LutherFieldIntegratorBuilder
Build a first order integrator.
buildIntegrator(Field<T>, Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.MidpointFieldIntegratorBuilder
Build a first order integrator.
buildIntegrator(Field<T>, Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.ThreeEighthesFieldIntegratorBuilder
Build a first order integrator.
buildIntegrator(FieldOrbit<T>, OrbitType) - Method in class org.orekit.propagation.conversion.AbstractFieldIntegratorBuilder
Build a first order integrator.
buildIntegrator(FieldOrbit<T>, OrbitType) - Method in interface org.orekit.propagation.conversion.FieldODEIntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.AdamsBashforthIntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.AdamsMoultonIntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.ClassicalRungeKuttaIntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.DormandPrince54IntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.DormandPrince853IntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.EulerIntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.GillIntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.GraggBulirschStoerIntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.HighamHall54IntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.LutherIntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.MidpointIntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in interface org.orekit.propagation.conversion.ODEIntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.ThreeEighthesIntegratorBuilder
Build a first order integrator.
buildIntegrator(AbsolutePVCoordinates) - Method in interface org.orekit.propagation.conversion.ODEIntegratorBuilder
Build a first order integrator.
buildIntegrator(FieldAbsolutePVCoordinates<T>) - Method in interface org.orekit.propagation.conversion.FieldODEIntegratorBuilder
Build a first order integrator.
buildLeastSquaresModel(PropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Method in class org.orekit.propagation.conversion.AbstractAnalyticalPropagatorBuilder
Build a new batch least squares model.
buildLeastSquaresModel(PropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder
Build a new batch least squares model.
buildLeastSquaresModel(PropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Method in class org.orekit.propagation.conversion.EphemerisPropagatorBuilder
Build a new batch least squares model.
buildLeastSquaresModel(PropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
Build a new batch least squares model.
buildLeastSquaresModel(PropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
Build a new batch least squares model.
buildNdmParser() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Build a parser for Navigation Data Messages.
buildNdmWriter() - Method in class org.orekit.files.ccsds.ndm.WriterBuilder
Build a writer for Navigation Data Messages.
buildOcmParser() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Build a parser for Orbit Comprehensive Messages.
buildOcmWriter() - Method in class org.orekit.files.ccsds.ndm.WriterBuilder
Build a writer for Orbit Comprehensive Messages.
buildOemParser() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Build a parser for Orbit Ephemeris Messages.
buildOemWriter() - Method in class org.orekit.files.ccsds.ndm.WriterBuilder
Build a writer for Orbit Ephemeris Messages.
buildOmmParser() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Build a parser for Orbit Mean elements Messages.
buildOmmWriter() - Method in class org.orekit.files.ccsds.ndm.WriterBuilder
Build a writer for Orbit Mean elements Messages.
buildOpmParser() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Build a parser for Orbit Parameters Messages.
buildOpmWriter() - Method in class org.orekit.files.ccsds.ndm.WriterBuilder
Build a writer for Orbit Parameters Messages.
buildPanels(double, double, double, ExtendedPVCoordinatesProvider, double, Vector3D, double, double, double, double) - Static method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Build the panels of a simple parallelepiped box plus one solar array panel.
buildPropagator() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
Build a propagator from current value of selected normalized parameters.
buildPropagator(double[]) - Method in class org.orekit.propagation.conversion.BrouwerLyddanePropagatorBuilder
Build a propagator.
buildPropagator(double[]) - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder
Build a propagator.
buildPropagator(double[]) - Method in class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder
Build a propagator.
buildPropagator(double[]) - Method in class org.orekit.propagation.conversion.EphemerisPropagatorBuilder
Build a propagator.
buildPropagator(double[]) - Method in class org.orekit.propagation.conversion.KeplerianPropagatorBuilder
Build a propagator.
buildPropagator(double[]) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
Build a propagator.
buildPropagator(double[]) - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
Build a propagator.
buildPropagator(double[]) - Method in class org.orekit.propagation.conversion.TLEPropagatorBuilder
Build a propagator.
buildPropagator(SpacecraftState) - Method in class org.orekit.control.indirect.shooting.AbstractFixedBoundaryCartesianSingleShooting
Create numerical propagator.
buildPropagator(SpacecraftState) - Method in class org.orekit.control.indirect.shooting.AbstractIndirectShooting
Create numerical propagator.
buildReferenceSlot(O) - Method in class org.orekit.orbits.WalkerConstellation
Create the reference slot, which is satellite 0 in plane 0.
buildRegularSlots(O) - Method in class org.orekit.orbits.WalkerConstellation
Create the regular slots.
buildRow(int, int, double) - Static method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Build a coefficients row.
buildSimpleZone(double, double[]...) - Static method in class org.orekit.models.earth.tessellation.EllipsoidTessellator
Build a simple zone (connected zone without holes).
buildSimpleZone(double, GeodeticPoint...) - Static method in class org.orekit.models.earth.tessellation.EllipsoidTessellator
Build a simple zone (connected zone without holes).
buildSlot(WalkerConstellationSlot<O>, int, double) - Method in class org.orekit.orbits.WalkerConstellation
Create one offset slot from an already existing slot.
buildTdmParser() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Build a parser for Tracking Data Messages.
buildTdmWriter() - Method in class org.orekit.files.ccsds.ndm.WriterBuilder
Build a writer for Tracking Data Messages.
buildTermsList(String) - Static method in class org.orekit.utils.units.Parser
Build the list of terms corresponding to a units specification.
buildTokens(boolean, boolean, String, String, Map<String, String>, int, String) - Method in class org.orekit.files.ccsds.ndm.adm.RotationXmlTokenBuilder
Create a list of parse tokens.
buildTokens(boolean, boolean, String, String, Map<String, String>, int, String) - Method in class org.orekit.files.ccsds.utils.lexical.MessageVersionXmlTokenBuilder
Create a list of parse tokens.
buildTokens(boolean, boolean, String, String, Map<String, String>, int, String) - Method in class org.orekit.files.ccsds.utils.lexical.RegularXmlTokenBuilder
Create a list of parse tokens.
buildTokens(boolean, boolean, String, String, Map<String, String>, int, String) - Method in class org.orekit.files.ccsds.utils.lexical.UserDefinedXmlTokenBuilder
Create a list of parse tokens.
buildTokens(boolean, boolean, String, String, Map<String, String>, int, String) - Method in interface org.orekit.files.ccsds.utils.lexical.XmlTokenBuilder
Create a list of parse tokens.
buildUncachedITRF(EOPHistory, UTCScale) - Static method in class org.orekit.frames.FramesFactory
Build an uncached International Terrestrial Reference Frame with specific EOP history.
buildUncachedITRF(UT1Scale) - Method in class org.orekit.frames.AbstractFrames
 
buildUncachedITRF(UT1Scale) - Method in interface org.orekit.frames.Frames
Build an uncached International Terrestrial Reference Frame with specific EOP history.
buildZeroMatrix2() - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities
Build the empty matrix of order 2.
buildZeroMatrix4() - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities
Build the empty matrix of order 4.
BULLETINA_FILENAME - Static variable in class org.orekit.frames.FramesFactory
Default regular expression for the BulletinA files (IAU1980 and IAU2000 compatibles).
BULLETINB_1980_FILENAME - Static variable in class org.orekit.frames.FramesFactory
Default regular expression for the BulletinB files (IAU1980 compatibles).
BULLETINB_2000_FILENAME - Static variable in class org.orekit.frames.FramesFactory
Default regular expression for the BulletinB files (IAU2000 compatibles).
BurstSelector - Class in org.orekit.time
Selector generating high rate bursts of dates separated by some rest period.
BurstSelector(int, double, double, TimeScale) - Constructor for class org.orekit.time.BurstSelector
Simple constructor.
BUS_MODEL - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Bus model name.
BWLS - org.orekit.files.ccsds.definitions.OdMethodType
Batch Weighted Least Squares.
ByteArrayEncodedMessage - Class in org.orekit.gnss.metric.parser
Encoded message as a byte array.
ByteArrayEncodedMessage(byte[]) - Constructor for class org.orekit.gnss.metric.parser.ByteArrayEncodedMessage
Simple constructor.

C

C - org.orekit.gnss.SignalCode
GPS C/A / GLONASS C/A / Galileo C / SBAS C/A / QZSS C/A / QZSS C/B / IRNSS C RS(P) codes.
C_2FASX4 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
C_2FASX4.
C_3FASX6 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
C_3FASX6.
C_FASX2 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
C_FASX2.
C_G22 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
C_G22.
C_G32 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
C_G32.
C_G44 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
C_G44.
C_G52 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
C_G52.
C_G54 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
C_G54.
C0 - org.orekit.gnss.ObservationType
Pseudorange for Rinex3.
C01 - org.orekit.gnss.Frequency
In the ANTEX files, both C01 and C02 refer to Beidou B1 signal (1561.098 MHz).
C02 - org.orekit.gnss.Frequency
In the ANTEX files, both C01 and C02 refer to Beidou B1 signal (1561.098 MHz).
C05 - org.orekit.gnss.Frequency
In the ANTEX files, C05 appears without much reference for consistency with Rinex 4 tables, we assume it is B2a (1176.45 MHz).
C06 - org.orekit.gnss.Frequency
In the ANTEX files, C06 appears without much reference, we assume it is B2 (1207.14 MHz).
C07 - org.orekit.gnss.Frequency
In the ANTEX files, C07 seems to refer to a signal close to E06, probably B3...
C08 - org.orekit.gnss.Frequency
In the ANTEX files, C08 appears without much reference for consistency with Rinex 4 tables, we assume it is B2 (B2a+B2b) (1191.795 MHz).
c1 - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
C1 from SPTRCK #3.
c1 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
C1 from SPTRCK #3.
C1 - org.orekit.gnss.ObservationType
Pseudorange GPS L1 / GLONASS G1 / Galileo E2-L1-E1 / SBAS L1 for Rinex2.
C1A - org.orekit.gnss.ObservationType
Pseudorange Galileo E1 A / Beidou B1A for Rinex3.
C1B - org.orekit.gnss.ObservationType
Pseudorange Galileo E1 I/NAV OS/CS/SoL / QZSS geo signal for Rinex3.
C1C - org.orekit.gnss.ObservationType
Pseudorange GPS L1 C/A / GLONASS G1 C/A / Galileo E1 C / SBAS L1 C/A / QZSS L1 C/A for Rinex3.
C1D - org.orekit.gnss.ObservationType
Pseudorange Beidou B1 Data for Rinex3.
C1E - org.orekit.gnss.ObservationType
Pseudorange QZSS L1 C/B for Rinex4.
C1I - org.orekit.gnss.ObservationType
Pseudorange Beidou B1 I for Rinex3.02.
C1L - org.orekit.gnss.ObservationType
Pseudorange GPS L1 L1C(P) / QZSS L1 L1C(P) for Rinex3, Beidou B1A for Rinex3.03.
C1L - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
C1L.
C1M - org.orekit.gnss.ObservationType
Pseudorange GPS L1 M for Rinex3.
C1P - org.orekit.gnss.ObservationType
Pseudorange GPS L1 P(AS off) / GLONASS G1 P / Beidou C1 Pilot for Rinex3.
C1Q - org.orekit.gnss.ObservationType
Pseudorange Beidou B1 Q for Rinex3.02.
C1S - org.orekit.gnss.ObservationType
Pseudorange GPS L1 L1C(D) / QZSS L1 L1C(D) for Rinex3, Beidou B1A for Rinex3.03.
C1SS - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
C1SS.
C1W - org.orekit.gnss.ObservationType
Pseudorange GPS L1 Z-tracking and similar (AS on) for Rinex3.
C1X - org.orekit.gnss.ObservationType
Pseudorange GPS L1 L1C (D+P) / Galileo E1 B+C / QZSS L1 L1C(D+P) / Beidou B1 Data+Pilot for Rinex3.
C1Y - org.orekit.gnss.ObservationType
Pseudorange GPS L1 Y for Rinex3.
C1Z - org.orekit.gnss.ObservationType
Pseudorange Galileo E1 C1Z A+B+C / QZSS L1 L1-SAIF for Rinex3, Beidou B1A for Rinex3.03.
c2 - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
C2 from SPTRCK #3.
c2 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
C2 from SPTRCK #3.
C2 - org.orekit.gnss.ObservationType
Pseudorange GPS L2 / GLONASS G2 / Beidou B02 for Rinex2.
C2C - org.orekit.gnss.ObservationType
Pseudorange GPS L2 C/A / GLONASS G2 C/A for Rinex3.
C2D - org.orekit.gnss.ObservationType
Pseudorange GPS L1(C/A)+(P2-P1) (semi-codeless) for Rinex3.
C2I - org.orekit.gnss.ObservationType
Pseudorange Beidou B1 I for Rinex3.03.
C2L - org.orekit.gnss.ObservationType
Pseudorange GPS L2 L2C(L) / QZSS L2 L2C(2) for Rinex3.
C2M - org.orekit.gnss.ObservationType
Pseudorange GPS L2 M for Rinex3.
C2P - org.orekit.gnss.ObservationType
Pseudorange GPS L2 P(AS off) / GLONASS G2 P for Rinex3.
C2Q - org.orekit.gnss.ObservationType
Pseudorange Beidou B1 Q for Rinex3.03.
C2S - org.orekit.gnss.ObservationType
Pseudorange GPS L2 L2C(M) / QZSS L2 L2C(M) for Rinex3.
C2W - org.orekit.gnss.ObservationType
Pseudorange GPS L2 Z-tracking and similar (AS on) for Rinex3.
C2X - org.orekit.gnss.ObservationType
Pseudorange GPS L2 L2C (M+L) / QZSS L2 L2C(M+L) for Rinex3, Beidou B1 I+Q for Rinex3.03.
C2Y - org.orekit.gnss.ObservationType
Pseudorange GPS L2 Y for Rinex3.
C3I - org.orekit.gnss.ObservationType
Pseudorange GLONASS G3 I for Rinex3.
C3Q - org.orekit.gnss.ObservationType
Pseudorange GLONASS G3 Q for Rinex3.
C3X - org.orekit.gnss.ObservationType
Pseudorange GLONASS G3 I+Q for Rinex3.
c4 - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
C4 from SPTRCK #3.
c4 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
C4 from SPTRCK #3.
C4A - org.orekit.gnss.ObservationType
Pseudorange GLONASS G1a L1OCd for Rinex3.
C4B - org.orekit.gnss.ObservationType
Pseudorange GLONASS G1a L1OCp for Rinex3.
C4X - org.orekit.gnss.ObservationType
Pseudorange GLONASS G1a L1OCd+L1OCd for Rinex3.
C5 - org.orekit.gnss.ObservationType
Pseudorange GPS L5 / Galileo E5a / SBAS L5 for Rinex2.
C5A - org.orekit.gnss.ObservationType
Pseudorange IRNSS L5 A for Rinex3.
C5B - org.orekit.gnss.ObservationType
Pseudorange IRNSS L5 B for Rinex3.
C5C - org.orekit.gnss.ObservationType
Pseudorange IRNSS L5 C for Rinex3.
C5D - org.orekit.gnss.ObservationType
Pseudorange QZSS L5 D / Beidou B2a Data for Rinex3.
C5I - org.orekit.gnss.ObservationType
Pseudorange GPS L5 I/ Galileo E5a F/NAV OS / SBAS L5 I / QZSS L5 I for Rinex3.
C5P - org.orekit.gnss.ObservationType
Pseudorange QZSS L5 P / Beidou B2a Pilot for Rinex3.
C5Q - org.orekit.gnss.ObservationType
Pseudorange GPS L5 Q/ Galileo E5a Q / SBAS L5 Q / QZSS L5 Q for Rinex3.
C5X - org.orekit.gnss.ObservationType
Pseudorange GPS L5 I+Q/ Galileo E5a I+Q / SBAS L5 I+Q / QZSS L5 I+Q / IRNSS L5 B+C / Beidou B2a Data+Pilot for Rinex3.
C5Z - org.orekit.gnss.ObservationType
Pseudorange QZSS L5 D+P for Rinex3.
C6 - org.orekit.gnss.ObservationType
Pseudorange Galileo E6 / Beidou B03 for Rinex2.
C6A - org.orekit.gnss.ObservationType
Pseudorange Galileo E6 A PRS / GLONASS G2a L2CSI / Beidou B3A for Rinex3.
C6B - org.orekit.gnss.ObservationType
Pseudorange Galileo E6 B C/NAV CS / GLONASS G2a L2OCp for Rinex3.
C6C - org.orekit.gnss.ObservationType
Pseudorange Galileo E6 C no data for Rinex3.
C6D - org.orekit.gnss.ObservationType
Pseudorange Beidou B3A for Rinex3.
C6E - org.orekit.gnss.ObservationType
Pseudorange QZSS L6E for Rinex3.
C6I - org.orekit.gnss.ObservationType
Pseudorange Beidou B3 I for Rinex3.
C6L - org.orekit.gnss.ObservationType
Pseudorange QZSS LEX(6) L for Rinex3.
C6P - org.orekit.gnss.ObservationType
Pseudorange Beidou B3A for Rinex3.
C6Q - org.orekit.gnss.ObservationType
Pseudorange Beidou B3 Q for Rinex3.
C6S - org.orekit.gnss.ObservationType
Pseudorange QZSS LEX(6) S for Rinex3.
C6X - org.orekit.gnss.ObservationType
Pseudorange Galileo E6 B+C / QZSS LEX(6) S+L / Beidou B3 I+Q / GLONASS G2a L2CSI+L2OCp for Rinex3.
C6Z - org.orekit.gnss.ObservationType
Pseudorange Galileo E6 A+B+C / QZSS L6(D+E) / Beidou B3A for Rinex3.
C7 - org.orekit.gnss.ObservationType
Pseudorange Galileo E5b / Beidou B02 for Rinex2.
C7D - org.orekit.gnss.ObservationType
Pseudorange Beidou B2b Data for Rinex3.
C7I - org.orekit.gnss.ObservationType
Pseudorange Galileo E5b I I/NAV OS/CS/SoL / Beidou B2 I for Rinex3.
C7P - org.orekit.gnss.ObservationType
Pseudorange Beidou B2b Pilot for Rinex3.
C7Q - org.orekit.gnss.ObservationType
Pseudorange Galileo Q no data / Beidou B2 Q for Rinex3.
C7X - org.orekit.gnss.ObservationType
Pseudorange Galileo E5b I+Q / Beidou B2 I+Q for Rinex3.
C7Z - org.orekit.gnss.ObservationType
Pseudorange Beidou B2b Data+Pilot for Rinex3.
C8 - org.orekit.gnss.ObservationType
Pseudorange Galileo E5a+b for Rinex2.
C8D - org.orekit.gnss.ObservationType
Pseudorange Beidou B2(B2a+B2b) Data for Rinex3.
C8I - org.orekit.gnss.ObservationType
Pseudorange Galileo E5(E5a+E5b) I for Rinex3.
C8P - org.orekit.gnss.ObservationType
Pseudorange Beidou B2(B2a+B2b) Pilot for Rinex3.
C8Q - org.orekit.gnss.ObservationType
Pseudorange Galileo E5(E5a+E5b) Q for Rinex3.
C8X - org.orekit.gnss.ObservationType
Pseudorange Galileo E5(E5a+E5b) I+Q / Beidou B2(B2a+B2b) Data+Pilot for Rinex3.
C9A - org.orekit.gnss.ObservationType
Pseudorange IRNSS S A for Rinex3.
C9B - org.orekit.gnss.ObservationType
Pseudorange IRNSS S B for Rinex3.
C9C - org.orekit.gnss.ObservationType
Pseudorange IRNSS S C for Rinex3.
C9X - org.orekit.gnss.ObservationType
Pseudorange IRNSS S B+C for Rinex3.
CA - org.orekit.gnss.ObservationType
Pseudorange GPS L1 C/A / GLONASS G1 C/A for Rinex2.
CachedNormalizedSphericalHarmonicsProvider - Class in org.orekit.forces.gravity.potential
CachedNormalizedSphericalHarmonicsProvider(NormalizedSphericalHarmonicsProvider, double, int, int, double, double) - Constructor for class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
Simple constructor.
cachesTidalCorrection() - Method in class org.orekit.frames.EOPHistory
Check if the instance caches tidal corrections.
calculateBetaAngle(FieldSpacecraftState<T>, FieldPVCoordinatesProvider<T>) - Static method in class org.orekit.propagation.events.FieldBetaAngleDetector
Calculate the beta angle between the orbit plane and the celestial body.
calculateBetaAngle(FieldSpacecraftState<T>, FieldPVCoordinatesProvider<T>, Frame) - Static method in class org.orekit.propagation.events.FieldBetaAngleDetector
Calculate the beta angle between the orbit plane and the celestial body.
calculateBetaAngle(SpacecraftState, PVCoordinatesProvider) - Static method in class org.orekit.propagation.events.BetaAngleDetector
Calculate the beta angle between the orbit plane and the celestial body.
calculateBetaAngle(SpacecraftState, PVCoordinatesProvider, Frame) - Static method in class org.orekit.propagation.events.BetaAngleDetector
Calculate the beta angle between the orbit plane and the celestial body.
CALCULATED - org.orekit.files.ccsds.ndm.cdm.CovarianceMethod
Calculated covariance.
calculateField(double, double, double) - Method in class org.orekit.models.earth.GeoMagneticField
Calculate the magnetic field at the specified geodetic point identified by latitude, longitude and altitude.
calculatePointAlongArc(double) - Method in class org.orekit.bodies.LoxodromeArc
Calculate a point at a specific percentage along the arc.
Calibration(AbsoluteDate, int, String, int, int, double, double, double, double, double, double, double, int, int, int, int, double) - Constructor for class org.orekit.files.ilrs.CRD.Calibration
Constructor.
CalibrationDetail(AbsoluteDate, int, String, int, int, double, double, double, double, double, double, double, int, int, int, int, double) - Constructor for class org.orekit.files.ilrs.CRD.CalibrationDetail
Constructor.
CalibrationTargetConfiguration() - Constructor for class org.orekit.files.ilrs.CRDConfiguration.CalibrationTargetConfiguration
Empty constructor.
canAdd(int, int) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Check if coefficients can be added.
CANDIDATE - org.orekit.files.ccsds.ndm.odm.ocm.ManBasis
Proposed operational or hypothetical future maneuver.
CANNOT_CHANGE_COVARIANCE_TYPE_IF_DEFINED_IN_LOF - org.orekit.errors.OrekitMessages
CANNOT_CHANGE_COVARIANCE_TYPE_IF_DEFINED_IN_LOF.
CANNOT_CHANGE_COVARIANCE_TYPE_IF_DEFINED_IN_NON_INERTIAL_FRAME - org.orekit.errors.OrekitMessages
CANNOT_CHANGE_COVARIANCE_TYPE_IF_DEFINED_IN_NON_INERTIAL_FRAME.
CANNOT_COMPUTE_AIMING_AT_SINGULAR_POINT - org.orekit.errors.OrekitMessages
CANNOT_COMPUTE_AIMING_AT_SINGULAR_POINT.
CANNOT_COMPUTE_LAGRANGIAN - org.orekit.errors.OrekitMessages
CANNOT_COMPUTE_LAGRANGIAN.
CANNOT_ESTIMATE_PRECESSION_WITHOUT_PROPER_DERIVATIVES - org.orekit.errors.OrekitMessages
CANNOT_ESTIMATE_PRECESSION_WITHOUT_PROPER_DERIVATIVES.
CANNOT_FIND_SATELLITE_IN_SYSTEM - org.orekit.errors.OrekitMessages
CANNOT_FIND_SATELLITE_IN_SYSTEM.
CANNOT_PARSE_BOTH_TAU_AND_GAMMA - org.orekit.errors.OrekitMessages
CANNOT_PARSE_BOTH_TAU_AND_GAMMA.
CANNOT_PARSE_GNSS_DATA - org.orekit.errors.OrekitMessages
CANNOT_PARSE_GNSS_DATA.
CANNOT_PARSE_SOURCETABLE - org.orekit.errors.OrekitMessages
CANNOT_PARSE_SOURCETABLE.
CANNOT_START_PROPAGATION_FROM_INFINITY - org.orekit.errors.OrekitMessages
CANNOT_START_PROPAGATION_FROM_INFINITY.
CANONICAL_I_J - Static variable in class org.orekit.estimation.measurements.gnss.Dipole
Canonical dipole, with primary vector set to Vector3D.PLUS_I and secondary vector set to Vector3D.PLUS_J.
CanonicalSaastamoinenModel - Class in org.orekit.models.earth.troposphere
The canonical Saastamoinen model.
CanonicalSaastamoinenModel() - Constructor for class org.orekit.models.earth.troposphere.CanonicalSaastamoinenModel
Create a new Saastamoinen model for the troposphere using the given environmental conditions and table from the reference book.
canReceiveNMEA() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord
Check if caster can receive NMEA messages.
CARRIER_PHASE - org.orekit.gnss.MeasurementType
Carrier-phase measurement.
CARRIER_POWER - org.orekit.files.ccsds.ndm.tdm.ObservationType
Data: Carrier power [dBW].
CarrierPhase - Enum in org.orekit.gnss.metric.ntrip
Enumerate for carrier phase in DataStreamRecord.
CARTESIAN - org.orekit.orbits.OrbitType
Type for orbital representation in CartesianOrbit and FieldCartesianOrbit parameters.
CartesianAdjointDerivativesProvider - Class in org.orekit.control.indirect.adjoint
Class defining the adjoint dynamics, as defined in the Pontryagin Maximum Principle, in the case where Cartesian coordinates in an inertial frame are the dependent variable.
CartesianAdjointDerivativesProvider(CartesianCost, CartesianAdjointEquationTerm...) - Constructor for class org.orekit.control.indirect.adjoint.CartesianAdjointDerivativesProvider
Constructor.
CartesianAdjointDynamicsProvider - Class in org.orekit.control.indirect.shooting.propagation
Class for Cartesian adjoint derivatives provider (both standard and Field).
CartesianAdjointDynamicsProvider(CartesianCost, CartesianAdjointEquationTerm...) - Constructor for class org.orekit.control.indirect.shooting.propagation.CartesianAdjointDynamicsProvider
Constructor.
CartesianAdjointEquationTerm - Interface in org.orekit.control.indirect.adjoint
Interface to define terms in the adjoint equations and Hamiltonian for Cartesian coordinates.
CartesianAdjointInertialTerm - Class in org.orekit.control.indirect.adjoint
Class defining inertial forces' contributions in the adjoint equations for Cartesian coordinates.
CartesianAdjointInertialTerm(Frame) - Constructor for class org.orekit.control.indirect.adjoint.CartesianAdjointInertialTerm
Constructor.
CartesianAdjointJ2Term - Class in org.orekit.control.indirect.adjoint
Class defining a (constant) J2 contributions in the adjoint equations for Cartesian coordinates.
CartesianAdjointJ2Term(double, double, double, Frame) - Constructor for class org.orekit.control.indirect.adjoint.CartesianAdjointJ2Term
Constructor.
CartesianAdjointKeplerianTerm - Class in org.orekit.control.indirect.adjoint
Class defining the Keplerian contributions in the adjoint equations for Cartesian coordinates.
CartesianAdjointKeplerianTerm(double) - Constructor for class org.orekit.control.indirect.adjoint.CartesianAdjointKeplerianTerm
Constructor.
CartesianAdjointSingleBodyTerm - Class in org.orekit.control.indirect.adjoint
Class defining the contributions of a point-mass, single body gravity in the adjoint equations for Cartesian coordinates.
CartesianAdjointSingleBodyTerm(double, ExtendedPositionProvider) - Constructor for class org.orekit.control.indirect.adjoint.CartesianAdjointSingleBodyTerm
Constructor.
CartesianAdjointThirdBodyTerm - Class in org.orekit.control.indirect.adjoint
Class defining the contributions of a point-mass, third body in the adjoint equations for Cartesian coordinates.
CartesianAdjointThirdBodyTerm(double, ExtendedPositionProvider) - Constructor for class org.orekit.control.indirect.adjoint.CartesianAdjointThirdBodyTerm
Constructor.
CartesianBoundaryConditionChecker - Interface in org.orekit.control.indirect.shooting.boundary
Interface defining convergence criterion when the terminal condition is on a Cartesian state.
cartesianBuilder(OneAxisEllipsoid) - Static method in class org.orekit.utils.WaypointPVBuilder
Construct a waypoint builder interpolating points using a linear cartesian interpolation.
CartesianCost - Interface in org.orekit.control.indirect.adjoint.cost
Interface to definite cost function in the frame of Pontryagin's Maximum Principle using Cartesian coordinates.
CartesianCovariance - Class in org.orekit.files.ccsds.ndm.odm
Container for OPM/OMM/OCM Cartesian covariance matrix.
CartesianCovariance(Supplier<FrameFacade>) - Constructor for class org.orekit.files.ccsds.ndm.odm.CartesianCovariance
Create an empty data set.
CartesianCovarianceKey - Enum in org.orekit.files.ccsds.ndm.odm
CartesianCovarianceUtils - Class in org.orekit.utils
Utility class for conversions related to Cartesian covariance matrices.
CartesianCovarianceWriter - Class in org.orekit.files.ccsds.ndm.odm
Writer for covariance matrix data.
CartesianCovarianceWriter(String, String, CartesianCovariance) - Constructor for class org.orekit.files.ccsds.ndm.odm.CartesianCovarianceWriter
Create a writer.
CartesianDerivativesFilter - Enum in org.orekit.utils
Enumerate for selecting which derivatives to use in TimeStampedPVCoordinates and TimeStampedFieldPVCoordinates interpolation.
CartesianOrbit - Class in org.orekit.orbits
This class holds Cartesian orbital parameters.
CartesianOrbit(Orbit) - Constructor for class org.orekit.orbits.CartesianOrbit
Constructor from any kind of orbital parameters.
CartesianOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CartesianOrbit
Constructor from Cartesian parameters.
CartesianOrbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.CartesianOrbit
Constructor from Cartesian parameters.
CARTP - org.orekit.files.ccsds.ndm.odm.ocm.OrbitElementsType
Cartesian 3-element position (X, Y, Z).
CARTPV - org.orekit.files.ccsds.ndm.odm.ocm.OrbitElementsType
Cartesian 6-element position and velocity (X, Y, Z, XD, YD, ZD).
CARTPVA - org.orekit.files.ccsds.ndm.odm.ocm.OrbitElementsType
Cartesian 9-element position, velocity and acceleration (X, Y, Z, XD, YD, ZD, XDD, YDD, ZDD).
CAS - org.orekit.gnss.metric.ntrip.RecordType
Casters.
CasterRecord - Class in org.orekit.gnss.metric.ntrip
Caster record in source table.
CasterRecord(String) - Constructor for class org.orekit.gnss.metric.ntrip.CasterRecord
Build a caster record by parsing a source table line.
CATALOG_NAME - org.orekit.files.ccsds.ndm.adm.acm.AcmMetadataKey
Specification of satellite catalog source.
CATALOG_NAME - org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey
Satellite catalog used for the object.
CATALOG_NAME - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Specification of satellite catalog source.
CB - org.orekit.gnss.ObservationType
Pseudorange GPS L1C for Rinex2.
CC - org.orekit.gnss.ObservationType
Pseudorange GPS L2C for Rinex2.
CCSDS_ACM_VERS - Static variable in class org.orekit.files.ccsds.ndm.adm.acm.AcmWriter
Version number implemented.
CCSDS_AEM_VERS - Static variable in class org.orekit.files.ccsds.ndm.adm.aem.AemWriter
Version number implemented.
CCSDS_APM_VERS - Static variable in class org.orekit.files.ccsds.ndm.adm.apm.ApmWriter
Version number implemented.
CCSDS_CDM_VERS - Static variable in class org.orekit.files.ccsds.ndm.cdm.CdmWriter
Version number implemented.
CCSDS_DATE_INVALID_LENGTH_TIME_FIELD - org.orekit.errors.OrekitMessages
CCSDS_DATE_INVALID_LENGTH_TIME_FIELD.
CCSDS_DATE_INVALID_PREAMBLE_FIELD - org.orekit.errors.OrekitMessages
CCSDS_DATE_INVALID_PREAMBLE_FIELD.
CCSDS_DATE_MISSING_AGENCY_EPOCH - org.orekit.errors.OrekitMessages
CCSDS_DATE_MISSING_AGENCY_EPOCH.
CCSDS_DIFFERENT_LVLH_DEFINITION - org.orekit.errors.OrekitMessages
CCSDS_DIFFERENT_LVLH_DEFINITION.
CCSDS_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Reference epoch for CCSDS Time Code Format (CCSDS 301.0-B-4): 1958-01-01T00:00:00 International Atomic Time (not UTC).
CCSDS_EPOCH - Static variable in class org.orekit.time.DateComponents
Reference epoch for CCSDS Time Code Format (CCSDS 301.0-B-4): 1958-01-01.
CCSDS_INCOMPATIBLE_KEYS_BOTH_USED - org.orekit.errors.OrekitMessages
CCSDS_INCOMPATIBLE_KEYS_BOTH_USED.
CCSDS_INCOMPLETE_DATA - org.orekit.errors.OrekitMessages
CCSDS_INCOMPLETE_DATA.
CCSDS_INCONSISTENT_NUMBER_OF_ATTITUDE_STATES - org.orekit.errors.OrekitMessages
CCSDS_INCONSISTENT_NUMBER_OF_ATTITUDE_STATES.
CCSDS_INCONSISTENT_TIME_SYSTEMS - org.orekit.errors.OrekitMessages
CCSDS_INCONSISTENT_TIME_SYSTEMS.
CCSDS_INVALID_FRAME - org.orekit.errors.OrekitMessages
CCSDS_INVALID_FRAME.
CCSDS_INVALID_ROTATION_SEQUENCE - org.orekit.errors.OrekitMessages
CCSDS_INVALID_ROTATION_SEQUENCE.
CCSDS_KEYWORD_NOT_ALLOWED_IN_VERSION - org.orekit.errors.OrekitMessages
CCSDS_KEYWORD_NOT_ALLOWED_IN_VERSION.
CCSDS_MANEUVER_MISSING_TIME - org.orekit.errors.OrekitMessages
CCSDS_MANEUVER_MISSING_TIME.
CCSDS_MANEUVER_UNITS_WRONG_NB_COMPONENTS - org.orekit.errors.OrekitMessages
CCSDS_MANEUVER_UNITS_WRONG_NB_COMPONENTS.
CCSDS_MISSING_KEYWORD - org.orekit.errors.OrekitMessages
CCSDS_MISSING_KEYWORD.
CCSDS_MISSING_SENSOR_INDEX - org.orekit.errors.OrekitMessages
CCSDS_MISSING_SENSOR_INDEX.
CCSDS_OCM_VERS - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.OcmWriter
Version number implemented.
CCSDS_OEM_VERS - Static variable in class org.orekit.files.ccsds.ndm.odm.oem.OemWriter
Version number implemented.
CCSDS_OMM_VERS - Static variable in class org.orekit.files.ccsds.ndm.odm.omm.OmmWriter
Version number implemented.
CCSDS_OPM_VERS - Static variable in class org.orekit.files.ccsds.ndm.odm.opm.OpmWriter
Version number implemented.
CCSDS_SENSOR_INDEX_ALREADY_USED - org.orekit.errors.OrekitMessages
CCSDS_SENSOR_INDEX_ALREADY_USED.
CCSDS_TDM_KEYWORD_NOT_FOUND - org.orekit.errors.OrekitMessages
CCSDS_TDM_KEYWORD_NOT_FOUND.
CCSDS_TDM_MISSING_RANGE_UNITS_CONVERTER - org.orekit.errors.OrekitMessages
CCSDS_TDM_MISSING_RANGE_UNITS_CONVERTER.
CCSDS_TDM_VERS - Static variable in class org.orekit.files.ccsds.ndm.tdm.TdmWriter
Version number implemented.
CCSDS_TIME_SYSTEM_NOT_IMPLEMENTED - org.orekit.errors.OrekitMessages
CCSDS_TIME_SYSTEM_NOT_IMPLEMENTED.
CCSDS_TIME_SYSTEM_NOT_READ_YET - org.orekit.errors.OrekitMessages
CCSDS_TIME_SYSTEM_NOT_READ_YET.
CCSDS_UNEXPECTED_KEYWORD - org.orekit.errors.OrekitMessages
CCSDS_UNEXPECTED_KEYWORD.
CCSDS_UNKNOWN_ATTITUDE_TYPE - org.orekit.errors.OrekitMessages
CCSDS_UNKNOWN_ATTITUDE_TYPE.
CCSDS_UNKNOWN_CONVENTIONS - org.orekit.errors.OrekitMessages
CCSDS_UNKNOWN_CONVENTIONS.
CCSDS_UNKNOWN_GM - org.orekit.errors.OrekitMessages
CCSDS_UNKNOWN_GM.
CCSDS_UNKNOWN_SPACECRAFT_MASS - org.orekit.errors.OrekitMessages
CCSDS_UNKNOWN_SPACECRAFT_MASS.
CCSDS_UNSUPPORTED_ELEMENT_SET_TYPE - org.orekit.errors.OrekitMessages
CCSDS_UNSUPPORTED_ELEMENT_SET_TYPE.
CCSDS_UNSUPPORTED_RETROGRADE_EQUINOCTIAL - org.orekit.errors.OrekitMessages
CCSDS_UNSUPPORTED_RETROGRADE_EQUINOCTIAL.
CD - org.orekit.gnss.ObservationType
Pseudorange GLONASS G2 for Rinex2.
CD_AREA_OVER_MASS - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
The object’s Cd x A/m used to propagate the state vector and covariance to TCA.
Cdm - Class in org.orekit.files.ccsds.ndm.cdm
This class stores all the information of the Conjunction Data Message (CDM) File parsed by CdmParser.
Cdm(CdmHeader, List<CdmSegment>, IERSConventions, DataContext) - Constructor for class org.orekit.files.ccsds.ndm.cdm.Cdm
Simple constructor.
CDM_MSG_LINK - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Unique identifier of Conjunction Data Message linked to this Orbit Data Message.
CdmData - Class in org.orekit.files.ccsds.ndm.cdm
Container for Conjunction Data Message data.
CdmData(CommentsContainer, ODParameters, AdditionalParameters, StateVector, RTNCovariance) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmData
Constructor with RTN covariance.
CdmData(CommentsContainer, ODParameters, AdditionalParameters, StateVector, RTNCovariance, AdditionalCovarianceMetadata) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmData
Constructor with RTN covariance.
CdmData(CommentsContainer, ODParameters, AdditionalParameters, StateVector, RTNCovariance, SigmaEigenvectorsCovariance, AdditionalCovarianceMetadata) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmData
Constructor with RTN and sigma/eigenvector covariance.
CdmData(CommentsContainer, ODParameters, AdditionalParameters, StateVector, RTNCovariance, XYZCovariance, AdditionalCovarianceMetadata) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmData
Constructor with RTN and XYZ covariance.
CdmHeader - Class in org.orekit.files.ccsds.ndm.cdm
Header of a CCSDS Conjunction Data Message.
CdmHeader() - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmHeader
Constructor.
CdmHeaderKey - Enum in org.orekit.files.ccsds.ndm.cdm
Keywords allowed in CdmHeader.
CdmHeaderProcessingState - Class in org.orekit.files.ccsds.ndm.cdm
CdmHeaderProcessingState(CdmParser) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmHeaderProcessingState
Simple constructor.
CdmMessageWriter - Class in org.orekit.files.ccsds.ndm.cdm
Cdm message writer.
CdmMessageWriter(String, String, double, ContextBinding) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter
Constructor used to create a new NDM writer configured with the necessary parameters to successfully fill in all required fields that aren't part of a standard object.
CdmMetadata - Class in org.orekit.files.ccsds.ndm.cdm
This class gathers the meta-data present in the Conjunction Data Message (CDM).
CdmMetadata() - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Simple constructor.
CdmMetadata(DataContext) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Simple constructor.
CdmMetadataKey - Enum in org.orekit.files.ccsds.ndm.cdm
Keys for CDM container entries.
CdmMetadataWriter - Class in org.orekit.files.ccsds.ndm.cdm
Writer for Metadata for CCSDS Conjunction Data Messages.
CdmMetadataWriter(CdmMetadata) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmMetadataWriter
Simple constructor.
CdmParser - Class in org.orekit.files.ccsds.ndm.cdm
Base class for Conjunction Data Message parsers.
CdmParser(IERSConventions, boolean, DataContext, ParsedUnitsBehavior, Function<ParseToken, List<ParseToken>>[]) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmParser
Complete constructor.
CdmRelativeMetadata - Class in org.orekit.files.ccsds.ndm.cdm
This class gathers the relative meta-data present in the Conjunction Data Message (CDM).
CdmRelativeMetadata() - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Simple constructor.
CdmRelativeMetadataKey - Enum in org.orekit.files.ccsds.ndm.cdm
Keys for CDM container entries.
CdmSegment - Class in org.orekit.files.ccsds.ndm.cdm
This class stores the metadata and data for one object.
CdmSegment(CdmMetadata, CdmData) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmSegment
Simple constructor.
CdmWriter - Class in org.orekit.files.ccsds.ndm.cdm
Writer for CCSDS Conjunction Data Message.
CdmWriter(IERSConventions, DataContext) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmWriter
Complete constructor.
CDRG_DRG - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [7,7].
CDRG_DRG - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [7,7].
CDRG_N - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [7,3].
CDRG_NDOT - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [7,6].
CDRG_R - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [7,1].
CDRG_RDOT - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [7,4].
CDRG_T - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [7,2].
CDRG_TDOT - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [7,5].
CDRG_X - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [7,1].
CDRG_XDOT - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [7,4].
CDRG_Y - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [7,2].
CDRG_YDOT - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [7,5].
CDRG_Z - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [7,3].
CDRG_ZDOT - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [7,6].
CELESTIAL_SOURCE - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Source and version of celestial body (e.g.
CelestialBodies - Interface in org.orekit.bodies
Commonly used celestial bodies.
CelestialBody - Interface in org.orekit.bodies
Interface for celestial bodies like Sun, Moon or solar system planets.
CelestialBodyFactory - Class in org.orekit.bodies
Factory class for bodies of the solar system.
CelestialBodyFrame - Enum in org.orekit.files.ccsds.definitions
Frames used in CCSDS Orbit Data Messages.
CelestialBodyLoader - Interface in org.orekit.bodies
Interface for loading celestial bodies.
CelestialBodyPointed - Class in org.orekit.attitudes
This class handles a celestial body pointed attitude provider.
CelestialBodyPointed(Frame, PVCoordinatesProvider, Vector3D, Vector3D, Vector3D) - Constructor for class org.orekit.attitudes.CelestialBodyPointed
Creates new instance.
CellInterpolator - Class in org.orekit.models.earth.weather
Interpolator within a grid cell.
CENTER_NAME - org.orekit.files.ccsds.ndm.adm.AdmMetadataKey
Center name entry.
CENTER_NAME - org.orekit.files.ccsds.ndm.odm.CommonMetadataKey
Center name entry.
CENTER_NAME - org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadataKey
Origin of the reference frame of the trajectory.
CENTER_OF_MASS_XYZ - org.orekit.files.rinex.section.RinexLabels
Center of mass.
CenterName - Enum in org.orekit.files.ccsds.definitions
Orbit central bodies for which a Celestial body can be created.
CENTRAL_ATTRACTION_COEFFICIENT - Static variable in class org.orekit.forces.gravity.NewtonianAttraction
Name of the single parameter of this model: the central attraction coefficient.
CENTRAL_ATTRACTION_COEFFICIENT - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction
Name of the single parameter of this model: the central attraction coefficient.
CENTRAL_BODY_ROTATION - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey
Central body angular rotation rate.
CHAN_1997 - org.orekit.files.ccsds.definitions.PocMethodType
Chan 1997 method.
CHAN_1997 - org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethodType
Probability of collision computing method described in :
"Chan,K.
CHAN_2003 - org.orekit.files.ccsds.definitions.PocMethodType
Chan 2003 method.
Chan1997 - Class in org.orekit.ssa.collision.shorttermencounter.probability.twod
Compute the probability of collision using the method described in :
"Chan, K.
Chan1997() - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.Chan1997
Empty constructor.
change(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.FieldAbstractStateModifier
Change main state.
change(SpacecraftState) - Method in class org.orekit.propagation.AbstractStateModifier
Change main state.
CHANGE_IN_TWO_RECEIVER_ONE_SATELLITE_CARRIER_PHASE - org.orekit.files.sp3.DataUsed
Change in 2-receiver/1-satellite carrier phase.
CHANGE_IN_TWO_RECEIVER_ONE_SATELLITE_CODE_PHASE - org.orekit.files.sp3.DataUsed
Change in 2-receiver/1-satellite code phase.
CHANGE_IN_TWO_RECEIVER_TWO_SATELLITE_CARRIER_PHASE - org.orekit.files.sp3.DataUsed
Change in 2-receiver/2-satellite carrier phase.
CHANGE_IN_TWO_RECEIVER_TWO_SATELLITE_CODE_PHASE - org.orekit.files.sp3.DataUsed
Change in 2-receiver/2-satellite code phase.
CHANGE_IN_UNDIFFERENTIATED_CARRIER_PHASE - org.orekit.files.sp3.DataUsed
Change in undifferenciated carrier phase.
CHANGE_IN_UNDIFFERENTIATED_CODE_PHASE - org.orekit.files.sp3.DataUsed
Change in undifferenciated code phase.
changeCovarianceFrame(FieldOrbit<T>, Frame) - Method in class org.orekit.propagation.FieldStateCovariance
Get the covariance in the output frame.
changeCovarianceFrame(FieldOrbit<T>, LOF) - Method in class org.orekit.propagation.FieldStateCovariance
Get the covariance in a given local orbital frame.
changeCovarianceFrame(Orbit, Frame) - Method in class org.orekit.propagation.StateCovariance
Get the covariance in the output frame.
changeCovarianceFrame(Orbit, LOF) - Method in class org.orekit.propagation.StateCovariance
Get the covariance in a given local orbital frame.
changeCovarianceType(FieldOrbit<T>, OrbitType, PositionAngleType) - Method in class org.orekit.propagation.FieldStateCovariance
Get the covariance matrix in another orbit type.
changeCovarianceType(Orbit, OrbitType, PositionAngleType) - Method in class org.orekit.propagation.StateCovariance
Get the covariance matrix in another orbit type.
changeFrame(SP3, Frame) - Static method in class org.orekit.files.sp3.SP3
Change the frame of an SP3 file.
changeReferenceFrame(Frame, RealMatrix, AbsoluteDate, Frame) - Static method in class org.orekit.utils.CartesianCovarianceUtils
Convert input position-velocity covariance matrix between reference frames.
ChaoMappingFunction - Class in org.orekit.models.earth.troposphere
Chao mapping function for radio wavelengths.
ChaoMappingFunction() - Constructor for class org.orekit.models.earth.troposphere.ChaoMappingFunction
Builds a new instance.
checkAllowed(double, Object, String, double, double) - Method in class org.orekit.files.ccsds.section.CommentsContainer
Complain if a key is not allowed.
checkDatesConsistency(AbsoluteDate, AbsoluteDate, double) - Static method in class org.orekit.time.TimeStampedPair
Check date consistency.
checkDimension(int, ParameterDriversList, ParameterDriversList, ParameterDriversList) - Static method in class org.orekit.estimation.sequential.KalmanEstimatorUtil
Check dimension.
checkEOPContinuity(double) - Method in class org.orekit.frames.EOPHistory
Check Earth orientation parameters continuity.
checkException() - Method in class org.orekit.gnss.metric.ntrip.NtripClient
Check if any of the streaming thread has thrown an exception.
checkExternalFrame(Enum<?>, Enum<?>) - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints
Check external frame is properly initialized.
checkFrameAndOrbitTypeConsistency(Frame, OrbitType) - Static method in class org.orekit.propagation.StateCovariance
Check constructor's inputs consistency.
checkInputConsistency(List<SpacecraftState>, TimeInterpolator<SpacecraftState>, List<StateCovariance>, TimeInterpolator<TimeStampedPair<Orbit, StateCovariance>>) - Static method in class org.orekit.propagation.analytical.Ephemeris
Check input consistency between states, covariances and their associated interpolators.
checkInterpolatorCompatibilityWithSampleSize(FieldTimeInterpolator<? extends FieldTimeStamped<T>, T>, int) - Static method in class org.orekit.time.AbstractFieldTimeInterpolator
Method checking if given interpolator is compatible with given sample size.
checkInterpolatorCompatibilityWithSampleSize(TimeInterpolator<? extends TimeStamped>, int) - Static method in class org.orekit.time.AbstractTimeInterpolator
Method checking if given interpolator is compatible with given sample size.
checkMandatoryEntriesExceptExternalFrame(double, Enum<?>, Enum<?>, Enum<?>) - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints
Check is mandatory entries except external frame have been initialized.
checkNotNaN(double, String) - Method in class org.orekit.files.ccsds.section.CommentsContainer
Complain if a field is NaN.
checkNotNegative(int, String) - Method in class org.orekit.files.ccsds.section.CommentsContainer
Complain if a field is negative.
checkNotNull(Object, Enum<?>) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Complain if a field is null.
checkNotNull(Object, String) - Method in class org.orekit.files.ccsds.section.CommentsContainer
Complain if a field is null.
checkOrbitsConsistency(Collection<Orbit>) - Static method in class org.orekit.orbits.AbstractOrbitInterpolator
Check orbits consistency by comparing their gravitational parameters µ.
checkParity(int, int) - Static method in class org.orekit.gnss.rflink.gps.SubFrame
Check parity.
checkSampleAndInterpolatorConsistency(List<SpacecraftState>, boolean, boolean) - Static method in class org.orekit.propagation.SpacecraftStateInterpolator
Check that an interpolator exist for given sample state definition.
checkScreenVolumeConditions() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Check screen volume conditions.
checkStatesAndCovariancesConsistency(List<SpacecraftState>, List<StateCovariance>) - Static method in class org.orekit.propagation.analytical.Ephemeris
Check that given states and covariances are consistent.
checkStatesDefinitionsConsistency(List<SpacecraftState>) - Static method in class org.orekit.propagation.SpacecraftStateInterpolator
Check that all state are either orbit defined or based on absolute position-velocity-acceleration.
checkStep(double) - Method in class org.orekit.propagation.conversion.AbstractFixedStepFieldIntegratorBuilder
Check that given step size is not equal to 0.
checkTimeSystems() - Method in class org.orekit.files.ccsds.ndm.odm.oem.Oem
Check that, according to the CCSDS standard, every OEMBlock has the same time system.
checkUnit(Unit) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
Check if parsed unit is compatible with field type.
ChronologicalComparator - Class in org.orekit.time
Comparator for TimeStamped instance.
ChronologicalComparator() - Constructor for class org.orekit.time.ChronologicalComparator
Simple constructor.
CIPM2007 - Class in org.orekit.models.earth.weather.water
Official model CIPM-2007 (identical to CIPM-1981/91) from Comité International des Poids et Mesures.
CIPM2007() - Constructor for class org.orekit.models.earth.weather.water.CIPM2007
 
CIRCULAR - org.orekit.orbits.OrbitType
Type for orbital representation in CircularOrbit and FieldCircularOrbit parameters.
CircularFieldOfView - Class in org.orekit.geometry.fov
Class representing a spacecraft sensor Field Of View with circular shape.
CircularFieldOfView(Vector3D, double, double) - Constructor for class org.orekit.geometry.fov.CircularFieldOfView
Build a new instance.
CircularLatitudeArgumentUtility - Class in org.orekit.orbits
Utility methods for converting between different latitude arguments used by CircularOrbit.
CircularOrbit - Class in org.orekit.orbits
This class handles circular orbital parameters.
CircularOrbit(double, double, double, double, double, double, double, double, double, double, double, double, PositionAngleType, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CircularOrbit
Creates a new instance with derivatives and with cached position angle same as value inputted.
CircularOrbit(double, double, double, double, double, double, double, double, double, double, double, double, PositionAngleType, PositionAngleType, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CircularOrbit
Creates a new instance.
CircularOrbit(double, double, double, double, double, double, PositionAngleType, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CircularOrbit
Creates a new instance without derivatives and with cached position angle same as value inputted.
CircularOrbit(double, double, double, double, double, double, PositionAngleType, PositionAngleType, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CircularOrbit
Creates a new instance.
CircularOrbit(Orbit) - Constructor for class org.orekit.orbits.CircularOrbit
Constructor from any kind of orbital parameters.
CircularOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CircularOrbit
Constructor from Cartesian parameters.
CircularOrbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.CircularOrbit
Constructor from Cartesian parameters.
CIRF_CONVENTIONS_1996_ACCURATE_EOP - org.orekit.frames.Predefined
CIRF frame, IERS 1996 conventions, with accurate EOP interpolation.
CIRF_CONVENTIONS_1996_SIMPLE_EOP - org.orekit.frames.Predefined
CIRF frame, IERS 1996 conventions, with simple EOP interpolation.
CIRF_CONVENTIONS_2003_ACCURATE_EOP - org.orekit.frames.Predefined
CIRF frame, IERS 2003 conventions, with accurate EOP interpolation.
CIRF_CONVENTIONS_2003_SIMPLE_EOP - org.orekit.frames.Predefined
CIRF frame, IERS 2003 conventions, with simple EOP interpolation.
CIRF_CONVENTIONS_2010_ACCURATE_EOP - org.orekit.frames.Predefined
CIRF frame, IERS 2010 conventions, with accurate EOP interpolation.
CIRF_CONVENTIONS_2010_SIMPLE_EOP - org.orekit.frames.Predefined
CIRF frame, IERS 2010 conventions, with simple EOP interpolation.
CIVIL_DAWN_DUSK_ELEVATION - Static variable in class org.orekit.propagation.events.GroundAtNightDetector
Sun elevation at civil dawn/dusk (6° below horizon).
CivilianNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data
Container for data contained in a GPS/QZNSS civilian navigation message.
CivilianNavigationMessage(boolean, double, double, int) - Constructor for class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage
Constructor.
CjSjCoefficient - Class in org.orekit.propagation.semianalytical.dsst.utilities
Compute the Sj(k, h) and the Cj(k, h) series and their partial derivatives with respect to k and h.
CjSjCoefficient(double, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
Cj(k, h) and Sj(k, h) constructor.
CK2 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
CK2.
CK4 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
CK4.
ClassicalRungeKuttaFieldIntegratorBuilder<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.conversion
Builder for ClassicalRungeKuttaFieldIntegrator.
ClassicalRungeKuttaFieldIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.ClassicalRungeKuttaFieldIntegratorBuilder
Constructor.
ClassicalRungeKuttaFieldIntegratorBuilder(T) - Constructor for class org.orekit.propagation.conversion.ClassicalRungeKuttaFieldIntegratorBuilder
Constructor using a "fielded" step.
ClassicalRungeKuttaIntegrationSettings - Class in org.orekit.control.indirect.shooting.propagation
Integration settings using the classical Runge-Kutta 4 scheme.
ClassicalRungeKuttaIntegrationSettings(double) - Constructor for class org.orekit.control.indirect.shooting.propagation.ClassicalRungeKuttaIntegrationSettings
Constructor.
ClassicalRungeKuttaIntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for ClassicalRungeKuttaIntegrator.
ClassicalRungeKuttaIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.ClassicalRungeKuttaIntegratorBuilder
Build a new instance.
CLASSIFICATION - org.orekit.files.ccsds.ndm.cdm.CdmHeaderKey
User-defined free-text message classification or caveats of this CDM.
CLASSIFICATION - org.orekit.files.ccsds.section.HeaderKey
Classification.
CLASSIFICATION_TYPE - org.orekit.files.ccsds.ndm.odm.omm.OmmTleKey
Classifiation type.
ClasspathCrawler - Class in org.orekit.data
Provider for data files stored as resources in the classpath.
ClasspathCrawler(ClassLoader, String...) - Constructor for class org.orekit.data.ClasspathCrawler
Build a data classpath crawler.
ClasspathCrawler(String...) - Constructor for class org.orekit.data.ClasspathCrawler
Build a data classpath crawler.
clear() - Method in class org.orekit.propagation.events.handlers.FieldRecordAndContinue
Clear all stored events.
clear() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue
Clear all stored events.
clear() - Method in class org.orekit.propagation.sampling.FieldStepHandlerMultiplexer
Remove all handlers managed by this multiplexer.
clear() - Method in class org.orekit.propagation.sampling.StepHandlerMultiplexer
Remove all handlers managed by this multiplexer.
clear() - Method in class org.orekit.utils.DoubleArrayDictionary
Remove all entries.
clear() - Method in class org.orekit.utils.FieldArrayDictionary
Remove all entries.
clearCelestialBodyCache() - Static method in class org.orekit.bodies.CelestialBodyFactory
Clear all loaded celestial bodies.
clearCelestialBodyCache() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
Clear all loaded celestial bodies.
clearCelestialBodyCache(String) - Static method in class org.orekit.bodies.CelestialBodyFactory
Clear the specified celestial body from the internal cache.
clearCelestialBodyCache(String) - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
Clear the specified celestial body from the internal cache.
clearCelestialBodyLoaders() - Static method in class org.orekit.bodies.CelestialBodyFactory
Clear loaders for all celestial bodies.
clearCelestialBodyLoaders() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
Clear loaders for all celestial bodies.
clearCelestialBodyLoaders(String) - Static method in class org.orekit.bodies.CelestialBodyFactory
Clear loaders for one celestial body.
clearCelestialBodyLoaders(String) - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
Clear loaders for one celestial body.
clearEOPHistoryLoaders() - Static method in class org.orekit.frames.FramesFactory
Clear loaders for Earth Orientation Parameters history.
clearEOPHistoryLoaders() - Method in class org.orekit.frames.LazyLoadedEop
Clear loaders for Earth Orientation Parameters history.
clearEOPHistoryLoaders() - Method in class org.orekit.frames.LazyLoadedFrames
Clear loaders for Earth Orientation Parameters history.
clearEventsDetectors() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Remove all events detectors.
clearEventsDetectors() - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Remove all events detectors.
clearEventsDetectors() - Method in interface org.orekit.propagation.FieldPropagator
Remove all events detectors.
clearEventsDetectors() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Remove all events detectors.
clearEventsDetectors() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Remove all events detectors.
clearEventsDetectors() - Method in interface org.orekit.propagation.Propagator
Remove all events detectors.
clearFilters() - Method in class org.orekit.data.FiltersManager
Remove all data filters.
clearHistory() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldShortPeriodicsInterpolatedCoefficient
Clear the recorded values from the interpolation grid.
clearHistory() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.ShortPeriodicsInterpolatedCoefficient
Clear the recorded values from the interpolation grid.
clearImpulseManeuvers() - Method in class org.orekit.propagation.conversion.AbstractAnalyticalPropagatorBuilder
Remove all impulse maneuvers.
clearImpulseManeuvers() - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
Remove all impulse maneuvers.
clearLoadedDataNames() - Method in class org.orekit.data.DataProvidersManager
Clear the set of data file names that have been loaded.
clearLoggedEvents() - Method in class org.orekit.propagation.events.EventsLogger
Clear the logged events.
clearLoggedEvents() - Method in class org.orekit.propagation.events.FieldEventsLogger
Clear the logged events.
clearOceanTidesReaders() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Clear ocean tides readers.
clearOceanTidesReaders() - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
Clear ocean tides readers.
clearPotentialCoefficientsReaders() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Clear gravity field readers.
clearPotentialCoefficientsReaders() - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
Clear gravity field readers.
clearProviders() - Method in class org.orekit.data.DataProvidersManager
Remove all data providers.
clearStepHandlers() - Method in interface org.orekit.propagation.FieldPropagator
Remove all step handlers.
clearStepHandlers() - Method in interface org.orekit.propagation.Propagator
Remove all step handlers.
clearUTCTAIOffsetsLoaders() - Method in class org.orekit.time.LazyLoadedTimeScales
Clear loaders for UTC-TAI offsets history files.
clearUTCTAIOffsetsLoaders() - Static method in class org.orekit.time.TimeScalesFactory
Clear loaders for UTC-TAI offsets history files.
CLOCK_ACCELERATION_PREFIX - Static variable in class org.orekit.estimation.measurements.ObservableSatellite
Prefix for clock acceleration parameter driver, the propagator index will be appended to it.
CLOCK_ACCURACY_UNIT - Static variable in class org.orekit.files.sp3.SP3Utils
Clock accuracy unit.
CLOCK_ADDITIONAL_STATE - Static variable in class org.orekit.files.sp3.SP3Utils
Additional state name for clock.
CLOCK_BIAS - org.orekit.files.ccsds.ndm.tdm.ObservationType
Data: Clock bias [s].
CLOCK_CORRECTIONS - Static variable in class org.orekit.propagation.analytical.gnss.ClockCorrectionsProvider
Name of the additional state for satellite clock corrections.
CLOCK_DRIFT - org.orekit.files.ccsds.ndm.tdm.ObservationType
Data: Clock drift [s/s].
CLOCK_DRIFT_PREFIX - Static variable in class org.orekit.estimation.measurements.ObservableSatellite
Prefix for clock drift parameter driver, the propagator index will be appended to it.
CLOCK_FILE_UNSUPPORTED_VERSION - org.orekit.errors.OrekitMessages
CLOCK_FILE_UNSUPPORTED_VERSION.
CLOCK_OFFSET_PREFIX - Static variable in class org.orekit.estimation.measurements.ObservableSatellite
Prefix for clock offset parameter driver, the propagator index will be appended to it.
CLOCK_RATE_ACCURACY_UNIT - Static variable in class org.orekit.files.sp3.SP3Utils
Clock rate accuracy unit.
CLOCK_RATE_UNIT - Static variable in class org.orekit.files.sp3.SP3Utils
Clock rate unit.
CLOCK_UNIT - Static variable in class org.orekit.files.sp3.SP3Utils
Clock unit.
ClockCorrection - Class in org.orekit.gnss.metric.messages.common
Container for SSR clock correction data.
ClockCorrection(double, double, double) - Constructor for class org.orekit.gnss.metric.messages.common.ClockCorrection
Constructor.
ClockCorrectionsProvider - Class in org.orekit.propagation.analytical.gnss
Provider for clock corrections as additional states.
ClockCorrectionsProvider(GNSSClockElements) - Constructor for class org.orekit.propagation.analytical.gnss.ClockCorrectionsProvider
Simple constructor.
ClockDataLine(RinexClock.ClockDataType, String, DateComponents, TimeComponents, int, double, double, double, double, double, double) - Constructor for class org.orekit.files.rinex.clock.RinexClock.ClockDataLine
Constructor.
ClockModel - Interface in org.orekit.time
Offset clock model.
ClockOffset - Class in org.orekit.time
Container for time stamped clock offset.
ClockOffset(AbsoluteDate, double, double, double) - Constructor for class org.orekit.time.ClockOffset
Simple constructor.
ClockOffsetHermiteInterpolator - Class in org.orekit.time
bHermite interpolator of time stamped clock offsets.
ClockOffsetHermiteInterpolator(int) - Constructor for class org.orekit.time.ClockOffsetHermiteInterpolator
Constructor with default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s).
ClockOffsetHermiteInterpolator(int, double) - Constructor for class org.orekit.time.ClockOffsetHermiteInterpolator
Constructor.
ClockTimeScale - Class in org.orekit.time
Time scale with clock offset from another time scale.
ClockTimeScale(String, TimeScale, ClockModel) - Constructor for class org.orekit.time.ClockTimeScale
Simple constructor.
clone() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
 
close() - Method in class org.orekit.data.LineOrientedFilteringReader
close() - Method in class org.orekit.files.ccsds.ndm.adm.aem.StreamingAemWriter
close() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.StreamingOcmWriter
close() - Method in class org.orekit.files.ccsds.ndm.odm.oem.StreamingOemWriter
close() - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Close the generator.
close() - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Close the generator.
close() - Method in class org.orekit.files.rinex.observation.RinexObservationWriter
CM_COEFFICIENTS - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Identifier for cMm coefficients.
CMR - org.orekit.gnss.metric.ntrip.DataFormat
CMR.
CMR_PLUS - org.orekit.gnss.metric.ntrip.DataFormat
CMR+.
CN_N - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [3,3].
CN_R - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [3,1].
CN_T - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [3,2].
CNAV - Static variable in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage
Identifier for message type.
CNDOT_N - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [6,3].
CNDOT_NDOT - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [6,6].
CNDOT_R - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [6,1].
CNDOT_RDOT - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [6,4].
CNDOT_T - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [6,2].
CNDOT_TDOT - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [6,5].
CNV1 - Static variable in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage
Identifier for Beidou-3 B1C message type.
CNV2 - Static variable in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage
Identifier for Beidou-3 B2A message type.
CNV2 - Static variable in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage
Identifier for message type.
CNV3 - Static variable in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage
Identifier for Beidou-3 B2B message type.
co2AB - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext
C / (2 * A * B) .
co2AB - Variable in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext
C / (2 * A * B) .
CodeBias - Class in org.orekit.gnss.metric.messages.common
Container for code bias data.
CodeBias(int, double) - Constructor for class org.orekit.gnss.metric.messages.common.CodeBias
Constructor.
CODELESS - org.orekit.gnss.SignalCode
Codeless.
coef - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
coef for SGP C3 computation.
coef - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
coef for SGP C3 computation.
coef1 - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
coef for SGP C5 computation.
coef1 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
coef for SGP C5 computation.
CoefficientsFactory - Class in org.orekit.propagation.semianalytical.dsst.utilities
This class is designed to provide coefficient from the DSST theory.
CoefficientsFactory.NSKey - Class in org.orekit.propagation.semianalytical.dsst.utilities
Key formed by two integer values.
COHERENT - org.orekit.files.ccsds.ndm.tdm.RangeMode
Range tones coherent with uplink carrier.
COLLISION_MAX_PC_METHOD - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
The method that was used to calculate the maximum collision probability.
COLLISION_MAX_PROBABILITY - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
The maximum collision probability that Object1 and Object2 will collide.
COLLISION_PERCENTILE - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
An array of 1 to n elements indicating the percentile(s) for which estimates of the collision probability are provided in the COLLISION_PROBABILITY variable.
COLLISION_PROBABILITY - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
The probability (between 0.0 and 1.0) that Object1 and Object2 will collide.
COLLISION_PROBABILITY_METHOD - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
The method that was used to calculate the collision probability.
COLUMN_DIM - Static variable in class org.orekit.propagation.AbstractStateCovarianceInterpolator
Default column dimension for position-velocity state covariance.
CombinationType - Enum in org.orekit.estimation.measurements.gnss
Enumerate for combination of measurements types.
combine(ObservationData, ObservationData) - Method in class org.orekit.estimation.measurements.gnss.AbstractDualFrequencyCombination
Combines observation data using a dual frequency combination of measurements.
combine(ObservationData, ObservationData) - Method in class org.orekit.estimation.measurements.gnss.AbstractSingleFrequencyCombination
Combines observation data using a single frequency combination of measurements.
combine(ObservationDataSet) - Method in class org.orekit.estimation.measurements.gnss.AbstractDualFrequencyCombination
Combines observation data using a combination of measurements.
combine(ObservationDataSet) - Method in class org.orekit.estimation.measurements.gnss.AbstractSingleFrequencyCombination
Combines observation data using a combination of measurements.
combine(ObservationDataSet) - Method in interface org.orekit.estimation.measurements.gnss.MeasurementCombination
Combines observation data using a combination of measurements.
combine(ObservationDataSet) - Method in class org.orekit.estimation.measurements.gnss.MelbourneWubbenaCombination
Combines observation data using a combination of measurements.
COMBINED_RANGE_PHASE - org.orekit.gnss.MeasurementType
Combined pseudo-range carrier-phase measurement.
combinedDerivatives(FieldSpacecraftState<T>) - Method in class org.orekit.control.indirect.adjoint.FieldCartesianAdjointDerivativesProvider
Compute the derivatives related to the additional state (and optionally main state increments).
combinedDerivatives(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.integration.FieldAdditionalDerivativesProvider
Compute the derivatives related to the additional state (and optionally main state increments).
combinedDerivatives(SpacecraftState) - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointDerivativesProvider
Compute the derivatives related to the additional state (and optionally main state increments).
combinedDerivatives(SpacecraftState) - Method in class org.orekit.forces.maneuvers.jacobians.MassDepletionDelay
Compute the derivatives related to the additional state (and optionally main state increments).
combinedDerivatives(SpacecraftState) - Method in interface org.orekit.propagation.integration.AdditionalDerivativesProvider
Compute the derivatives related to the additional state (and optionally main state increments).
combinedDerivatives(SpacecraftState) - Method in class org.orekit.propagation.numerical.cr3bp.STMEquations
Compute the derivatives related to the additional state (and optionally main state increments).
combinedDerivatives(SpacecraftState) - Method in class org.orekit.propagation.numerical.EpochDerivativesEquations
Compute the derivatives related to the additional state (and optionally main state increments).
CombinedDerivatives - Class in org.orekit.propagation.integration
Container for additional derivatives.
CombinedDerivatives(double[], double[]) - Constructor for class org.orekit.propagation.integration.CombinedDerivatives
Simple constructor.
CombinedObservationData - Class in org.orekit.estimation.measurements.gnss
Combined observation data.
CombinedObservationData(double, double, CombinationType, MeasurementType, List<ObservationData>) - Constructor for class org.orekit.estimation.measurements.gnss.CombinedObservationData
Constructor.
CombinedObservationData(CombinationType, MeasurementType, double, double, List<ObservationData>) - Constructor for class org.orekit.estimation.measurements.gnss.CombinedObservationData
CombinedObservationDataSet - Class in org.orekit.estimation.measurements.gnss
Combined observation data set.
CombinedObservationDataSet(SatelliteSystem, int, AbsoluteDate, double, List<CombinedObservationData>) - Constructor for class org.orekit.estimation.measurements.gnss.CombinedObservationDataSet
Simple constructor.
COMMA_SEP - Static variable in exception org.orekit.errors.UnsupportedParameterException
Comma separator for printing list of supported parameter drivers.
COMMENT - org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadataKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuverKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalPropertiesKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadataKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.adm.apm.AngularVelocityKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternionKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.adm.apm.EulerKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.adm.apm.InertiaKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.adm.apm.ManeuverKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.adm.apm.SpinStabilizedKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadataKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.cdm.ODParametersKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.cdm.SigmaEigenvectorsCovarianceKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.cdm.StateVectorKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.cdm.XmlSubStructureKey
General comment.
COMMENT - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.odm.KeplerianElementsKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadataKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadataKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.odm.omm.OmmTleKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.odm.opm.ManeuverKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.odm.SpacecraftParametersKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.odm.StateVectorKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.tdm.TdmDataKey
Comment entry.
COMMENT - org.orekit.files.ccsds.section.HeaderKey
Header comment.
COMMENT - org.orekit.files.ccsds.section.MetadataKey
Comment entry.
COMMENT - org.orekit.files.rinex.section.RinexLabels
Comments.
CommentsContainer - Class in org.orekit.files.ccsds.section
Container for comments in various CCSDS messages.
CommentsContainer() - Constructor for class org.orekit.files.ccsds.section.CommentsContainer
Create a new meta-data.
CommonGnssData - Class in org.orekit.propagation.analytical.gnss.data
Container for common GNSS data contained in almanac and navigation messages.
CommonGnssData(double, double, int) - Constructor for class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Constructor.
CommonMetadataKey - Enum in org.orekit.files.ccsds.ndm.odm
Keys for common ODM container entries.
CommonMetadataWriter - Class in org.orekit.files.ccsds.ndm.odm
Writer for Common metadata for CCSDS Orbit Parameter/Ephemeris/Mean Messages.
CommonMetadataWriter(OdmCommonMetadata, TimeConverter) - Constructor for class org.orekit.files.ccsds.ndm.odm.CommonMetadataWriter
Simple constructor.
CommonParametersWithDerivatives - Class in org.orekit.estimation.measurements
Common intermediate parameters used to estimate measurements where receiver is a ground station.
CommonParametersWithDerivatives(SpacecraftState, Map<String, Integer>, Gradient, SpacecraftState, TimeStampedFieldPVCoordinates<Gradient>) - Constructor for class org.orekit.estimation.measurements.CommonParametersWithDerivatives
Simple constructor.
CommonParametersWithoutDerivatives - Class in org.orekit.estimation.measurements
Common intermediate parameters used to estimate measurements.
CommonParametersWithoutDerivatives(SpacecraftState, double, SpacecraftState, TimeStampedPVCoordinates) - Constructor for class org.orekit.estimation.measurements.CommonParametersWithoutDerivatives
Simple constructor.
CommonPhysicalProperties - Class in org.orekit.files.ccsds.ndm
Container for common physical properties for both OrbitPhysicalProperties and AdditionalParameters.
CommonPhysicalProperties() - Constructor for class org.orekit.files.ccsds.ndm.CommonPhysicalProperties
Simple constructor.
ComparableMeasurement - Interface in org.orekit.estimation.measurements
Base interface for comparing measurements regardless of their type.
compare(IntegerLeastSquareSolution, IntegerLeastSquareSolution) - Method in class org.orekit.estimation.measurements.gnss.IntegerLeastSquareComparator
The comparison is based on the squared distance to the float solution.
compare(FieldTimeStamped<KK>, FieldTimeStamped<KK>) - Method in class org.orekit.time.FieldChronologicalComparator
Compare two time-stamped instances.
compare(TimeStamped, TimeStamped) - Method in class org.orekit.time.ChronologicalComparator
Compare two time-stamped instances.
compareTo(ComparableMeasurement) - Method in interface org.orekit.estimation.measurements.ComparableMeasurement
compareTo(AbstractSolarActivityDataLoader.LineParameters) - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityDataLoader.LineParameters
compareTo(AbstractSolarActivityDataLoader.LineParameters) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
compareTo(AbstractSolarActivityDataLoader.LineParameters) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimationLoader.LineParameters
compareTo(CoefficientsFactory.NSKey) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey
compareTo(AbsoluteDate) - Method in class org.orekit.time.AbsoluteDate
Compare the instance with another date.
compareTo(DateComponents) - Method in class org.orekit.time.DateComponents
compareTo(DateTimeComponents) - Method in class org.orekit.time.DateTimeComponents
compareTo(FieldAbsoluteDate<T>) - Method in class org.orekit.time.FieldAbsoluteDate
Compare the instance with another date.
compareTo(TimeComponents) - Method in class org.orekit.time.TimeComponents
COMPASS - org.orekit.files.sp3.SP3FileType
COMPASS only file.
compile(PoissonSeries...) - Static method in class org.orekit.data.PoissonSeries
Join several nutation series, for fast simultaneous evaluation.
complain(String, boolean) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Complain about a missing value.
completed() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver
Check if maneuver has been completed.
components(AbsoluteDate) - Method in class org.orekit.files.ccsds.definitions.TimeConverter
Generate calendar components.
compose(AbsoluteDate, KinematicTransform, KinematicTransform) - Static method in interface org.orekit.frames.KinematicTransform
Build a transform by combining two existing ones.
compose(AbsoluteDate, StaticTransform, StaticTransform) - Static method in interface org.orekit.frames.StaticTransform
Build a transform by combining two existing ones.
compose(FieldAbsoluteDate<T>, FieldKinematicTransform<T>, FieldKinematicTransform<T>) - Static method in interface org.orekit.frames.FieldKinematicTransform
Build a transform by combining two existing ones.
compose(FieldAbsoluteDate<T>, FieldStaticTransform<T>, FieldStaticTransform<T>) - Static method in interface org.orekit.frames.FieldStaticTransform
Build a transform by combining two existing ones.
CompositeDataContext - Class in org.orekit.data
A simple implementation of DataContext that composes the constituent factories into a data context.
CompositeDataContext(TimeScales, Frames, CelestialBodies, GravityFields, GeoMagneticFields) - Constructor for class org.orekit.data.CompositeDataContext
Simple constructor.
compositeRotation(FieldStaticTransform<T>, FieldStaticTransform<T>) - Static method in interface org.orekit.frames.FieldStaticTransform
Compute a composite rotation.
compositeRotation(StaticTransform, StaticTransform) - Static method in interface org.orekit.frames.StaticTransform
Compute a composite rotation.
compositeRotationRate(FieldKinematicTransform<T>, FieldKinematicTransform<T>) - Static method in interface org.orekit.frames.FieldKinematicTransform
Compute a composite rotation rate.
compositeRotationRate(KinematicTransform, KinematicTransform) - Static method in interface org.orekit.frames.KinematicTransform
Compute a composite rotation rate.
compositeTranslation(FieldStaticTransform<T>, FieldStaticTransform<T>) - Static method in interface org.orekit.frames.FieldStaticTransform
Compute a composite translation.
compositeTranslation(StaticTransform, StaticTransform) - Static method in interface org.orekit.frames.StaticTransform
Compute a composite translation.
compositeVelocity(FieldKinematicTransform<T>, FieldKinematicTransform<T>) - Static method in interface org.orekit.frames.FieldKinematicTransform
Compute a composite velocity.
compositeVelocity(KinematicTransform, KinematicTransform) - Static method in interface org.orekit.frames.KinematicTransform
Compute a composite velocity.
compute() - Method in class org.orekit.utils.AbstractMultipleShooting
Return the list of corrected patch points.
compute() - Method in interface org.orekit.utils.MultipleShooting
Return the list of corrected patch points.
compute(double, double, double, double, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractAlfriend1999
Compute the probability of collision using arguments specific to the rotated encounter frame.
compute(double, double, double, double, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter1DNumerical2DPOCMethod
Compute the probability of collision using arguments specific to the rotated encounter frame.
compute(double, double, double, double, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Alfano2005
Compute the probability of collision using arguments specific to the rotated encounter frame.
compute(double, double, double, double, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Chan1997
Compute the probability of collision using arguments specific to the rotated encounter frame.
compute(double, double, double, double, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Laas2015
Compute the probability of collision using arguments specific to the rotated encounter frame.
compute(double, double, double, double, double) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod
Compute the probability of collision using arguments specific to the rotated encounter frame.
compute(double, double, double, double, double, UnivariateIntegrator, int) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter1DNumerical2DPOCMethod
Compute the probability of collision using arguments specific to the rotated encounter frame and custom numerical configuration.
compute(double, double, double, double, double, UnivariateIntegrator, int) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Patera2005
Compute the probability of collision using arguments specific to the rotated encounter frame and custom numerical configuration.
compute(Cdm, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter2DPOCMethod
Compute the probability of collision using a Conjunction Data Message (CDM).
compute(Cdm, double) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod
Compute the probability of collision using a Conjunction Data Message (CDM).
compute(Cdm, double, double) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod
Compute the probability of collision using a Conjunction Data Message (CDM).
compute(Cdm, double, double, UnivariateIntegrator, int, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter1DNumerical2DPOCMethod
Compute the probability of collision using an Orekit Conjunction Data Message.
compute(Cdm, T) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod
Compute the probability of collision using a Conjunction Data Message (CDM).
compute(Cdm, T, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter2DPOCMethod
Compute the probability of collision using a Conjunction Data Message (CDM).
compute(Cdm, T, double) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod
Compute the probability of collision using a Conjunction Data Message (CDM).
compute(Cdm, T, T) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod
Compute the probability of collision using a Conjunction Data Message (CDM).
compute(Cdm, T, T, FieldUnivariateIntegrator<T>, int, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter1DNumerical2DPOCMethod
Compute the probability of collision using an Orekit Conjunction Data Message.
compute(FieldOrbit<T>, FieldStateCovariance<T>, FieldOrbit<T>, FieldStateCovariance<T>, T) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod
Compute the probability of collision using parameters necessary for creating a collision definition instance.
compute(FieldOrbit<T>, FieldStateCovariance<T>, FieldOrbit<T>, FieldStateCovariance<T>, T, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter2DPOCMethod
Compute the probability of collision using parameters necessary for creating a collision definition instance.
compute(FieldOrbit<T>, FieldStateCovariance<T>, FieldOrbit<T>, FieldStateCovariance<T>, T, double) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod
Compute the probability of collision using parameters necessary for creating a collision definition instance.
compute(FieldOrbit<T>, FieldStateCovariance<T>, T, FieldOrbit<T>, FieldStateCovariance<T>, T) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod
Compute the probability of collision using parameters necessary for creating a collision definition instance.
compute(FieldOrbit<T>, FieldStateCovariance<T>, T, FieldOrbit<T>, FieldStateCovariance<T>, T, FieldUnivariateIntegrator<T>, int, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter1DNumerical2DPOCMethod
Compute the probability of collision using parameters necessary for creating a collision definition instance.
compute(LibrationOrbitType) - Method in class org.orekit.orbits.CR3BPDifferentialCorrection
Return the real starting PVCoordinates on the Libration orbit type after differential correction from a first guess.
compute(Orbit, StateCovariance, double, Orbit, StateCovariance, double) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod
Compute the probability of collision using parameters necessary for creating a collision definition instance.
compute(Orbit, StateCovariance, double, Orbit, StateCovariance, double, UnivariateIntegrator, int, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter1DNumerical2DPOCMethod
Compute the probability of collision using parameters necessary for creating a collision definition instance.
compute(Orbit, StateCovariance, Orbit, StateCovariance, double) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod
Compute the probability of collision using parameters necessary for creating a collision definition instance.
compute(Orbit, StateCovariance, Orbit, StateCovariance, double, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter2DPOCMethod
Compute the probability of collision using parameters necessary for creating a collision definition instance.
compute(Orbit, StateCovariance, Orbit, StateCovariance, double, double) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod
Compute the probability of collision using parameters necessary for creating a collision definition instance.
compute(FieldShortTermEncounter2DDefinition<T>) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod
Compute the probability of collision using given collision definition.
compute(FieldShortTermEncounter2DDefinition<T>, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter2DPOCMethod
Compute the probability of collision using given collision definition.
compute(FieldShortTermEncounter2DDefinition<T>, double) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod
Compute the probability of collision using given collision definition.
compute(FieldShortTermEncounter2DDefinition<T>, FieldUnivariateIntegrator<T>, int, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter1DNumerical2DPOCMethod
Compute the probability of collision using given collision definition.
compute(ShortTermEncounter2DDefinition) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod
Compute the probability of collision using given collision definition.
compute(ShortTermEncounter2DDefinition, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter2DPOCMethod
Compute the probability of collision using given collision definition.
compute(ShortTermEncounter2DDefinition, double) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod
Compute the probability of collision using given collision definition.
compute(ShortTermEncounter2DDefinition, UnivariateIntegrator, int, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter1DNumerical2DPOCMethod
Compute the probability of collision using a given collision definition.
compute(AbsoluteDate, List<Propagator>) - Method in class org.orekit.gnss.DOPComputer
Compute the DOP at a given date for a set of GNSS spacecrafts.
compute(T, T, T, T, T) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractAlfriend1999
Compute the probability of collision using arguments specific to the rotated encounter frame.
compute(T, T, T, T, T) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter1DNumerical2DPOCMethod
Compute the probability of collision using arguments specific to the rotated encounter frame.
compute(T, T, T, T, T) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Alfano2005
Compute the probability of collision using arguments specific to the rotated encounter frame.
compute(T, T, T, T, T) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Chan1997
Compute the probability of collision using arguments specific to the rotated encounter frame.
compute(T, T, T, T, T) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Laas2015
Compute the probability of collision using arguments specific to the rotated encounter frame.
compute(T, T, T, T, T) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod
Compute the probability of collision using arguments specific to the rotated encounter frame.
compute(T, T, T, T, T, FieldUnivariateIntegrator<T>, int) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter1DNumerical2DPOCMethod
Compute the probability of collision using arguments specific to the rotated encounter frame and custom numerical configuration.
compute(T, T, T, T, T, FieldUnivariateIntegrator<T>, int) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Patera2005
Compute the probability of collision using arguments specific to the rotated encounter frame and custom numerical configuration.
computeAccelerationInJ2Frame(FieldVector3D<T>, double, double, T) - Static method in class org.orekit.forces.gravity.J2OnlyPerturbation
Compute acceleration in J2 frame.
computeAccelerationInJ2Frame(Vector3D, double, double, double) - Static method in class org.orekit.forces.gravity.J2OnlyPerturbation
Compute acceleration in J2 frame.
computeAdditionalConstraints(List<SpacecraftState>) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPMultipleShooter
Compute the additional constraints.
computeAdditionalConstraints(List<SpacecraftState>) - Method in class org.orekit.utils.AbstractMultipleShooting
Compute the additional constraints.
computeAdditionalConstraints(List<SpacecraftState>) - Method in class org.orekit.utils.MultipleShooter
Compute the additional constraints.
computeAdditionalJacobianMatrix(List<SpacecraftState>) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPMultipleShooter
Compute a part of the Jacobian matrix from additional constraints.
computeAdditionalJacobianMatrix(List<SpacecraftState>) - Method in class org.orekit.utils.AbstractMultipleShooting
Compute a part of the Jacobian matrix from additional constraints.
computeAdditionalJacobianMatrix(List<SpacecraftState>) - Method in class org.orekit.utils.MultipleShooter
Compute a part of the Jacobian matrix from additional constraints.
computeAlbedo(AbsoluteDate, double) - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel
Compute Earth albedo.
computeAlbedo(FieldAbsoluteDate<T>, T) - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel
Compute Earth albedo.
computeC2Z(DSSTJ2SquaredClosedFormContext) - Method in class org.orekit.propagation.semianalytical.dsst.forces.ZeisModel
Get the value of the Zeis constant.
computeC2Z(FieldDSSTJ2SquaredClosedFormContext<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.ZeisModel
Get the value of the Zeis constant.
computeCombinedCovarianceInEncounterFrame() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Compute the combined covariance expressed in the encounter frame.
computeCombinedCovarianceInEncounterFrame() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition
Compute the combined covariance expressed in the encounter frame.
computeCombinedCovarianceInReferenceTNW() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Takes both covariance matrices (expressed in their respective RTN local orbital frame) from reference and other collision object with which this instance was created and sum them in the reference collision object TNW local orbital frame.
computeCombinedCovarianceInReferenceTNW() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition
Takes both covariance matrices (expressed in their respective RTN local orbital frame) from reference and other collision object with which this instance was created and sum them in the reference collision object TNW local orbital frame.
computeCommonParametersWith(SpacecraftState[], boolean) - Method in class org.orekit.estimation.measurements.gnss.AbstractOnBoardMeasurement
Compute common estimation parameters.
computeCommonParametersWithDerivatives(SpacecraftState) - Method in class org.orekit.estimation.measurements.GroundReceiverMeasurement
Compute common estimation parameters.
computeCommonParametersWithout(SpacecraftState) - Method in class org.orekit.estimation.measurements.GroundReceiverMeasurement
Compute common estimation parameters.
computeCommonParametersWithout(SpacecraftState[], boolean) - Method in class org.orekit.estimation.measurements.gnss.AbstractOnBoardMeasurement
Compute common estimation parameters.
computeCoppolaEncounterDuration() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Compute the Encounter duration (s) evaluated using Coppola's formula described in : "COPPOLA, Vincent, et al.
computeCoppolaEncounterDuration() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition
Compute the Encounter duration (s) evaluated using Coppola's formula described in : "COPPOLA, Vincent, et al.
computeDeltaPV(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldExtremumApproachDetector
Deprecated.
The output type of this method shall be modified in the future to improve code efficiency (though it will still give access to the relative position and velocity)
computeDeltaPV(SpacecraftState) - Method in class org.orekit.propagation.events.ExtremumApproachDetector
Deprecated.
The output type of this method shall be modified in the future to improve code efficiency (though it will still give access to the relative position and velocity)
computeDerivatives(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.integration.FieldAbstractIntegratedPropagator.MainStateEquations
Compute differential equations for main state.
computeDerivatives(SpacecraftState) - Method in interface org.orekit.propagation.integration.AbstractIntegratedPropagator.MainStateEquations
Compute differential equations for main state.
computeElementaryFlux(FieldSpacecraftState<T>, FieldVector3D<T>, FieldVector3D<T>, OneAxisEllipsoid, T) - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel
Compute elementary rediffused flux on satellite.
computeElementaryFlux(SpacecraftState, Vector3D, Vector3D, OneAxisEllipsoid, double) - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel
Compute elementary rediffused flux on satellite.
computeEmissivity(AbsoluteDate, double) - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel
Compute Earth emisivity.
computeEmissivity(FieldAbsoluteDate<T>, T) - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel
Compute Earth emisivity.
computeEpochJacobianMatrix(List<SpacecraftState>) - Method in class org.orekit.utils.AbstractMultipleShooting
Compute a part of the Jacobian matrix with derivatives from epoch.
computeGsHs(double, double, double, double, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory
Compute recursively Gs and Hs polynomials from equation 3.1-(5).
computeGsHs(T, T, T, T, int, Field<T>) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory
Compute recursively Gs and Hs polynomials from equation 3.1-(5).
computeHaloFirstGuess(double, LibrationOrbitFamily, double, double) - Method in class org.orekit.orbits.RichardsonExpansion
Calculate first Guess.
computeHeightCorrection(double, double) - Static method in class org.orekit.models.earth.troposphere.TroposphericModelUtils
This method computes the height correction for the hydrostatic component of the mapping function.
computeHeightCorrection(T, T, Field<T>) - Static method in class org.orekit.models.earth.troposphere.TroposphericModelUtils
This method computes the height correction for the hydrostatic component of the mapping function.
computeInitValues(double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenZonalLinear
Compute the roots for the Hansen coefficients and their derivatives.
computeInitValues(double, double, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenTesseralLinear
Compute the values for the first four coefficients and their derivatives by means of series.
computeInitValues(double, double, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenThirdBodyLinear
Compute the initial values (see Collins, 4-255, 4-256 and 4.259)
computeInitValues(T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenZonalLinear
Compute the roots for the Hansen coefficients and their derivatives.
computeInitValues(T, T, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenTesseralLinear
Compute the values for the first four coefficients and their derivatives by means of series.
computeInitValues(T, T, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenThirdBodyLinear
Compute the initial values (see Collins, 4-255, 4-256 and 4.259)
computeInnovationVector(EstimatedMeasurement<?>) - Static method in class org.orekit.estimation.sequential.KalmanEstimatorUtil
Compute the unnormalized innovation vector from the given predicted measurement.
computeInnovationVector(EstimatedMeasurement<?>, double[]) - Static method in class org.orekit.estimation.sequential.KalmanEstimatorUtil
Compute the normalized innovation vector from the given predicted measurement.
computeInterpolatedCovarianceInOrbitFrame(List<TimeStampedPair<Orbit, StateCovariance>>, Orbit) - Method in class org.orekit.propagation.AbstractStateCovarianceInterpolator
Compute the interpolated covariance expressed in the interpolated orbit frame.
computeInterpolatedCovarianceInOrbitFrame(List<TimeStampedPair<Orbit, StateCovariance>>, Orbit) - Method in class org.orekit.propagation.StateCovarianceBlender
Compute the interpolated covariance expressed in the interpolated orbit frame.
computeInterpolatedCovarianceInOrbitFrame(List<TimeStampedPair<Orbit, StateCovariance>>, Orbit) - Method in class org.orekit.propagation.StateCovarianceKeplerianHermiteInterpolator
Compute the interpolated covariance expressed in the interpolated orbit frame.
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.CartesianOrbit
 
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.CircularOrbit
Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.EquinoctialOrbit
Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.FieldCartesianOrbit
 
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.FieldCircularOrbit
Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.FieldOrbit
Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.KeplerianOrbit
Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.Orbit
Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.CartesianOrbit
 
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.CircularOrbit
Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.EquinoctialOrbit
Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.FieldCartesianOrbit
 
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.FieldCircularOrbit
Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.FieldOrbit
Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.KeplerianOrbit
Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.Orbit
Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.CartesianOrbit
 
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.CircularOrbit
Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.EquinoctialOrbit
Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.FieldCartesianOrbit
 
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.FieldCircularOrbit
Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.FieldOrbit
Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.KeplerianOrbit
Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.Orbit
Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.
computeKeplerianDurationFromPreviousApoapsis(double, double) - Static method in class org.orekit.propagation.events.intervals.ApsideDetectionAdaptableIntervalFactory
Method computing time elapsed since last apoapsis, assuming Keplerian motion.
computeKeplerianDurationFromPreviousPeriapsis(double, double) - Static method in class org.orekit.propagation.events.intervals.ApsideDetectionAdaptableIntervalFactory
Method computing time elapsed since last periapsis, assuming Keplerian motion.
computeLimitVisibilityPoint(double, double, double) - Method in class org.orekit.frames.TopocentricFrame
Compute the limit visibility point for a satellite in a given direction.
computeLyapunov() - Method in class org.orekit.orbits.CR3BPDifferentialCorrection
Return the real starting PVCoordinates on the Lyapunov orbit after differential correction from a first guess.
computeLyapunovFirstGuess(double, double, double) - Method in class org.orekit.orbits.RichardsonExpansion
Calculate first Guess.
computeMahalanobisDistance() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Compute the Mahalanobis distance computed with the other collision object projected onto the collision plane (commonly called B-Plane) and expressed in the rotated encounter frame (frame in which the combined covariance matrix is diagonalized, see FieldShortTermEncounter2DDefinition.computeEncounterPlaneRotationMatrix(double) for more details).
computeMahalanobisDistance() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition
Compute the Mahalanobis distance computed with the other collision object projected onto the collision plane (commonly called B-Plane) and expressed in the rotated encounter frame (frame in which the combined covariance matrix is diagonalized, see ShortTermEncounter2DDefinition.computeEncounterPlaneRotationMatrix(double) for more details).
computeMahalanobisDistance(double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Compute the Mahalanobis distance computed with the other collision object projected onto the collision plane (commonly called B-Plane) and expressed in the rotated encounter frame (frame in which the combined covariance matrix is diagonalized, see FieldShortTermEncounter2DDefinition.computeEncounterPlaneRotationMatrix(double) for more details).
computeMahalanobisDistance(double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition
Compute the Mahalanobis distance computed with the other collision object projected onto the collision plane (commonly called B-Plane) and expressed in the rotated encounter frame (frame in which the combined covariance matrix is diagonalized, see ShortTermEncounter2DDefinition.computeEncounterPlaneRotationMatrix(double) for more details).
computeMeanEquinoctialSecondOrderTerms(DSSTJ2SquaredClosedFormContext) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.J2SquaredModel
Compute the J2-squared second-order terms in equinoctial elements.
computeMeanEquinoctialSecondOrderTerms(DSSTJ2SquaredClosedFormContext) - Method in class org.orekit.propagation.semianalytical.dsst.forces.ZeisModel
Compute the J2-squared second-order terms in equinoctial elements.
computeMeanEquinoctialSecondOrderTerms(FieldDSSTJ2SquaredClosedFormContext<T>) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.J2SquaredModel
Compute the J2-squared second-order terms in equinoctial elements.
computeMeanEquinoctialSecondOrderTerms(FieldDSSTJ2SquaredClosedFormContext<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.ZeisModel
Compute the J2-squared second-order terms in equinoctial elements.
computeMeanOrbit(FieldOrbit<T>, double, double, double, double, double, double, double, double, int) - Static method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Conversion from osculating to mean orbit.
computeMeanOrbit(FieldOrbit<T>, double, double, double, double, double, double, double, double, int) - Static method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Conversion from osculating to mean orbit.
computeMeanOrbit(FieldOrbit<T>, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics) - Static method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Conversion from osculating to mean orbit.
computeMeanOrbit(FieldOrbit<T>, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double) - Static method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Conversion from osculating to mean orbit.
computeMeanOrbit(FieldOrbit<T>, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double, double, int) - Static method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Conversion from osculating to mean orbit.
computeMeanOrbit(FieldOrbit<T>, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double, int) - Static method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Conversion from osculating to mean orbit.
computeMeanOrbit(Orbit, double, double, double, double, double, double, double, double, int) - Static method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Conversion from osculating to mean orbit.
computeMeanOrbit(Orbit, double, double, double, double, double, double, double, double, int) - Static method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Conversion from osculating to mean orbit.
computeMeanOrbit(Orbit, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics) - Static method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Conversion from osculating to mean orbit.
computeMeanOrbit(Orbit, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double) - Static method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Conversion from osculating to mean orbit.
computeMeanOrbit(Orbit, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double, double, int) - Static method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Conversion from osculating to mean orbit.
computeMeanOrbit(Orbit, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double, int) - Static method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Conversion from osculating to mean orbit.
computeMeanState(FieldSpacecraftState<T>, AttitudeProvider, Collection<DSSTForceModel>) - Static method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Conversion from osculating to mean orbit.
computeMeanState(FieldSpacecraftState<T>, AttitudeProvider, Collection<DSSTForceModel>, double, int) - Static method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Conversion from osculating to mean orbit.
computeMeanState(SpacecraftState, AttitudeProvider, Collection<DSSTForceModel>) - Static method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Conversion from osculating to mean orbit.
computeMeanState(SpacecraftState, AttitudeProvider, Collection<DSSTForceModel>, double, int) - Static method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Conversion from osculating to mean orbit.
computeMissDistance() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Compute the miss distance at time of closest approach.
computeMissDistance() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition
Compute the miss distance at time of closest approach.
computeOsculatingState(FieldSpacecraftState<T>, AttitudeProvider, Collection<DSSTForceModel>) - Static method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Conversion from mean to osculating orbit.
computeOsculatingState(SpacecraftState, AttitudeProvider, Collection<DSSTForceModel>) - Static method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Conversion from mean to osculating orbit.
computeOtherPositionInCollisionPlane() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Compute the other collision object position projected onto the collision plane.
computeOtherPositionInCollisionPlane() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition
Compute the other collision object position projected onto the collision plane.
computeOtherPositionInRotatedCollisionPlane() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Compute the other collision object position in the rotated collision plane.
computeOtherPositionInRotatedCollisionPlane() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition
Compute the other collision object position in the rotated collision plane.
computeOtherPositionInRotatedCollisionPlane(double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Compute the other collision object position in the rotated collision plane.
computeOtherPositionInRotatedCollisionPlane(double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition
Compute the other collision object position in the rotated collision plane.
computeOtherRelativeToReferencePVInReferenceInertial() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Compute the other collision position and velocity relative to the reference collision object.
computeOtherRelativeToReferencePVInReferenceInertial() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition
Compute the other collision position and velocity relative to the reference collision object.
computeProjectedAndDiagonalizedCombinedPositionalCovarianceMatrix() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Compute the combined covariance matrix diagonalized and projected onto the collision plane.
computeProjectedAndDiagonalizedCombinedPositionalCovarianceMatrix() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition
Compute the combined covariance matrix diagonalized and projected onto the collision plane.
computeProjectedCombinedPositionalCovarianceMatrix() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Compute the projected combined covariance matrix onto the collision plane.
computeProjectedCombinedPositionalCovarianceMatrix() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition
Compute the projected combined covariance matrix onto the collision plane.
computeProjectionMatrix() - Method in interface org.orekit.frames.encounter.EncounterLOF
Get the 2x3 projection matrix that projects values expressed in this encounter local orbital frame to the collision plane.
computeProjectionMatrix(Field<T>) - Method in interface org.orekit.frames.encounter.EncounterLOF
Get the 2x3 projection matrix that projects values expressed in this encounter local orbital frame to the collision plane defined by this same encounter local orbital frame.
computeQns(double, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory
Compute the Qn,s coefficients evaluated at γ from the recurrence formula 2.8.3-(2).
computeQns(T, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory
Compute the Qn,s coefficients evaluated at γ from the recurrence formula 2.8.3-(2).
computeReferenceInertialToCollisionPlaneProjectionMatrix() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Compute the projection matrix from the reference collision object inertial frame to the collision plane.
computeReferenceInertialToCollisionPlaneProjectionMatrix() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition
Compute the projection matrix from the reference collision object inertial frame to the collision plane.
computeSolarFlux(FieldVector3D<T>) - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel
Compute total solar flux impacting Earth.
computeSolarFlux(Vector3D) - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel
Compute total solar flux impacting Earth.
computeSquaredMahalanobisDistance() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Compute the squared Mahalanobis distance computed with the other collision object projected onto the collision plane (commonly called B-Plane) and expressed in the rotated encounter frame (frame in which the combined covariance matrix is diagonalized, see FieldShortTermEncounter2DDefinition.computeEncounterPlaneRotationMatrix(double) for more details).
computeSquaredMahalanobisDistance() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition
Compute the squared Mahalanobis distance computed with the other collision object projected onto the collision plane (commonly called B-Plane) and expressed in the rotated encounter frame (frame in which the combined covariance matrix is diagonalized, see ShortTermEncounter2DDefinition.computeEncounterPlaneRotationMatrix(double) for more details).
computeSquaredMahalanobisDistance(double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Compute the squared Mahalanobis distance computed with the other collision object projected onto the collision plane (commonly called B-Plane) and expressed in the rotated encounter frame (frame in which the combined covariance matrix is diagonalized, see FieldShortTermEncounter2DDefinition.computeEncounterPlaneRotationMatrix(double) for more details).
computeSquaredMahalanobisDistance(double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition
Compute the squared Mahalanobis distance computed with the other collision object projected onto the collision plane (commonly called B-Plane) and expressed in the rotated encounter frame (frame in which the combined covariance matrix is diagonalized, see ShortTermEncounter2DDefinition.computeEncounterPlaneRotationMatrix(double) for more details).
computeSquaredMahalanobisDistance(double, double, double, double) - Static method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition
Compute the squared Mahalanobis distance.
computeSquaredMahalanobisDistance(FieldVector2D<T>, FieldMatrix<T>) - Static method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Compute the squared Mahalanobis distance.
computeSquaredMahalanobisDistance(Vector2D, RealMatrix) - Static method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition
Compute the squared Mahalanobis distance.
computeSquaredMahalanobisDistance(T, T, T, T) - Static method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Compute the squared Mahalanobis distance.
computeThrustDirection(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.forces.maneuvers.propulsion.ConstantThrustDirectionProvider
 
computeThrustDirection(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustDirectionProvider
Compute the thrust direction corresponding to an orbital state.
computeValue(double, double, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Alfriend1999Max
Compute the value of the probability of collision.
computeValue(T, T, T) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Alfriend1999Max
Compute the value of the probability of collision.
computeVns(int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory
Compute the Vn,s coefficients from 2.8.2-(1)(2).
computeZenithDelay(FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.MendesPavlisModel
This method allows the computation of the zenith hydrostatic and zenith wet delay.
computeZenithDelay(FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.ViennaOneModel
Deprecated.
This method allows the computation of the zenith hydrostatic and zenith wet delay.
computeZenithDelay(FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.ViennaThreeModel
Deprecated.
This method allows the computation of the zenith hydrostatic and zenith wet delay.
computeZenithDelay(GeodeticPoint, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.MendesPavlisModel
This method allows the computation of the zenith hydrostatic and zenith wet delay.
computeZenithDelay(GeodeticPoint, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.ViennaOneModel
Deprecated.
This method allows the computation of the zenith hydrostatic and zenith wet delay.
computeZenithDelay(GeodeticPoint, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.ViennaThreeModel
Deprecated.
This method allows the computation of the zenith hydrostatic and zenith wet delay.
CONE - org.orekit.files.ccsds.ndm.odm.ocm.ShadowModel
Cone model, umbra only.
ConfigurableLowThrustManeuver - Class in org.orekit.forces.maneuvers
This class implements a configurable low thrust maneuver.
ConfigurableLowThrustManeuver(ThrustDirectionAndAttitudeProvider, ManeuverTriggers, double, double) - Constructor for class org.orekit.forces.maneuvers.ConfigurableLowThrustManeuver
Constructor.
configureHarvester(Propagator) - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel
Configure the propagator to compute derivatives.
configureHarvester(Propagator) - Method in class org.orekit.estimation.leastsquares.BatchLSModel
Configure the propagator to compute derivatives.
configureHarvester(Propagator) - Method in class org.orekit.estimation.leastsquares.DSSTBatchLSModel
Configure the propagator to compute derivatives.
configureOceanLoadDeformationCoefficients(OceanLoadDeformationCoefficients) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Configure ocean load deformation coefficients.
configureOceanLoadDeformationCoefficients(OceanLoadDeformationCoefficients) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
Configure ocean load deformation coefficients.
configureOrbits(MatricesHarvester, Propagator) - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel
Configure the current estimated orbits.
configureOrbits(MatricesHarvester, Propagator) - Method in class org.orekit.estimation.leastsquares.BatchLSModel
Configure the current estimated orbits.
configureOrbits(MatricesHarvester, Propagator) - Method in class org.orekit.estimation.leastsquares.DSSTBatchLSModel
Configure the current estimated orbits.
ConicallyShadowedLightFluxModel - Class in org.orekit.forces.radiation
Class defining a flux model from a single occulted body, casting a shadow on a spherical occulting body.
ConicallyShadowedLightFluxModel(double, double, ExtendedPositionProvider, double) - Constructor for class org.orekit.forces.radiation.ConicallyShadowedLightFluxModel
Constructor with default event detection settings.
ConicallyShadowedLightFluxModel(double, double, ExtendedPositionProvider, double, EventDetectionSettings) - Constructor for class org.orekit.forces.radiation.ConicallyShadowedLightFluxModel
Constructor.
ConicallyShadowedLightFluxModel(double, ExtendedPositionProvider, double) - Constructor for class org.orekit.forces.radiation.ConicallyShadowedLightFluxModel
Constructor with default value for reference flux.
CONJUNCTION_ID - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
The Originator’s ID that uniquely identifies the conjunction to which the message refers.
CONNECTION_ERROR - org.orekit.errors.OrekitMessages
CONNECTION_ERROR.
CONSIDER_N - org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey
Number of consider parameters.
CONSIDER_PARAMS - org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey
Description of consider parameters.
CONSTANT - org.orekit.files.ccsds.ndm.tdm.RangeMode
Range tones have constant frequency.
constantAfter() - Method in class org.orekit.utils.WaypointPVBuilder
Indicate the resulting PVCoordinatesProvider provide a constant location of the last waypoint after to the last time.
ConstantAzimuthAiming - Class in org.orekit.models.earth.tessellation
Class used to orient tiles with respect to a geographic azimuth.
ConstantAzimuthAiming(OneAxisEllipsoid, double) - Constructor for class org.orekit.models.earth.tessellation.ConstantAzimuthAiming
Simple constructor.
ConstantAzimuthalGradientProvider - Class in org.orekit.models.earth.troposphere
ConstantAzimuthalGradientProvider(AzimuthalGradientCoefficients) - Constructor for class org.orekit.models.earth.troposphere.ConstantAzimuthalGradientProvider
Simple constructor.
constantBefore() - Method in class org.orekit.utils.WaypointPVBuilder
Indicate the resulting PVCoordinatesProvider provide a constant location of the first waypoint prior to the first time.
ConstantOffsetTimeScale - Class in org.orekit.time
Base class for time scales with constant offset with respecto to TAI.
ConstantOffsetTimeScale(String, double) - Constructor for class org.orekit.time.ConstantOffsetTimeScale
Simple constructor.
ConstantPressureTemperatureHumidityProvider - Class in org.orekit.models.earth.weather
Provider for constant weather parameters.
ConstantPressureTemperatureHumidityProvider(PressureTemperatureHumidity) - Constructor for class org.orekit.models.earth.weather.ConstantPressureTemperatureHumidityProvider
Simple constructor.
ConstantProcessNoise - Class in org.orekit.estimation.sequential
Provider for constant process noise matrices.
ConstantProcessNoise(RealMatrix) - Constructor for class org.orekit.estimation.sequential.ConstantProcessNoise
Simple constructor.
ConstantProcessNoise(RealMatrix, RealMatrix) - Constructor for class org.orekit.estimation.sequential.ConstantProcessNoise
Simple constructor.
ConstantPVCoordinatesProvider - Class in org.orekit.utils
Provider based on a single point.
ConstantPVCoordinatesProvider(Vector3D, Frame) - Constructor for class org.orekit.utils.ConstantPVCoordinatesProvider
Create the PVCoordinatesProvider from a fixed point in a frame.
ConstantPVCoordinatesProvider(GeodeticPoint, OneAxisEllipsoid) - Constructor for class org.orekit.utils.ConstantPVCoordinatesProvider
Create a the provider from a fixed lat/lon/alt on a central body.
ConstantPVCoordinatesProvider(PVCoordinates, Frame) - Constructor for class org.orekit.utils.ConstantPVCoordinatesProvider
Create the PVCoordinatesProvider from a fixed point in a frame.
Constants - Interface in org.orekit.utils
Set of useful physical constants.
ConstantThrustDirectionProvider - Class in org.orekit.forces.maneuvers.propulsion
Simple implementation of VariableThrustDirectionVector, providing a constant direction.
ConstantThrustDirectionProvider(Vector3D) - Constructor for class org.orekit.forces.maneuvers.propulsion.ConstantThrustDirectionProvider
Constructor.
ConstantThrustManeuver - Class in org.orekit.forces.maneuvers
This class implements a simple maneuver with constant thrust.
ConstantThrustManeuver(AttitudeProvider, DateBasedManeuverTriggers, AbstractConstantThrustPropulsionModel) - Constructor for class org.orekit.forces.maneuvers.ConstantThrustManeuver
Simple constructor for a constant direction and constant thrust.
ConstantThrustManeuver(AbsoluteDate, double, double, double, Vector3D) - Constructor for class org.orekit.forces.maneuvers.ConstantThrustManeuver
Simple constructor for a constant direction and constant thrust.
ConstantThrustManeuver(AbsoluteDate, double, double, double, Vector3D, String) - Constructor for class org.orekit.forces.maneuvers.ConstantThrustManeuver
Simple constructor for a constant direction and constant thrust.
ConstantThrustManeuver(AbsoluteDate, double, double, double, AttitudeProvider, Vector3D) - Constructor for class org.orekit.forces.maneuvers.ConstantThrustManeuver
Simple constructor for a constant direction and constant thrust.
ConstantThrustManeuver(AbsoluteDate, double, double, double, AttitudeProvider, Vector3D, String) - Constructor for class org.orekit.forces.maneuvers.ConstantThrustManeuver
Simple constructor for a constant direction and constant thrust.
ConstantThrustManeuver(AbsoluteDate, double, double, double, AttitudeProvider, Vector3D, Control3DVectorCostType, String) - Constructor for class org.orekit.forces.maneuvers.ConstantThrustManeuver
Simple constructor for a constant direction and constant thrust.
ConstantThrustManeuver(AbsoluteDate, double, AttitudeProvider, AbstractConstantThrustPropulsionModel) - Constructor for class org.orekit.forces.maneuvers.ConstantThrustManeuver
Simple constructor for a constant direction and constant thrust.
ConstantTroposphericModel - Class in org.orekit.models.earth.troposphere
Defines a constant tropospheric model.
ConstantTroposphericModel(TroposphericDelay) - Constructor for class org.orekit.models.earth.troposphere.ConstantTroposphericModel
Simple constructor.
ConstantViennaAProvider - Class in org.orekit.models.earth.troposphere
Provider for constant Vienna A coefficients.
ConstantViennaAProvider(ViennaACoefficients) - Constructor for class org.orekit.models.earth.troposphere.ConstantViennaAProvider
Simple constructor.
CONSTELLATION - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Name of the constellation this space object belongs to.
containsSatellite(String) - Method in class org.orekit.files.sp3.SP3
Tests whether a satellite with the given id is contained in this orbit file.
ContextBinding - Class in org.orekit.files.ccsds.utils
Context for parsing/writing Navigation Data Message.
ContextBinding(Supplier<IERSConventions>, BooleanSupplier, Supplier<DataContext>, Supplier<ParsedUnitsBehavior>, Supplier<AbsoluteDate>, Supplier<TimeSystem>, DoubleSupplier, DoubleSupplier) - Constructor for class org.orekit.files.ccsds.utils.ContextBinding
Create a new context.
ContinueOnEvent - Class in org.orekit.propagation.events.handlers
Event handler which will always return continue as a state.
ContinueOnEvent() - Constructor for class org.orekit.propagation.events.handlers.ContinueOnEvent
Empty constructor.
CONTINUOUS - org.orekit.files.ccsds.definitions.DutyCycleType
Full/continuous thrust.
ContinuousScheduler<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.generation
Scheduler generating measurements sequences continuously.
ContinuousScheduler(MeasurementBuilder<T>, DatesSelector) - Constructor for class org.orekit.estimation.measurements.generation.ContinuousScheduler
Simple constructor.
Control3DVectorCostType - Enum in org.orekit.forces.maneuvers
Enumerate on types of cost for 3D control vector (thrust as a force or acceleration, including an impulse) at a given time.
convert() - Method in class org.orekit.propagation.conversion.OsculatingToMeanElementsConverter
Convert an osculating orbit into a mean orbit, in DSST sense.
convert(double) - Method in class org.orekit.utils.units.UnitsConverter
Convert a value.
convert(double[]) - Method in interface org.orekit.data.SimpleTimeStampedTableParser.RowConverter
Convert a row.
convert(List<SpacecraftState>, boolean, String...) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Find the propagator that minimize the mean square error for a sample of states.
convert(List<SpacecraftState>, boolean, String...) - Method in interface org.orekit.propagation.conversion.PropagatorConverter
Find the propagator that minimize the mean square error for a sample of states.
convert(List<SpacecraftState>, boolean, List<String>) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Find the propagator that minimize the mean square error for a sample of states.
convert(List<SpacecraftState>, boolean, List<String>) - Method in interface org.orekit.propagation.conversion.PropagatorConverter
Find the propagator that minimize the mean square error for a sample of states.
convert(FieldPressureTemperatureHumidity<T>, T) - Method in class org.orekit.models.earth.weather.HeightDependentPressureTemperatureHumidityConverter
Convert weather parameters.
convert(PressureTemperatureHumidity, double) - Method in class org.orekit.models.earth.weather.HeightDependentPressureTemperatureHumidityConverter
Convert weather parameters.
convert(Propagator, double, int, String...) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Convert a propagator to another.
convert(Propagator, double, int, String...) - Method in interface org.orekit.propagation.conversion.PropagatorConverter
Convert a propagator into another one.
convert(Propagator, double, int, List<String>) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Convert a propagator to another.
convert(Propagator, double, int, List<String>) - Method in interface org.orekit.propagation.conversion.PropagatorConverter
Convert a propagator into another one.
CONVERT_COMPATIBLE - org.orekit.files.ccsds.ndm.ParsedUnitsBehavior
Allow compatible units, performing conversion.
convert2DigitsYear(int) - Static method in class org.orekit.files.rinex.utils.parsing.RinexUtils
Convert a 2 digits year to a complete year.
convertAlpha(PositionAngleType, double, double, double, PositionAngleType) - Static method in class org.orekit.orbits.CircularLatitudeArgumentUtility
Convert argument of latitude.
convertAlpha(PositionAngleType, T, T, T, PositionAngleType) - Static method in class org.orekit.orbits.FieldCircularLatitudeArgumentUtility
Convert argument of latitude.
convertAnomaly(PositionAngleType, double, double, PositionAngleType) - Static method in class org.orekit.orbits.KeplerianAnomalyUtility
Convert anomaly.
convertAnomaly(PositionAngleType, T, T, PositionAngleType) - Static method in class org.orekit.orbits.FieldKeplerianAnomalyUtility
Convert anomaly.
convertFromLofType(LOFType, RealMatrix, Vector3D, Vector3D) - Static method in class org.orekit.utils.CartesianCovarianceUtils
Convert input position-velocity covariance matrix from local frame to reference one.
convertIntervalDetector(Field<S>, ParameterDrivenDateIntervalDetector) - Method in class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers
Convert a primitive firing intervals detector into a field firing intervals detector.
convertIntervalDetector(Field<S>, T) - Method in class org.orekit.forces.maneuvers.trigger.IntervalEventTrigger
Convert a primitive firing intervals detector into a field firing intervals detector.
convertL(PositionAngleType, double, double, double, PositionAngleType) - Static method in class org.orekit.orbits.EquinoctialLongitudeArgumentUtility
Convert argument of longitude.
convertL(PositionAngleType, T, T, T, PositionAngleType) - Static method in class org.orekit.orbits.FieldEquinoctialLongitudeArgumentUtility
Convert argument of longitude.
convertStartDetector(Field<S>, A) - Method in class org.orekit.forces.maneuvers.trigger.StartStopEventsTrigger
Convert a primitive firing start detector into a field firing start detector.
convertStopDetector(Field<S>, O) - Method in class org.orekit.forces.maneuvers.trigger.StartStopEventsTrigger
Convert a primitive firing stop detector into a field firing stop detector.
convertToAveraged(Orbit) - Method in interface org.orekit.propagation.conversion.averaging.converters.OsculatingToAveragedConverter
Convert osculating orbit to averaged orbital state according to underlying theory.
convertToAveraged(Orbit) - Method in class org.orekit.propagation.conversion.averaging.converters.OsculatingToBrouwerLyddaneConverter
Convert osculating orbit to averaged orbital state according to underlying theory.
convertToAveraged(Orbit) - Method in class org.orekit.propagation.conversion.averaging.converters.OsculatingToDSST6X0Converter
Convert osculating orbit to averaged orbital state according to underlying theory.
convertToAveraged(Orbit) - Method in class org.orekit.propagation.conversion.averaging.converters.OsculatingToEcksteinHechlerConverter
Convert osculating orbit to averaged orbital state according to underlying theory.
convertToAveraged(Orbit) - Method in class org.orekit.propagation.conversion.averaging.converters.OsculatingToSGP4Converter
Convert osculating orbit to averaged orbital state according to underlying theory.
convertToFieldOrbit(Field<T>, Orbit) - Method in enum org.orekit.orbits.OrbitType
Convert an orbit to the "Fielded" instance type.
convertToLofType(Vector3D, Vector3D, RealMatrix, LOFType) - Static method in class org.orekit.utils.CartesianCovarianceUtils
Convert input position-velocity covariance matrix from reference frame to local one.
convertType(FieldOrbit<T>) - Method in enum org.orekit.orbits.OrbitType
Convert an orbit to the instance type.
convertType(Orbit) - Method in enum org.orekit.orbits.OrbitType
Convert an orbit to the instance type.
copy() - Method in class org.orekit.propagation.conversion.BrouwerLyddanePropagatorBuilder
Deprecated.
copy() - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder
Deprecated.
copy() - Method in class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder
Deprecated.
copy() - Method in class org.orekit.propagation.conversion.EphemerisPropagatorBuilder
Deprecated.
copy() - Method in class org.orekit.propagation.conversion.KeplerianPropagatorBuilder
Deprecated.
copy() - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
Deprecated.
copy() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
Deprecated.
as of 12.2, replaced by Object.clone()
copy() - Method in class org.orekit.propagation.conversion.TLEPropagatorBuilder
Deprecated.
copy(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Copy the instance, making sure mandatory fields have been initialized.
copy(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Copy the instance, making sure mandatory fields have been initialized.
copyObservationData(ObservationData) - Method in class org.orekit.estimation.measurements.filtering.DualFrequencySmoother
Copy an ObservationData object.
copyObservationData(ObservationData) - Method in class org.orekit.estimation.measurements.filtering.SingleFrequencySmoother
Copy an ObservationData object.
correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.BeidouGeo
Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.BeidouMeo
Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.Galileo
Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.GenericGNSS
Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.Glonass
Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.GPSBlockIIA
Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.GPSBlockIIF
Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.GPSBlockIIR
Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSFieldAttitudeContext<T>) - Method in class org.orekit.gnss.attitude.BeidouGeo
Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSFieldAttitudeContext<T>) - Method in class org.orekit.gnss.attitude.BeidouMeo
Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSFieldAttitudeContext<T>) - Method in class org.orekit.gnss.attitude.Galileo
Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSFieldAttitudeContext<T>) - Method in class org.orekit.gnss.attitude.GenericGNSS
Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSFieldAttitudeContext<T>) - Method in class org.orekit.gnss.attitude.Glonass
Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSFieldAttitudeContext<T>) - Method in class org.orekit.gnss.attitude.GPSBlockIIA
Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSFieldAttitudeContext<T>) - Method in class org.orekit.gnss.attitude.GPSBlockIIF
Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSFieldAttitudeContext<T>) - Method in class org.orekit.gnss.attitude.GPSBlockIIR
Compute GNSS attitude with midnight/noon yaw turn correction.
CORRECTION_ABERRATION_DIURNAL - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Diurnal aberration correction entry.
CORRECTION_ABERRATION_YEARLY - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Yearly aberration correction entry.
CORRECTION_ANGLE_1 - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Angle 1 correction entry.
CORRECTION_ANGLE_2 - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Angle 2 correction entry.
CORRECTION_DOPPLER - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Doppler correction entry.
CORRECTION_MAG - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Magnitude correction entry.
CORRECTION_RANGE - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Range correction entry (beware the unit is Range Units here).
CORRECTION_RCS - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Radar Cross Section correction entry.
CORRECTION_RECEIVE - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Receive correction entry.
CORRECTION_TRANSMIT - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Transmit correction entry.
CorrectionApplied - Enum in org.orekit.files.ccsds.ndm.tdm
Indicator for corrections application.
CORRECTIONS_APPLIED - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Applied correction entry.
CORRUPTED_FILE - org.orekit.errors.OrekitMessages
CORRUPTED_FILE.
cosi0 - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
cosinus original inclination.
cosi0 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
cosinus original inclination.
COULOMB - Static variable in class org.orekit.utils.units.Unit
Coulomb unit.
countAtDate(AbsoluteDate) - Method in class org.orekit.time.SatelliteClockScale
Compute clock count corresponding to some date.
COUNTRY - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Name of the country where the space object owner is based.
cov - org.orekit.files.ccsds.ndm.adm.acm.AcmDataSubStructureKey
Covariance time history section.
cov - org.orekit.files.ccsds.ndm.odm.ocm.OcmDataSubStructureKey
Covariance time history section.
COV - org.orekit.files.ccsds.ndm.adm.acm.AcmDataSubStructureKey
Covariance time history section.
COV - org.orekit.files.ccsds.ndm.adm.acm.AcmElements
Covariance time history.
COV - org.orekit.files.ccsds.ndm.odm.ocm.OcmDataSubStructureKey
Covariance time history section.
COV - org.orekit.files.ccsds.ndm.odm.ocm.OcmElements
Covariance time history.
COV_BASIS - org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadataKey
Basis of this covariance time history data.
COV_BASIS - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadataKey
Basis of this covariance time history data.
COV_BASIS_ID - org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadataKey
Identification number of the orbit determination or simulation upon which this covariance is based.
COV_BASIS_ID - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadataKey
Identification number of the orbit determination or simulation upon which this covariance is based.
COV_CONFIDENCE - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
A measure of the confidence in the covariance errors matching reality.
COV_CONFIDENCE - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadataKey
Masure of confidence in covariance error matching reality.
COV_CONFIDENCE_METHOD - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
The method used for the calculation of COV_CONFIDENCE.
COV_FRAME_EPOCH - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadataKey
COV_ID - org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadataKey
Covariance identification number.
COV_ID - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadataKey
Covariance identification number.
COV_LINE - Static variable in class org.orekit.files.ccsds.ndm.adm.acm.Acm
Covariance line element for XML messages.
COV_LINE - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.Ocm
Covariance line element for XML messages.
COV_NEXT_ID - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadataKey
Identification number of next covariance.
COV_ORDERING - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadataKey
Covariance ordering.
COV_PREV_ID - org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadataKey
Identification number of previous covariance.
COV_PREV_ID - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadataKey
Identification number of previous covariance.
COV_REF_FRAME - org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadataKey
Reference frame of the covariance.
COV_REF_FRAME - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey
Coordinate system for covariance matrix.
COV_REF_FRAME - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadataKey
Reference frame of the covariance.
COV_SCALE_MAX - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadataKey
Maximum scale factor to apply to achieve realism.
COV_SCALE_MIN - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadataKey
Minimum scale factor to apply to achieve realism.
COV_TYPE - org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadataKey
Covariance element set type.
COV_TYPE - org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationKey
Type of attitude error state.
COV_TYPE - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadataKey
Covariance element set type.
COV_UNITS - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadataKey
SI units for each elements of the covariance.
COVARIANCE_METHOD - org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey
Method used to calculate the covariance.
COVARIANCE_SOURCE - org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey
The source from which the covariance data used in the report for both Object 1 and Object 2 originates.
covarianceMatrix - org.orekit.files.ccsds.ndm.cdm.XmlSubStructureKey
Covariance Matrix section.
CovarianceMatrixProvider - Interface in org.orekit.estimation.sequential
Provider for process noise matrices.
CovarianceMethod - Enum in org.orekit.files.ccsds.ndm.cdm
Maneuvrable possibilities used in CCSDS Conjunction Data Messages.
CP - org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalPropertiesKey
Center of pressure.
CP_REF_FRAME - org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalPropertiesKey
Reference frame for center of pressure.
CPF - Class in org.orekit.files.ilrs
This class stores all the information of the Consolidated laser ranging Prediction File (CPF) parsed by CPFParser.
CPF() - Constructor for class org.orekit.files.ilrs.CPF
Constructor.
CPF_UNEXPECTED_END_OF_FILE - org.orekit.errors.OrekitMessages
CPF_UNEXPECTED_END_OF_FILE.
CPF.CPFCoordinate - Class in org.orekit.files.ilrs
A single record of position and possibility velocity in an SP3 file.
CPF.CPFEphemeris - Class in org.orekit.files.ilrs
An ephemeris entry for a single satellite contains in a CPF file.
CPFCoordinate(AbsoluteDate, Vector3D, int) - Constructor for class org.orekit.files.ilrs.CPF.CPFCoordinate
Constructor with null velocity vector.
CPFCoordinate(AbsoluteDate, Vector3D, Vector3D, int) - Constructor for class org.orekit.files.ilrs.CPF.CPFCoordinate
Constructor.
CPFEphemeris(String) - Constructor for class org.orekit.files.ilrs.CPF.CPFEphemeris
Constructor.
CPFHeader - Class in org.orekit.files.ilrs
Container for Consolidated laser ranging Prediction File (CPF) header.
CPFHeader() - Constructor for class org.orekit.files.ilrs.CPFHeader
Empty constructor.
CPFParser - Class in org.orekit.files.ilrs
A parser for the CPF orbit file format.
CPFParser() - Constructor for class org.orekit.files.ilrs.CPFParser
Default constructor.
CPFParser(double, int, IERSConventions, TimeScale, Frames) - Constructor for class org.orekit.files.ilrs.CPFParser
Constructor.
CPFWriter - Class in org.orekit.files.ilrs
An CPF Writer class that can take in a general EphemerisFile object and export it as a valid CPF file.
CPFWriter(CPFHeader, TimeScale) - Constructor for class org.orekit.files.ilrs.CPFWriter
Constructor.
CPFWriter(CPFHeader, TimeScale, boolean) - Constructor for class org.orekit.files.ilrs.CPFWriter
Constructor.
CR - org.orekit.files.rinex.clock.RinexClock.ClockDataType
Calibration measurement for a single GPS receiver.
CR_AREA_OVER_MASS - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
The object’s Cr x A/m used to propagate the state vector and covariance to TCA.
CR_R - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [1,1].
CR3BPConstants - Class in org.orekit.propagation.numerical.cr3bp
Set of useful physical CR3BP constants using JPL data.
CR3BPDifferentialCorrection - Class in org.orekit.orbits
Class implementing the differential correction method for Halo or Lyapunov Orbits.
CR3BPDifferentialCorrection(PVCoordinates, CR3BPSystem, double) - Constructor for class org.orekit.orbits.CR3BPDifferentialCorrection
Simple Constructor.
CR3BPFactory - Class in org.orekit.bodies
Factory class creating predefined CR3BP system using CR3BPSystem class.
CR3BPForceModel - Class in org.orekit.propagation.numerical.cr3bp
Class calculating the acceleration induced by CR3BP model.
CR3BPForceModel(CR3BPSystem) - Constructor for class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel
Simple constructor.
CR3BPMultipleShooter - Class in org.orekit.propagation.numerical.cr3bp
Multiple shooting method applicable for orbits, either propagation in CR3BP, or in an ephemeris model.
CR3BPMultipleShooter(List<SpacecraftState>, List<NumericalPropagator>, List<STMEquations>, double, int) - Constructor for class org.orekit.propagation.numerical.cr3bp.CR3BPMultipleShooter
Simple Constructor.
CR3BPRotatingFrame - Class in org.orekit.frames
Class creating the rotating frame centered on the barycenter of the CR3BP System.
CR3BPRotatingFrame(double, CelestialBody, CelestialBody) - Constructor for class org.orekit.frames.CR3BPRotatingFrame
Simple constructor.
CR3BPSystem - Class in org.orekit.bodies
Class creating, from two different celestial bodies, the corresponding system with respect to the Circular Restricted Three Body problem hypotheses.
CR3BPSystem(CelestialBody, CelestialBody, double) - Constructor for class org.orekit.bodies.CR3BPSystem
Simple constructor.
CR3BPSystem(CelestialBody, CelestialBody, double, double) - Constructor for class org.orekit.bodies.CR3BPSystem
Simple constructor.
CRD - Class in org.orekit.files.ilrs
This class stores all the information of the Consolidated laser ranging Data Format (CRD) parsed by CRDParser.
CRD() - Constructor for class org.orekit.files.ilrs.CRD
Constructor.
CRD_UNEXPECTED_END_OF_FILE - org.orekit.errors.OrekitMessages
CRD_UNEXPECTED_END_OF_FILE.
CRD.AnglesMeasurement - Class in org.orekit.files.ilrs
Pointing angles record.
CRD.Calibration - Class in org.orekit.files.ilrs
Calibration Record.
CRD.CalibrationDetail - Class in org.orekit.files.ilrs
Calibration Detail Record.
CRD.CRDDataBlock - Class in org.orekit.files.ilrs
Data block containing a set of data contain in the CRD file.
CRD.FrRangeMeasurement - Class in org.orekit.files.ilrs
Range record -- Full rate, Sampled Engineering/Quicklook.
CRD.Meteo - Class in org.orekit.files.ilrs
Meteorological data.
CRD.MeteorologicalMeasurement - Class in org.orekit.files.ilrs
This data record contains a minimal set of meteorological data.
CRD.NptRangeMeasurement - Class in org.orekit.files.ilrs
Range record -- Normal Point.
CRD.RangeMeasurement - Class in org.orekit.files.ilrs
Range record.
CRD.RangeSupplement - Class in org.orekit.files.ilrs
Range Supplement Record.
CRD.SessionStatistics - Class in org.orekit.files.ilrs
Session (Pass) Statistics Record.
CRDConfiguration - Class in org.orekit.files.ilrs
Container for Consolidated laser ranging Data Format (CDR) configuration records.
CRDConfiguration() - Constructor for class org.orekit.files.ilrs.CRDConfiguration
Constructor.
CRDConfiguration.BaseConfiguration - Class in org.orekit.files.ilrs
Base class for configuration record.
CRDConfiguration.CalibrationTargetConfiguration - Class in org.orekit.files.ilrs
Container for calibration target configuration record.
CRDConfiguration.DetectorConfiguration - Class in org.orekit.files.ilrs
Container for detector configuration record.
CRDConfiguration.LaserConfiguration - Class in org.orekit.files.ilrs
Container for laser configuration record.
CRDConfiguration.MeteorologicalConfiguration - Class in org.orekit.files.ilrs
Container for meteorological configuration record.
CRDConfiguration.SoftwareConfiguration - Class in org.orekit.files.ilrs
Container for software configuration record.
CRDConfiguration.SystemConfiguration - Class in org.orekit.files.ilrs
Container for system configuration record.
CRDConfiguration.TimingSystemConfiguration - Class in org.orekit.files.ilrs
Container for timing system configuration record.
CRDConfiguration.TransponderConfiguration - Class in org.orekit.files.ilrs
Container for transponder configuration record.
CRDDataBlock() - Constructor for class org.orekit.files.ilrs.CRD.CRDDataBlock
Constructor.
CRDHeader - Class in org.orekit.files.ilrs
Container for Consolidated laser ranging Data Format (CDR) header.
CRDHeader() - Constructor for class org.orekit.files.ilrs.CRDHeader
Empty constructor.
CRDHeader.DataType - Enum in org.orekit.files.ilrs
Data type for CRD data.
CRDHeader.RangeType - Enum in org.orekit.files.ilrs
Range type for SLR data.
CRDOT_N - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [4,3].
CRDOT_R - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [4,1].
CRDOT_RDOT - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [4,4].
CRDOT_T - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [4,2].
CRDParser - Class in org.orekit.files.ilrs
A parser for the CRD data file format.
CRDParser() - Constructor for class org.orekit.files.ilrs.CRDParser
Default constructor.
CRDParser(TimeScale) - Constructor for class org.orekit.files.ilrs.CRDParser
Constructor.
create(OneAxisEllipsoid, GeodeticPoint) - Static method in class org.orekit.gnss.DOPComputer
Creates a DOP computer for one location.
create(CenterName) - Static method in class org.orekit.files.ccsds.definitions.BodyFacade
Create a body facade from an input center name.
create(CenterName, CelestialBodies) - Static method in class org.orekit.files.ccsds.definitions.BodyFacade
Create a body facade from an input center name.
create(CenterName, DataContext) - Static method in class org.orekit.files.ccsds.definitions.BodyFacade
Create a body facade from an input center name.
create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
Build a new instance.
create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.AbstractDetector
Deprecated.
as of 12.2. Will be removed in 13.0 and only the other signature shall remain
create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.AlignmentDetector
Build a new instance.
create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.AltitudeDetector
Build a new instance.
create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.AngularSeparationDetector
Build a new instance.
create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.AngularSeparationFromSatelliteDetector
Build a new instance.
create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.ApsideDetector
Build a new instance.
create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.BetaAngleDetector
Build a new instance.
create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.BooleanDetector
 
create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.CylindricalShadowEclipseDetector
Build a new instance.
create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.DateDetector
Build a new instance.
create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.EclipseDetector
Build a new instance.
create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.ElevationDetector
Build a new instance.
create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.ElevationExtremumDetector
Build a new instance.
create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.EventEnablingPredicateFilter
Build a new instance.
create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.EventShifter
Build a new instance.
create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.EventSlopeFilter
Build a new instance.
create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.ExtremumApproachDetector
Build a new instance.
create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.FieldOfViewDetector
Build a new instance.
create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.FootprintOverlapDetector
Build a new instance.
create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.FunctionalDetector
 
create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.GeographicZoneDetector
Build a new instance.
create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.GroundAtNightDetector
Build a new instance.
create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.GroundFieldOfViewDetector
Build a new instance.
create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.HaloXZPlaneCrossingDetector
Build a new instance.
create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.InterSatDirectViewDetector
Build a new instance.
create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.LatitudeCrossingDetector
Build a new instance.
create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.LatitudeExtremumDetector
Build a new instance.
create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.LatitudeRangeCrossingDetector
Build a new instance.
create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.LongitudeCrossingDetector
Build a new instance.
create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.LongitudeExtremumDetector
Build a new instance.
create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.LongitudeRangeCrossingDetector
Build a new instance.
create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.MagneticFieldDetector
Build a new instance.
create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.NegateDetector
 
create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.NodeDetector
Build a new instance.
create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector
Build a new instance.
create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.PositionAngleDetector
Build a new instance.
create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.propagation.events.RelativeDistanceDetector
Build a new instance.
create(EventDetectionSettings, EventHandler) - Method in class org.orekit.propagation.events.AbstractDetector
Build a new instance.
create(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Method in class org.orekit.forces.maneuvers.FieldImpulseManeuver
Build a new instance.
create(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldAbstractDetector
Deprecated.
as of 12.2
create(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldAltitudeDetector
Build a new instance.
create(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldApsideDetector
Build a new instance.
create(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldBetaAngleDetector
Build a new instance.
create(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldBooleanDetector
 
create(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldCylindricalShadowEclipseDetector
Build a new instance.
create(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldDateDetector
Build a new instance.
create(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldEclipseDetector
Build a new instance.
create(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldElevationDetector
Build a new instance.
create(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldElevationExtremumDetector
Build a new instance.
create(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldEventEnablingPredicateFilter
Build a new instance.
create(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldEventSlopeFilter
Build a new instance.
create(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldExtremumApproachDetector
Build a new instance.
create(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldFunctionalDetector
 
create(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldLatitudeCrossingDetector
Build a new instance.
create(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldLatitudeRangeCrossingDetector
Build a new instance.
create(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldLongitudeCrossingDetector
Build a new instance.
create(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldLongitudeRangeCrossingDetector
Build a new instance.
create(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldNegateDetector
 
create(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldNodeDetector
Build a new instance.
create(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector
Build a new instance.
create(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldRelativeDistanceDetector
Build a new instance.
create(FieldEventDetectionSettings<T>, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldAbstractDetector
Build a new instance.
create(AbsoluteDate, GeodeticPoint, AbsoluteDate, GeodeticPoint, OneAxisEllipsoid) - Method in interface org.orekit.utils.WaypointPVBuilder.InterpolationFactory
Create a PVCoordinatesProvider which interpolates between the provided waypoints.
create(IERSConventions, double, double, DataContext, AbsoluteDate, RangeUnitsConverter) - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder
Build an instance.
create(IERSConventions, double, double, DataContext, AbsoluteDate, RangeUnitsConverter) - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Build an instance.
create(IERSConventions, double, double, DataContext, AbsoluteDate, RangeUnitsConverter) - Method in class org.orekit.files.ccsds.ndm.WriterBuilder
Build an instance.
createBesselianEpoch(double) - Static method in class org.orekit.time.AbsoluteDate
Build an instance corresponding to a Besselian Epoch (BE).
createBesselianEpoch(double) - Method in class org.orekit.time.AbstractTimeScales
 
createBesselianEpoch(double) - Method in interface org.orekit.time.TimeScales
Build an instance corresponding to a Besselian Epoch (BE).
createBesselianEpoch(T) - Static method in class org.orekit.time.FieldAbsoluteDate
Build an instance corresponding to a Besselian Epoch (BE).
createBesselianEpoch(T, TimeScales) - Static method in class org.orekit.time.FieldAbsoluteDate
Build an instance corresponding to a Besselian Epoch (BE).
createDataFields(boolean, boolean, RotationOrder, boolean, TimeStampedAngularCoordinates) - Method in enum org.orekit.files.ccsds.ndm.adm.AttitudeType
Get the attitude data fields corresponding to the attitude type.
createDefaultDut1FitterLongTermPrediction() - Static method in class org.orekit.frames.SingleParameterFitter
Create fitter with default parameters adapted for fitting orientation parameters dUT1 and LOD for long term prediction.
createDefaultDut1FitterShortTermPrediction() - Static method in class org.orekit.frames.SingleParameterFitter
Create fitter with default parameters adapted for fitting orientation parameters dUT1 and LOD for short term prediction.
createDefaultNutationFitterLongTermPrediction() - Static method in class org.orekit.frames.SingleParameterFitter
Create fitter with default parameters adapted for fitting nutation parameters dx and dy for long term prediction.
createDefaultNutationFitterShortTermPrediction() - Static method in class org.orekit.frames.SingleParameterFitter
Create fitter with default parameters adapted for fitting nutation parameters dx and dy for long term prediction.
createDefaultPoleFitterLongTermPrediction() - Static method in class org.orekit.frames.SingleParameterFitter
Create fitter with default parameters adapted for fitting pole parameters Xp and Yp for long term prediction.
createDefaultPoleFitterShortTermPrediction() - Static method in class org.orekit.frames.SingleParameterFitter
Create fitter with default parameters adapted for fitting pole parameters Xp and Yp for long term prediction.
createFieldStateWithMassAndAdjoint(double, double[]) - Method in class org.orekit.control.indirect.shooting.AbstractFixedBoundaryCartesianSingleShooting
Create initial state with input mass and adjoint vector.
createFilter(ObservationData, ObservationData, ObservationData, SatelliteSystem) - Method in class org.orekit.estimation.measurements.filtering.DualFrequencySmoother
Creates an Hatch filter given initial data.
createFilter(ObservationData, ObservationData, SatelliteSystem) - Method in class org.orekit.estimation.measurements.filtering.SingleFrequencySmoother
Creates an Hatch filter given initial data.
createFinal(AbsoluteDate, GeodeticPoint) - Method in class org.orekit.utils.WaypointPVBuilder
Create the final provider.
createForces(UnnormalizedSphericalHarmonicsProvider) - Static method in class org.orekit.propagation.conversion.averaging.DSST6X0OrbitalState
Create collection of fist 6 zonal DSST forces.
createFromModifiedRodrigues(double[][]) - Static method in class org.orekit.utils.AngularCoordinates
Convert a modified Rodrigues vector and derivatives to angular coordinates.
createFromModifiedRodrigues(T[][]) - Static method in class org.orekit.utils.FieldAngularCoordinates
Convert a modified Rodrigues vector and derivatives to angular coordinates.
createFromWeekComponents(int, int, int) - Static method in class org.orekit.time.DateComponents
Build a date from week components.
createGPSDate(int, T) - Static method in class org.orekit.time.FieldAbsoluteDate
Build an instance corresponding to a GPS date.
createGPSDate(int, T, TimeScale) - Static method in class org.orekit.time.FieldAbsoluteDate
Build an instance corresponding to a GPS date.
createHarvester(String, RealMatrix, DoubleArrayDictionary) - Method in class org.orekit.propagation.AbstractPropagator
Create the harvester suitable for propagator.
createHarvester(String, RealMatrix, DoubleArrayDictionary) - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Create the harvester suitable for propagator.
createHarvester(String, RealMatrix, DoubleArrayDictionary) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Create the harvester suitable for propagator.
createHarvester(String, RealMatrix, DoubleArrayDictionary) - Method in class org.orekit.propagation.analytical.Ephemeris
Create the harvester suitable for propagator.
createHarvester(String, RealMatrix, DoubleArrayDictionary) - Method in class org.orekit.propagation.analytical.KeplerianPropagator
Create the harvester suitable for propagator.
createHarvester(String, RealMatrix, DoubleArrayDictionary) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
Create the harvester suitable for propagator.
createHarvester(String, RealMatrix, DoubleArrayDictionary) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Create the harvester suitable for propagator.
createHarvester(String, RealMatrix, DoubleArrayDictionary) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Create the harvester suitable for propagator.
createInitial(AbsoluteDate, GeodeticPoint) - Method in class org.orekit.utils.WaypointPVBuilder
Create the initial provider.
createInitialOrbit() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Build an initial orbit using the current selected parameters.
createJDDate(int, double, TimeScale) - Static method in class org.orekit.time.AbsoluteDate
Build an instance corresponding to a Julian Day date.
createJDDate(int, double, TimeScale, TimeScale) - Static method in class org.orekit.time.AbsoluteDate
Build an instance corresponding to a Julian Day date.
createJDDate(int, T, TimeScale) - Static method in class org.orekit.time.FieldAbsoluteDate
Build an instance corresponding to a Julian Day date.
createJDDate(int, T, TimeScale, TimeScale) - Static method in class org.orekit.time.FieldAbsoluteDate
Build an instance corresponding to a Julian Day date.
createJulianEpoch(double) - Static method in class org.orekit.time.AbsoluteDate
Build an instance corresponding to a Julian Epoch (JE).
createJulianEpoch(double) - Method in class org.orekit.time.AbstractTimeScales
 
createJulianEpoch(double) - Method in interface org.orekit.time.TimeScales
Build an instance corresponding to a Julian Epoch (JE).
createJulianEpoch(T) - Static method in class org.orekit.time.FieldAbsoluteDate
Build an instance corresponding to a Julian Epoch (JE).
createJulianEpoch(T, TimeScales) - Static method in class org.orekit.time.FieldAbsoluteDate
Build an instance corresponding to a Julian Epoch (JE).
createMapper(AbsoluteDate, double, OrbitType, PositionAngleType, AttitudeProvider, Frame) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Create a mapper between raw double components and spacecraft state.
createMapper(AbsoluteDate, double, OrbitType, PositionAngleType, AttitudeProvider, Frame) - Method in class org.orekit.propagation.numerical.GLONASSNumericalPropagator
 
createMapper(AbsoluteDate, double, OrbitType, PositionAngleType, AttitudeProvider, Frame) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Create a mapper between raw double components and spacecraft state.
createMapper(AbsoluteDate, double, OrbitType, PositionAngleType, AttitudeProvider, Frame) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Create a mapper between raw double components and spacecraft state.
createMapper(FieldAbsoluteDate<T>, T, OrbitType, PositionAngleType, AttitudeProvider, Frame) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Create a mapper between raw double components and spacecraft state.
createMapper(FieldAbsoluteDate<T>, T, OrbitType, PositionAngleType, AttitudeProvider, Frame) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Create a mapper between raw double components and spacecraft state.
createMapper(FieldAbsoluteDate<T>, T, OrbitType, PositionAngleType, AttitudeProvider, Frame) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Create a mapper between raw double components and spacecraft state.
createMJDDate(int, double, TimeScale) - Static method in class org.orekit.time.AbsoluteDate
Build an instance corresponding to a Modified Julian Day date.
createMJDDate(int, T, TimeScale) - Static method in class org.orekit.time.FieldAbsoluteDate
Build an instance corresponding to a Modified Julian Day date.
createPropagators(RealVector) - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel
Create the propagators and parameters corresponding to an evaluation point.
createSlot(FieldSpacecraftState<T>...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldGaussianShortPeriodicCoefficients
Get the slot valid for some date.
createSlot(SpacecraftState...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.GaussianShortPeriodicCoefficients
Get the slot valid for some date.
createStateWithMassAndAdjoint(double, double[]) - Method in class org.orekit.control.indirect.shooting.AbstractFixedBoundaryCartesianSingleShooting
Create initial state with input mass and adjoint vector.
createTransformedITRF(Frame, String) - Method in enum org.orekit.frames.HelmertTransformation.Predefined
Create an ITRF frame by transforming another ITRF frame.
createTransformedITRF(Frame, String, TimeScale) - Method in enum org.orekit.frames.HelmertTransformation.Predefined
Create an ITRF frame by transforming another ITRF frame.
createVertex(Vector3D, Vector3D, double, int) - Method in enum org.orekit.geometry.fov.PolygonalFieldOfView.DefiningConeType
Create a vertex.
CREATION_DATE - org.orekit.files.ccsds.section.HeaderKey
Creation date.
crossProduct(FieldPVCoordinates<T>) - Method in class org.orekit.utils.FieldPVCoordinates
Compute the cross-product of two instances.
crossProduct(PVCoordinates, PVCoordinates) - Static method in class org.orekit.utils.PVCoordinates
Compute the cross-product of two instances.
CSCALE_FACTOR - org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadataKey
The (median) suggested covariance scale factor.
CSCALE_FACTOR_MAX - org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadataKey
The maximum suggested covariance scale factor.
CSCALE_FACTOR_MIN - org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadataKey
The minimum suggested covariance scale factor.
CSIG3EIGVEC3 - org.orekit.files.ccsds.ndm.cdm.AltCovarianceType
Sigma/Eigenvector Format.
CSIG3EIGVEC3 - org.orekit.files.ccsds.ndm.cdm.SigmaEigenvectorsCovarianceKey
The 3x3 positional covariance one-sigma dispersions corresponding to the major, intermediate and minor eigenvalues, followed by the associated eigenvectors.
CSRP_DRG - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [8,7].
CSRP_DRG - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [8,7].
CSRP_N - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [8,3].
CSRP_NDOT - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [8,6].
CSRP_R - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [8,1].
CSRP_RDOT - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [8,4].
CSRP_SRP - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [8,9].
CSRP_SRP - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [8,9].
CSRP_T - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [8,2].
CSRP_TDOT - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [8,5].
CSRP_X - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [8,1].
CSRP_XDOT - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [8,4].
CSRP_Y - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [8,2].
CSRP_YDOT - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [8,5].
CSRP_Z - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [8,3].
CSRP_ZDOT - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [8,6].
CSS - org.orekit.files.ccsds.definitions.SpacecraftBodyFrame.BaseEquipment
Coarse Sun Sensor.
CssiSpaceWeatherData - Class in org.orekit.models.earth.atmosphere.data
This class provides three-hourly and daily solar activity data needed by atmospheric models: F107 solar flux, Ap and Kp indexes.
CssiSpaceWeatherData(String) - Constructor for class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
Simple constructor.
CssiSpaceWeatherData(String, DataProvidersManager, TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
Constructor that allows specifying the source of the CSSI space weather file.
CssiSpaceWeatherData(String, CssiSpaceWeatherDataLoader, DataProvidersManager, TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
Constructor that allows specifying the source of the CSSI space weather file.
CssiSpaceWeatherData(String, CssiSpaceWeatherDataLoader, DataProvidersManager, TimeScale, int, double, double) - Constructor for class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
Constructor that allows specifying the source of the CSSI space weather file and customizable thread safe cache configuration.
CssiSpaceWeatherData(DataSource) - Constructor for class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
Simple constructor which use the default data context.
CssiSpaceWeatherData(DataSource, CssiSpaceWeatherDataLoader, TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
Simple constructor.
CssiSpaceWeatherData(DataSource, CssiSpaceWeatherDataLoader, TimeScale, int, double, double) - Constructor for class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
Simple constructor with customizable thread safe cache configuration.
CssiSpaceWeatherData(DataSource, TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
Simple constructor.
CssiSpaceWeatherDataLoader - Class in org.orekit.models.earth.atmosphere.data
This class reads solar activity data from CSSI Space Weather files for the class CssiSpaceWeatherData.
CssiSpaceWeatherDataLoader(TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader
Constructor.
CssiSpaceWeatherDataLoader.LineParameters - Class in org.orekit.models.earth.atmosphere.data
Container class for Solar activity indexes.
CSV_FILENAME - Static variable in class org.orekit.frames.FramesFactory
Default regular expression for the csv files (IAU1980 and IAU2000 compatibles).
CT_R - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [2,1].
CT_T - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [2,2].
CTDOT_N - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [5,3].
CTDOT_R - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [5,1].
CTDOT_RDOT - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [5,4].
CTDOT_T - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [5,2].
CTDOT_TDOT - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [5,5].
CTHR_DRG - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [9,7].
CTHR_DRG - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [9,7].
CTHR_N - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [9,3].
CTHR_NDOT - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [9,6].
CTHR_R - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [9,1].
CTHR_RDOT - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [9,4].
CTHR_SRP - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [9,8].
CTHR_SRP - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [9,8].
CTHR_T - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [9,2].
CTHR_TDOT - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [9,5].
CTHR_THR - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [9,9].
CTHR_THR - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [9,9].
CTHR_X - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [9,1].
CTHR_XDOT - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [9,4].
CTHR_Y - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [9,2].
CTHR_YDOT - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [9,5].
CTHR_Z - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [9,3].
CTHR_ZDOT - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [9,6].
currentInterval(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.events.FieldAdaptableInterval
Get the current value of maximal time interval between events handler checks.
currentInterval(SpacecraftState) - Method in interface org.orekit.propagation.events.AdaptableInterval
Get the current value of maximal time interval between events handler checks.
CX_DOT_X - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey
Covariance matrix [4, 1] element.
CX_DOT_X_DOT - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey
Covariance matrix [4, 4] element.
CX_DOT_Y - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey
Covariance matrix [4, 2] element.
CX_DOT_Z - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey
Covariance matrix [4, 3] element.
CX_X - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [1,1].
CX_X - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey
Covariance matrix [1, 1] element.
CXDOT_X - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [4,1].
CXDOT_XDOT - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [4,4].
CXDOT_Y - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [4,2].
CXDOT_Z - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [4,3].
CY_DOT_X - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey
Covariance matrix [5, 1] element.
CY_DOT_X_DOT - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey
Covariance matrix [5, 4] element.
CY_DOT_Y - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey
Covariance matrix [5, 2] element.
CY_DOT_Y_DOT - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey
Covariance matrix [5, 5] element.
CY_DOT_Z - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey
Covariance matrix [5, 3] element.
CY_X - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [2,1].
CY_X - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey
Covariance matrix [2, 1] element.
CY_Y - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [2,2].
CY_Y - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey
Covariance matrix [2, 2] element.
cycleSlipDataSet(String, AbsoluteDate, double, Frequency) - Method in class org.orekit.estimation.measurements.gnss.AbstractCycleSlipDetector
Set the data: collect data at the current Date, at the current frequency, for a given satellite, add it within the attributes data and stuff.
CycleSlipDetectorResults - Class in org.orekit.estimation.measurements.gnss
This class is used to contains all the data computed within cycle-slip detector.
CycleSlipDetectors - Interface in org.orekit.estimation.measurements.gnss
Interface for phase measurement cycle-slip detection.
CYDOT_X - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [5,1].
CYDOT_XDOT - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [5,4].
CYDOT_Y - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [5,2].
CYDOT_YDOT - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [5,5].
CYDOT_Z - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [5,3].
CYLINDRICAL - org.orekit.files.ccsds.ndm.odm.ocm.ShadowModel
Cylindrical model.
CylindricallyShadowedLightFluxModel - Class in org.orekit.forces.radiation
Class defining a flux model with a single occulting body, casting a shadow whose shape is a circular cylinder (equivalent to the light source being infinitely distant).
CylindricallyShadowedLightFluxModel(double, ExtendedPositionProvider, double) - Constructor for class org.orekit.forces.radiation.CylindricallyShadowedLightFluxModel
Constructor with default event detection settings.
CylindricallyShadowedLightFluxModel(double, ExtendedPositionProvider, double, EventDetectionSettings) - Constructor for class org.orekit.forces.radiation.CylindricallyShadowedLightFluxModel
Constructor.
CylindricallyShadowedLightFluxModel(ExtendedPositionProvider, double) - Constructor for class org.orekit.forces.radiation.CylindricallyShadowedLightFluxModel
Constructor with default value for reference flux.
CylindricalShadowEclipseDetector - Class in org.orekit.propagation.events
Event detector for eclipses from a single, infinitely-distant light source, occulted by a spherical central body.
CylindricalShadowEclipseDetector(PVCoordinatesProvider, double, AdaptableInterval, double, int, EventHandler) - Constructor for class org.orekit.propagation.events.CylindricalShadowEclipseDetector
Deprecated.
since 12.2
CylindricalShadowEclipseDetector(PVCoordinatesProvider, double, EventDetectionSettings, EventHandler) - Constructor for class org.orekit.propagation.events.CylindricalShadowEclipseDetector
Constructor.
CylindricalShadowEclipseDetector(PVCoordinatesProvider, double, EventHandler) - Constructor for class org.orekit.propagation.events.CylindricalShadowEclipseDetector
Constructor with default detection settings.
CZ_DOT_X - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey
Covariance matrix [6, 1] element.
CZ_DOT_X_DOT - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey
Covariance matrix [6, 4] element.
CZ_DOT_Y - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey
Covariance matrix [6, 2] element.
CZ_DOT_Y_DOT - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey
Covariance matrix [6, 5] element.
CZ_DOT_Z - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey
Covariance matrix [6, 3] element.
CZ_DOT_Z_DOT - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey
Covariance matrix [6, 6] element.
CZ_X - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [3,1].
CZ_X - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey
Covariance matrix [3, 1] element.
CZ_Y - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [3,2].
CZ_Y - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey
Covariance matrix [3, 2] element.
CZ_Z - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [3,3].
CZ_Z - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey
Covariance matrix [3, 3] element.
CZDOT_X - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [6,1].
CZDOT_XDOT - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [6,4].
CZDOT_Y - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [6,2].
CZDOT_YDOT - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [6,5].
CZDOT_Z - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [6,3].
CZDOT_ZDOT - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [6,6].

D

D - org.orekit.gnss.SignalCode
GPS L1(C/A) + (P2-P1) / QZSS L5D / Beidou Data codes.
D0 - org.orekit.gnss.ObservationType
Doppler for Rinex3.
D1 - org.orekit.gnss.ObservationType
Doppler GPS L1 / GLONASS G1 / Galileo E2-L1-E1 / SBAS L1 for Rinex2.
D1 - Static variable in class org.orekit.propagation.analytical.gnss.data.BeidouLegacyNavigationMessage
Identifier for message type.
D1A - org.orekit.gnss.ObservationType
Doppler Galileo E1 A / Beidou B1 B1A for Rinex3.
D1B - org.orekit.gnss.ObservationType
Doppler Galileo E1 I/NAV OS/CS/SoL / QZSS geo signal for Rinex3.
D1C - org.orekit.gnss.ObservationType
Doppler GPS L1 C/A / GLONASS G1 C/A / Galileo E1 C / SBAS L1 C/A / QZSS L1 C/A for Rinex3.
D1D - org.orekit.gnss.ObservationType
Doppler Beidou B1 Data for Rinex3.
D1E - org.orekit.gnss.ObservationType
Doppler QZSS L1 C/B for Rinex4.
D1I - org.orekit.gnss.ObservationType
Doppler Beidou B1 I for Rinex3.
D1L - org.orekit.gnss.ObservationType
Doppler GPS L1 L1C(P) / QZSS L1 L1C(P) for Rinex3, Beidou B1A for Rinex3.03.
D1M - org.orekit.gnss.ObservationType
Doppler GPS L2 M for Rinex3.
D1N - org.orekit.gnss.ObservationType
Doppler GPS L1 codeless / Beidou B1 codeless for Rinex3.
D1P - org.orekit.gnss.ObservationType
Doppler GPS L2 P(AS off) / GLONASS G2 P / Beidou B1 Pilot for Rinex3.
D1S - org.orekit.gnss.ObservationType
Doppler GPS L1 L1C(D) / QZSS L1 L1C(D) for Rinex3, Beidou B1A for Rinex3.03.
D1W - org.orekit.gnss.ObservationType
Doppler GPS L1 Z-tracking and similar (AS on) for Rinex3.
D1X - org.orekit.gnss.ObservationType
Doppler GPS L1 L1C (D+P) / Galileo E1 B+C / QZSS L1 L1C(D+P) / Beidou B1 Data+Pilot for Rinex3.
D1Y - org.orekit.gnss.ObservationType
Doppler GPS L1 Y for Rinex3.
D1Z - org.orekit.gnss.ObservationType
Doppler Galileo E1 C1Z A+B+C / QZSS L1 L1-SAIF for Rinex3, Beidou B1A for Rinex3.03.
D2 - org.orekit.gnss.ObservationType
Doppler GPS L2 / GLONASS G2 / Beidou BO2 for Rinex2.
D2 - Static variable in class org.orekit.propagation.analytical.gnss.data.BeidouLegacyNavigationMessage
Identifier for message type.
D2C - org.orekit.gnss.ObservationType
Doppler GPS L2 C/A / GLONASS G2 C/A for Rinex3.
D2D - org.orekit.gnss.ObservationType
Doppler GPS L1(C/A)+(P2-P1) (semi-codeless) for Rinex3.
D2I - org.orekit.gnss.ObservationType
Doppler Beidou B1 I for Rinex3.03.
D2L - org.orekit.gnss.ObservationType
Doppler GPS L2 L2C(L) / QZSS L2 L2C(2) for Rinex3.
D2M - org.orekit.gnss.ObservationType
Doppler GPS L2 M for Rinex3.
D2N - org.orekit.gnss.ObservationType
Doppler GPS L2 codeless for Rinex3.
D2P - org.orekit.gnss.ObservationType
Doppler GPS L2 P(AS off) / GLONASS G2 P for Rinex3.
D2Q - org.orekit.gnss.ObservationType
Doppler Beidou B1 Q for Rinex3.03.
D2S - org.orekit.gnss.ObservationType
Doppler GPS L2 L2C(M) / QZSS L2 L2C(M) for Rinex3.
D2W - org.orekit.gnss.ObservationType
Doppler GPS L2 Z-tracking and similar (AS on) for Rinex3.
D2X - org.orekit.gnss.ObservationType
Doppler GPS L2 L2C (M+L) / QZSS L2 L2C(M+L) for Rinex3, Beidou B1 I+Q for Rinex3.03.
D2Y - org.orekit.gnss.ObservationType
Doppler GPS L2 Y for Rinex3.
D3I - org.orekit.gnss.ObservationType
Doppler GLONASS G3 I for Rinex3.
D3Q - org.orekit.gnss.ObservationType
Doppler GLONASS G3 Q for Rinex3.
D3X - org.orekit.gnss.ObservationType
Doppler GLONASS G3 I+Q for Rinex3.
D4A - org.orekit.gnss.ObservationType
Doppler GLONASS G1a L1OCd for Rinex3.
D4B - org.orekit.gnss.ObservationType
Doppler GLONASS G1a L1OCp for Rinex3.
D4X - org.orekit.gnss.ObservationType
Doppler GLONASS G1a L1OCd+L1OCd for Rinex3.
D5 - org.orekit.gnss.ObservationType
Doppler GPS L5 / Galileo E5a / SBAS L5 for Rinex2.
D5A - org.orekit.gnss.ObservationType
Doppler IRNSS L5 A for Rinex3.
D5B - org.orekit.gnss.ObservationType
Doppler IRNSS L5 B for Rinex3.
D5C - org.orekit.gnss.ObservationType
Doppler IRNSS L5 C for Rinex3.
D5D - org.orekit.gnss.ObservationType
Doppler QZSS L5 D / Beidou B2a Data for Rinex3.
D5I - org.orekit.gnss.ObservationType
Doppler GPS L5 I/ Galileo E5a F/NAV OS / SBAS L5 I / QZSS L5 I for Rinex3.
D5P - org.orekit.gnss.ObservationType
Doppler QZSS L5 P / Beidou B2a Pilot for Rinex3.
D5Q - org.orekit.gnss.ObservationType
Doppler GPS L5 Q/ Galileo E5a Q / SBAS L5 Q / QZSS L5 Q for Rinex3.
D5X - org.orekit.gnss.ObservationType
Doppler GPS L5 I+Q/ Galileo E5a I+Q / SBAS L5 I+Q / QZSS L5 I+Q / IRNSS L5 B+C / Beidou B2a Data+Pilot for Rinex3.
D5Z - org.orekit.gnss.ObservationType
Doppler QZSS L5 D+P for Rinex3.
D6 - org.orekit.gnss.ObservationType
Doppler Galileo E6 / Beidou B03 for Rinex2.
D6A - org.orekit.gnss.ObservationType
Doppler Galileo E6 A PRS / GLONASS L2CSI / Beidou B3A for Rinex3.
D6B - org.orekit.gnss.ObservationType
Doppler Galileo E6 B C/NAV CS / GLONASS L2OCp for Rinex3.
D6C - org.orekit.gnss.ObservationType
Doppler Galileo E6 C no data for Rinex3.
D6D - org.orekit.gnss.ObservationType
Doppler Beidou B3A for Rinex3.
D6E - org.orekit.gnss.ObservationType
Doppler QZSS L6E for Rinex3.
D6I - org.orekit.gnss.ObservationType
Doppler Beidou B3 I for Rinex3.
D6L - org.orekit.gnss.ObservationType
Doppler QZSS LEX(6) L for Rinex3.
D6P - org.orekit.gnss.ObservationType
Doppler Beidou B3A for Rinex3.
D6Q - org.orekit.gnss.ObservationType
Doppler Beidou B3 Q for Rinex3.
D6S - org.orekit.gnss.ObservationType
Doppler QZSS LEX(6) S for Rinex3.
D6X - org.orekit.gnss.ObservationType
Doppler Galileo E6 B+C / QZSS LEX(6) S+L / Beidou B3 I+Q / GLONASS G2a L2CSI+L2OCp for Rinex3.
D6Z - org.orekit.gnss.ObservationType
Doppler Galileo E6 A+B+C / QZSS L6(D+E) / Beidou B3A for Rinex3.
D7 - org.orekit.gnss.ObservationType
Doppler Galileo E5b / Beidou B02 for Rinex2.
D7D - org.orekit.gnss.ObservationType
Doppler Beidou B2b Data for Rinex3.
D7I - org.orekit.gnss.ObservationType
Doppler Galileo E5b I I/NAV OS/CS/SoL / Beidou B2 I for Rinex3.
D7P - org.orekit.gnss.ObservationType
Doppler Beidou B2b Pilot for Rinex3.
D7Q - org.orekit.gnss.ObservationType
Doppler Galileo Q no data / Beidou B2 Q for Rinex3.
D7X - org.orekit.gnss.ObservationType
Doppler Galileo E5b I+Q / Beidou B2 I+Q for Rinex3.
D7Z - org.orekit.gnss.ObservationType
Doppler Beidou B2b Data+Pilot for Rinex3.
D8 - org.orekit.gnss.ObservationType
Doppler Galileo E5a+b for Rinex2.
D8D - org.orekit.gnss.ObservationType
Doppler Beidou B2(B2a+B2b) Data for Rinex3.
D8I - org.orekit.gnss.ObservationType
Doppler Galileo E5(E5a+E5b) I for Rinex3.
D8P - org.orekit.gnss.ObservationType
Doppler Beidou B2(B2a+B2b) Pilot for Rinex3.
D8Q - org.orekit.gnss.ObservationType
Doppler Galileo E5(E5a+E5b) Q for Rinex3.
D8X - org.orekit.gnss.ObservationType
Doppler Galileo E5(E5a+E5b) I+Q / B2(B2a+B2b) Data+Pilot for Rinex3.
D9A - org.orekit.gnss.ObservationType
Doppler IRNSS S A for Rinex3.
D9B - org.orekit.gnss.ObservationType
Doppler IRNSS S B for Rinex3.
D9C - org.orekit.gnss.ObservationType
Doppler IRNSS S C for Rinex3.
D9X - org.orekit.gnss.ObservationType
Doppler IRNSS S B+C for Rinex3.
DA - org.orekit.gnss.ObservationType
Doppler GPS L1 C/A / GLONASS G1 C/A for Rinex2.
DAMPING_DEFAULT - Static variable in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Default value for damping.
data - org.orekit.files.ccsds.section.XmlStructureKey
XML data structure.
Data - Interface in org.orekit.files.ccsds.section
This marker interface represents segment data.
DATA - org.orekit.files.ccsds.section.KvnStructureKey
Data structure.
DATA_QUALITY - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
data quality entry.
DATA_ROOT_DIRECTORY_DOES_NOT_EXIST - org.orekit.errors.OrekitMessages
DATA_ROOT_DIRECTORY_DOES_NOT_EXIST.
DATA_TYPES - org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey
Observation data types used.
DATA_TYPES - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Lit of data types in the data section.
dataContext(DataContext) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagatorBuilder
Sets the data context used by the propagator.
DataContext - Interface in org.orekit.data
Provides auxiliary data for portions of the application.
DataField - Interface in org.orekit.gnss.metric.parser
Interface for data fields used to parsed encoded messages.
DataFilter - Interface in org.orekit.data
Interface for filtering data (typically uncompressing it) in data providers before passing it to data loaders.
DataFormat - Enum in org.orekit.gnss.metric.ntrip
Enumerate for data format in DataStreamRecord.
DataLoader - Interface in org.orekit.data
Interface for loading data files from data providers.
DataProvider - Interface in org.orekit.data
Interface for providing data files to file loaders.
DataProvidersManager - Class in org.orekit.data
This class manages supported data providers.
DataProvidersManager() - Constructor for class org.orekit.data.DataProvidersManager
Build an instance with default configuration.
DataQuality - Enum in org.orekit.files.ccsds.ndm.tdm
Quality of the data.
DataSource - Class in org.orekit.data
Container associating a name with a stream or reader that can be opened lazily.
DataSource(File) - Constructor for class org.orekit.data.DataSource
Build an instance from a file on the local file system.
DataSource(String) - Constructor for class org.orekit.data.DataSource
Build an instance from file name only.
DataSource(String, DataSource.ReaderOpener) - Constructor for class org.orekit.data.DataSource
Complete constructor.
DataSource(String, DataSource.StreamOpener) - Constructor for class org.orekit.data.DataSource
Complete constructor.
DataSource(URI) - Constructor for class org.orekit.data.DataSource
Build an instance from URI only.
DataSource.Opener - Interface in org.orekit.data
Interface for lazy-opening data streams one time.
DataSource.ReaderOpener - Interface in org.orekit.data
Interface for lazy-opening a characters stream one time.
DataSource.StreamOpener - Interface in org.orekit.data
Interface for lazy-opening a binary stream one time.
DataStreamRecord - Class in org.orekit.gnss.metric.ntrip
Data stream record in source table.
DataStreamRecord(String) - Constructor for class org.orekit.gnss.metric.ntrip.DataStreamRecord
Build a data stream record by parsing a source table line.
DATATION_ACCURACY - Static variable in interface org.orekit.propagation.events.EventDetectorsProvider
Accuracy of switching events dates (s).
DataType - Enum in org.orekit.gnss.metric.parser
Enum containing all low level data types that can be parsed to build a message.
DataUsed - Enum in org.orekit.files.sp3
Enumerate for data used.
DATE_AFTER - Static variable in class org.orekit.forces.drag.TimeSpanDragForce
Deprecated.
Prefix for dates after in the parameter drivers' name.
DATE_AFTER - Static variable in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
Prefix for dates after in the parameter drivers' name.
DATE_AFTER - Static variable in class org.orekit.models.earth.troposphere.TimeSpanEstimatedModel
Prefix for dates after in the tropospheric parameter drivers' name.
DATE_AFTER - Static variable in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
Deprecated.
Prefix for dates after in the tropospheric parameter drivers' name.
DATE_BEFORE - Static variable in class org.orekit.forces.drag.TimeSpanDragForce
Deprecated.
Prefix for dates before in the parameter drivers' name.
DATE_BEFORE - Static variable in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
Prefix for dates before in the parameter drivers' name.
DATE_BEFORE - Static variable in class org.orekit.models.earth.troposphere.TimeSpanEstimatedModel
Prefix for dates before in the tropospheric parameter drivers' name.
DATE_BEFORE - Static variable in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
Deprecated.
Prefix for dates before in the tropospheric parameter drivers' name.
dateAtCount(double) - Method in class org.orekit.time.SatelliteClockScale
Compute date corresponding to some clock count.
DateBasedManeuverTriggers - Class in org.orekit.forces.maneuvers.trigger
Maneuver triggers based on a start and end date.
DateBasedManeuverTriggers(String, AbsoluteDate, double) - Constructor for class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers
Simple constructor.
DateBasedManeuverTriggers(AbsoluteDate, double) - Constructor for class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers
Simple constructor.
DateComponents - Class in org.orekit.time
Class representing a date broken up as year, month and day components.
DateComponents(int) - Constructor for class org.orekit.time.DateComponents
Build a date from its offset with respect to a DateComponents.J2000_EPOCH.
DateComponents(int, int) - Constructor for class org.orekit.time.DateComponents
Build a date from a year and day number.
DateComponents(int, int, int) - Constructor for class org.orekit.time.DateComponents
Build a date from its components.
DateComponents(int, Month, int) - Constructor for class org.orekit.time.DateComponents
Build a date from its components.
DateComponents(DateComponents, int) - Constructor for class org.orekit.time.DateComponents
Build a date from its offset with respect to a reference epoch.
DateDetector - Class in org.orekit.propagation.events
Finder for date events.
DateDetector(AdaptableInterval, double, int, EventHandler, double, TimeStamped...) - Constructor for class org.orekit.propagation.events.DateDetector
Deprecated.
as of 12.2
DateDetector(EventDetectionSettings, EventHandler, double, TimeStamped...) - Constructor for class org.orekit.propagation.events.DateDetector
Protected constructor with full parameters.
DateDetector(TimeStamped...) - Constructor for class org.orekit.propagation.events.DateDetector
Build a new instance.
DateDriver - Class in org.orekit.utils
Parameter driver allowing to drive a date.
DateDriver(AbsoluteDate, String, boolean) - Constructor for class org.orekit.utils.DateDriver
Simple constructor.
DATES_MISMATCH - org.orekit.errors.OrekitMessages
DATES_MISMATCH.
DatesSelector - Interface in org.orekit.time
Interface for selecting dates within an interval.
DateTimeComponents - Class in org.orekit.time
Holder for date and time components.
DateTimeComponents(int, int, int) - Constructor for class org.orekit.time.DateTimeComponents
Build an instance from raw level components.
DateTimeComponents(int, int, int, int, int, double) - Constructor for class org.orekit.time.DateTimeComponents
Build an instance from raw level components.
DateTimeComponents(int, Month, int) - Constructor for class org.orekit.time.DateTimeComponents
Build an instance from raw level components.
DateTimeComponents(int, Month, int, int, int, double) - Constructor for class org.orekit.time.DateTimeComponents
Build an instance from raw level components.
DateTimeComponents(DateComponents, TimeComponents) - Constructor for class org.orekit.time.DateTimeComponents
Build a new instance from its components.
DateTimeComponents(DateTimeComponents, double) - Constructor for class org.orekit.time.DateTimeComponents
Build an instance from a seconds offset with respect to another one.
DateTimeComponents(DateTimeComponents, long, TimeUnit) - Constructor for class org.orekit.time.DateTimeComponents
Build an instance from a seconds offset with respect to another one.
dateToCalendarString(TimeConverter, AbsoluteDate) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Convert a date to calendar string value with high precision.
dateToCalendarString(TimeConverter, AbsoluteDate) - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Convert a date to calendar string value with high precision.
dateToString(int, int, int, int, int, double) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Convert a date to string value with high precision.
dateToString(int, int, int, int, int, double) - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Convert a date to string value with high precision.
dateToString(TimeConverter, AbsoluteDate) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Convert a date to string value with high precision.
dateToString(TimeConverter, AbsoluteDate) - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Convert a date to string value with high precision.
DAY - Static variable in class org.orekit.utils.units.Unit
Day unit.
DAYS_SINCE_FIRST_OBS - org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey
Time elapsed between first accepted observation on epoch.
DAYS_SINCE_LAST_OBS - org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey
Time elapsed between last accepted observation on epoch.
DAYS_TO_SECONDS - Static variable in class org.orekit.utils.units.UnitsConverter
Days to seconds converter.
DB - org.orekit.gnss.ObservationType
Doppler GPS L1C for Rinex2.
DC - org.orekit.gnss.ObservationType
Doppler GPS L2C for Rinex2.
DC_BODY_FRAME - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey
Spacecraft body frame in which OrbitManeuverHistoryMetadataKey.DC_BODY_TRIGGER is specified.
DC_BODY_TRIGGER - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey
Direction in body frame for triggering duty cycle.
DC_EXEC_START - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey
Start time of initial duty cycle-based maneuver execution.
DC_EXEC_STOP - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey
End time of final duty cycle-based maneuver execution.
DC_MAX_CYCLES - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey
Maximum number of "ON" duty cycles.
DC_MIN_CYCLES - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey
Minimum number of "ON" duty cycles.
DC_PA_START_ANGLE - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey
Phase angle of pulse start.
DC_PA_STOP_ANGLE - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey
Phase angle of pulse stop.
DC_REF_DIR - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey
Reference direction for triggering duty cycle.
DC_REF_TIME - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey
Duty cycle thrust reference time.
DC_TIME_PULSE_DURATION - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey
Duty cycle pulse "ON" duration.
DC_TIME_PULSE_PERIOD - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey
Duty cycle elapsed time between start of a pulse and start of next pulse.
DC_TYPE - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey
Type of duty cycle.
DC_WIN_CLOSE - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey
Start time of duty cycle-based maneuver window.
DC_WIN_OPEN - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey
Start time of duty cycle-based maneuver window.
Dcb - Class in org.orekit.files.sinex
Class to store DCB Solution data parsed in the SinexLoader.
Dcb() - Constructor for class org.orekit.files.sinex.Dcb
Simple constructor.
DcbDescription - Class in org.orekit.files.sinex
Class to store the DCB description parameters.
DcbDescription() - Constructor for class org.orekit.files.sinex.DcbDescription
Simple constructor.
DcbSatellite - Class in org.orekit.files.sinex
Class based on DCB, used to store the data parsed in SinexLoader for Differential Code Biases computed for satellites.
DcbSatellite(String) - Constructor for class org.orekit.files.sinex.DcbSatellite
Constructor for the DCBSatellite class.
DcbStation - Class in org.orekit.files.sinex
Class based on DCB, used to store the data parsed in SinexLoader for Differential Code Biases computed for stations.
DcbStation(String) - Constructor for class org.orekit.files.sinex.DcbStation
Simple constructor.
DCM - org.orekit.files.ccsds.ndm.adm.acm.AttitudeElementsType
Direction cosine matrix.
DCP_SENSITIVITY_VECTOR_POSITION - org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadataKey
The Drag Consider Parameter (DCP) sensitivity vector (position errors at TCA).
DCP_SENSITIVITY_VECTOR_VELOCITY - org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadataKey
The Drag Consider Parameter (DCP) sensitivity vector (velocity errors at TCA).
DD - org.orekit.gnss.ObservationType
Doppler GLONASS G2 for Rinex2.
DEBRIS - org.orekit.files.ccsds.ndm.odm.ocm.ObjectType
Debris.
DECAYED - org.orekit.files.ccsds.ndm.odm.ocm.OpsStatus
Decayed object.
DECEMBER - org.orekit.time.Month
December.
decode(EncodedMessage) - Method in enum org.orekit.gnss.metric.parser.DataType
Decode a piece of data extracted from an encoded message.
decomposer(MatrixDecomposer) - Method in class org.orekit.estimation.sequential.KalmanEstimatorBuilder
Configure the matrix decomposer.
decomposer(MatrixDecomposer) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimatorBuilder
Configure the matrix decomposer.
decomposer(MatrixDecomposer) - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanEstimatorBuilder
Configure the matrix decomposer.
decomposer(MatrixDecomposer) - Method in class org.orekit.estimation.sequential.UnscentedKalmanEstimatorBuilder
Configure the matrix decomposer.
decorate(ObservedMeasurement<?>, AbsoluteDate) - Static method in class org.orekit.estimation.sequential.KalmanEstimatorUtil
Decorate an observed measurement.
decorateUnscented(ObservedMeasurement<?>, AbsoluteDate) - Static method in class org.orekit.estimation.sequential.KalmanEstimatorUtil
Decorate an observed measurement for an Unscented Kalman Filter.
deepPeriodicEffects(double) - Method in class org.orekit.propagation.analytical.tle.DeepSDP4
Computes periodic terms from current coordinates and epoch.
deepPeriodicEffects(T) - Method in class org.orekit.propagation.analytical.tle.FieldDeepSDP4
Computes periodic terms from current coordinates and epoch.
DeepSDP4 - Class in org.orekit.propagation.analytical.tle
This class contains the methods that compute deep space perturbation terms.
DeepSDP4(TLE, AttitudeProvider, double) - Constructor for class org.orekit.propagation.analytical.tle.DeepSDP4
Constructor for a unique initial TLE.
DeepSDP4(TLE, AttitudeProvider, double, Frame) - Constructor for class org.orekit.propagation.analytical.tle.DeepSDP4
Constructor for a unique initial TLE.
deepSecularEffects(double) - Method in class org.orekit.propagation.analytical.tle.DeepSDP4
Computes secular terms from current coordinates and epoch.
deepSecularEffects(T) - Method in class org.orekit.propagation.analytical.tle.FieldDeepSDP4
Computes secular terms from current coordinates and epoch.
DEFAULT - org.orekit.files.ccsds.ndm.cdm.CovarianceMethod
Non-calculated default value was used.
DEFAULT - org.orekit.frames.encounter.EncounterLOFType
Default encounter local orbital frame based on Figure 1.3 from Romain Serra's thesis.
DEFAULT - Static variable in class org.orekit.propagation.analytical.tle.FieldTLE
Identifier for default type of ephemeris (SGP4/SDP4).
DEFAULT - Static variable in class org.orekit.propagation.analytical.tle.TLE
Identifier for default type of ephemeris (SGP4/SDP4).
DEFAULT_ANTEX_SUPPORTED_NAMES - Static variable in class org.orekit.gnss.antenna.AntexLoader
Default supported files name pattern for antex files.
DEFAULT_BLQ_SUPPORTED_NAMES - Static variable in class org.orekit.models.earth.displacement.OceanLoadingCoefficientsBLQFactory
Default supported files name pattern for Onsala Space Observatory files in BLQ format.
DEFAULT_CACHE - Static variable in class org.orekit.estimation.measurements.gnss.AmbiguityCache
Deprecated.
this default cache is only a temporary hack for compatibility purposes it will be removed in Orekit 13.0
DEFAULT_CACHED_SLOTS_NUMBER - Static variable in class org.orekit.utils.GenericTimeStampedCache
Default number of independent cached time slots.
DEFAULT_CLOCK_RATE_VALUE - Static variable in class org.orekit.files.sp3.SP3Utils
Bad or absent clock rate values are to be set to 999999.999999.
DEFAULT_CLOCK_VALUE - Static variable in class org.orekit.files.sp3.SP3Utils
Bad or absent clock values are to be set to 999999.999999.
DEFAULT_CORRECTION_FACTOR - Static variable in class org.orekit.models.earth.EarthStandardAtmosphereRefraction
Default correction factor value.
DEFAULT_CRD_SUPPORTED_NAMES - Static variable in class org.orekit.files.ilrs.CRDParser
Default supported files name pattern for CRD files.
DEFAULT_DATE_EQUALITY_THRESHOLD - Static variable in class org.orekit.time.FieldTimeStampedPair
Default date equality threshold of 1 ns.
DEFAULT_DATE_EQUALITY_THRESHOLD - Static variable in class org.orekit.time.TimeStampedPair
Default date equality threshold of 1 ns.
DEFAULT_DC_TYPE - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Default duty cycle type.
DEFAULT_DE_SUPPORTED_NAMES - Static variable in class org.orekit.bodies.JPLEphemeridesLoader
Default supported files name pattern for JPL DE files.
DEFAULT_ELEVATION_SWITCH - Static variable in class org.orekit.propagation.events.intervals.ElevationDetectionAdaptableIntervalFactory
Default elevation abovde which interval should be switched to fine interval (-5°).
DEFAULT_EPSILON - Static variable in class org.orekit.propagation.conversion.averaging.converters.FixedPointOsculatingToAveragedConverter
Default convergence threshold.
DEFAULT_EXTRAPOLATION_THRESHOLD_SEC - Static variable in class org.orekit.time.AbstractFieldTimeInterpolator
Default extrapolation time threshold: 1ms.
DEFAULT_EXTRAPOLATION_THRESHOLD_SEC - Static variable in class org.orekit.time.AbstractTimeInterpolator
Default extrapolation time threshold: 1ms.
DEFAULT_FILE_NAME - Static variable in class org.orekit.files.ccsds.ndm.odm.oem.OemWriter
Default file name for error messages.
DEFAULT_ID - Static variable in class org.orekit.files.ilrs.CPF
Default satellite ID, used if header is null when initializing the ephemeris.
DEFAULT_INDENT - Static variable in class org.orekit.files.ccsds.utils.generation.XmlGenerator
Default number of space for each indentation level.
DEFAULT_INPOP_SUPPORTED_NAMES - Static variable in class org.orekit.bodies.JPLEphemeridesLoader
Default supported files name pattern for IMCCE INPOP files.
DEFAULT_INTERPOLATION_DEGREE - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Default interpolation degree.
DEFAULT_INTERPOLATION_DEGREE - Static variable in class org.orekit.frames.EOPHistory
Default interpolation degree.
DEFAULT_INTERPOLATION_METHOD - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Default interpolation method.
DEFAULT_INTERPOLATION_METHOD - Static variable in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitSatelliteAttitudeEphemeris
Default interpolation sample size if it is not specified.
DEFAULT_INTERPOLATION_POINTS - Static variable in class org.orekit.time.AbstractFieldTimeInterpolator
Default number of interpolation points.
DEFAULT_INTERPOLATION_POINTS - Static variable in class org.orekit.time.AbstractTimeInterpolator
Default number of interpolation points.
DEFAULT_INTERPOLATION_SIZE - Static variable in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitSatelliteAttitudeEphemeris
Default interpolation sample size if it is not specified.
DEFAULT_INTERPOLATION_SIZE - Static variable in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
Defines the default interpolation sample size if it is not specified on a segment.
DEFAULT_LOW_ELEVATION_THRESHOLD - Static variable in class org.orekit.models.earth.troposphere.CanonicalSaastamoinenModel
Default lowest acceptable elevation angle [rad].
DEFAULT_LOW_ELEVATION_THRESHOLD - Static variable in class org.orekit.models.earth.troposphere.ModifiedSaastamoinenModel
Default lowest acceptable elevation angle [rad].
DEFAULT_LOW_ELEVATION_THRESHOLD - Static variable in class org.orekit.models.earth.troposphere.SaastamoinenModel
Deprecated.
Default lowest acceptable elevation angle [rad].
DEFAULT_MASS - Static variable in interface org.orekit.propagation.FieldPropagator
Default mass.
DEFAULT_MASS - Static variable in interface org.orekit.propagation.Propagator
Default mass.
DEFAULT_MASS - Static variable in class org.orekit.propagation.SpacecraftState
Default mass.
DEFAULT_MAX_CHECK - Static variable in class org.orekit.propagation.events.DateDetector
Default value for max check.
DEFAULT_MAX_CHECK - Static variable in class org.orekit.propagation.events.FieldDateDetector
Default value for max check.
DEFAULT_MAX_ITER - Static variable in class org.orekit.propagation.events.AbstractDetector
Default maximum number of iterations in the event time search.
DEFAULT_MAX_ITER - Static variable in class org.orekit.propagation.events.EventDetectionSettings
Default maximum number of iterations in the event time search.
DEFAULT_MAX_ITER - Static variable in class org.orekit.propagation.events.FieldAbstractDetector
Default maximum number of iterations in the event time search.
DEFAULT_MAX_ITER - Static variable in class org.orekit.propagation.events.FieldEventDetectionSettings
Default maximum number of iterations in the event time search.
DEFAULT_MAX_ITERATIONS - Static variable in class org.orekit.propagation.analytical.tle.generation.LeastSquaresTleGenerationAlgorithm
Default value for maximum number of iterations.
DEFAULT_MAX_ITERATIONS - Static variable in class org.orekit.propagation.conversion.averaging.converters.FixedPointOsculatingToAveragedConverter
Default maximum number of iterations.
DEFAULT_MAX_RECONNECT - Static variable in class org.orekit.gnss.metric.ntrip.NtripClient
Default maximum number of reconnect a attempts without readin any data.
DEFAULT_MAXCHECK - Static variable in class org.orekit.propagation.events.AbstractDetector
Default maximum checking interval (s).
DEFAULT_MAXCHECK - Static variable in class org.orekit.propagation.events.EventDetectionSettings
Default maximum checking interval (s).
DEFAULT_MAXCHECK - Static variable in class org.orekit.propagation.events.FieldAbstractDetector
Default maximum checking interval (s).
DEFAULT_MAXCHECK - Static variable in class org.orekit.propagation.events.FieldEventDetectionSettings
Default maximum checking interval (s).
DEFAULT_MIN_GAP - Static variable in class org.orekit.propagation.events.DateDetector
Default value for minimum gap between added dates.
DEFAULT_MIN_GAP - Static variable in class org.orekit.propagation.events.FieldDateDetector
Default value for minimum gap between added dates.
DEFAULT_NAME - Static variable in class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers
Default name for trigger.
DEFAULT_ORIGINATOR - Static variable in class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter
Default value for HeaderKey.ORIGINATOR.
DEFAULT_ORIGINATOR - Static variable in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter
Default value for HeaderKey.ORIGINATOR.
DEFAULT_POINTS - Static variable in class org.orekit.forces.gravity.OceanTides
Default number of points tides field sampling.
DEFAULT_POINTS - Static variable in class org.orekit.forces.gravity.SolidTides
Default number of points tides field sampling.
DEFAULT_PORT - Static variable in class org.orekit.gnss.metric.ntrip.NtripClient
Default port for ntrip communication.
DEFAULT_POSITION_ANGLE - Static variable in class org.orekit.propagation.AbstractStateCovarianceInterpolator
Default position angle for covariance expressed in Cartesian elements.
DEFAULT_PRESSURE - Static variable in class org.orekit.models.earth.EarthStandardAtmosphereRefraction
Default local pressure at viewpoint (Pa).
DEFAULT_RECONNECT_DELAY - Static variable in class org.orekit.gnss.metric.ntrip.NtripClient
Default delay before we reconnect after connection close (s).
DEFAULT_RECONNECT_DELAY_FACTOR - Static variable in class org.orekit.gnss.metric.ntrip.NtripClient
Default factor by which reconnection delay is multiplied after each attempt.
DEFAULT_RINEX_2_NAMES - Static variable in class org.orekit.files.rinex.observation.RinexObservationParser
Default name pattern for rinex 2 observation files.
DEFAULT_RINEX_3_NAMES - Static variable in class org.orekit.files.rinex.observation.RinexObservationParser
Default name pattern for rinex 3 observation files.
DEFAULT_SCALING_THRESHOLD - Static variable in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Laas2015
Default scaling threshold to use when sum becomes large.
DEFAULT_SCLK_OFFSET_AT_EPOCH - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Default value for SCLK_OFFSET_AT_EPOCH.
DEFAULT_SCLK_SEC_PER_SI_SEC - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Default value for SCLK_SEC_PER_SI_SEC.
DEFAULT_STEP - Static variable in class org.orekit.forces.gravity.OceanTides
Default step for tides field sampling (seconds).
DEFAULT_STEP - Static variable in class org.orekit.forces.gravity.SolidTides
Default step for tides field sampling (seconds).
DEFAULT_SUPPORTED_NAMES - Static variable in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
Default regular expression for supported names that works with all officially published files.
DEFAULT_SUPPORTED_NAMES - Static variable in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
Default regular expression for the supported name that work with all officially published files.
DEFAULT_SUPPORTED_NAMES - Static variable in class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader
Default supported files name pattern.
DEFAULT_SUPPORTED_NAMES - Static variable in class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader
Default supported files name pattern.
DEFAULT_SUPPORTED_NAMES - Static variable in class org.orekit.models.earth.weather.GlobalPressureTemperature2Model
Deprecated.
Default supported files name pattern.
DEFAULT_SUPPORTED_NAMES - Static variable in class org.orekit.time.AGILeapSecondFilesLoader
Default supported files name pattern.
DEFAULT_SUPPORTED_NAMES - Static variable in class org.orekit.time.TAIUTCDatFilesLoader
Default supported files name pattern.
DEFAULT_SUPPORTED_NAMES_DTC - Static variable in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData
Default regular expression for supported names that works with test and published files for the DTCFILE file.
DEFAULT_SUPPORTED_NAMES_SOLFSMY - Static variable in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData
Default regular expression for supported names that works with test and published files for the SOLFSMY file.
DEFAULT_TCA_DIFFERENCE_TOLERANCE - Static variable in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter2DPOCMethod
Default time of closest approach difference tolerance.
DEFAULT_TEMPERATURE - Static variable in class org.orekit.models.earth.EarthStandardAtmosphereRefraction
Default local temperature at viewpoint (K).
DEFAULT_THRESHOLD - Static variable in class org.orekit.propagation.events.AbstractDetector
Default convergence threshold (s).
DEFAULT_THRESHOLD - Static variable in class org.orekit.propagation.events.DateDetector
Default value for convergence threshold.
DEFAULT_THRESHOLD - Static variable in class org.orekit.propagation.events.EventDetectionSettings
Default convergence threshold (s).
DEFAULT_THRESHOLD - Static variable in class org.orekit.propagation.events.FieldAbstractDetector
Default convergence threshold (s).
DEFAULT_THRESHOLD - Static variable in class org.orekit.propagation.events.FieldDateDetector
Default value for convergence threshold.
DEFAULT_THRESHOLD - Static variable in class org.orekit.propagation.events.FieldEventDetectionSettings
Default convergence threshold (s).
DEFAULT_TIMEOUT - Static variable in class org.orekit.gnss.metric.ntrip.NtripClient
Default timeout for connections and reads (ms).
DEFAULT_TOLERANCE_MASS_ADJOINT - Static variable in class org.orekit.control.indirect.shooting.AbstractIndirectShooting
Default value for convergence tolerance on mass adjoint variable.
DEFAULT_V00_PATTERN - Static variable in class org.orekit.files.sp3.NsgfV00Filter
Default regular expression for NSGF V00 files.
DEFAULT_YAW_BIAS - Static variable in class org.orekit.gnss.attitude.GPSBlockIIA
Default yaw bias (rad).
DEFAULT_YAW_BIAS - Static variable in class org.orekit.gnss.attitude.GPSBlockIIF
Default yaw bias (rad).
DEFAULT_YAW_RATE - Static variable in class org.orekit.gnss.attitude.Galileo
Default yaw rates for all spacecrafts in radians per seconds.
DEFAULT_YAW_RATE - Static variable in class org.orekit.gnss.attitude.Glonass
Default yaw rates for all spacecrafts in radians per seconds.
DEFAULT_YAW_RATE - Static variable in class org.orekit.gnss.attitude.GPSBlockIIF
Default yaw rates for all spacecrafts in radians per seconds.
DEFAULT_YAW_RATE - Static variable in class org.orekit.gnss.attitude.GPSBlockIIR
Default yaw rates for all spacecrafts in radians per seconds.
DEFAULT_ZERO_THRESHOLD - Static variable in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod
Threshold below which values are considered equal to zero.
DefaultDataContext - Annotation Type in org.orekit.annotation
Indicates that the annotated method, field, or constructor uses the default data context.
DefaultDataContextPlugin - Class in org.orekit.compiler.plugin
Processes DefaultDataContext to issue warnings at compile time.
DefaultDataContextPlugin() - Constructor for class org.orekit.compiler.plugin.DefaultDataContextPlugin
Empty constructor.
DefaultEncounterLOF - Class in org.orekit.frames.encounter
Default encounter local orbital frame.
DefaultEncounterLOF(FieldPVCoordinates<T>) - Constructor for class org.orekit.frames.encounter.DefaultEncounterLOF
Field constructor.
DefaultEncounterLOF(PVCoordinates) - Constructor for class org.orekit.frames.encounter.DefaultEncounterLOF
Constructor.
DEG_PER_S - Static variable in class org.orekit.files.ccsds.definitions.Units
Degree per second unit.
DEG_PER_S_1_2 - Static variable in class org.orekit.files.ccsds.definitions.Units
Degree per second^1/2 unit.
DEG_PER_S_3_2 - Static variable in class org.orekit.files.ccsds.definitions.Units
Degree per second^3/2 unit.
DEGRADED - org.orekit.files.ccsds.ndm.tdm.DataQuality
Data exhibits quality issues.
DEGREE - Static variable in class org.orekit.utils.units.Unit
Degree unit.
DEGREES - org.orekit.data.PolynomialParser.Unit
Degrees angles.
DELAUNAY - org.orekit.files.ccsds.ndm.odm.ocm.OrbitElementsType
Delaunay elements (L, G, H, l, g, h).
DelaunayArguments - Class in org.orekit.data
Delaunay arguments used for nutation or tides.
DelaunayArguments(AbsoluteDate, double, double, double, double, double, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.data.DelaunayArguments
Simple constructor.
DELAUNAYMOD - org.orekit.files.ccsds.ndm.odm.ocm.OrbitElementsType
Modified Delaunay elements (Lm, Gm, Hm, lm, gm, hm).
DELTA_MASS - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
Mass change.
DELTA_R_FILE_NAME - Static variable in class org.orekit.models.earth.troposphere.ModifiedSaastamoinenModel
Default file name for δR correction term table.
DELTA_R_FILE_NAME - Static variable in class org.orekit.models.earth.troposphere.SaastamoinenModel
Deprecated.
Default file name for δR correction term table.
DENSITY_FORECAST_UNCERTAINTY - org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadataKey
The atmospheric density forecast error.
dependsOnAttitudeRate() - Method in class org.orekit.forces.drag.DragForce
Check if force model depends on attitude's rotation rate or acceleration at a given, fixed date.
dependsOnAttitudeRate() - Method in interface org.orekit.forces.drag.DragSensitive
Check if model depends on attitude's rotation rate or acceleration at a given, fixed date.
dependsOnAttitudeRate() - Method in interface org.orekit.forces.ForceModel
Check if force model depends on attitude's rotation rate or acceleration at a given, fixed date.
dependsOnPositionOnly() - Method in class org.orekit.forces.drag.AbstractDragForceModel
Check if force model depends on position only at a given, fixed date.
dependsOnPositionOnly() - Method in class org.orekit.forces.empirical.ParametricAcceleration
Check if force model depends on position only at a given, fixed date.
dependsOnPositionOnly() - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
Check if force model depends on position only at a given, fixed date.
dependsOnPositionOnly() - Method in interface org.orekit.forces.ForceModel
Check if force model depends on position only at a given, fixed date.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.AbstractBodyAttraction
Check if force model depends on position only at a given, fixed date.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.DeSitterRelativity
Check if force model depends on position only at a given, fixed date.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Check if force model depends on position only at a given, fixed date.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.J2OnlyPerturbation
Check if force model depends on position only at a given, fixed date.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.LenseThirringRelativity
Check if force model depends on position only at a given, fixed date.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.NewtonianAttraction
Check if force model depends on position only at a given, fixed date.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.OceanTides
Check if force model depends on position only at a given, fixed date.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.Relativity
Check if force model depends on position only at a given, fixed date.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.SolidTides
Check if force model depends on position only at a given, fixed date.
dependsOnPositionOnly() - Method in class org.orekit.forces.inertia.InertialForces
Check if force model depends on position only at a given, fixed date.
dependsOnPositionOnly() - Method in class org.orekit.forces.maneuvers.Maneuver
Check if force model depends on position only at a given, fixed date.
dependsOnPositionOnly() - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel
Check if force model depends on position only at a given, fixed date.
dependsOnPositionOnly() - Method in interface org.orekit.forces.radiation.RadiationForceModel
Check if force model depends on position only at a given, fixed date.
dependsOnPositionOnly() - Method in class org.orekit.forces.radiation.RadiationPressureModel
Check if force model depends on position only at a given, fixed date.
dependsOnPositionOnly() - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Check if force model depends on position only at a given, fixed date.
dependsOnPositionOnly() - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel
Check if force model depends on position only at a given, fixed date.
DEPLOY_DIR_SIGMA - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
One σ angular off-nominal deployment vector direction.
DEPLOY_DV_CDA - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
Typical (50th percentile) product of drag coefficient times cross-sectional area of deployed "child" object.
DEPLOY_DV_RATIO - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
Ratio of child-to-host ΔV vectors.
DEPLOY_DV_SIGMA - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
One σ percent error on deployment ΔV magnitude.
DEPLOY_DV_X - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
Velocity increment of deployed "child" object along X axis.
DEPLOY_DV_Y - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
Velocity increment of deployed "child" object along Y axis.
DEPLOY_DV_Z - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
Velocity increment of deployed "child" object along Z axis.
DEPLOY_ID - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
Identifier of resulting "child" object deployed from this host.
DEPLOY_MASS - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
Decrement in host mass as a result of deployment (shall be ≤ 0).
derivative(double) - Method in class org.orekit.data.PolynomialNutation
Evaluate the time derivative of the polynomial.
derivative(BodiesElements) - Method in interface org.orekit.data.PoissonSeries.CompiledSeries
Evaluate time derivative of a set of Poisson series.
derivative(FieldBodiesElements<S>) - Method in interface org.orekit.data.PoissonSeries.CompiledSeries
Evaluate time derivative of a set of Poisson series.
derivative(T) - Method in class org.orekit.data.PolynomialNutation
Evaluate the time derivative of the polynomial.
deselectDynamicParameters() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Deselects orbital and propagation drivers.
DeSitterRelativity - Class in org.orekit.forces.gravity
De Sitter post-Newtonian correction force due to general relativity.
DeSitterRelativity() - Constructor for class org.orekit.forces.gravity.DeSitterRelativity
Constructor.
DeSitterRelativity(CelestialBody, CelestialBody) - Constructor for class org.orekit.forces.gravity.DeSitterRelativity
Simple constructor.
detect(List<ObservationDataSet>) - Method in class org.orekit.estimation.measurements.gnss.AbstractCycleSlipDetector
Detects if a cycle-slip occurs for a given list of observation data set.
detect(List<ObservationDataSet>) - Method in interface org.orekit.estimation.measurements.gnss.CycleSlipDetectors
Detects if a cycle-slip occurs for a given list of observation data set.
DetectorConfiguration() - Constructor for class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Empty constructor.
DETERMINED_OD - org.orekit.files.ccsds.ndm.odm.ocm.ManBasis
Past maneuver reconstructed from orbit determination.
DETERMINED_TLM - org.orekit.files.ccsds.ndm.odm.ocm.ManBasis
Past maneuver reconstructed from telemetry.
DF002 - org.orekit.gnss.metric.parser.RtcmDataField
RTCM Message number.
DF009 - org.orekit.gnss.metric.parser.RtcmDataField
GPS Satellite ID.
DF038 - org.orekit.gnss.metric.parser.RtcmDataField
GLONASS Satellite ID.
DF040 - org.orekit.gnss.metric.parser.RtcmDataField
GLONASS Satellite Frequency Channel Number.
DF068 - org.orekit.gnss.metric.parser.RtcmDataField
GNSS satellite ID.
DF071 - org.orekit.gnss.metric.parser.RtcmDataField
GPS IODE (Issue Of Data, Ephemeris).
DF076 - org.orekit.gnss.metric.parser.RtcmDataField
GPS Week number.
DF077 - org.orekit.gnss.metric.parser.RtcmDataField
GPS SV Accuracy.
DF078 - org.orekit.gnss.metric.parser.RtcmDataField
GPS CODE ON L2.
DF079 - org.orekit.gnss.metric.parser.RtcmDataField
GPS Rate of Inclination Angle.
DF081 - org.orekit.gnss.metric.parser.RtcmDataField
GPS toc.
DF082 - org.orekit.gnss.metric.parser.RtcmDataField
GPS af2.
DF083 - org.orekit.gnss.metric.parser.RtcmDataField
GPS af1.
DF084 - org.orekit.gnss.metric.parser.RtcmDataField
GPS af0.
DF085 - org.orekit.gnss.metric.parser.RtcmDataField
GPS IODC (Issue Of Data, Clock).
DF086 - org.orekit.gnss.metric.parser.RtcmDataField
GPS Crs.
DF087 - org.orekit.gnss.metric.parser.RtcmDataField
GPS Δn (DELTA n).
DF088 - org.orekit.gnss.metric.parser.RtcmDataField
GPS M0.
DF089 - org.orekit.gnss.metric.parser.RtcmDataField
GPS Cuc.
DF090 - org.orekit.gnss.metric.parser.RtcmDataField
GPS Eccentricity (e).
DF091 - org.orekit.gnss.metric.parser.RtcmDataField
GPS Cus.
DF092 - org.orekit.gnss.metric.parser.RtcmDataField
GPS A1/2.
DF093 - org.orekit.gnss.metric.parser.RtcmDataField
GPS toe.
DF094 - org.orekit.gnss.metric.parser.RtcmDataField
GPS Cic.
DF095 - org.orekit.gnss.metric.parser.RtcmDataField
GPS Ω0 (OMEGA)0.
DF096 - org.orekit.gnss.metric.parser.RtcmDataField
GPS Cis.
DF097 - org.orekit.gnss.metric.parser.RtcmDataField
GPS i0.
DF098 - org.orekit.gnss.metric.parser.RtcmDataField
GPS Crc.
DF099 - org.orekit.gnss.metric.parser.RtcmDataField
GPS ω (Argument of Perigee).
DF100 - org.orekit.gnss.metric.parser.RtcmDataField
GPS OMEGADOT (Rate of Right Ascension).
DF101 - org.orekit.gnss.metric.parser.RtcmDataField
GPS tGD.
DF102 - org.orekit.gnss.metric.parser.RtcmDataField
GPS SV HEALTH.
DF103 - org.orekit.gnss.metric.parser.RtcmDataField
GPS L2 P data flag.
DF104 - org.orekit.gnss.metric.parser.RtcmDataField
GLONASS almanac health (Cn word).
DF105 - org.orekit.gnss.metric.parser.RtcmDataField
GLONASS almanac health availability indicator.
DF106 - org.orekit.gnss.metric.parser.RtcmDataField
GLONASS P1.
DF107 - org.orekit.gnss.metric.parser.RtcmDataField
GLONASS tk (s).
DF108 - org.orekit.gnss.metric.parser.RtcmDataField
GLONASS MSB of Bn word.
DF109 - org.orekit.gnss.metric.parser.RtcmDataField
GLONASS P2 Flag.
DF110 - org.orekit.gnss.metric.parser.RtcmDataField
GLONASS tb.
DF111 - org.orekit.gnss.metric.parser.RtcmDataField
GLONASS xn (tb), first derivative.
DF112 - org.orekit.gnss.metric.parser.RtcmDataField
GLONASS xn (tb).
DF113 - org.orekit.gnss.metric.parser.RtcmDataField
GLONASS xn (tb), second derivative.
DF114 - org.orekit.gnss.metric.parser.RtcmDataField
GLONASS yn (tb), first derivative.
DF115 - org.orekit.gnss.metric.parser.RtcmDataField
GLONASS yn (tb).
DF116 - org.orekit.gnss.metric.parser.RtcmDataField
GLONASS yn (tb), second derivative.
DF117 - org.orekit.gnss.metric.parser.RtcmDataField
GLONASS zn (tb), first derivative.
DF118 - org.orekit.gnss.metric.parser.RtcmDataField
GLONASS zn (tb).
DF119 - org.orekit.gnss.metric.parser.RtcmDataField
GLONASS zn (tb), second derivative.
DF120 - org.orekit.gnss.metric.parser.RtcmDataField
GLONASS P3 Flag.
DF121 - org.orekit.gnss.metric.parser.RtcmDataField
GLONASS γn (tb).
DF122 - org.orekit.gnss.metric.parser.RtcmDataField
GLONASS-M P.
DF123 - org.orekit.gnss.metric.parser.RtcmDataField
GLONASS-M ln (third string).
DF124 - org.orekit.gnss.metric.parser.RtcmDataField
GLONASS τn (tb).
DF125 - org.orekit.gnss.metric.parser.RtcmDataField
GLONASS Δτn.
DF126 - org.orekit.gnss.metric.parser.RtcmDataField
GLONASS En.
DF127 - org.orekit.gnss.metric.parser.RtcmDataField
GLONASS-M P4.
DF128 - org.orekit.gnss.metric.parser.RtcmDataField
GLONASS-M FT.
DF129 - org.orekit.gnss.metric.parser.RtcmDataField
GLONASS-M NT.
DF130 - org.orekit.gnss.metric.parser.RtcmDataField
GLONASS-M M.
DF131 - org.orekit.gnss.metric.parser.RtcmDataField
GLONASS The Availability of Additional Data.
DF132 - org.orekit.gnss.metric.parser.RtcmDataField
GLONASS NA.
DF133 - org.orekit.gnss.metric.parser.RtcmDataField
GLONASS τc.
DF134 - org.orekit.gnss.metric.parser.RtcmDataField
GLONASS-M N4.
DF135 - org.orekit.gnss.metric.parser.RtcmDataField
GLONASS τGPS.
DF136 - org.orekit.gnss.metric.parser.RtcmDataField
GLONASS-M ln (fifth string).
DF137 - org.orekit.gnss.metric.parser.RtcmDataField
GPS Fit Interval.
DF252 - org.orekit.gnss.metric.parser.RtcmDataField
Galileo Satellite ID.
DF289 - org.orekit.gnss.metric.parser.RtcmDataField
Galileo Week Number (WN).
DF290 - org.orekit.gnss.metric.parser.RtcmDataField
Galileo IODnav.
DF291 - org.orekit.gnss.metric.parser.RtcmDataField
Galileo SV SISA.
DF292 - org.orekit.gnss.metric.parser.RtcmDataField
Galileo IDOT.
DF293 - org.orekit.gnss.metric.parser.RtcmDataField
Galileo toc.
DF294 - org.orekit.gnss.metric.parser.RtcmDataField
Galileo af2.
DF295 - org.orekit.gnss.metric.parser.RtcmDataField
Galileo af1.
DF296 - org.orekit.gnss.metric.parser.RtcmDataField
Galileo af0.
DF297 - org.orekit.gnss.metric.parser.RtcmDataField
Galileo Crs.
DF298 - org.orekit.gnss.metric.parser.RtcmDataField
Galileo Δn.
DF299 - org.orekit.gnss.metric.parser.RtcmDataField
Galileo M0.
DF300 - org.orekit.gnss.metric.parser.RtcmDataField
Galileo Cuc.
DF301 - org.orekit.gnss.metric.parser.RtcmDataField
Galileo e.
DF302 - org.orekit.gnss.metric.parser.RtcmDataField
Galileo Cus.
DF303 - org.orekit.gnss.metric.parser.RtcmDataField
Galileo A1/2.
DF304 - org.orekit.gnss.metric.parser.RtcmDataField
Galileo toe.
DF305 - org.orekit.gnss.metric.parser.RtcmDataField
Galileo Cic.
DF306 - org.orekit.gnss.metric.parser.RtcmDataField
Galileo Ω0.
DF307 - org.orekit.gnss.metric.parser.RtcmDataField
Galileo Cis.
DF308 - org.orekit.gnss.metric.parser.RtcmDataField
Galileo i0.
DF309 - org.orekit.gnss.metric.parser.RtcmDataField
Galileo Crc.
DF310 - org.orekit.gnss.metric.parser.RtcmDataField
Galileo ω.
DF311 - org.orekit.gnss.metric.parser.RtcmDataField
Galileo OMEGADOT (Rate of Right Ascension).
DF312 - org.orekit.gnss.metric.parser.RtcmDataField
Galileo BGD (E1/E5a).
DF313 - org.orekit.gnss.metric.parser.RtcmDataField
Galileo BGD (E5b/E1).
DF314 - org.orekit.gnss.metric.parser.RtcmDataField
E5a SIGNAL Health Status.
DF315 - org.orekit.gnss.metric.parser.RtcmDataField
E5a Data Validity Status.
DF316 - org.orekit.gnss.metric.parser.RtcmDataField
Galileo SOL NAV Signal Health Status (SOLHS).
DF317 - org.orekit.gnss.metric.parser.RtcmDataField
Galileo SOL NAV Data Validity Status (SOLDVS).
DF365 - org.orekit.gnss.metric.parser.RtcmDataField
Delta Orbit Radial (m).
DF366 - org.orekit.gnss.metric.parser.RtcmDataField
Delta Along-Track (m).
DF367 - org.orekit.gnss.metric.parser.RtcmDataField
Delta Cross-Track (m).
DF368 - org.orekit.gnss.metric.parser.RtcmDataField
Dot Delta Radial (m/s).
DF369 - org.orekit.gnss.metric.parser.RtcmDataField
Dot Delta Along-Track (m/s).
DF370 - org.orekit.gnss.metric.parser.RtcmDataField
Dot Delta Cross-Track (m/s).
DF375 - org.orekit.gnss.metric.parser.RtcmDataField
Satellite Reference Datum.
DF376 - org.orekit.gnss.metric.parser.RtcmDataField
Delta Clock C0.
DF377 - org.orekit.gnss.metric.parser.RtcmDataField
Delta Clock C1.
DF378 - org.orekit.gnss.metric.parser.RtcmDataField
Delta Clock C2.
DF384 - org.orekit.gnss.metric.parser.RtcmDataField
GLONASS Satellite ID.
DF385 - org.orekit.gnss.metric.parser.RtcmDataField
GPS Epoch Time 1s.
DF386 - org.orekit.gnss.metric.parser.RtcmDataField
GLONASS Epoch Time 1s.
DF387 - org.orekit.gnss.metric.parser.RtcmDataField
No.
DF388 - org.orekit.gnss.metric.parser.RtcmDataField
Multiple Message Indicator.
DF391 - org.orekit.gnss.metric.parser.RtcmDataField
SSR Update Interval.
DF392 - org.orekit.gnss.metric.parser.RtcmDataField
GLONASS Issue Of Date (IOD).
DF413 - org.orekit.gnss.metric.parser.RtcmDataField
IOD SSR.
DF414 - org.orekit.gnss.metric.parser.RtcmDataField
SSR Provider ID.
DF415 - org.orekit.gnss.metric.parser.RtcmDataField
SSR Solution ID.
DF429 - org.orekit.gnss.metric.parser.RtcmDataField
QZSS Satellite ID.
DF430 - org.orekit.gnss.metric.parser.RtcmDataField
QZSS toc.
DF431 - org.orekit.gnss.metric.parser.RtcmDataField
QZSS af2.
DF432 - org.orekit.gnss.metric.parser.RtcmDataField
QZSS af1.
DF433 - org.orekit.gnss.metric.parser.RtcmDataField
QZSS af0.
DF434 - org.orekit.gnss.metric.parser.RtcmDataField
QZSS IODE.
DF435 - org.orekit.gnss.metric.parser.RtcmDataField
QZSS Crs.
DF436 - org.orekit.gnss.metric.parser.RtcmDataField
QZSS Δn.
DF437 - org.orekit.gnss.metric.parser.RtcmDataField
QZSS M0.
DF438 - org.orekit.gnss.metric.parser.RtcmDataField
QZSS Cuc.
DF439 - org.orekit.gnss.metric.parser.RtcmDataField
QZSS e.
DF440 - org.orekit.gnss.metric.parser.RtcmDataField
QZSS Cus.
DF441 - org.orekit.gnss.metric.parser.RtcmDataField
QZSS A1/2.
DF442 - org.orekit.gnss.metric.parser.RtcmDataField
QZSS toe.
DF443 - org.orekit.gnss.metric.parser.RtcmDataField
QZSS Cic.
DF444 - org.orekit.gnss.metric.parser.RtcmDataField
QZSS Ω0.
DF445 - org.orekit.gnss.metric.parser.RtcmDataField
QZSS Cis.
DF446 - org.orekit.gnss.metric.parser.RtcmDataField
QZSS i0.
DF447 - org.orekit.gnss.metric.parser.RtcmDataField
QZSS Crc.
DF448 - org.orekit.gnss.metric.parser.RtcmDataField
QZSS ω.
DF449 - org.orekit.gnss.metric.parser.RtcmDataField
QZSS OMEGADOT (Rate of Right Ascension).
DF450 - org.orekit.gnss.metric.parser.RtcmDataField
QZSS iDOT.
DF451 - org.orekit.gnss.metric.parser.RtcmDataField
QZSS Codes on L2 Channel.
DF452 - org.orekit.gnss.metric.parser.RtcmDataField
QZSS Week Number.
DF453 - org.orekit.gnss.metric.parser.RtcmDataField
QZSS URA Number.
DF454 - org.orekit.gnss.metric.parser.RtcmDataField
QZSS SV health.
DF455 - org.orekit.gnss.metric.parser.RtcmDataField
QZSS tGD.
DF456 - org.orekit.gnss.metric.parser.RtcmDataField
QZSS IODC.
DF457 - org.orekit.gnss.metric.parser.RtcmDataField
QZSS Fit Interval.
DF458 - org.orekit.gnss.metric.parser.RtcmDataField
Galileo Epoch Time 1s.
DF488 - org.orekit.gnss.metric.parser.RtcmDataField
BDS Satellite ID.
DF489 - org.orekit.gnss.metric.parser.RtcmDataField
BDS Week Number.
DF490 - org.orekit.gnss.metric.parser.RtcmDataField
BDS SV URA Index.
DF491 - org.orekit.gnss.metric.parser.RtcmDataField
BDS IDOT.
DF492 - org.orekit.gnss.metric.parser.RtcmDataField
BDS AODE.
DF493 - org.orekit.gnss.metric.parser.RtcmDataField
BDS toc.
DF494 - org.orekit.gnss.metric.parser.RtcmDataField
BDS af2.
DF495 - org.orekit.gnss.metric.parser.RtcmDataField
BDS af1.
DF496 - org.orekit.gnss.metric.parser.RtcmDataField
BDS af0.
DF497 - org.orekit.gnss.metric.parser.RtcmDataField
BDS AODC.
DF498 - org.orekit.gnss.metric.parser.RtcmDataField
BDS Crs.
DF499 - org.orekit.gnss.metric.parser.RtcmDataField
BDS Δn.
DF500 - org.orekit.gnss.metric.parser.RtcmDataField
BDS M0.
DF501 - org.orekit.gnss.metric.parser.RtcmDataField
BDS Cuc.
DF502 - org.orekit.gnss.metric.parser.RtcmDataField
BDS e.
DF503 - org.orekit.gnss.metric.parser.RtcmDataField
BDS Cus.
DF504 - org.orekit.gnss.metric.parser.RtcmDataField
BDS a1/2.
DF505 - org.orekit.gnss.metric.parser.RtcmDataField
BDS toe.
DF506 - org.orekit.gnss.metric.parser.RtcmDataField
BDS Cic.
DF507 - org.orekit.gnss.metric.parser.RtcmDataField
BDS Ω0.
DF508 - org.orekit.gnss.metric.parser.RtcmDataField
BDS Cis.
DF509 - org.orekit.gnss.metric.parser.RtcmDataField
BDS i0.
DF510 - org.orekit.gnss.metric.parser.RtcmDataField
BDS Crc.
DF511 - org.orekit.gnss.metric.parser.RtcmDataField
BDS ω.
DF512 - org.orekit.gnss.metric.parser.RtcmDataField
BDS OMEGADOT (Rate of Right Ascension).
DF513 - org.orekit.gnss.metric.parser.RtcmDataField
BDS tGD1.
DF514 - org.orekit.gnss.metric.parser.RtcmDataField
BDS tGD2.
DF515 - org.orekit.gnss.metric.parser.RtcmDataField
BDS SV Health.
DIFFERENT_STATE_DEFINITION - org.orekit.errors.OrekitMessages
DIFFERENT_STATE_DEFINITION.
DIFFERENT_TIME_OF_CLOSEST_APPROACH - org.orekit.errors.OrekitMessages
DIFFERENT_TIME_OF_CLOSEST_APPROACH.
differentiate(ParameterFunction, int, double) - Static method in class org.orekit.utils.Differentiation
Differentiate a scalar function using finite differences.
differentiate(StateFunction, int, AttitudeProvider, OrbitType, PositionAngleType, double, int) - Static method in class org.orekit.utils.Differentiation
Differentiate a vector function using finite differences.
Differentiation - Class in org.orekit.utils
Utility class for differentiating various kinds of functions.
DIGEST - org.orekit.gnss.metric.ntrip.Authentication
Digest.
DIMENSION_INCONSISTENT_WITH_PARAMETERS - org.orekit.errors.OrekitMessages
DIMENSION_INCONSISTENT_WITH_PARAMETERS.
Dipole - Class in org.orekit.estimation.measurements.gnss
Dipole configuration for satellite-to-ground and inter-satellites wind-up effects.
Dipole(Vector3D, Vector3D) - Constructor for class org.orekit.estimation.measurements.gnss.Dipole
Simple constructor.
directionAt(double) - Method in class org.orekit.geometry.fov.CircularFieldOfView
Get boundary direction at angle.
directionAt(double) - Method in class org.orekit.geometry.fov.EllipticalFieldOfView
Get boundary direction at angle.
directionAt(double) - Method in class org.orekit.geometry.fov.SmoothFieldOfView
Get boundary direction at angle.
DirectoryCrawler - Class in org.orekit.data
Provider for data files stored in a directories tree on filesystem.
DirectoryCrawler(File) - Constructor for class org.orekit.data.DirectoryCrawler
Build a data files crawler.
discreteSearch() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Find the best solutions to the Integer Least Square problem.
discreteSearch() - Method in class org.orekit.estimation.measurements.gnss.IntegerBootstrapping
Compute the solution by the bootstrap method from equation (13) in P.J.G.
discreteSearch() - Method in class org.orekit.estimation.measurements.gnss.LambdaMethod
Find the best solutions to the Integer Least Square problem.
discreteSearch() - Method in class org.orekit.estimation.measurements.gnss.ModifiedLambdaMethod
Find the best solutions to the Integer Least Square problem.
DiscreteTroposphericModel - Interface in org.orekit.models.earth.troposphere
Deprecated.
as of 12.1, replaced by TroposphericModel
displacement(BodiesElements, Frame, Vector3D) - Method in class org.orekit.models.earth.displacement.OceanLoading
Compute displacement of a ground reference point.
displacement(BodiesElements, Frame, Vector3D) - Method in class org.orekit.models.earth.displacement.PostSeismicDeformation
Compute displacement of a ground reference point.
displacement(BodiesElements, Frame, Vector3D) - Method in interface org.orekit.models.earth.displacement.StationDisplacement
Compute displacement of a ground reference point.
displacement(BodiesElements, Frame, Vector3D) - Method in class org.orekit.models.earth.displacement.TectonicsDisplacement
Compute displacement of a ground reference point.
displacement(BodiesElements, Frame, Vector3D) - Method in class org.orekit.models.earth.displacement.TidalDisplacement
Compute displacement of a ground reference point.
displacement(AbsoluteDate, GeodeticPoint) - Method in class org.orekit.models.earth.displacement.PsdCorrection
Compute displacement.
DivertedSingularityAiming - Class in org.orekit.models.earth.tessellation
Class used to orient tiles such that there are no singularities within the zone of interest.
DivertedSingularityAiming(SphericalPolygonsSet) - Constructor for class org.orekit.models.earth.tessellation.DivertedSingularityAiming
Simple constructor.
divide(String, Unit) - Method in class org.orekit.utils.units.Unit
Create quotient of units.
DOCKED_WITH - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Other space objects this object is docked to.
doEvent(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldEventState
Notify the user's listener of the event.
doEvent(SpacecraftState) - Method in class org.orekit.propagation.events.EventState
Notify the user's listener of the event.
DOI - org.orekit.files.rinex.section.RinexLabels
DOI.
doModify(EstimationModifier<T>, EstimatedMeasurement<T>) - Method in class org.orekit.estimation.measurements.modifiers.AbstractAmbiguityModifier
Deprecated.
Modify measurement.
doModify(EstimationModifier<T>, EstimatedMeasurementBase<T>) - Method in class org.orekit.estimation.measurements.modifiers.AbstractShapiroBaseModifier
Modify measurement.
doModifyWithoutDerivatives(EstimationModifier<T>, EstimatedMeasurementBase<T>) - Method in class org.orekit.estimation.measurements.modifiers.AbstractAmbiguityModifier
Deprecated.
Modify measurement.
DOP - Class in org.orekit.gnss
This class is a container for the result of a single DOP computation.
DOP(GeodeticPoint, AbsoluteDate, int, double, double, double, double, double) - Constructor for class org.orekit.gnss.DOP
Constructor.
DOP_MIN_ELEVATION - Static variable in class org.orekit.gnss.DOPComputer
Minimum elevation : 0°.
DOPComputer - Class in org.orekit.gnss
This class aims at computing the dilution of precision.
DOPPLER - org.orekit.gnss.MeasurementType
Doppler measurement.
DOPPLER_COUNT - org.orekit.files.ccsds.ndm.tdm.ObservationType
Data: Doppler counts [n/a].
DOPPLER_COUNT_BIAS - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Bias that was added to Doppler count in the data section.
DOPPLER_COUNT_ROLLOVER - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Indicator for occurred rollover in Doppler count.
DOPPLER_COUNT_SCALE - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Scaled by which Doppler count was multiplied in the data section.
DOPPLER_INSTANTANEOUS - org.orekit.files.ccsds.ndm.tdm.ObservationType
Data: Doppler instantaneous [km/s].
DOPPLER_INTEGRATED - org.orekit.files.ccsds.ndm.tdm.ObservationType
Data: Doppler integrated [km/s].
DOR - org.orekit.files.ccsds.ndm.tdm.ObservationType
Data: DOR [s].
DormandPrince54FieldIntegratorBuilder<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.conversion
Builder for DormandPrince54FieldIntegrator.
DormandPrince54FieldIntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.DormandPrince54FieldIntegratorBuilder
Build a new instance.
DormandPrince54FieldIntegratorBuilder(double, double, double, double) - Constructor for class org.orekit.propagation.conversion.DormandPrince54FieldIntegratorBuilder
Build a new instance.
DormandPrince54IntegrationSettings - Class in org.orekit.control.indirect.shooting.propagation
Integration settings using the Dormand-Prince 5(4) scheme.
DormandPrince54IntegrationSettings(double, double, double, double) - Constructor for class org.orekit.control.indirect.shooting.propagation.DormandPrince54IntegrationSettings
Constructor.
DormandPrince54IntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for DormandPrince54Integrator.
DormandPrince54IntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.DormandPrince54IntegratorBuilder
Build a new instance.
DormandPrince54IntegratorBuilder(double, double, double, double) - Constructor for class org.orekit.propagation.conversion.DormandPrince54IntegratorBuilder
Build a new instance.
DormandPrince853FieldIntegratorBuilder<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.conversion
Builder for DormandPrince853FieldIntegrator.
DormandPrince853FieldIntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.DormandPrince853FieldIntegratorBuilder
Build a new instance.
DormandPrince853FieldIntegratorBuilder(double, double, double, double) - Constructor for class org.orekit.propagation.conversion.DormandPrince853FieldIntegratorBuilder
Build a new instance.
DormandPrince853IntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for DormandPrince853Integrator.
DormandPrince853IntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.DormandPrince853IntegratorBuilder
Build a new instance.
DormandPrince853IntegratorBuilder(double, double, double, double) - Constructor for class org.orekit.propagation.conversion.DormandPrince853IntegratorBuilder
Build a new instance.
DoubleArrayDictionary - Class in org.orekit.utils
String → double[] mapping, for small number of keys.
DoubleArrayDictionary() - Constructor for class org.orekit.utils.DoubleArrayDictionary
Constructor with default initial capacity.
DoubleArrayDictionary(int) - Constructor for class org.orekit.utils.DoubleArrayDictionary
Constructor with specified capacity.
DoubleArrayDictionary(Map<String, double[]>) - Constructor for class org.orekit.utils.DoubleArrayDictionary
Constructor from a map.
DoubleArrayDictionary(DoubleArrayDictionary) - Constructor for class org.orekit.utils.DoubleArrayDictionary
Constructor from another dictionary.
DoubleArrayDictionary.Entry - Class in org.orekit.utils
Entry in a dictionary.
DoubleDihedraFieldOfView - Class in org.orekit.geometry.fov
Class representing a spacecraft sensor Field Of View with dihedral shape (i.e.
DoubleDihedraFieldOfView(Vector3D, Vector3D, double, Vector3D, double, double) - Constructor for class org.orekit.geometry.fov.DoubleDihedraFieldOfView
Build a Field Of View with dihedral shape (i.e.
doubleToString(double) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Convert a double to string value with high precision.
doubleToString(double) - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Convert a double to string value with high precision.
doubleValue(EncodedMessage) - Method in interface org.orekit.gnss.metric.parser.DataField
Get the value of the field as a double.
dP - Variable in class org.orekit.propagation.conversion.AbstractVariableStepFieldIntegratorBuilder
Position error (m).
dP - Variable in class org.orekit.propagation.conversion.AbstractVariableStepIntegratorBuilder
Position error (m).
DR - org.orekit.files.rinex.clock.RinexClock.ClockDataType
Discontinuity measurements for a single GPS receiver.
DRAG_AREA - org.orekit.files.ccsds.ndm.odm.SpacecraftParametersKey
Drag area.
DRAG_COEFF - org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalPropertiesKey
Drag coefficient.
DRAG_COEFF - org.orekit.files.ccsds.ndm.odm.SpacecraftParametersKey
Drag coefficient.
DRAG_COEFF_NOM - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Nominal drag coefficient.
DRAG_COEFFICIENT - Static variable in interface org.orekit.forces.drag.DragSensitive
Parameter name for drag coefficient.
DRAG_CONST_AREA - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Attitude-independent drag cross-sectional area, not already into attitude-dependent area along OEB.
DRAG_UNCERTAINTY - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Drag coefficient 1σ uncertainty.
dragAcceleration(FieldSpacecraftState<T>, T, FieldVector3D<T>, T[]) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Compute the acceleration due to drag.
dragAcceleration(FieldSpacecraftState<T>, T, FieldVector3D<T>, T[]) - Method in interface org.orekit.forces.drag.DragSensitive
Compute the acceleration due to drag.
dragAcceleration(FieldSpacecraftState<T>, T, FieldVector3D<T>, T[]) - Method in class org.orekit.forces.drag.IsotropicDrag
Compute the acceleration due to drag.
dragAcceleration(SpacecraftState, double, Vector3D, double[]) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Compute the acceleration due to drag.
dragAcceleration(SpacecraftState, double, Vector3D, double[]) - Method in interface org.orekit.forces.drag.DragSensitive
Compute the acceleration due to drag.
dragAcceleration(SpacecraftState, double, Vector3D, double[]) - Method in class org.orekit.forces.drag.IsotropicDrag
Compute the acceleration due to drag.
DragForce - Class in org.orekit.forces.drag
Atmospheric drag force model.
DragForce(Atmosphere, DragSensitive) - Constructor for class org.orekit.forces.drag.DragForce
Constructor with default flag for finite differences.
DragForce(Atmosphere, DragSensitive, boolean) - Constructor for class org.orekit.forces.drag.DragForce
Simple constructor.
DragSensitive - Interface in org.orekit.forces.drag
Interface for spacecraft that are sensitive to atmospheric drag forces.
DRIFT_RATE_SHIFT_DEG_PER_DAY - Static variable in class org.orekit.propagation.analytical.intelsat.IntelsatElevenElements
Longitude drift rate.
DRIFT_SUFFIX - Static variable in class org.orekit.estimation.measurements.GroundStation
Suffix for ground clock drift parameters name.
DRY_MASS - org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalPropertiesKey
Mass without propellant.
DRY_MASS - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Mass without propellant.
DSS - org.orekit.files.ccsds.definitions.SpacecraftBodyFrame.BaseEquipment
Digital Sun Sensor.
DSST_ECC_NO_NUMERICAL_AVERAGING_METHOD - org.orekit.errors.OrekitMessages
DSST_ECC_NO_NUMERICAL_AVERAGING_METHOD.
DSST_NEWCOMB_OPERATORS_COMPUTATION - org.orekit.errors.OrekitMessages
DSST_NEWCOMB_OPERATORS_COMPUTATION.
DSST_SPR_SHADOW_INCONSISTENT - org.orekit.errors.OrekitMessages
DSST_SPR_SHADOW_INCONSISTENT.
DSST_THEORY - Static variable in class org.orekit.files.ccsds.ndm.odm.omm.OmmMetadata
Constant for DSST mean elements theory.
DSST_VMNS_COEFFICIENT_ERROR_MS - org.orekit.errors.OrekitMessages
DSST_VMNS_COEFFICIENT_ERROR_MS.
DSST6X0OrbitalState - Class in org.orekit.propagation.conversion.averaging
Class representing an averaged orbital state as in the DSST theory using only the first 6 zonal harmonics as perturbations.
DSST6X0OrbitalState(AbsoluteDate, AveragedEquinoctialWithMeanAngle, Frame, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.conversion.averaging.DSST6X0OrbitalState
Constructor.
DSSTAtmosphericDrag - Class in org.orekit.propagation.semianalytical.dsst.forces
Atmospheric drag contribution to the DSSTPropagator.
DSSTAtmosphericDrag(DragForce, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Simple constructor with custom force.
DSSTAtmosphericDrag(Atmosphere, double, double, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Simple constructor assuming spherical spacecraft.
DSSTAtmosphericDrag(Atmosphere, DragSensitive, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Simple constructor with custom spacecraft.
DSSTBatchLSModel - Class in org.orekit.estimation.leastsquares
DSSTBatchLSModel(PropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver, PropagationType) - Constructor for class org.orekit.estimation.leastsquares.DSSTBatchLSModel
Simple constructor.
DSSTForceModel - Interface in org.orekit.propagation.semianalytical.dsst.forces
This interface represents a force modifying spacecraft motion for a DSSTPropagator.
DSSTGravityContext - Class in org.orekit.propagation.semianalytical.dsst.forces
This class is a container for the common parameters used in DSSTTesseral and DSSTZonal.
DSSTHarvester - Class in org.orekit.propagation.semianalytical.dsst
Harvester between two-dimensional Jacobian matrices and one-dimensional additional state arrays.
DSSTJ2SquaredClosedForm - Class in org.orekit.propagation.semianalytical.dsst.forces
Second order J2-squared force model.
DSSTJ2SquaredClosedForm(J2SquaredModel, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTJ2SquaredClosedForm
Constructor.
DSSTJ2SquaredClosedFormContext - Class in org.orekit.propagation.semianalytical.dsst.forces
This class is a container for the common parameters used in DSSTJ2SquaredClosedForm.
DSSTJ2SquaredClosedFormContext(AuxiliaryElements, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTJ2SquaredClosedFormContext
Simple constructor.
DSSTNewtonianAttraction - Class in org.orekit.propagation.semianalytical.dsst.forces
Force model for Newtonian central body attraction for the DSST propagator.
DSSTNewtonianAttraction(double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction
Simple constructor.
DSSTNewtonianAttractionContext - Class in org.orekit.propagation.semianalytical.dsst.forces
This class is a container for the common parameters used in DSSTNewtonianAttraction.
DSSTNewtonianAttractionContext(AuxiliaryElements, double[]) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttractionContext
Simple constructor.
DSSTPropagator - Class in org.orekit.propagation.semianalytical.dsst
This class propagates orbits using the DSST theory.
DSSTPropagator(ODEIntegrator) - Constructor for class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Create a new instance of DSSTPropagator.
DSSTPropagator(ODEIntegrator, PropagationType) - Constructor for class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Create a new instance of DSSTPropagator.
DSSTPropagator(ODEIntegrator, PropagationType, AttitudeProvider) - Constructor for class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Create a new instance of DSSTPropagator.
DSSTPropagatorBuilder - Class in org.orekit.propagation.conversion
Builder for DSST propagator.
DSSTPropagatorBuilder(Orbit, ODEIntegratorBuilder, double, PropagationType, PropagationType) - Constructor for class org.orekit.propagation.conversion.DSSTPropagatorBuilder
Build a new instance.
DSSTPropagatorBuilder(Orbit, ODEIntegratorBuilder, double, PropagationType, PropagationType, AttitudeProvider) - Constructor for class org.orekit.propagation.conversion.DSSTPropagatorBuilder
Build a new instance.
DSSTSolarRadiationPressure - Class in org.orekit.propagation.semianalytical.dsst.forces
Solar radiation pressure contribution to the DSSTPropagator.
DSSTSolarRadiationPressure(double, double, double, double, ExtendedPVCoordinatesProvider, OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Constructor with customizable reference values but spherical spacecraft.
DSSTSolarRadiationPressure(double, double, ExtendedPVCoordinatesProvider, OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Simple constructor with default reference values and spherical spacecraft.
DSSTSolarRadiationPressure(double, double, ExtendedPVCoordinatesProvider, OneAxisEllipsoid, RadiationSensitive, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Complete constructor.
DSSTSolarRadiationPressure(ExtendedPVCoordinatesProvider, OneAxisEllipsoid, RadiationSensitive, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Simple constructor with default reference values, but custom spacecraft.
DSSTTesseral - Class in org.orekit.propagation.semianalytical.dsst.forces
Tesseral contribution to the central body gravitational perturbation.
DSSTTesseral(Frame, double, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Simple constructor with default reference values.
DSSTTesseral(Frame, double, UnnormalizedSphericalHarmonicsProvider, int, int, int, int, int, int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Simple constructor.
DSSTTesseralContext - Class in org.orekit.propagation.semianalytical.dsst.forces
This class is a container for the common parameters used in DSSTTesseral.
DSSTThirdBody - Class in org.orekit.propagation.semianalytical.dsst.forces
Third body attraction perturbation to the DSSTPropagator.
DSSTThirdBody(CelestialBody, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Complete constructor.
DSSTThirdBodyDynamicContext - Class in org.orekit.propagation.semianalytical.dsst.forces
This class is a container for the common parameters used in DSSTThirdBody.
DSSTThirdBodyDynamicContext(AuxiliaryElements, CelestialBody, double[]) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext
Constructor.
DSSTThirdBodyStaticContext - Class in org.orekit.propagation.semianalytical.dsst.forces
This class is a container for the common parameters used in DSSTThirdBody.
DSSTThirdBodyStaticContext(AuxiliaryElements, double, double, double[]) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyStaticContext
Constructor.
DSSTZonal - Class in org.orekit.propagation.semianalytical.dsst.forces
Zonal contribution to the central body gravitational perturbation.
DSSTZonal(UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Constructor with bodyFixedFrame = orbit frame, and default reference values.
DSSTZonal(UnnormalizedSphericalHarmonicsProvider, int, int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Constructor with bodyFixedFrame = orbit frame.
DSSTZonal(Frame, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Constructor with default reference values.
DSSTZonal(Frame, UnnormalizedSphericalHarmonicsProvider, int, int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Constructor.
DSSTZonalContext - Class in org.orekit.propagation.semianalytical.dsst.forces
This class is a container for the common parameters used in DSSTZonal.
DtcDataLoader - Class in org.orekit.models.earth.atmosphere.data
This class reads solar activity data from DTCFILE files for the class JB2008SpaceEnvironmentData.
DtcDataLoader(TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.data.DtcDataLoader
Constructor.
DtcDataLoader.LineParameters - Class in org.orekit.models.earth.atmosphere.data
Container class for Solar activity indexes.
DTM2000 - Class in org.orekit.models.earth.atmosphere
This atmosphere model is the realization of the DTM-2000 model.
DTM2000(DTM2000InputParameters, PVCoordinatesProvider, BodyShape) - Constructor for class org.orekit.models.earth.atmosphere.DTM2000
Simple constructor for independent computation.
DTM2000(DTM2000InputParameters, PVCoordinatesProvider, BodyShape, TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.DTM2000
Simple constructor for independent computation.
DTM2000InputParameters - Interface in org.orekit.models.earth.atmosphere
Container for solar activity data, compatible with DTM2000 Atmosphere model.
DUAL_CONE - org.orekit.files.ccsds.ndm.odm.ocm.ShadowModel
Cone model, penumbra and umbra.
DualFrequencyHatchFilter - Class in org.orekit.estimation.measurements.filtering
Hatch Filter using Carrier-Phase measurements taken at two different frequencies, to form a Divergence-Free phase combination.
DualFrequencyHatchFilter(ObservationData, ObservationData, ObservationData, double, double, double, int) - Constructor for class org.orekit.estimation.measurements.filtering.DualFrequencyHatchFilter
Constructor for the Dual Frequency Hatch Filter.
DualFrequencySmoother - Class in org.orekit.estimation.measurements.filtering
Handler to perform pseudo-range smoothing using Divergence-Free phase combinations.
DualFrequencySmoother(double, int) - Constructor for class org.orekit.estimation.measurements.filtering.DualFrequencySmoother
Simple constructor.
DUMMY - Static variable in class org.orekit.files.sp3.SP3Coordinate
Dummy coordinate with all fields set to 0.0.
DummyMappingFunction - Class in org.orekit.models.earth.troposphere
Dummy mapping function.
DummyMappingFunction() - Constructor for class org.orekit.models.earth.troposphere.DummyMappingFunction
Builds a new instance.
DUPLICATED_GRAVITY_FIELD_COEFFICIENT_IN_FILE - org.orekit.errors.OrekitMessages
DUPLICATED_GRAVITY_FIELD_COEFFICIENT_IN_FILE.
Duration - Class in org.orekit.forces.maneuvers.jacobians
Generator for one column of a Jacobian matrix for special case of maneuver duration.
Duration(String, String, String) - Constructor for class org.orekit.forces.maneuvers.jacobians.Duration
Simple constructor.
DURATION_SUFFIX - Static variable in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector
Default suffix for duration driver.
DURATION_SUFFIX - Static variable in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector
Default suffix for duration driver.
durationFrom(AbsoluteDate) - Method in class org.orekit.time.AbsoluteDate
Compute the physically elapsed duration between two instants.
durationFrom(AbsoluteDate) - Method in class org.orekit.time.FieldAbsoluteDate
Compute the physically elapsed duration between two instants.
durationFrom(AbsoluteDate, TimeUnit) - Method in class org.orekit.time.AbsoluteDate
Compute the physically elapsed duration between two instants.
durationFrom(AbsoluteDate, TimeUnit) - Method in class org.orekit.time.FieldAbsoluteDate
Compute the physically elapsed duration between two instants.
durationFrom(FieldAbsoluteDate<T>) - Method in class org.orekit.time.FieldAbsoluteDate
Compute the physically elapsed duration between two instants.
durationFrom(FieldAbsoluteDate<T>, TimeUnit) - Method in class org.orekit.time.FieldAbsoluteDate
Compute the physically elapsed duration between two instants.
durationFrom(FieldTimeStamped<T>) - Method in interface org.orekit.time.FieldTimeStamped
Compute the physically elapsed duration between two instants.
durationFrom(TimeStamped) - Method in interface org.orekit.time.TimeStamped
Compute the physically elapsed duration between two instants.
DutyCycleType - Enum in org.orekit.files.ccsds.definitions
Type of duty cycle used in CCSDS Orbit Comprehensive Messages.
dV - Variable in class org.orekit.propagation.conversion.AbstractVariableStepFieldIntegratorBuilder
Velocity error (m/s).
dV - Variable in class org.orekit.propagation.conversion.AbstractVariableStepIntegratorBuilder
Velocity error (m/s).
DV_BOL - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Total ΔV capability at beginning of life.
DV_DIR_SIGMA - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
One σ angular off-nominal ΔV direction.
DV_MAG_SIGMA - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
One σ percent error on ΔV magnitude.
DV_REMAINING - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Total ΔV remaining for spacecraft.
DV_X - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
Velocity increment along X axis.
DV_Y - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
Velocity increment along Y axis.
DV_Z - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
Velocity increment along Z axis.
DynamicOutlierFilter<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.modifiers
Modifier that sets estimated measurement weight to 0 if residual is too far from expected domain.
DynamicOutlierFilter(int, double) - Constructor for class org.orekit.estimation.measurements.modifiers.DynamicOutlierFilter
Simple constructor.

E

e - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
final eccentricity.
e - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
final eccentricity.
E - org.orekit.gnss.SignalCode
QZSS L6E and L6 (D+E) codes.
E_X - Static variable in enum org.orekit.orbits.OrbitType
Name for eccentricity vector first component.
E_Y - Static variable in enum org.orekit.orbits.OrbitType
Name for eccentricity vector second component.
E01 - org.orekit.gnss.Frequency
Galileo, "E1" (1575.42 MHz).
E05 - org.orekit.gnss.Frequency
Galileo E5a (1176.45 MHz).
E06 - org.orekit.gnss.Frequency
Galileo E6 (1278.75 MHz).
E07 - org.orekit.gnss.Frequency
Galileo E5b (1207.14 MHz).
E08 - org.orekit.gnss.Frequency
Galileo E5 (E5a + E5b) (1191.795MHz).
e0sq - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
original eccentricity squared.
e0sq - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
original eccentricity squared.
EARTH - org.orekit.attitudes.PredefinedTarget
Earth direction (assumes the frame is Earth centered).
EARTH - org.orekit.bodies.JPLEphemeridesLoader.EphemerisType
Constant for the Earth.
EARTH - org.orekit.files.ccsds.definitions.CenterName
Earth body.
EARTH - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Earth.
EARTH_ANGULAR_VELOCITY - Static variable in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
Earth Angular Velocity, in rad/s, from TIRF model.
EARTH_MOON - org.orekit.bodies.JPLEphemeridesLoader.EphemerisType
Constant for the Earth-Moon barycenter.
EARTH_MOON - org.orekit.files.ccsds.definitions.CenterName
Earth-Moon barycenter bodies pair.
EARTH_MOON - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Earth-Moon barycenter.
EARTH_RADII - Static variable in class org.orekit.utils.units.Unit
Earth Radii used as Bstar unit in CCSDS OMM.
EARTH_RADIUS - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
Earth radius in km.
EARTH_TIDES - org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey
Is solid Earth and ocean tides used for the OD of the object ?
EarthITU453AtmosphereRefraction - Class in org.orekit.models.earth
Implementation of refraction model for Earth exponential atmosphere based on ITU-R P.834-7 recommendation.
EarthITU453AtmosphereRefraction(double) - Constructor for class org.orekit.models.earth.EarthITU453AtmosphereRefraction
Creates a new default instance.
EarthOrientationParameterMessage - Class in org.orekit.files.rinex.navigation
Container for data contained in a Earth Orientation Parameter navigation message.
EarthOrientationParameterMessage(SatelliteSystem, int, String) - Constructor for class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage
Simple constructor.
EarthShape - Interface in org.orekit.models.earth
All models of Earth's shape have some common properties that are not shared with arbitrary BodyShapes.
EarthStandardAtmosphereRefraction - Class in org.orekit.models.earth
Implementation of refraction model for Earth standard atmosphere.
EarthStandardAtmosphereRefraction() - Constructor for class org.orekit.models.earth.EarthStandardAtmosphereRefraction
Creates a new default instance.
EarthStandardAtmosphereRefraction(double, double) - Constructor for class org.orekit.models.earth.EarthStandardAtmosphereRefraction
Creates an instance given a specific pressure and temperature.
EAST - org.orekit.attitudes.PredefinedTarget
East direction.
EAST - org.orekit.models.earth.displacement.PsdCorrection.Axis
East axis.
ECC - Static variable in enum org.orekit.orbits.OrbitType
Name for eccentricity.
ECC_ANOM - Static variable in enum org.orekit.orbits.OrbitType
Name for eccentric anomaly.
ECC_LAT_ARG - Static variable in enum org.orekit.orbits.OrbitType
Name for eccentric argument of latitude.
ECC_LON_ARG - Static variable in enum org.orekit.orbits.OrbitType
Name for eccentric argument of longitude.
ECCENTRIC - org.orekit.orbits.PositionAngleType
Eccentric angle.
ECCENTRICITY - org.orekit.files.ccsds.ndm.odm.KeplerianElementsKey
Orbit eccentricity.
eccentricToMean(double, double, double) - Static method in class org.orekit.orbits.CircularLatitudeArgumentUtility
Computes the mean latitude argument from the eccentric latitude argument.
eccentricToMean(double, double, double) - Static method in class org.orekit.orbits.CircularOrbit
Deprecated.
eccentricToMean(double, double, double) - Static method in class org.orekit.orbits.EquinoctialLongitudeArgumentUtility
Computes the mean longitude argument from the eccentric longitude argument.
eccentricToMean(double, double, double) - Static method in class org.orekit.orbits.EquinoctialOrbit
Deprecated.
eccentricToMean(T, T, T) - Static method in class org.orekit.orbits.FieldCircularLatitudeArgumentUtility
Computes the mean latitude argument from the eccentric latitude argument.
eccentricToMean(T, T, T) - Static method in class org.orekit.orbits.FieldCircularOrbit
Deprecated.
eccentricToMean(T, T, T) - Static method in class org.orekit.orbits.FieldEquinoctialLongitudeArgumentUtility
Computes the mean longitude argument from the eccentric longitude argument.
eccentricToMean(T, T, T) - Static method in class org.orekit.orbits.FieldEquinoctialOrbit
Deprecated.
eccentricToTrue(double, double, double) - Static method in class org.orekit.orbits.CircularLatitudeArgumentUtility
Computes the true latitude argument from the eccentric latitude argument.
eccentricToTrue(double, double, double) - Static method in class org.orekit.orbits.CircularOrbit
Deprecated.
eccentricToTrue(double, double, double) - Static method in class org.orekit.orbits.EquinoctialLongitudeArgumentUtility
Computes the true longitude argument from the eccentric longitude argument.
eccentricToTrue(double, double, double) - Static method in class org.orekit.orbits.EquinoctialOrbit
Deprecated.
eccentricToTrue(T, T, T) - Static method in class org.orekit.orbits.FieldCircularLatitudeArgumentUtility
Computes the true latitude argument from the eccentric latitude argument.
eccentricToTrue(T, T, T) - Static method in class org.orekit.orbits.FieldCircularOrbit
Deprecated.
eccentricToTrue(T, T, T) - Static method in class org.orekit.orbits.FieldEquinoctialLongitudeArgumentUtility
Computes the true longitude argument from the eccentric longitude argument.
eccentricToTrue(T, T, T) - Static method in class org.orekit.orbits.FieldEquinoctialOrbit
Deprecated.
ecef(Frame) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagatorBuilder
Sets the Earth Centered Earth Fixed frame assimilated to the WGS84 ECEF.
ecef(Frame) - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagatorBuilder
Sets the Earth Centered Earth Fixed frame assimilated to the WGS84 ECEF.
ecef(Frame) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagatorBuilder
Sets the Earth Centered Earth Fixed frame assimilated to the WGS84 ECEF.
eci(Frame) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagatorBuilder
Sets the Earth Centered Inertial frame used for propagation.
eci(Frame) - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagatorBuilder
Sets the Earth Centered Inertial frame used for propagation.
eci(Frame) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagatorBuilder
Sets the Earth Centered Inertial frame used for propagation.
eci(Frame) - Method in class org.orekit.propagation.numerical.GLONASSNumericalPropagatorBuilder
Sets the Earth Centered Inertial frame used for propagation.
EcksteinHechlerOrbitalState - Class in org.orekit.propagation.conversion.averaging
Class representing an averaged orbital state as in the Eckstein-Hechler theory.
EcksteinHechlerOrbitalState(AbsoluteDate, AveragedCircularWithMeanAngle, Frame, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.conversion.averaging.EcksteinHechlerOrbitalState
Constructor.
EcksteinHechlerPropagator - Class in org.orekit.propagation.analytical
This class propagates a SpacecraftState using the analytical Eckstein-Hechler model.
EcksteinHechlerPropagator(Orbit, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit and potential.
EcksteinHechlerPropagator(Orbit, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit, mass and potential.
EcksteinHechlerPropagator(Orbit, double, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit, mass and potential provider.
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit, attitude provider and potential.
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit, attitude provider, mass and potential.
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double, double, PropagationType) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit, attitude provider, mass and potential.
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double, double, PropagationType, double, int) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit, attitude provider, mass and potential.
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit, attitude provider, mass and potential provider.
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Private helper constructor.
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, PropagationType) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Private helper constructor.
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider, PropagationType) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit, attitude provider, mass and potential provider.
EcksteinHechlerPropagator(Orbit, AttitudeProvider, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit, attitude provider and potential provider.
EcksteinHechlerPropagator(Orbit, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit and potential provider.
EcksteinHechlerPropagator(Orbit, UnnormalizedSphericalHarmonicsProvider, PropagationType) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit and potential provider.
EcksteinHechlerPropagatorBuilder - Class in org.orekit.propagation.conversion
Builder for Eckstein-Hechler propagator.
EcksteinHechlerPropagatorBuilder(Orbit, double, double, TideSystem, double, double, double, double, double, OrbitType, PositionAngleType, double) - Constructor for class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder
Build a new instance.
EcksteinHechlerPropagatorBuilder(Orbit, UnnormalizedSphericalHarmonicsProvider, PositionAngleType, double) - Constructor for class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder
Build a new instance.
EcksteinHechlerPropagatorBuilder(Orbit, UnnormalizedSphericalHarmonicsProvider, PositionAngleType, double, AttitudeProvider) - Constructor for class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder
Build a new instance.
EclipseDetector - Class in org.orekit.propagation.events
Finder for satellite eclipse related events.
EclipseDetector(AdaptableInterval, double, int, EventHandler, OccultationEngine, double, boolean) - Constructor for class org.orekit.propagation.events.EclipseDetector
Deprecated.
as of 12.2
EclipseDetector(EventDetectionSettings, EventHandler, OccultationEngine, double, boolean) - Constructor for class org.orekit.propagation.events.EclipseDetector
Protected constructor with full parameters.
EclipseDetector(ExtendedPVCoordinatesProvider, double, OneAxisEllipsoid) - Constructor for class org.orekit.propagation.events.EclipseDetector
Build a new eclipse detector.
EclipseDetector(OccultationEngine) - Constructor for class org.orekit.propagation.events.EclipseDetector
Build a new eclipse detector.
ECLIPTIC_CONVENTIONS_1996 - org.orekit.frames.Predefined
Ecliptic framen IERS 1996 conventions.
ECLIPTIC_CONVENTIONS_2003 - org.orekit.frames.Predefined
Ecliptic framen IERS 2003 conventions.
ECLIPTIC_CONVENTIONS_2010 - org.orekit.frames.Predefined
Ecliptic framen IERS 2010 conventions.
EclipticProvider - Class in org.orekit.frames
An inertial frame aligned with the ecliptic.
EclipticProvider(IERSConventions) - Constructor for class org.orekit.frames.EclipticProvider
Create a transform provider from MOD to an ecliptically aligned frame.
EclipticProvider(IERSConventions, TimeScales) - Constructor for class org.orekit.frames.EclipticProvider
Create a transform provider from MOD to an ecliptically aligned frame.
ECOM_COEFFICIENT - Static variable in class org.orekit.forces.radiation.ECOM2
Parameter name for ECOM model coefficients enabling Jacobian processing.
ECOM2 - Class in org.orekit.forces.radiation
The Empirical CODE Orbit Model 2 (ECOM2) of the Center for Orbit Determination in Europe (CODE).
ECOM2(int, int, double, ExtendedPVCoordinatesProvider, double) - Constructor for class org.orekit.forces.radiation.ECOM2
Constructor.
eeta - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
original eccentricity * eta.
eeta - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
original eccentricity * eta.
EGM_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory
Default regular expression for EGM files.
EGM96_EARTH_C20 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized second zonal coefficient from EGM96 model: -1.08262668355315e-3.
EGM96_EARTH_C30 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized third zonal coefficient from EGM96 model: 2.53265648533224e-6.
EGM96_EARTH_C40 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized fourth zonal coefficient from EGM96 model: 1.619621591367e-6.
EGM96_EARTH_C50 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized fifth zonal coefficient from EGM96 model: 2.27296082868698e-7.
EGM96_EARTH_C60 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized sixth zonal coefficient from EGM96 model: -5.40681239107085e-7.
EGM96_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Earth equatorial radius from EGM96 model: 6378136.3 m.
EGM96_EARTH_MU - Static variable in interface org.orekit.utils.Constants
Earth gravitational constant from EGM96 model: 3.986004415e14 m³/s².
EGMFormatReader - Class in org.orekit.forces.gravity.potential
This reader is adapted to the EGM Format.
EGMFormatReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.EGMFormatReader
Simple constructor.
EGMFormatReader(String, boolean, boolean) - Constructor for class org.orekit.forces.gravity.potential.EGMFormatReader
Simple constructor that allows overriding 'standard' EGM96 ae and mu with WGS84 variants.
EGNOS - org.orekit.files.rinex.navigation.SbasId
European Geostationary Navigation Overlay Service.
EGO - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCategory
Extended Geostationary Orbit, 37948 < a < 46380 km, e < 0.25, i < 25°.
EIGEN5C_EARTH_C20 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized second zonal coefficient from EIGEN5C model: -1.082626457231767e-3.
EIGEN5C_EARTH_C30 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized third zonal coefficient from EIGEN5C model: 2.532547231862799e-6.
EIGEN5C_EARTH_C40 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized fourth zonal coefficient from EIGEN5C model: 1.619964434136e-6.
EIGEN5C_EARTH_C50 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized fifth zonal coefficient from EIGEN5C model: 2.277928487005437e-7.
EIGEN5C_EARTH_C60 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized sixth zonal coefficient from EIGEN5C model: -5.406653715879098e-7.
EIGEN5C_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Earth equatorial radius from EIGEN5C model: 6378136.46 m.
EIGEN5C_EARTH_MU - Static variable in interface org.orekit.utils.Constants
Earth gravitational constant from EIGEN5C model: 3.986004415e14 m³/s².
EIGVAL3EIGVEC3 - org.orekit.files.ccsds.ndm.odm.ocm.OrbitElementsType
12 elements eigenvalue/eigenvectors (EigMaj, EigMed, EigMin, EigVecMaj, EigVecMed, EigVecMin).
EKF - org.orekit.files.ccsds.definitions.AdMethodType
Extended Kalman Filter.
EKF - org.orekit.files.ccsds.definitions.OdMethodType
Extended Kalman Filter.
ELEMENT_SET_NO - org.orekit.files.ccsds.ndm.odm.omm.OmmTleKey
Element set number for this satellite.
ElevationDetectionAdaptableIntervalFactory - Class in org.orekit.propagation.events.intervals
Factory class for AdaptableInterval suitable for elevation detection on eccentric orbits.
ElevationDetector - Class in org.orekit.propagation.events
Finder for satellite raising/setting events that allows for the setting of azimuth and/or elevation bounds or a ground azimuth/elevation mask input.
ElevationDetector(double, double, TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationDetector
Creates an instance of Elevation detector based on passed in topocentric frame and overrides of default maximal checking interval and convergence threshold values.
ElevationDetector(TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationDetector
Creates an instance of Elevation detector based on passed in topocentric frame and the minimum elevation angle.
ElevationDetector(AdaptableInterval, double, int, EventHandler, double, ElevationMask, AtmosphericRefractionModel, TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationDetector
Protected constructor with full parameters.
ElevationDetector(AdaptableInterval, double, TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationDetector
Creates an instance of Elevation detector based on passed in topocentric frame and overrides of default maximal checking interval and convergence threshold values.
ElevationExtremumDetector - Class in org.orekit.propagation.events
Detector for elevation extremum with respect to a ground point.
ElevationExtremumDetector(double, double, TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationExtremumDetector
Build a detector.
ElevationExtremumDetector(TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationExtremumDetector
Build a new detector.
ElevationExtremumDetector(AdaptableInterval, double, int, EventHandler, TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationExtremumDetector
Protected constructor with full parameters.
ElevationFilter<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.filtering
Elevation pre-processing filter.
ElevationFilter(GroundStation, double) - Constructor for class org.orekit.estimation.measurements.filtering.ElevationFilter
Constructor.
ElevationMask - Class in org.orekit.utils
Class for modeling the ground elevation values around a given point.
ElevationMask(double[][]) - Constructor for class org.orekit.utils.ElevationMask
Creates an instance of an Elevation mask based on the passed in parameter.
Ellipse - Class in org.orekit.bodies
Model of a 2D ellipse in 3D space.
Ellipse(Vector3D, Vector3D, Vector3D, double, double, Frame) - Constructor for class org.orekit.bodies.Ellipse
Simple constructor.
Ellipsoid - Class in org.orekit.bodies
Modeling of a general three-axes ellipsoid.
Ellipsoid(Frame, double, double, double) - Constructor for class org.orekit.bodies.Ellipsoid
Simple constructor.
ELLIPSOID - org.orekit.files.ccsds.ndm.cdm.ScreenVolumeShape
Ellipsoid.
EllipsoidTessellator - Class in org.orekit.models.earth.tessellation
Class used to tessellate an interest zone on an ellipsoid in either tiles or grids of geodetic points.
EllipsoidTessellator(OneAxisEllipsoid, TileAiming, int) - Constructor for class org.orekit.models.earth.tessellation.EllipsoidTessellator
Simple constructor.
EllipticalFieldOfView - Class in org.orekit.geometry.fov
Class representing a spacecraft sensor Field Of View with elliptical shape.
EllipticalFieldOfView(Vector3D, Vector3D, double, double, double) - Constructor for class org.orekit.geometry.fov.EllipticalFieldOfView
Build a new instance.
ellipticEccentricToMean(double, double) - Static method in class org.orekit.orbits.KeplerianAnomalyUtility
Computes the elliptic mean anomaly from the elliptic eccentric anomaly.
ellipticEccentricToMean(T, T) - Static method in class org.orekit.orbits.FieldKeplerianAnomalyUtility
Computes the elliptic mean anomaly from the elliptic eccentric anomaly.
ellipticEccentricToTrue(double, double) - Static method in class org.orekit.orbits.KeplerianAnomalyUtility
Computes the elliptic true anomaly from the elliptic eccentric anomaly.
ellipticEccentricToTrue(T, T) - Static method in class org.orekit.orbits.FieldKeplerianAnomalyUtility
Computes the elliptic true anomaly from the elliptic eccentric anomaly.
ellipticMeanToEccentric(double, double) - Static method in class org.orekit.orbits.KeplerianAnomalyUtility
Computes the elliptic eccentric anomaly from the elliptic mean anomaly.
ellipticMeanToEccentric(T, T) - Static method in class org.orekit.orbits.FieldKeplerianAnomalyUtility
Computes the elliptic eccentric anomaly from the elliptic mean anomaly.
ellipticMeanToTrue(double, double) - Static method in class org.orekit.orbits.KeplerianAnomalyUtility
Computes the elliptic true anomaly from the elliptic mean anomaly.
ellipticMeanToTrue(T, T) - Static method in class org.orekit.orbits.FieldKeplerianAnomalyUtility
Computes the elliptic true anomaly from the elliptic mean anomaly.
ellipticTrueToEccentric(double, double) - Static method in class org.orekit.orbits.KeplerianAnomalyUtility
Computes the elliptic eccentric anomaly from the elliptic true anomaly.
ellipticTrueToEccentric(T, T) - Static method in class org.orekit.orbits.FieldKeplerianAnomalyUtility
Computes the elliptic eccentric anomaly from the elliptic true anomaly.
ellipticTrueToMean(double, double) - Static method in class org.orekit.orbits.KeplerianAnomalyUtility
Computes the elliptic mean anomaly from the elliptic true anomaly.
ellipticTrueToMean(T, T) - Static method in class org.orekit.orbits.FieldKeplerianAnomalyUtility
Computes the elliptic mean anomaly from the elliptic true anomaly.
EME2000 - org.orekit.files.ccsds.definitions.CelestialBodyFrame
Earth Mean Equator and Equinox of J2000.
EME2000 - org.orekit.frames.Predefined
EME2000 frame.
emitterToInert(EstimatedMeasurementBase<InterSatellitesPhase>) - Method in class org.orekit.estimation.measurements.gnss.InterSatellitesWindUp
Compute rotation from emitter to inertial frame.
emitterToInert(EstimatedMeasurementBase<Phase>) - Method in class org.orekit.estimation.measurements.gnss.WindUp
Compute rotation from emitter to inertial frame.
emitterToInert(EstimatedMeasurementBase<T>) - Method in class org.orekit.estimation.measurements.gnss.AbstractWindUp
Compute rotation from emitter to inertial frame.
EMPTY - org.orekit.gnss.metric.ntrip.NavigationSystem
No navigation system for this stream.
emptyCache() - Static method in class org.orekit.utils.ImmutableFieldTimeStampedCache
Get an empty immutable cache.
emptyCache() - Static method in class org.orekit.utils.ImmutableTimeStampedCache
Get an empty immutable cache, cast to the correct type.
emptyCache(Field<CFE>) - Static method in class org.orekit.utils.ImmutableFieldTimeStampedCache
Deprecated.
EnablingPredicate - Interface in org.orekit.propagation.events
This interface represents an event enabling predicate function.
EncodedMessage - Interface in org.orekit.gnss.metric.parser
Interface for getting bits forming encoded messages.
EncounterLOF - Interface in org.orekit.frames.encounter
Interface for encounter local orbital frame.
EncounterLOFType - Enum in org.orekit.frames.encounter
Enum for encounter local orbital frame.
END - org.orekit.files.ccsds.ndm.tdm.IntegrationReference
Time tag at integration interval end.
END - org.orekit.files.rinex.section.RinexLabels
End of header.
END_OF_ENCODED_MESSAGE - org.orekit.errors.OrekitMessages
END_OF_ENCODED_MESSAGE.
endMessage(String) - Method in interface org.orekit.files.ccsds.utils.generation.Generator
End CCSDS message.
endMessage(String) - Method in class org.orekit.files.ccsds.utils.generation.KvnGenerator
End CCSDS message.
endMessage(String) - Method in class org.orekit.files.ccsds.utils.generation.XmlGenerator
End CCSDS message.
endParse() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
End parsing.
ensureCompatible(String, List<Unit>, boolean, List<Unit>) - Static method in class org.orekit.utils.units.Unit
Ensure some units are compatible with reference units.
ensureCompatibleAdditionalStates(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.FieldSpacecraftState
Check if two instances have the same set of additional states available.
ensureCompatibleAdditionalStates(SpacecraftState) - Method in class org.orekit.propagation.SpacecraftState
Check if two instances have the same set of additional states available.
enterSection(String) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Enter into a new section.
enterSection(String) - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Enter into a new section.
enterSection(String) - Method in class org.orekit.files.ccsds.utils.generation.KvnGenerator
Enter into a new section.
enterSection(String) - Method in class org.orekit.files.ccsds.utils.generation.XmlGenerator
Enter into a new section.
enterSection(Generator) - Method in class org.orekit.files.ccsds.section.AbstractWriter
Enter the section.
ENTRY - org.orekit.files.ccsds.utils.lexical.TokenType
Entry content token.
EOP_SOURCE - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Source and version of Earth Orientation Parameters.
EOPBasedTransformProvider - Interface in org.orekit.frames
Interface for Transform providers that use Earth Orientation Parameters.
EOPC04_1980_FILENAME - Static variable in class org.orekit.frames.FramesFactory
Default regular expression for the EOPC04 files (IAU1980 compatibles).
EOPC04_2000_FILENAME - Static variable in class org.orekit.frames.FramesFactory
Default regular expression for the EOPC04 files (IAU2000 compatibles).
EOPEntry - Class in org.orekit.frames
This class holds an Earth Orientation Parameters entry.
EOPEntry(int, double, double, double, double, double, double, double, double, double, double, ITRFVersion, AbsoluteDate) - Constructor for class org.orekit.frames.EOPEntry
Simple constructor.
EOPFittedModel - Class in org.orekit.frames
Container for fitted model for Earth Orientation Parameters.
EOPFittedModel(SecularAndHarmonic, SecularAndHarmonic, SecularAndHarmonic, SecularAndHarmonic, SecularAndHarmonic) - Constructor for class org.orekit.frames.EOPFittedModel
Simple constructor.
EOPFitter - Class in org.orekit.frames
Earth Orientation Parameters fitter for EOP prediction.
EOPFitter(SingleParameterFitter, SingleParameterFitter, SingleParameterFitter, SingleParameterFitter, SingleParameterFitter) - Constructor for class org.orekit.frames.EOPFitter
Simple constructor.
EOPHistory - Class in org.orekit.frames
This class loads any kind of Earth Orientation Parameter data throughout a large time range.
EOPHistory(IERSConventions, int, Collection<? extends EOPEntry>, boolean) - Constructor for class org.orekit.frames.EOPHistory
Simple constructor.
EOPHistory(IERSConventions, int, Collection<? extends EOPEntry>, boolean, TimeScales) - Constructor for class org.orekit.frames.EOPHistory
Simple constructor.
EopHistoryLoader - Interface in org.orekit.frames
Interface for loading Earth Orientation Parameters history.
EopHistoryLoader.Parser - Interface in org.orekit.frames
Interface for parsing EOP data files.
Ephemeris - Class in org.orekit.propagation.analytical
This class is designed to accept and handle tabulated orbital entries.
Ephemeris(List<SpacecraftState>, int) - Constructor for class org.orekit.propagation.analytical.Ephemeris
Legacy constructor with tabulated states and default Hermite interpolation.
Ephemeris(List<SpacecraftState>, TimeInterpolator<SpacecraftState>) - Constructor for class org.orekit.propagation.analytical.Ephemeris
Constructor with tabulated states.
Ephemeris(List<SpacecraftState>, TimeInterpolator<SpacecraftState>, List<StateCovariance>, TimeInterpolator<TimeStampedPair<Orbit, StateCovariance>>) - Constructor for class org.orekit.propagation.analytical.Ephemeris
Constructor with tabulated states and associated covariances.
Ephemeris(List<SpacecraftState>, TimeInterpolator<SpacecraftState>, List<StateCovariance>, TimeInterpolator<TimeStampedPair<Orbit, StateCovariance>>, AttitudeProvider) - Constructor for class org.orekit.propagation.analytical.Ephemeris
Constructor with tabulated states and associated covariances.
Ephemeris(List<SpacecraftState>, TimeInterpolator<SpacecraftState>, AttitudeProvider) - Constructor for class org.orekit.propagation.analytical.Ephemeris
Constructor with tabulated states.
EPHEMERIS_NAME - org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey
Unique name of the external ephemeris file used for the object or NONE.
EPHEMERIS_NAME_1 - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
External ephemeris file for the participant 1.
EPHEMERIS_NAME_2 - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
External ephemeris file for the participant 2.
EPHEMERIS_NAME_3 - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
External ephemeris file for the participant 3.
EPHEMERIS_NAME_4 - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
External ephemeris file for the participant 4.
EPHEMERIS_NAME_5 - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
External ephemeris file for the participant 5.
EPHEMERIS_TYPE - org.orekit.files.ccsds.ndm.odm.omm.OmmTleKey
Ephemeris Type, only required if MEAN_ELEMENT_THEORY = SGP/SGP4.
EPHEMERIS_TYPE_PPT3 - Static variable in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
Constant for EPHEMERIS_TYPE PPT3.
EPHEMERIS_TYPE_SGP - Static variable in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
Constant for EPHEMERIS_TYPE SGP.
EPHEMERIS_TYPE_SGP4 - Static variable in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
Constant for EPHEMERIS_TYPE SGP4.
EPHEMERIS_TYPE_SGP4_XP - Static variable in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
Constant for EPHEMERIS_TYPE SGP4-XP.
EPHEMERIS_TYPE_SPECIAL_PERTURBATIONS - Static variable in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
Constant for EPHEMERIS_TYPE Special Perturbations.
EphemerisFile<C extends TimeStampedPVCoordinates,​S extends EphemerisFile.EphemerisSegment<C>> - Interface in org.orekit.files.general
An interface for accessing the data stored in an ephemeris file and using the data to create a working Propagator.
EphemerisFile.EphemerisSegment<C extends TimeStampedPVCoordinates> - Interface in org.orekit.files.general
A segment of an ephemeris for a satellite.
EphemerisFile.SatelliteEphemeris<C extends TimeStampedPVCoordinates,​S extends EphemerisFile.EphemerisSegment<C>> - Interface in org.orekit.files.general
Contains the information about a single satellite from an EphemerisFile.
EphemerisFileParser<T extends EphemerisFile<?,​?>> - Interface in org.orekit.files.general
Parse an ephemeris file.
EphemerisFileWriter - Interface in org.orekit.files.general
An interface for writing out ephemeris files to disk.
EphemerisGenerator - Interface in org.orekit.propagation
Generator for ephemerides.
EphemerisOcmWriter - Class in org.orekit.files.ccsds.ndm.odm.ocm
An EphemerisFileWriter generating OCM files.
EphemerisOcmWriter(OcmWriter, OdmHeader, OcmMetadata, TrajectoryStateHistoryMetadata, FileFormat, String, double, int) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.EphemerisOcmWriter
Constructor used to create a new OCM writer configured with the necessary parameters to successfully fill in all required fields that aren't part of a standard object.
EphemerisOemWriter - Class in org.orekit.files.ccsds.ndm.odm.oem
An EphemerisFileWriter generating OEM files.
EphemerisOemWriter(OemWriter, OdmHeader, OemMetadata, FileFormat, String, double, int) - Constructor for class org.orekit.files.ccsds.ndm.odm.oem.EphemerisOemWriter
Constructor used to create a new OEM writer configured with the necessary parameters to successfully fill in all required fields that aren't part of a standard object.
EphemerisPropagatorBuilder - Class in org.orekit.propagation.conversion
Builder for Ephemeris propagator.
EphemerisPropagatorBuilder(List<SpacecraftState>, int, double, AttitudeProvider) - Constructor for class org.orekit.propagation.conversion.EphemerisPropagatorBuilder
Constructor.
EphemerisPropagatorBuilder(List<SpacecraftState>, TimeInterpolator<SpacecraftState>) - Constructor for class org.orekit.propagation.conversion.EphemerisPropagatorBuilder
Constructor using the default attitude provider.
EphemerisPropagatorBuilder(List<SpacecraftState>, TimeInterpolator<SpacecraftState>, List<StateCovariance>, TimeInterpolator<TimeStampedPair<Orbit, StateCovariance>>) - Constructor for class org.orekit.propagation.conversion.EphemerisPropagatorBuilder
Constructor with covariances and default attitude provider.
EphemerisPropagatorBuilder(List<SpacecraftState>, TimeInterpolator<SpacecraftState>, List<StateCovariance>, TimeInterpolator<TimeStampedPair<Orbit, StateCovariance>>, AttitudeProvider) - Constructor for class org.orekit.propagation.conversion.EphemerisPropagatorBuilder
Constructor.
EphemerisPropagatorBuilder(List<SpacecraftState>, TimeInterpolator<SpacecraftState>, AttitudeProvider) - Constructor for class org.orekit.propagation.conversion.EphemerisPropagatorBuilder
Constructor.
EphemerisSegmentPropagator<C extends TimeStampedPVCoordinates> - Class in org.orekit.files.general
EphemerisSegmentPropagator(EphemerisFile.EphemerisSegment<C>, AttitudeProvider) - Constructor for class org.orekit.files.general.EphemerisSegmentPropagator
Create a Propagator from an ephemeris segment.
EPOCH - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Entry epoch.
EPOCH - org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternionKey
Epoch entry (only for ADM V1).
EPOCH - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey
Epoch entry (only for OEM files).
EPOCH - org.orekit.files.ccsds.ndm.odm.KeplerianElementsKey
Epoch of Keplerian elements.
EPOCH - org.orekit.files.ccsds.ndm.odm.StateVectorKey
Epoch of state vector and optional Keplerian elements.
EPOCH - org.orekit.files.ccsds.ndm.tdm.TdmDataKey
Epoch entry.
EPOCH_TZERO - org.orekit.files.ccsds.ndm.adm.acm.AcmMetadataKey
Default epoch to which all relative times are referenced in data blocks, unless overridden by block-specific AcmMetadataKey.EPOCH_TZERO values.
EPOCH_TZERO - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Default epoch to which all relative times are referenced in data blocks, unless overridden by block-specific OcmMetadataKey.EPOCH_TZERO values.
EpochDerivativesEquations - Class in org.orekit.propagation.numerical
Computes derivatives of the acceleration, including ThirdBodyAttraction.
EpochDerivativesEquations(String, NumericalPropagator) - Constructor for class org.orekit.propagation.numerical.EpochDerivativesEquations
Simple constructor.
EPSILON_DEFAULT - Static variable in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Default convergence threshold for mean parameters conversion.
EPSILON_DEFAULT - Static variable in class org.orekit.propagation.analytical.tle.generation.FixedPointTleGenerationAlgorithm
Default value for epsilon.
equals(Object) - Method in class org.orekit.bodies.FieldGeodeticPoint
 
equals(Object) - Method in class org.orekit.bodies.GeodeticPoint
 
equals(Object) - Method in class org.orekit.estimation.measurements.ObservableSatellite
equals(Object) - Method in class org.orekit.files.ilrs.CRDConfiguration.BaseConfiguration
 
equals(Object) - Method in class org.orekit.gnss.SatInSystem
 
equals(Object) - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityDataLoader.LineParameters
Check if the instance represents the same parameters as given line parameters.
equals(Object) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
Check if the instance represents the same parameters as given line parameters.
equals(Object) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimationLoader.LineParameters
Check if the instance represents the same parameters as given line parameters.
equals(Object) - Method in class org.orekit.models.earth.displacement.Tide
 
equals(Object) - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Check if this tle equals the provided tle.
equals(Object) - Method in class org.orekit.propagation.analytical.tle.TLE
Check if this tle equals the provided tle.
equals(Object) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey
equals(Object) - Method in class org.orekit.time.AbsoluteDate
Check if the instance represents the same time as another instance.
equals(Object) - Method in class org.orekit.time.DateComponents
equals(Object) - Method in class org.orekit.time.DateTimeComponents
equals(Object) - Method in class org.orekit.time.FieldAbsoluteDate
Check if the instance represents the same time as another instance.
equals(Object) - Method in class org.orekit.time.TimeComponents
equals(Object) - Method in class org.orekit.utils.units.Unit
Check if the instance represents the same unit as another instance.
EQUATORIAL_RADIUS - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey
Oblate spheroid equatorial radius of central body.
EQUINOCTIAL - org.orekit.files.ccsds.ndm.odm.ocm.OrbitElementsType
Equinoctial elements (a, af, ag, L=M+ω+frΩ, χ, ψ, fr).
EQUINOCTIAL - org.orekit.orbits.OrbitType
Type for orbital representation in EquinoctialOrbit and FieldEquinoctialOrbit parameters.
EquinoctialLongitudeArgumentUtility - Class in org.orekit.orbits
Utility methods for converting between different longitude arguments used by EquinoctialOrbit.
EQUINOCTIALMOD - org.orekit.files.ccsds.ndm.odm.ocm.OrbitElementsType
Modified equinoctial elements (p=a(1−e²), af, ag, L'=υ+ω+frΩ, χ, ψ, fr).
EquinoctialOrbit - Class in org.orekit.orbits
This class handles equinoctial orbital parameters, which can support both circular and equatorial orbits.
EquinoctialOrbit(double, double, double, double, double, double, double, double, double, double, double, double, PositionAngleType, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit
Creates a new instance with derivatives and with cached position angle same as value inputted.
EquinoctialOrbit(double, double, double, double, double, double, double, double, double, double, double, double, PositionAngleType, PositionAngleType, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit
Creates a new instance.
EquinoctialOrbit(double, double, double, double, double, double, PositionAngleType, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit
Creates a new instance without derivatives and with cached position angle same as value inputted.
EquinoctialOrbit(double, double, double, double, double, double, PositionAngleType, PositionAngleType, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit
Creates a new instance.
EquinoctialOrbit(Orbit) - Constructor for class org.orekit.orbits.EquinoctialOrbit
Constructor from any kind of orbital parameters.
EquinoctialOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit
Constructor from Cartesian parameters.
EquinoctialOrbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit
Constructor from Cartesian parameters.
EQW - org.orekit.frames.LOFType
Constant for Equinoctial Coordinate System (X axis aligned with ascending node, Z axis aligned with orbital momentum).
EQW_INERTIAL - org.orekit.files.ccsds.definitions.OrbitRelativeFrame
Equinoctial coordinate system (X towards ascending node, Z towards momentum).
ErrorState - Class in org.orekit.files.ccsds.utils.parsing
Special ProcessingState that always generate an error message.
ErrorState() - Constructor for class org.orekit.files.ccsds.utils.parsing.ErrorState
Empty constructor.
ESA - org.orekit.files.ccsds.definitions.SpacecraftBodyFrame.BaseEquipment
Earth Sensor Assembly.
ESO - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCategory
Escape Orbit.
estimate() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Estimate the orbital, propagation and measurements parameters.
estimate(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Estimate the theoretical value of the measurement, with derivatives.
estimate(int, int, SpacecraftState[]) - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
Estimate the theoretical value of the measurement, with derivatives.
estimate(Frame, boolean, int, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate) - Method in class org.orekit.estimation.iod.IodLambert
Estimate a Keplerian orbit given two position vectors and a duration.
estimate(Frame, boolean, int, Position, Position) - Method in class org.orekit.estimation.iod.IodLambert
Estimate an initial orbit from two position measurements.
estimate(Frame, boolean, int, PV, PV) - Method in class org.orekit.estimation.iod.IodLambert
Estimate an initial orbit from two PV measurements.
estimate(Frame, Vector3D, Vector3D, Vector3D, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate, double, double) - Method in class org.orekit.estimation.iod.IodGooding
Estimate orbit from three line of sight.
estimate(Frame, Vector3D, Vector3D, Vector3D, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate, double, double, int, boolean) - Method in class org.orekit.estimation.iod.IodGooding
Estimate orbit from three line of sight.
estimate(Frame, Vector3D, AbsoluteDate, Vector3D, Vector3D, AbsoluteDate, Vector3D, Vector3D, AbsoluteDate, Vector3D) - Method in class org.orekit.estimation.iod.IodGauss
Estimate and orbit based on Gauss Intial Orbit Determination method.
estimate(Frame, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate) - Method in class org.orekit.estimation.iod.IodGibbs
Give an initial orbit estimation, assuming Keplerian motion.
estimate(Frame, AngularAzEl, AngularAzEl, AngularAzEl) - Method in class org.orekit.estimation.iod.IodGauss
Estimate and orbit based on Gauss Intial Orbit Determination method.
estimate(Frame, AngularAzEl, AngularAzEl, AngularAzEl) - Method in class org.orekit.estimation.iod.IodLaplace
Estimate the orbit from three angular observations at the same location.
estimate(Frame, AngularAzEl, AngularAzEl, AngularAzEl, double, double) - Method in class org.orekit.estimation.iod.IodGooding
Estimate orbit from three angular observations.
estimate(Frame, AngularAzEl, AngularAzEl, AngularAzEl, double, double, int, boolean) - Method in class org.orekit.estimation.iod.IodGooding
Estimate orbit from three angular observations.
estimate(Frame, AngularRaDec, AngularRaDec, AngularRaDec) - Method in class org.orekit.estimation.iod.IodGauss
Estimate and orbit based on Gauss Intial Orbit Determination method.
estimate(Frame, AngularRaDec, AngularRaDec, AngularRaDec) - Method in class org.orekit.estimation.iod.IodLaplace
Estimate the orbit from three angular observations at the same location.
estimate(Frame, AngularRaDec, AngularRaDec, AngularRaDec, double, double) - Method in class org.orekit.estimation.iod.IodGooding
Estimate orbit from three angular observations.
estimate(Frame, AngularRaDec, AngularRaDec, AngularRaDec, double, double, int, boolean) - Method in class org.orekit.estimation.iod.IodGooding
Estimate orbit from three angular observations.
estimate(Frame, Position, Position, Position) - Method in class org.orekit.estimation.iod.IodGibbs
Give an initial orbit estimation, assuming Keplerian motion.
estimate(Frame, PV, PV, PV) - Method in class org.orekit.estimation.iod.IodGibbs
Give an initial orbit estimation, assuming Keplerian motion.
estimate(Frame, PVCoordinates, AbsoluteDate, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate, Vector3D) - Method in class org.orekit.estimation.iod.IodLaplace
Estimate orbit from three line of sight angles at the same location.
EstimatedEarthFrameProvider - Class in org.orekit.estimation.measurements
Class modeling an Earth frame whose Earth Orientation Parameters can be estimated.
EstimatedEarthFrameProvider(UT1Scale) - Constructor for class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
Build an estimated Earth frame.
EstimatedIonosphericModel - Class in org.orekit.models.earth.ionosphere
An estimated ionospheric model.
EstimatedIonosphericModel(IonosphericMappingFunction, double) - Constructor for class org.orekit.models.earth.ionosphere.EstimatedIonosphericModel
Build a new instance.
EstimatedMeasurement<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements
Class holding an estimated theoretical value associated to an observed measurement.
EstimatedMeasurement(EstimatedMeasurementBase<T>) - Constructor for class org.orekit.estimation.measurements.EstimatedMeasurement
Constructor from measurement base.
EstimatedMeasurement(T, int, int, SpacecraftState[], TimeStampedPVCoordinates[]) - Constructor for class org.orekit.estimation.measurements.EstimatedMeasurement
Simple constructor.
EstimatedMeasurementBase<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements
Class holding an estimated theoretical value associated to an observed measurement.
EstimatedMeasurementBase(T, int, int, SpacecraftState[], TimeStampedPVCoordinates[]) - Constructor for class org.orekit.estimation.measurements.EstimatedMeasurementBase
Simple constructor.
EstimatedMeasurementBase.Status - Enum in org.orekit.estimation.measurements
Enumerate for the status of the measurement.
estimatedMeasurementsParameters(ParameterDriversList, CovarianceMatrixProvider) - Method in class org.orekit.estimation.sequential.KalmanEstimatorBuilder
Configure the estimated measurement parameters.
estimatedMeasurementsParameters(ParameterDriversList, CovarianceMatrixProvider) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimatorBuilder
Configure the estimated measurement parameters.
estimatedMeasurementsParameters(ParameterDriversList, CovarianceMatrixProvider) - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanEstimatorBuilder
Configure the estimated measurement parameters.
estimatedMeasurementsParameters(ParameterDriversList, CovarianceMatrixProvider) - Method in class org.orekit.estimation.sequential.UnscentedKalmanEstimatorBuilder
Configure the estimated measurement parameters.
EstimatedModel - Class in org.orekit.models.earth.troposphere
An estimated tropospheric model.
EstimatedModel(double, double, double, TroposphereMappingFunction, double) - Constructor for class org.orekit.models.earth.troposphere.EstimatedModel
Build a new instance using the given environmental conditions.
EstimatedModel(TroposphereMappingFunction, double) - Constructor for class org.orekit.models.earth.troposphere.EstimatedModel
Build a new instance using a standard atmosphere model.
EstimatedModel(TroposphericModel, TroposphereMappingFunction, double) - Constructor for class org.orekit.models.earth.troposphere.EstimatedModel
Build a new instance using the given environmental conditions.
EstimatedTroposphericModel - Class in org.orekit.models.earth.troposphere
Deprecated.
as of 12.1, replaced by EstimatedModel
EstimatedTroposphericModel(double, double, MappingFunction, double) - Constructor for class org.orekit.models.earth.troposphere.EstimatedTroposphericModel
Deprecated.
Build a new instance using the given environmental conditions.
EstimatedTroposphericModel(DiscreteTroposphericModel, MappingFunction, double) - Constructor for class org.orekit.models.earth.troposphere.EstimatedTroposphericModel
Deprecated.
Build a new instance using the given environmental conditions.
EstimatedTroposphericModel(MappingFunction, double) - Constructor for class org.orekit.models.earth.troposphere.EstimatedTroposphericModel
Deprecated.
Build a new instance using a standard atmosphere model.
estimateRate(FieldRotation<T>, FieldRotation<T>, double) - Static method in class org.orekit.utils.FieldAngularCoordinates
Estimate rotation rate between two orientations.
estimateRate(FieldRotation<T>, FieldRotation<T>, T) - Static method in class org.orekit.utils.FieldAngularCoordinates
Estimate rotation rate between two orientations.
estimateRate(Rotation, Rotation, double) - Static method in class org.orekit.utils.AngularCoordinates
Estimate rotation rate between two orientations.
estimateVelocity(FieldVector3D<T>, FieldVector3D<T>, double) - Static method in class org.orekit.utils.FieldPVCoordinates
Estimate velocity between two positions.
estimateVelocity(Vector3D, Vector3D, double) - Static method in class org.orekit.utils.PVCoordinates
Estimate velocity between two positions.
estimateWithoutDerivatives(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Estimate the theoretical value of the measurement, without derivatives.
estimateWithoutDerivatives(int, int, SpacecraftState[]) - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
Estimate the theoretical value of the measurement, without derivatives.
estimateWithoutDerivatives(SpacecraftState[]) - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
Estimate the theoretical value of the measurement, without derivatives.
EstimationModifier<T extends ObservedMeasurement<T>> - Interface in org.orekit.estimation.measurements
Interface for estimated measurements modifiers used for orbit determination.
EstimationsProvider - Interface in org.orekit.estimation.measurements
Interface for retrieving estimated measurements during orbit determination.
estimationStep(ObservedMeasurement<?>) - Method in class org.orekit.estimation.sequential.KalmanEstimator
Process a single measurement.
estimationStep(ObservedMeasurement<?>) - Method in class org.orekit.estimation.sequential.UnscentedKalmanEstimator
Process a single measurement.
estimationTypeChanged(boolean, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver
Notify that a parameter estimation type (continuous or step) has been changed.
eta - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
eta from SPTRCK #3.
eta - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
eta from SPTRCK #3.
etasq - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
eta squared.
etasq - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
eta squared.
Euler - Class in org.orekit.files.ccsds.ndm.adm.apm
Container for Euler rotations entries.
Euler() - Constructor for class org.orekit.files.ccsds.ndm.adm.apm.Euler
Simple constructor.
EULER_ANGLE - org.orekit.files.ccsds.ndm.adm.AttitudeType
Euler angles.
EULER_ANGLE_ANGVEL - org.orekit.files.ccsds.ndm.adm.AttitudeType
Euler angles and angular velocity.
EULER_ANGLE_DERIVATIVE - org.orekit.files.ccsds.ndm.adm.AttitudeType
Euler angles and rotation rate.
EULER_ANGLES - org.orekit.files.ccsds.ndm.adm.acm.AttitudeElementsType
Euler angles.
EULER_DIR - org.orekit.files.ccsds.ndm.adm.apm.EulerKey
Rotation direction entry (ADM V1 only).
EULER_FRAME_A - org.orekit.files.ccsds.ndm.adm.apm.EulerKey
First reference frame entry (only for ADM V1).
EULER_FRAME_B - org.orekit.files.ccsds.ndm.adm.apm.EulerKey
Second reference frame entry (only for ADM V1).
EULER_RATE - org.orekit.files.ccsds.ndm.adm.acm.RateElementsType
Euler rates.
EULER_ROT_SEQ - org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationKey
Rotation sequence entry.
EULER_ROT_SEQ - org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadataKey
Rotation sequence entry.
EULER_ROT_SEQ - org.orekit.files.ccsds.ndm.adm.aem.AemMetadataKey
Rotation order entry for Euler angles.
EULER_ROT_SEQ - org.orekit.files.ccsds.ndm.adm.apm.EulerKey
Rotation sequence entry.
eulerAngle - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Euler angle sub-section.
eulerAngleAngVel - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Euler angle/angular velocity sub-section.
eulerAngleDerivative - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Euler angle/derivative sub-section.
eulerAngleRate - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Euler angle/rate sub-section (only for ADM V1).
EulerFieldIntegratorBuilder<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.conversion
Builder for EulerFieldIntegrator.
EulerFieldIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.EulerFieldIntegratorBuilder
Constructor.
EulerFieldIntegratorBuilder(T) - Constructor for class org.orekit.propagation.conversion.EulerFieldIntegratorBuilder
Constructor using a "fielded" step.
EulerIntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for EulerIntegrator.
EulerIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.EulerIntegratorBuilder
Build a new instance.
EulerKey - Enum in org.orekit.files.ccsds.ndm.adm.apm
Keys for APM Euler angles entries.
evaluate(FieldVector3D<T>) - Method in enum org.orekit.forces.maneuvers.Control3DVectorCostType
Evaluate the cost of the input seen as a 3D control vector.
evaluate(Vector3D) - Method in enum org.orekit.forces.maneuvers.Control3DVectorCostType
Evaluate the cost of the input seen as a 3D control vector.
evaluate(GroundStation, FieldSpacecraftState<Gradient>, Gradient[]) - Method in interface org.orekit.estimation.measurements.modifiers.ParametricModelEffectGradient
Evaluate the parametric model effect.
evaluate(GroundStation, SpacecraftState) - Method in interface org.orekit.estimation.measurements.modifiers.ParametricModelEffect
Evaluate the parametric model effect.
evaluateAll(AbsoluteDate) - Method in class org.orekit.data.FundamentalNutationArguments
Evaluate all fundamental arguments for the current date (Delaunay plus planetary).
evaluateAll(FieldAbsoluteDate<T>) - Method in class org.orekit.data.FundamentalNutationArguments
Evaluate all fundamental arguments for the current date (Delaunay plus planetary).
evaluateHamiltonian(FieldSpacecraftState<T>) - Method in class org.orekit.control.indirect.adjoint.FieldCartesianAdjointDerivativesProvider
Evaluate the Hamiltonian from Pontryagin's Maximum Principle.
evaluateHamiltonian(SpacecraftState) - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointDerivativesProvider
Evaluate the Hamiltonian from Pontryagin's Maximum Principle.
evaluateStep(FieldOrekitStepInterpolator<T>) - Method in class org.orekit.propagation.events.FieldEventState
Evaluate the impact of the proposed step on the event detector.
evaluateStep(OrekitStepInterpolator) - Method in class org.orekit.propagation.events.EventState
Evaluate the impact of the proposed step on the event detector.
evaluateTC(AbsoluteDate) - Method in enum org.orekit.utils.IERSConventions
Evaluate the date offset between the current date and the reference date.
evaluateTC(AbsoluteDate, TimeScales) - Method in enum org.orekit.utils.IERSConventions
Evaluate the date offset between the current date and the reference date.
evaluateTC(FieldAbsoluteDate<T>) - Method in enum org.orekit.utils.IERSConventions
Evaluate the date offset between the current date and the reference date.
evaluateTC(FieldAbsoluteDate<T>, TimeScales) - Method in enum org.orekit.utils.IERSConventions
Evaluate the date offset between the current date and the reference date.
evaluationPerformed(int, int, Orbit[], ParameterDriversList, ParameterDriversList, ParameterDriversList, EstimationsProvider, LeastSquaresProblem.Evaluation) - Method in interface org.orekit.estimation.leastsquares.BatchLSObserver
Notification callback for the end of each evaluation.
evaluationPerformed(KalmanEstimation) - Method in interface org.orekit.estimation.sequential.KalmanObserver
Notification callback after each one of a Kalman filter estimation.
EVENT_DATE_TOO_CLOSE - org.orekit.errors.OrekitMessages
EVENT_DATE_TOO_CLOSE.
EventBasedScheduler<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.generation
Scheduler based on EventDetector for generating measurements sequences.
EventBasedScheduler(MeasurementBuilder<T>, DatesSelector, Propagator, EventDetector, SignSemantic) - Constructor for class org.orekit.estimation.measurements.generation.EventBasedScheduler
Simple constructor.
EventDetectionSettings - Class in org.orekit.propagation.events
Class containing parameters for event detection.
EventDetectionSettings(double, double, int) - Constructor for class org.orekit.propagation.events.EventDetectionSettings
Constructor with maximum check as double.
EventDetectionSettings(AdaptableInterval, double, int) - Constructor for class org.orekit.propagation.events.EventDetectionSettings
Constructor.
EventDetector - Interface in org.orekit.propagation.events
This interface represents space-dynamics aware events detectors.
EventDetectorsProvider - Interface in org.orekit.propagation.events
Interface for building event detectors for force models and maneuver parameters.
EventEnablingPredicateFilter - Class in org.orekit.propagation.events
Wrapper used to detect events only when enabled by an external predicated function.
EventEnablingPredicateFilter(AdaptableInterval, double, int, EventHandler, EventDetector, EnablingPredicate) - Constructor for class org.orekit.propagation.events.EventEnablingPredicateFilter
Protected constructor with full parameters.
EventEnablingPredicateFilter(EventDetector, EnablingPredicate) - Constructor for class org.orekit.propagation.events.EventEnablingPredicateFilter
EventHandler - Interface in org.orekit.propagation.events.handlers
An interface defining how to handle events occurring during propagation.
eventIsEnabled(FieldSpacecraftState<T>, FieldEventDetector<T>, T) - Method in interface org.orekit.propagation.events.FieldEnablingPredicate
Compute an event enabling function of state.
eventIsEnabled(SpacecraftState, EventDetector, double) - Method in interface org.orekit.propagation.events.EnablingPredicate
Compute an event enabling function of state.
EventMultipleHandler - Class in org.orekit.propagation.events.handlers
Facade handlers that allows to use several handlers for one detector.
EventMultipleHandler() - Constructor for class org.orekit.propagation.events.handlers.EventMultipleHandler
Constructor with list initialisation.
eventOccurred(FieldSpacecraftState<T>, FieldEventDetector<T>, boolean) - Method in class org.orekit.propagation.events.handlers.FieldContinueOnEvent
Specific implementation of the eventOccurred interface.
eventOccurred(FieldSpacecraftState<T>, FieldEventDetector<T>, boolean) - Method in interface org.orekit.propagation.events.handlers.FieldEventHandler
Handle an event.
eventOccurred(FieldSpacecraftState<T>, FieldEventDetector<T>, boolean) - Method in class org.orekit.propagation.events.handlers.FieldRecallLastOccurrence
Handle an event.
eventOccurred(FieldSpacecraftState<T>, FieldEventDetector<T>, boolean) - Method in class org.orekit.propagation.events.handlers.FieldRecordAndContinue
 
eventOccurred(FieldSpacecraftState<T>, FieldEventDetector<T>, boolean) - Method in class org.orekit.propagation.events.handlers.FieldResetDerivativesOnEvent
Specific implementation of the eventOccurred interface.
eventOccurred(FieldSpacecraftState<T>, FieldEventDetector<T>, boolean) - Method in class org.orekit.propagation.events.handlers.FieldStopOnDecreasing
Handle a detection event and choose what to do next.
eventOccurred(FieldSpacecraftState<T>, FieldEventDetector<T>, boolean) - Method in class org.orekit.propagation.events.handlers.FieldStopOnEvent
Specific implementation of the eventOccurred interface.
eventOccurred(FieldSpacecraftState<T>, FieldEventDetector<T>, boolean) - Method in class org.orekit.propagation.events.handlers.FieldStopOnIncreasing
Handle a detection event and choose what to do next.
eventOccurred(SpacecraftState, EventDetector, boolean) - Method in class org.orekit.attitudes.AttitudesSequence.Switch
Handle an event.
eventOccurred(SpacecraftState, EventDetector, boolean) - Method in class org.orekit.propagation.events.handlers.ContinueOnEvent
Specific implementation of the eventOccurred interface.
eventOccurred(SpacecraftState, EventDetector, boolean) - Method in interface org.orekit.propagation.events.handlers.EventHandler
Handle an event.
eventOccurred(SpacecraftState, EventDetector, boolean) - Method in class org.orekit.propagation.events.handlers.EventMultipleHandler
Handle an event.
eventOccurred(SpacecraftState, EventDetector, boolean) - Method in class org.orekit.propagation.events.handlers.RecallLastOccurrence
Handle an event.
eventOccurred(SpacecraftState, EventDetector, boolean) - Method in class org.orekit.propagation.events.handlers.RecordAndContinue
 
eventOccurred(SpacecraftState, EventDetector, boolean) - Method in class org.orekit.propagation.events.handlers.ResetDerivativesOnEvent
Specific implementation of the eventOccurred interface.
eventOccurred(SpacecraftState, EventDetector, boolean) - Method in class org.orekit.propagation.events.handlers.StopOnDecreasing
Handle a detection event and choose what to do next.
eventOccurred(SpacecraftState, EventDetector, boolean) - Method in class org.orekit.propagation.events.handlers.StopOnEvent
Specific implementation of the eventOccurred interface.
eventOccurred(SpacecraftState, EventDetector, boolean) - Method in class org.orekit.propagation.events.handlers.StopOnIncreasing
Handle a detection event and choose what to do next.
EventShifter - Class in org.orekit.propagation.events
Wrapper shifting events occurrences times.
EventShifter(AdaptableInterval, double, int, EventHandler, EventDetector, boolean, double, double) - Constructor for class org.orekit.propagation.events.EventShifter
Protected constructor with full parameters.
EventShifter(EventDetector, boolean, double, double) - Constructor for class org.orekit.propagation.events.EventShifter
Build a new instance.
EventsLogger - Class in org.orekit.propagation.events
This class logs events detectors events during propagation.
EventsLogger() - Constructor for class org.orekit.propagation.events.EventsLogger
Simple constructor.
EventsLogger.LoggedEvent - Class in org.orekit.propagation.events
Class for logged events entries.
EventSlopeFilter<T extends EventDetector> - Class in org.orekit.propagation.events
Wrapper used to detect only increasing or decreasing events.
EventSlopeFilter(AdaptableInterval, double, int, EventHandler, T, FilterType) - Constructor for class org.orekit.propagation.events.EventSlopeFilter
Protected constructor with full parameters.
EventSlopeFilter(T, FilterType) - Constructor for class org.orekit.propagation.events.EventSlopeFilter
EventState<T extends EventDetector> - Class in org.orekit.propagation.events
This class handles the state for one event detector during integration steps.
EventState(T) - Constructor for class org.orekit.propagation.events.EventState
Simple constructor.
EventState.EventOccurrence - Class in org.orekit.propagation.events
Class to hold the data related to an event occurrence that is needed to decide how to modify integration.
EXCEPTIONAL_DATA_CONTEXT - org.orekit.errors.OrekitMessages
EXCEPTIONAL_DATA_CONTEXT.
ExceptionalDataContext - Class in org.orekit.data
A data context that always throws a runtime exception when it's methods are used.
ExceptionalDataContext() - Constructor for class org.orekit.data.ExceptionalDataContext
Empty constructor.
exitSection() - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Exit last section.
exitSection() - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Exit last section.
exitSection() - Method in class org.orekit.files.ccsds.utils.generation.KvnGenerator
Exit last section.
exitSection() - Method in class org.orekit.files.ccsds.utils.generation.XmlGenerator
Exit last section.
exitSection(Generator) - Method in class org.orekit.files.ccsds.section.AbstractWriter
Exit the section.
EXP - org.orekit.models.earth.displacement.PsdCorrection.TimeEvolution
Exponential evolution.
expressCovarianceInDesiredOutput(Orbit, StateCovariance) - Method in class org.orekit.propagation.AbstractStateCovarianceInterpolator
Express covariance in output configuration defined at this instance construction.
EXT - org.orekit.files.sp3.SP3OrbitType
extrapolated or predicted.
extend(Gradient, int) - Method in class org.orekit.propagation.integration.AbstractGradientConverter
Add zero derivatives.
extend(FieldRotation<Gradient>, int) - Method in class org.orekit.propagation.integration.AbstractGradientConverter
Add zero derivatives.
extend(FieldVector3D<Gradient>, int) - Method in class org.orekit.propagation.integration.AbstractGradientConverter
Add zero derivatives.
extend(FieldAbsoluteDate<Gradient>, int) - Method in class org.orekit.propagation.integration.AbstractGradientConverter
Add zero derivatives.
EXTENDED_MISSION - org.orekit.files.ccsds.ndm.odm.ocm.OpsStatus
Object in extended mission.
ExtendedPositionProvider - Interface in org.orekit.utils
Interface for position providers (including for Field).
ExtendedPVCoordinatesProvider - Interface in org.orekit.utils
Interface for PV coordinates providers that also support fields.
ExtendedPVCoordinatesProviderAdapter - Class in org.orekit.utils
ExtendedPVCoordinatesProviderAdapter(Frame, ExtendedPVCoordinatesProvider, String) - Constructor for class org.orekit.utils.ExtendedPVCoordinatesProviderAdapter
Simple constructor.
extractAccelerationModelRange(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
Extract a range of the AccelerationModel map.
extractBits(int) - Method in class org.orekit.gnss.metric.parser.AbstractEncodedMessage
Extract the next n bits from the encoded message.
extractBits(int) - Method in interface org.orekit.gnss.metric.parser.EncodedMessage
Extract the next n bits from the encoded message.
extractClockModel() - Method in class org.orekit.files.sp3.SP3Ephemeris
Extract the clock model.
extractClockModel() - Method in class org.orekit.files.sp3.SP3Segment
Extract the clock model.
extractClockModel(int) - Method in class org.orekit.files.rinex.observation.RinexObservation
Extract the receiver clock model.
extractClockModel(String, int) - Method in class org.orekit.files.rinex.clock.RinexClock
Extract the clock model.
extractDragSensitiveRange(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.forces.drag.TimeSpanDragForce
Deprecated.
Extract a range of the DragSensitive map.
extractParameters(double[], AbsoluteDate) - Method in class org.orekit.forces.drag.TimeSpanDragForce
Deprecated.
Extract the proper parameter drivers' values from the array in input of the acceleration method.
extractParameters(double[], AbsoluteDate) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
Extract the proper parameter drivers' values from the array in input of the acceleration method.
extractParameters(double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedModel
Extract the proper parameter drivers' values from the array in input of the pathDelay method.
extractParameters(double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
Deprecated.
Extract the proper parameter drivers' values from the array in input of the pathDelay method.
extractParameters(double[], AbsoluteDate) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Extract the proper parameter drivers' values from the array in input of the updateShortPeriodTerms method.
extractParameters(T[], FieldAbsoluteDate<T>) - Method in class org.orekit.forces.drag.TimeSpanDragForce
Deprecated.
Extract the proper parameter drivers' values from the array in input of the acceleration method.
extractParameters(T[], FieldAbsoluteDate<T>) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
Extract the proper parameter drivers' values from the array in input of the acceleration method.
extractParameters(T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedModel
Extract the proper parameter drivers' values from the array in input of the pathDelay method.
extractParameters(T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
Deprecated.
Extract the proper parameter drivers' values from the array in input of the pathDelay method.
extractParameters(T[], FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Extract the proper parameter drivers' values from the array in input of the updateShortPeriodTerms method.
extractRange(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.utils.TimeSpanMap
Extract a range of the map.
ExtremumApproachDetector - Class in org.orekit.propagation.events
Finder for extremum approach events.
ExtremumApproachDetector(AdaptableInterval, double, int, EventHandler, PVCoordinatesProvider) - Constructor for class org.orekit.propagation.events.ExtremumApproachDetector
Constructor.
ExtremumApproachDetector(EventDetectionSettings, EventHandler, PVCoordinatesProvider) - Constructor for class org.orekit.propagation.events.ExtremumApproachDetector
Constructor.
ExtremumApproachDetector(PVCoordinatesProvider) - Constructor for class org.orekit.propagation.events.ExtremumApproachDetector
Constructor with default values.

F

F0 - Static variable in enum org.orekit.gnss.Frequency
Deprecated.
as of 12.1, replaced by GnssSignal.F0
F0 - Static variable in interface org.orekit.gnss.GnssSignal
Common frequency F0 in Hz (10.23 MHz).
FactoryManagedFrame - Class in org.orekit.frames
Base class for the predefined frames that are managed by Frames.
FactoryManagedFrame(Frame, TransformProvider, boolean, Predefined) - Constructor for class org.orekit.frames.FactoryManagedFrame
Simple constructor.
FAILED_AUTHENTICATION - org.orekit.errors.OrekitMessages
FAILED_AUTHENTICATION.
FDOA - Class in org.orekit.estimation.measurements
Class modeling a Frequency Difference of Arrival measurement with a satellite as emitter and two ground stations as receivers.
FDOA(GroundStation, GroundStation, double, AbsoluteDate, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.FDOA
Simple constructor.
FDOABuilder - Class in org.orekit.estimation.measurements.generation
Builder for FDOA measurements.
FDOABuilder(CorrelatedRandomVectorGenerator, GroundStation, GroundStation, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.FDOABuilder
Simple constructor.
FEASIBLE_MEASUREMENT_WHEN_NEGATIVE - org.orekit.estimation.measurements.generation.SignSemantic
Semantic for detectors that have negative g function when measurements are feasible.
FEASIBLE_MEASUREMENT_WHEN_POSITIVE - org.orekit.estimation.measurements.generation.SignSemantic
Semantic for detectors that have positive g function when measurements are feasible.
FEBRUARY - org.orekit.time.Month
February.
feed(String, DataLoader) - Method in class org.orekit.data.DataProvidersManager
Feed a data file loader by browsing all data providers.
feed(Pattern, DataLoader, DataProvidersManager) - Method in class org.orekit.data.AbstractListCrawler
Feed a data file loader by browsing the data collection.
feed(Pattern, DataLoader, DataProvidersManager) - Method in class org.orekit.data.ClasspathCrawler
Feed a data file loader by browsing the data collection.
feed(Pattern, DataLoader, DataProvidersManager) - Method in interface org.orekit.data.DataProvider
Feed a data file loader by browsing the data collection.
feed(Pattern, DataLoader, DataProvidersManager) - Method in class org.orekit.data.DirectoryCrawler
Feed a data file loader by browsing the data collection.
feed(Pattern, DataLoader, DataProvidersManager) - Method in class org.orekit.data.ZipJarCrawler
Feed a data file loader by browsing the data collection.
feed(DataLoader) - Method in class org.orekit.data.AbstractSelfFeedingLoader
FES_CHAT_EPSILON_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory
Default regular expression for FES C hat and epsilon tides files.
FES_CNM_SNM_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory
Default regular expression for FES Cnm, Snm tides files.
FES_HF_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory
Default regular expression for FES Hf tides files.
FESCHatEpsilonReader - Class in org.orekit.forces.gravity.potential
Reader for ocean tides files following the fes2004.dat format.
FESCHatEpsilonReader(String, double, double, OceanLoadDeformationCoefficients, Map<Integer, Double>) - Constructor for class org.orekit.forces.gravity.potential.FESCHatEpsilonReader
Simple constructor.
FESCnmSnmReader - Class in org.orekit.forces.gravity.potential
Reader for ocean tides files following the fes2004_Cnm-Snm.dat format.
FESCnmSnmReader(String, double) - Constructor for class org.orekit.forces.gravity.potential.FESCnmSnmReader
Simple constructor.
fetchByte() - Method in class org.orekit.gnss.metric.ntrip.StreamMonitor
Fetch the next byte from the message.
fetchByte() - Method in class org.orekit.gnss.metric.parser.AbstractEncodedMessage
Fetch the next byte from the message.
fetchByte() - Method in class org.orekit.gnss.metric.parser.ByteArrayEncodedMessage
Fetch the next byte from the message.
fetchByte() - Method in class org.orekit.gnss.metric.parser.HexadecimalSequenceEncodedMessage
Fetch the next byte from the message.
fetchByte() - Method in class org.orekit.gnss.metric.parser.InputStreamEncodedMessage
Fetch the next byte from the message.
fetchEvaluatedMeasurement(int, EstimatedMeasurement<?>) - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel
Fetch a measurement that was evaluated during propagation.
FIELD_TOO_LONG - org.orekit.errors.OrekitMessages
FIELD_TOO_LONG.
FieldAbsoluteDate<T extends CalculusFieldElement<T>> - Class in org.orekit.time
This class represents a specific instant in time.
FieldAbsoluteDate(Field<T>) - Constructor for class org.orekit.time.FieldAbsoluteDate
Create an instance with a default value (FieldAbsoluteDate.getJ2000Epoch(Field)).
FieldAbsoluteDate(Field<T>, int, int, int, int, int, double, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from a location in a time scale.
FieldAbsoluteDate(Field<T>, int, int, int, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from a location in a time scale.
FieldAbsoluteDate(Field<T>, int, Month, int, int, int, double, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from a location in a time scale.
FieldAbsoluteDate(Field<T>, int, Month, int, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from a location in a time scale.
FieldAbsoluteDate(Field<T>, String, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from a location (parsed from a string) in a time scale.
FieldAbsoluteDate(Field<T>, Instant) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from an instant in utc time scale.
FieldAbsoluteDate(Field<T>, Instant, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from an instant in a time scale.
FieldAbsoluteDate(Field<T>, Instant, UTCScale) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from an instant in the time scale.
FieldAbsoluteDate(Field<T>, Date, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from a location in a time scale.
FieldAbsoluteDate(Field<T>, AbsoluteDate) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from an AbsoluteDate.
FieldAbsoluteDate(Field<T>, DateComponents, TimeComponents, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from a location in a time scale.
FieldAbsoluteDate(Field<T>, DateComponents, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from a location in a time scale.
FieldAbsoluteDate(Field<T>, DateTimeComponents, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from a location in a time scale.
FieldAbsoluteDate(AbsoluteDate, long, TimeUnit, Field<T>) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from an elapsed duration since to another instant.
FieldAbsoluteDate(AbsoluteDate, T) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from an elapsed duration since to another instant.
FieldAbsoluteDate(FieldAbsoluteDate<T>, double) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from an elapsed duration since to another instant.
FieldAbsoluteDate(FieldAbsoluteDate<T>, double, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from an apparent clock offset with respect to another instant in the perspective of a specific time scale.
FieldAbsoluteDate(FieldAbsoluteDate<T>, long, TimeUnit) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from an elapsed duration since to another instant.
FieldAbsoluteDate(FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from an elapsed duration since to another instant.
FieldAbsolutePVCoordinates<T extends CalculusFieldElement<T>> - Class in org.orekit.utils
Field implementation of AbsolutePVCoordinates.
FieldAbsolutePVCoordinates(Field<T>, AbsolutePVCoordinates) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates
Build from Field and non-Fielded object.
FieldAbsolutePVCoordinates(Frame, FieldAbsoluteDate<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates
Build from position and velocity.
FieldAbsolutePVCoordinates(Frame, FieldAbsoluteDate<T>, FieldVector3D<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates
Build from position, velocity, acceleration.
FieldAbsolutePVCoordinates(Frame, FieldAbsoluteDate<T>, FieldVector3D<U>) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates
Builds a FieldAbsolutePVCoordinates triplet from a FieldVector3D<DerivativeStructure>.
FieldAbsolutePVCoordinates(Frame, FieldAbsoluteDate<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates
Build from frame, date and FieldPVA coordinates.
FieldAbsolutePVCoordinates(Frame, TimeStampedFieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates
Build from frame and TimeStampedFieldPVCoordinates.
FieldAbsolutePVCoordinates(FieldAbsoluteDate<T>, FieldAbsolutePVCoordinates<T>, FieldAbsolutePVCoordinates<T>) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates
Subtractive constructor
FieldAbsolutePVCoordinates(FieldAbsoluteDate<T>, T, FieldAbsolutePVCoordinates<T>) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates
Multiplicative constructor
FieldAbsolutePVCoordinates(FieldAbsoluteDate<T>, T, FieldAbsolutePVCoordinates<T>, T, FieldAbsolutePVCoordinates<T>) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates
Linear constructor
FieldAbsolutePVCoordinates(FieldAbsoluteDate<T>, T, FieldAbsolutePVCoordinates<T>, T, FieldAbsolutePVCoordinates<T>, T, FieldAbsolutePVCoordinates<T>) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates
Linear constructor
FieldAbsolutePVCoordinates(FieldAbsoluteDate<T>, T, FieldAbsolutePVCoordinates<T>, T, FieldAbsolutePVCoordinates<T>, T, FieldAbsolutePVCoordinates<T>, T, FieldAbsolutePVCoordinates<T>) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates
Linear constructor
FieldAbsolutePVCoordinatesHermiteInterpolator<KK extends CalculusFieldElement<KK>> - Class in org.orekit.utils
Class using a Hermite interpolator to interpolate absolute position-velocity-acceleration coordinates.
FieldAbsolutePVCoordinatesHermiteInterpolator(int, double, Frame, CartesianDerivativesFilter) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinatesHermiteInterpolator
Constructor.
FieldAbsolutePVCoordinatesHermiteInterpolator(int, Frame) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinatesHermiteInterpolator
Constructor with : Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of position and two time derivatives during interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).
FieldAbsolutePVCoordinatesHermiteInterpolator(int, Frame, CartesianDerivativesFilter) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinatesHermiteInterpolator
Constructor with default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s).
FieldAbsolutePVCoordinatesHermiteInterpolator(Frame) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinatesHermiteInterpolator
Constructor with : Default number of interpolation points of DEFAULT_INTERPOLATION_POINTS Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of position and two time derivatives during interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).
FieldAbstractAnalyticalPropagator<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical
Common handling of FieldPropagator methods for analytical propagators.
FieldAbstractAnalyticalPropagator(Field<T>, AttitudeProvider) - Constructor for class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Build a new instance.
FieldAbstractDetector<D extends FieldAbstractDetector<D,​T>,​T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events
Common parts shared by several orbital events finders.
FieldAbstractDetector(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Constructor for class org.orekit.propagation.events.FieldAbstractDetector
Deprecated.
as of 12.2
FieldAbstractDetector(FieldEventDetectionSettings<T>, FieldEventHandler<T>) - Constructor for class org.orekit.propagation.events.FieldAbstractDetector
Build a new instance.
FieldAbstractGaussianContributionContext<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.forces
This class is a container for the common "field" parameters used in AbstractGaussianContribution.
FieldAbstractIntegratedPropagator<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.integration
Common handling of FieldPropagator methods for both numerical and semi-analytical propagators.
FieldAbstractIntegratedPropagator(Field<T>, FieldODEIntegrator<T>, PropagationType) - Constructor for class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Build a new instance.
FieldAbstractIntegratedPropagator.MainStateEquations<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation.integration
Differential equations for the main state (orbit, attitude and mass).
FieldAbstractPropagator<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation
Common handling of Propagator methods for analytical propagators.
FieldAbstractPropagator(Field<T>) - Constructor for class org.orekit.propagation.FieldAbstractPropagator
Build a new instance.
FieldAbstractStateModifier<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation
Abstract base class for modifying state during propagation.
FieldAbstractStateModifier() - Constructor for class org.orekit.propagation.FieldAbstractStateModifier
 
FieldAdaptableInterval<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation.events
This interface represents an event checking interval that depends on state.
FieldAdapterDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events
Base class for adapting an existing detector.
FieldAdapterDetector(FieldEventDetector<T>) - Constructor for class org.orekit.propagation.events.FieldAdapterDetector
Build an adaptor wrapping an existing detector.
FieldAdditionalDerivativesProvider<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation.integration
Provider for additional derivatives.
FieldAdditionalStateProvider<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation
This interface allows to modify FieldSpacecraftState and set up additional state data.
FieldAltitudeDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events
Finder for satellite altitude crossing events.
FieldAltitudeDetector(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>, T, BodyShape) - Constructor for class org.orekit.propagation.events.FieldAltitudeDetector
Protected constructor with full parameters.
FieldAltitudeDetector(T, BodyShape) - Constructor for class org.orekit.propagation.events.FieldAltitudeDetector
Build a new altitude detector.
FieldAltitudeDetector(T, T, BodyShape) - Constructor for class org.orekit.propagation.events.FieldAltitudeDetector
Build a new altitude detector.
FieldAltitudeDetector(T, T, T, BodyShape) - Constructor for class org.orekit.propagation.events.FieldAltitudeDetector
Build a new altitude detector.
FieldAngularCoordinates<T extends CalculusFieldElement<T>> - Class in org.orekit.utils
Simple container for rotation / rotation rate pairs, using CalculusFieldElement.
FieldAngularCoordinates(Field<T>, AngularCoordinates) - Constructor for class org.orekit.utils.FieldAngularCoordinates
Builds a FieldAngularCoordinates from a field and a regular AngularCoordinates.
FieldAngularCoordinates(FieldRotation<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldAngularCoordinates
Builds a rotation/rotation rate pair.
FieldAngularCoordinates(FieldRotation<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldAngularCoordinates
Builds a rotation / rotation rate / rotation acceleration triplet.
FieldAngularCoordinates(FieldRotation<U>) - Constructor for class org.orekit.utils.FieldAngularCoordinates
Builds a FieldAngularCoordinates from a FieldRotation<FieldDerivativeStructure>.
FieldAngularCoordinates(FieldPVCoordinates<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>, double) - Constructor for class org.orekit.utils.FieldAngularCoordinates
Build the rotation that transforms a pair of pv coordinates into another one.
FieldApsideDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events
Finder for apside crossing events.
FieldApsideDetector(FieldOrbit<T>) - Constructor for class org.orekit.propagation.events.FieldApsideDetector
Build a new instance.
FieldApsideDetector(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Constructor for class org.orekit.propagation.events.FieldApsideDetector
Protected constructor with full parameters.
FieldApsideDetector(T) - Constructor for class org.orekit.propagation.events.FieldApsideDetector
Build a new instance.
FieldApsideDetector(T, FieldOrbit<T>) - Constructor for class org.orekit.propagation.events.FieldApsideDetector
Build a new instance.
FieldArrayDictionary<T extends CalculusFieldElement<T>> - Class in org.orekit.utils
String → CalculusFieldElement[] mapping, for small number of keys.
FieldArrayDictionary(Field<T>) - Constructor for class org.orekit.utils.FieldArrayDictionary
Constructor with default initial capacity.
FieldArrayDictionary(Field<T>, int) - Constructor for class org.orekit.utils.FieldArrayDictionary
Constructor with specified capacity.
FieldArrayDictionary(Field<T>, Map<String, T[]>) - Constructor for class org.orekit.utils.FieldArrayDictionary
Constructor from a map.
FieldArrayDictionary(FieldArrayDictionary<T>) - Constructor for class org.orekit.utils.FieldArrayDictionary
Constructor from another dictionary.
FieldArrayDictionary.Entry - Class in org.orekit.utils
Entry in a dictionary.
FieldAttitude<T extends CalculusFieldElement<T>> - Class in org.orekit.attitudes
This class handles attitude definition at a given date.
FieldAttitude(Field<T>, Attitude) - Constructor for class org.orekit.attitudes.FieldAttitude
Builds an instance for a regular Attitude.
FieldAttitude(Frame, TimeStampedFieldAngularCoordinates<T>) - Constructor for class org.orekit.attitudes.FieldAttitude
Creates a new instance.
FieldAttitude(FieldAbsoluteDate<T>, Frame, FieldRotation<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.attitudes.FieldAttitude
Creates a new instance.
FieldAttitude(FieldAbsoluteDate<T>, Frame, Rotation, Vector3D, Vector3D, Field<T>) - Constructor for class org.orekit.attitudes.FieldAttitude
Creates a new instance.
FieldAttitude(FieldAbsoluteDate<T>, Frame, FieldAngularCoordinates<T>) - Constructor for class org.orekit.attitudes.FieldAttitude
Creates a new instance.
FieldAttitudeInterpolator<KK extends CalculusFieldElement<KK>> - Class in org.orekit.attitudes
Class for attitude interpolation.
FieldAttitudeInterpolator(Frame, FieldTimeInterpolator<TimeStampedFieldAngularCoordinates<KK>, KK>) - Constructor for class org.orekit.attitudes.FieldAttitudeInterpolator
Constructor.
FieldAuxiliaryElements<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities
Container class for common parameters used by all DSST forces.
FieldAuxiliaryElements(FieldOrbit<T>, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Simple constructor.
FieldAzimuthalGradientCoefficients<T extends CalculusFieldElement<T>> - Class in org.orekit.models.earth.troposphere
Container for the azimuthal gradient coefficients gnh, geh, gnw and gew.
FieldAzimuthalGradientCoefficients(T, T, T, T) - Constructor for class org.orekit.models.earth.troposphere.FieldAzimuthalGradientCoefficients
Simple constructor.
FieldBetaAngleDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events
Finder for beta angle crossing events.
FieldBetaAngleDetector(Field<T>, T, FieldPVCoordinatesProvider<T>, Frame) - Constructor for class org.orekit.propagation.events.FieldBetaAngleDetector
Class constructor.
FieldBetaAngleDetector(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>, T, FieldPVCoordinatesProvider<T>, Frame) - Constructor for class org.orekit.propagation.events.FieldBetaAngleDetector
Protected constructor with full parameters.
FieldBetaAngleDetector(T) - Constructor for class org.orekit.propagation.events.FieldBetaAngleDetector
Solar beta angle constructor.
FieldBodiesElements<T extends CalculusFieldElement<T>> - Class in org.orekit.data
Elements of the bodies having an effect on nutation.
FieldBodiesElements(FieldAbsoluteDate<T>, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T) - Constructor for class org.orekit.data.FieldBodiesElements
Simple constructor.
FieldBooleanDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events
This class provides AND and OR operations for event detectors.
FieldBooleanDetector(List<FieldEventDetector<T>>, FieldBooleanDetector.Operator, FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Constructor for class org.orekit.propagation.events.FieldBooleanDetector
Private constructor with all the parameters.
FieldBoundedPropagator<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation
This interface is intended for ephemerides valid only during a time range.
FieldBrouwerLyddanePropagator<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical
This class propagates a FieldSpacecraftState using the analytical Brouwer-Lyddane model (from J2 to J5 zonal harmonics).
FieldBrouwerLyddanePropagator(FieldOrbit<T>, double, T, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Build a propagator from orbit and potential.
FieldBrouwerLyddanePropagator(FieldOrbit<T>, AttitudeProvider, double, T, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Build a propagator from orbit, attitude provider and potential.
FieldBrouwerLyddanePropagator(FieldOrbit<T>, AttitudeProvider, UnnormalizedSphericalHarmonicsProvider, double) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Build a propagator from orbit, attitude provider and potential provider.
FieldBrouwerLyddanePropagator(FieldOrbit<T>, AttitudeProvider, T, double, T, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Build a propagator from orbit, attitude provider, mass and potential.
FieldBrouwerLyddanePropagator(FieldOrbit<T>, AttitudeProvider, T, double, T, double, double, double, double, PropagationType, double) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Build a propagator from orbit, attitude provider, mass and potential.
FieldBrouwerLyddanePropagator(FieldOrbit<T>, AttitudeProvider, T, double, T, double, double, double, double, PropagationType, double, double, int) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Build a propagator from orbit, attitude provider, mass and potential.
FieldBrouwerLyddanePropagator(FieldOrbit<T>, AttitudeProvider, T, UnnormalizedSphericalHarmonicsProvider, double) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Build a propagator from orbit, attitude provider, mass and potential provider.
FieldBrouwerLyddanePropagator(FieldOrbit<T>, AttitudeProvider, T, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Private helper constructor.
FieldBrouwerLyddanePropagator(FieldOrbit<T>, AttitudeProvider, T, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, PropagationType, double) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Private helper constructor.
FieldBrouwerLyddanePropagator(FieldOrbit<T>, AttitudeProvider, T, UnnormalizedSphericalHarmonicsProvider, PropagationType, double) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Build a propagator from orbit, attitude provider, mass and potential provider.
FieldBrouwerLyddanePropagator(FieldOrbit<T>, UnnormalizedSphericalHarmonicsProvider, double) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Build a propagator from orbit and potential provider.
FieldBrouwerLyddanePropagator(FieldOrbit<T>, UnnormalizedSphericalHarmonicsProvider, PropagationType, double) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Build a propagator from orbit and potential provider.
FieldBrouwerLyddanePropagator(FieldOrbit<T>, T, double, T, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Build a propagator from orbit, mass and potential.
FieldBrouwerLyddanePropagator(FieldOrbit<T>, T, UnnormalizedSphericalHarmonicsProvider, double) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Build a propagator from orbit, mass and potential provider.
FieldCartesianAdjointDerivativesProvider<T extends CalculusFieldElement<T>> - Class in org.orekit.control.indirect.adjoint
Class defining the Field version of the adjoint dynamics for Cartesian coordinates, as defined in the Pontryagin Maximum Principle.
FieldCartesianAdjointDerivativesProvider(CartesianCost, CartesianAdjointEquationTerm...) - Constructor for class org.orekit.control.indirect.adjoint.FieldCartesianAdjointDerivativesProvider
Constructor.
FieldCartesianOrbit<T extends CalculusFieldElement<T>> - Class in org.orekit.orbits
This class holds Cartesian orbital parameters.
FieldCartesianOrbit(Field<T>, CartesianOrbit) - Constructor for class org.orekit.orbits.FieldCartesianOrbit
Constructor from Field and CartesianOrbit.
FieldCartesianOrbit(Field<T>, Orbit) - Constructor for class org.orekit.orbits.FieldCartesianOrbit
Constructor from Field and Orbit.
FieldCartesianOrbit(FieldOrbit<T>) - Constructor for class org.orekit.orbits.FieldCartesianOrbit
Constructor from any kind of orbital parameters.
FieldCartesianOrbit(FieldPVCoordinates<T>, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldCartesianOrbit
Constructor from Cartesian parameters.
FieldCartesianOrbit(TimeStampedFieldPVCoordinates<T>, Frame, T) - Constructor for class org.orekit.orbits.FieldCartesianOrbit
Constructor from Cartesian parameters.
FieldCellInterpolator<T extends CalculusFieldElement<T>> - Class in org.orekit.models.earth.weather
Interpolator within a grid cell.
FieldChronologicalComparator<KK extends CalculusFieldElement<KK>> - Class in org.orekit.time
Comparator for FieldTimeStamped instance.
FieldChronologicalComparator() - Constructor for class org.orekit.time.FieldChronologicalComparator
Simple constructor.
FieldCircularLatitudeArgumentUtility - Class in org.orekit.orbits
Utility methods for converting between different latitude arguments used by FieldCircularOrbit.
FieldCircularOrbit<T extends CalculusFieldElement<T>> - Class in org.orekit.orbits
This class handles circular orbital parameters.
FieldCircularOrbit(Field<T>, CircularOrbit) - Constructor for class org.orekit.orbits.FieldCircularOrbit
Constructor from Field and CircularOrbit.
FieldCircularOrbit(Field<T>, Orbit) - Constructor for class org.orekit.orbits.FieldCircularOrbit
Constructor from Field and Orbit.
FieldCircularOrbit(FieldOrbit<T>) - Constructor for class org.orekit.orbits.FieldCircularOrbit
Constructor from any kind of orbital parameters.
FieldCircularOrbit(FieldPVCoordinates<T>, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldCircularOrbit
Constructor from Cartesian parameters.
FieldCircularOrbit(TimeStampedFieldPVCoordinates<T>, Frame, T) - Constructor for class org.orekit.orbits.FieldCircularOrbit
Constructor from Cartesian parameters.
FieldCircularOrbit(T, T, T, T, T, T, PositionAngleType, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldCircularOrbit
Creates a new instance without derivatives and with cached position angle same as value inputted.
FieldCircularOrbit(T, T, T, T, T, T, PositionAngleType, PositionAngleType, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldCircularOrbit
Creates a new instance.
FieldCircularOrbit(T, T, T, T, T, T, T, T, T, T, T, T, PositionAngleType, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldCircularOrbit
Creates a new instance.
FieldCircularOrbit(T, T, T, T, T, T, T, T, T, T, T, T, PositionAngleType, PositionAngleType, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldCircularOrbit
Creates a new instance.
FieldCjSjCoefficient<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities
Compute the Sj(k, h) and the Cj(k, h) series and their partial derivatives with respect to k and h.
FieldCjSjCoefficient(T, T, Field<T>) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient
Cj(k, h) and Sj(k, h) constructor.
FieldClockOffset<T extends CalculusFieldElement<T>> - Class in org.orekit.time
Container for time stamped clock offset.
FieldClockOffset(FieldAbsoluteDate<T>, T, T, T) - Constructor for class org.orekit.time.FieldClockOffset
Simple constructor.
FieldClockOffsetHermiteInterpolator<T extends CalculusFieldElement<T>> - Class in org.orekit.time
bHermite interpolator of time stamped clock offsets.
FieldClockOffsetHermiteInterpolator(int) - Constructor for class org.orekit.time.FieldClockOffsetHermiteInterpolator
Constructor with default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s).
FieldClockOffsetHermiteInterpolator(int, double) - Constructor for class org.orekit.time.FieldClockOffsetHermiteInterpolator
Constructor.
FieldCombinedDerivatives<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.integration
Container for additional derivatives.
FieldCombinedDerivatives(T[], T[]) - Constructor for class org.orekit.propagation.integration.FieldCombinedDerivatives
Simple constructor.
FieldContinueOnEvent<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events.handlers
Event handler which will always return continue as a state.
FieldContinueOnEvent() - Constructor for class org.orekit.propagation.events.handlers.FieldContinueOnEvent
Empty constructor.
FieldCylindricalShadowEclipseDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events
Event detector for eclipses from a single, infinitely-distant light source, occulted by a spherical central body.
FieldCylindricalShadowEclipseDetector(ExtendedPositionProvider, T, FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>) - Constructor for class org.orekit.propagation.events.FieldCylindricalShadowEclipseDetector
Deprecated.
since 12.2
FieldCylindricalShadowEclipseDetector(ExtendedPositionProvider, T, FieldEventDetectionSettings<T>, FieldEventHandler<T>) - Constructor for class org.orekit.propagation.events.FieldCylindricalShadowEclipseDetector
Constructor.
FieldCylindricalShadowEclipseDetector(ExtendedPositionProvider, T, FieldEventHandler<T>) - Constructor for class org.orekit.propagation.events.FieldCylindricalShadowEclipseDetector
Constructor with default detection settings.
FieldDateDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events
Finder for date events.
FieldDateDetector(Field<T>, FieldTimeStamped<T>...) - Constructor for class org.orekit.propagation.events.FieldDateDetector
Build a new instance.
FieldDateDetector(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>, double, FieldTimeStamped<T>...) - Constructor for class org.orekit.propagation.events.FieldDateDetector
Protected constructor with full parameters.
FieldDeepSDP4<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical.tle
This class contains the methods that compute deep space perturbation terms.
FieldDeepSDP4(FieldTLE<T>, AttitudeProvider, T, Frame, T[]) - Constructor for class org.orekit.propagation.analytical.tle.FieldDeepSDP4
Constructor for a unique initial TLE.
FieldDeepSDP4(FieldTLE<T>, AttitudeProvider, T, T[]) - Constructor for class org.orekit.propagation.analytical.tle.FieldDeepSDP4
Constructor for a unique initial TLE.
FieldDelaunayArguments<T extends CalculusFieldElement<T>> - Class in org.orekit.data
Delaunay arguments used for nutation or tides.
FieldDelaunayArguments(FieldAbsoluteDate<T>, T, T, T, T, T, T, T, T, T, T, T, T, T) - Constructor for class org.orekit.data.FieldDelaunayArguments
Simple constructor.
FieldDSSTGravityContext<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.forces
This class is a container for the common parameters used in DSSTTesseral and DSSTZonal.
FieldDSSTJ2SquaredClosedFormContext<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.forces
This class is a container for the common parameters used in DSSTJ2SquaredClosedForm.
FieldDSSTJ2SquaredClosedFormContext(FieldAuxiliaryElements<T>, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTJ2SquaredClosedFormContext
Simple constructor.
FieldDSSTNewtonianAttractionContext<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.forces
This class is a container for the common "field" parameters used in DSSTNewtonianAttraction.
FieldDSSTPropagator<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst
This class propagates orbits using the DSST theory.
FieldDSSTPropagator(Field<T>, FieldODEIntegrator<T>) - Constructor for class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Create a new instance of DSSTPropagator.
FieldDSSTPropagator(Field<T>, FieldODEIntegrator<T>, AttitudeProvider) - Constructor for class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Create a new instance of DSSTPropagator.
FieldDSSTPropagator(Field<T>, FieldODEIntegrator<T>, PropagationType) - Constructor for class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Create a new instance of DSSTPropagator.
FieldDSSTPropagator(Field<T>, FieldODEIntegrator<T>, PropagationType, AttitudeProvider) - Constructor for class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Create a new instance of DSSTPropagator.
FieldDSSTTesseralContext<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.forces
This class is a container for the common "field" parameters used in DSSTTesseral.
FieldDSSTThirdBodyDynamicContext<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.forces
This class is a container for the common "field" parameters used in DSSTThirdBody.
FieldDSSTThirdBodyDynamicContext(FieldAuxiliaryElements<T>, CelestialBody, T[]) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext
Constructor.
FieldDSSTZonalContext<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.forces
This class is a container for the common "field" parameters used in DSSTZonal.
FieldEcksteinHechlerPropagator<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical
This class propagates a FieldSpacecraftState using the analytical Eckstein-Hechler model.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, double, T, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Build a propagator from FieldOrbit and potential.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, double, T, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Build a propagator from FieldOrbit, attitude provider and potential.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Build a propagator from FieldOrbit, attitude provider and potential provider.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, T, double, T, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Build a propagator from FieldOrbit, attitude provider, mass and potential.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, T, double, T, double, double, double, double, double, PropagationType) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Build a propagator from FieldOrbit, attitude provider, mass and potential.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, T, double, T, double, double, double, double, double, PropagationType, double, int) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Build a propagator from FieldOrbit, attitude provider, mass and potential.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, T, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Build a propagator from FieldOrbit, attitude provider, mass and potential provider.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, T, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Private helper constructor.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, T, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, PropagationType) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Private helper constructor.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, T, UnnormalizedSphericalHarmonicsProvider, PropagationType) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Build a propagator from orbit, attitude provider, mass and potential provider.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Build a propagator from FieldOrbit and potential provider.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, UnnormalizedSphericalHarmonicsProvider, PropagationType) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Build a propagator from orbit and potential provider.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, T, double, T, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Build a propagator from FieldOrbit, mass and potential.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, T, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Build a propagator from FieldOrbit, mass and potential provider.
FieldEclipseDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events
Finder for satellite eclipse related events.
FieldEclipseDetector(Field<T>, ExtendedPVCoordinatesProvider, double, OneAxisEllipsoid) - Constructor for class org.orekit.propagation.events.FieldEclipseDetector
Build a new eclipse detector.
FieldEclipseDetector(Field<T>, OccultationEngine) - Constructor for class org.orekit.propagation.events.FieldEclipseDetector
Build a new eclipse detector.
FieldEclipseDetector(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>, OccultationEngine, T, boolean) - Constructor for class org.orekit.propagation.events.FieldEclipseDetector
Protected constructor with full parameters.
FieldElevationDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events
Finder for satellite raising/setting events that allows for the setting of azimuth and/or elevation bounds or a ground azimuth/elevation mask input.
FieldElevationDetector(Field<T>, TopocentricFrame) - Constructor for class org.orekit.propagation.events.FieldElevationDetector
Creates an instance of Elevation detector based on passed in topocentric frame and the minimum elevation angle.
FieldElevationDetector(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>, double, ElevationMask, AtmosphericRefractionModel, TopocentricFrame) - Constructor for class org.orekit.propagation.events.FieldElevationDetector
Deprecated.
as of 12.2
FieldElevationDetector(FieldEventDetectionSettings<T>, FieldEventHandler<T>, double, ElevationMask, AtmosphericRefractionModel, TopocentricFrame) - Constructor for class org.orekit.propagation.events.FieldElevationDetector
Protected constructor with full parameters.
FieldElevationDetector(T, T, TopocentricFrame) - Constructor for class org.orekit.propagation.events.FieldElevationDetector
Creates an instance of Elevation detector based on passed in topocentric frame and overrides of default maximal checking interval and convergence threshold values.
FieldElevationExtremumDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events
Detector for elevation extremum with respect to a ground point.
FieldElevationExtremumDetector(Field<T>, TopocentricFrame) - Constructor for class org.orekit.propagation.events.FieldElevationExtremumDetector
Build a new detector.
FieldElevationExtremumDetector(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>, TopocentricFrame) - Constructor for class org.orekit.propagation.events.FieldElevationExtremumDetector
Protected constructor with full parameters.
FieldElevationExtremumDetector(T, T, TopocentricFrame) - Constructor for class org.orekit.propagation.events.FieldElevationExtremumDetector
Build a detector.
FieldEllipse<T extends CalculusFieldElement<T>> - Class in org.orekit.bodies
Model of a 2D ellipse in 3D space.
FieldEllipse(FieldVector3D<T>, FieldVector3D<T>, FieldVector3D<T>, T, T, Frame) - Constructor for class org.orekit.bodies.FieldEllipse
Simple constructor.
FieldEnablingPredicate<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation.events
This interface represents an event enabling predicate function.
FieldEphemerisGenerator<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation
Generator for ephemerides.
FieldEquinoctialLongitudeArgumentUtility - Class in org.orekit.orbits
Utility methods for converting between different longitude arguments used by FieldEquinoctialOrbit.
FieldEquinoctialOrbit<T extends CalculusFieldElement<T>> - Class in org.orekit.orbits
This class handles equinoctial orbital parameters, which can support both circular and equatorial orbits.
FieldEquinoctialOrbit(Field<T>, EquinoctialOrbit) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit
Constructor from Field and EquinoctialOrbit.
FieldEquinoctialOrbit(Field<T>, Orbit) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit
Constructor from Field and Orbit.
FieldEquinoctialOrbit(FieldOrbit<T>) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit
Constructor from any kind of orbital parameters.
FieldEquinoctialOrbit(FieldPVCoordinates<T>, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit
Constructor from Cartesian parameters.
FieldEquinoctialOrbit(TimeStampedFieldPVCoordinates<T>, Frame, T) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit
Constructor from Cartesian parameters.
FieldEquinoctialOrbit(T, T, T, T, T, T, PositionAngleType, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit
Creates a new instance.
FieldEquinoctialOrbit(T, T, T, T, T, T, PositionAngleType, PositionAngleType, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit
Creates a new instance.
FieldEquinoctialOrbit(T, T, T, T, T, T, T, T, T, T, T, T, PositionAngleType, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit
Creates a new instance.
FieldEquinoctialOrbit(T, T, T, T, T, T, T, T, T, T, T, T, PositionAngleType, PositionAngleType, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit
Creates a new instance.
FieldEventDetectionSettings<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events
Class containing parameters for event detection.
FieldEventDetectionSettings(double, T, int) - Constructor for class org.orekit.propagation.events.FieldEventDetectionSettings
Constructor with maximum check as double.
FieldEventDetectionSettings(Field<T>, EventDetectionSettings) - Constructor for class org.orekit.propagation.events.FieldEventDetectionSettings
Constructor from non-Field settings.
FieldEventDetectionSettings(FieldAdaptableInterval<T>, T, int) - Constructor for class org.orekit.propagation.events.FieldEventDetectionSettings
Constructor.
FieldEventDetector<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation.events
This interface represents space-dynamics aware events detectors.
FieldEventEnablingPredicateFilter<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events
Wrapper used to detect events only when enabled by an external predicated function.
FieldEventEnablingPredicateFilter(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>, FieldEventDetector<T>, FieldEnablingPredicate<T>) - Constructor for class org.orekit.propagation.events.FieldEventEnablingPredicateFilter
Protected constructor with full parameters.
FieldEventEnablingPredicateFilter(FieldEventDetector<T>, FieldEnablingPredicate<T>) - Constructor for class org.orekit.propagation.events.FieldEventEnablingPredicateFilter
FieldEventHandler<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation.events.handlers
An interface defining how to handle events occurring during propagation..
FieldEventsLogger<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events
This class logs events detectors events during propagation.
FieldEventsLogger() - Constructor for class org.orekit.propagation.events.FieldEventsLogger
Simple constructor.
FieldEventsLogger.FieldLoggedEvent<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events
Class for logged events entries.
FieldEventSlopeFilter<D extends FieldEventDetector<T>,​T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events
Wrapper used to detect only increasing or decreasing events.
FieldEventSlopeFilter(D, FilterType) - Constructor for class org.orekit.propagation.events.FieldEventSlopeFilter
FieldEventSlopeFilter(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>, D, FilterType) - Constructor for class org.orekit.propagation.events.FieldEventSlopeFilter
Protected constructor with full parameters.
FieldEventState<D extends FieldEventDetector<T>,​T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events
This class handles the state for one event detector during integration steps.
FieldEventState(D) - Constructor for class org.orekit.propagation.events.FieldEventState
Simple constructor.
FieldEventState.EventOccurrence<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events
Class to hold the data related to an event occurrence that is needed to decide how to modify integration.
FieldExtremumApproachDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events
Finder for extremum approach events.
FieldExtremumApproachDetector(Field<T>, FieldPVCoordinatesProvider<T>) - Constructor for class org.orekit.propagation.events.FieldExtremumApproachDetector
Constructor with default values.
FieldExtremumApproachDetector(Field<T>, PVCoordinatesProvider) - Constructor for class org.orekit.propagation.events.FieldExtremumApproachDetector
Constructor with default values.
FieldExtremumApproachDetector(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>, FieldPVCoordinatesProvider<T>) - Constructor for class org.orekit.propagation.events.FieldExtremumApproachDetector
Constructor.
FieldExtremumApproachDetector(T, T, int, FieldEventHandler<T>, FieldPVCoordinatesProvider<T>) - Constructor for class org.orekit.propagation.events.FieldExtremumApproachDetector
Constructor.
FieldFixedNumberInterpolationGrid<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities
Interpolation grid where a fixed number of points are evenly spaced between the start and the end of the integration step.
FieldFixedNumberInterpolationGrid(Field<T>, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FieldFixedNumberInterpolationGrid
Constructor.
FieldForceModelContext<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.forces
Base class for dsst force models parameter containers.
FieldForceModelContext(FieldAuxiliaryElements<T>) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.FieldForceModelContext
Simple constructor.
FieldFunctionalDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events
A detector that implements the FieldFunctionalDetector.g(FieldSpacecraftState) function using a lambda that can be set using FieldFunctionalDetector.withFunction(Function).
FieldFunctionalDetector(Field<T>) - Constructor for class org.orekit.propagation.events.FieldFunctionalDetector
Create an event detector with the default values.
FieldFunctionalDetector(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>, Function<FieldSpacecraftState<T>, T>) - Constructor for class org.orekit.propagation.events.FieldFunctionalDetector
Private constructor.
FieldGammaMnsFunction<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities
Compute the Γmn,s(γ) function from equation 2.7.1-(13).
FieldGammaMnsFunction(int, T, int, Field<T>) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FieldGammaMnsFunction
Simple constructor.
FieldGeodeticPoint<T extends CalculusFieldElement<T>> - Class in org.orekit.bodies
Point location relative to a 2D body surface, using CalculusFieldElement.
FieldGeodeticPoint(Field<T>, GeodeticPoint) - Constructor for class org.orekit.bodies.FieldGeodeticPoint
Build a new instance from a GeodeticPoint.
FieldGeodeticPoint(T, T, T) - Constructor for class org.orekit.bodies.FieldGeodeticPoint
Build a new instance.
FieldGHIJjsPolynomials<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities
Compute the Gjs, Hjs, Ijs and Jjs polynomials in the equinoctial elements h, k and the direction cosines α and β and their partial derivatives with respect to k, h, α and β.
FieldGHIJjsPolynomials(T, T, T, T) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Create a set of Gjs, Hjs, Ijs and Jjs polynomials.
FieldGHmsjPolynomials<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities
Compute the Gmsj and the Hmsj polynomials in the equinoctial elements h, k and the direction cosines α and β and their partial derivatives with respect to k, h, α and β.
FieldGHmsjPolynomials(T, T, T, T, int, Field<T>) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials
Create a set of Gmsj and Hmsj polynomials.
FieldHansenTesseralLinear<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen
Hansen coefficients K(t,n,s) for t!=0 and n < 0.
FieldHansenTesseralLinear(int, int, int, int, int, Field<T>) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenTesseralLinear
Constructor.
FieldHansenThirdBodyLinear<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen
Hansen coefficients K(t,n,s) for t=0 and n > 0.
FieldHansenThirdBodyLinear(int, int, Field<T>) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenThirdBodyLinear
Constructor.
FieldHansenZonalLinear<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen
Hansen coefficients K(t,n,s) for t=0 and n < 0.
FieldHansenZonalLinear(int, int, Field<T>) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenZonalLinear
Constructor.
Fieldifier - Class in org.orekit.utils
Utility class used to convert class to their Field equivalent.
fieldify(Field<T>, RealMatrix) - Static method in class org.orekit.utils.Fieldifier
Fieldify given matrix with given field.
fieldify(Field<T>, Orbit) - Static method in class org.orekit.utils.Fieldifier
Deprecated. 
fieldify(Field<T>, StateCovariance) - Static method in class org.orekit.utils.Fieldifier
Fieldify given state covariance with given field.
FieldImpulseManeuver<D extends FieldEventDetector<T>,​T extends CalculusFieldElement<T>> - Class in org.orekit.forces.maneuvers
Impulse maneuver model for propagators working with Fields.
FieldImpulseManeuver(D, FieldVector3D<T>, T) - Constructor for class org.orekit.forces.maneuvers.FieldImpulseManeuver
Build a new instance.
FieldImpulseManeuver(D, AttitudeProvider, FieldVector3D<T>, T) - Constructor for class org.orekit.forces.maneuvers.FieldImpulseManeuver
Build a new instance.
FieldImpulseManeuver(D, AttitudeProvider, FieldVector3D<T>, T, Control3DVectorCostType) - Constructor for class org.orekit.forces.maneuvers.FieldImpulseManeuver
Build a new instance.
FieldInertia<T extends CalculusFieldElement<T>> - Class in org.orekit.attitudes
Container for inertia of a 3D object.
FieldInertiaAxis<T extends CalculusFieldElement<T>> - Class in org.orekit.attitudes
Container for inertial axis.
FieldInertiaAxis(T, FieldVector3D<T>) - Constructor for class org.orekit.attitudes.FieldInertiaAxis
Simple constructor to pair a moment of inertia with its associated axis.
FieldIntegrableFunction(FieldSpacecraftState<T>, boolean, int, T[], Field<T>) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldIntegrableFunction
Build a new instance with a new field.
FieldIntegratedEphemeris<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.integration
This class stores sequentially generated orbital parameters for later retrieval.
FieldIntegratedEphemeris(FieldAbsoluteDate<T>, FieldAbsoluteDate<T>, FieldAbsoluteDate<T>, FieldStateMapper<T>, PropagationType, FieldDenseOutputModel<T>, FieldArrayDictionary<T>, List<FieldAdditionalStateProvider<T>>, String[], int[]) - Constructor for class org.orekit.propagation.integration.FieldIntegratedEphemeris
Creates a new instance of IntegratedEphemeris.
FieldIntelsatElevenElements<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical.intelsat
This class is a container for a single set of Intelsat's 11 Elements data.
FieldIntelsatElevenElements(FieldAbsoluteDate<T>, T, T, T, T, T, T, T, T, T, T, T) - Constructor for class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElements
Constructor.
FieldIntelsatElevenElementsPropagator<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical.intelsat
This class provides elements to propagate Intelsat's 11 elements.
FieldIntelsatElevenElementsPropagator(FieldIntelsatElevenElements<T>) - Constructor for class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElementsPropagator
Default constructor.
FieldIntelsatElevenElementsPropagator(FieldIntelsatElevenElements<T>, Frame, Frame) - Constructor for class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElementsPropagator
Constructor.
FieldIntelsatElevenElementsPropagator(FieldIntelsatElevenElements<T>, Frame, Frame, AttitudeProvider, T) - Constructor for class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElementsPropagator
Constructor.
FieldInterpolationGrid<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation.semianalytical.dsst.utilities
Interface for interpolation grids.
FieldKeplerianAnomalyUtility - Class in org.orekit.orbits
Utility methods for converting between different Keplerian anomalies.
FieldKeplerianOrbit<T extends CalculusFieldElement<T>> - Class in org.orekit.orbits
This class handles traditional Keplerian orbital parameters.
FieldKeplerianOrbit(Field<T>, KeplerianOrbit) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit
Constructor from Field and KeplerianOrbit.
FieldKeplerianOrbit(Field<T>, Orbit) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit
Constructor from Field and Orbit.
FieldKeplerianOrbit(FieldOrbit<T>) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit
Constructor from any kind of orbital parameters.
FieldKeplerianOrbit(FieldPVCoordinates<T>, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit
Constructor from Cartesian parameters.
FieldKeplerianOrbit(TimeStampedFieldPVCoordinates<T>, Frame, T) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit
Constructor from Cartesian parameters.
FieldKeplerianOrbit(T, T, T, T, T, T, PositionAngleType, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit
Creates a new instance.
FieldKeplerianOrbit(T, T, T, T, T, T, PositionAngleType, PositionAngleType, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit
Creates a new instance.
FieldKeplerianOrbit(T, T, T, T, T, T, T, T, T, T, T, T, PositionAngleType, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit
Creates a new instance.
FieldKeplerianOrbit(T, T, T, T, T, T, T, T, T, T, T, T, PositionAngleType, PositionAngleType, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit
Creates a new instance.
FieldKeplerianPropagator<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical
Simple Keplerian orbit propagator.
FieldKeplerianPropagator(FieldOrbit<T>) - Constructor for class org.orekit.propagation.analytical.FieldKeplerianPropagator
Build a propagator from orbit only.
FieldKeplerianPropagator(FieldOrbit<T>, AttitudeProvider) - Constructor for class org.orekit.propagation.analytical.FieldKeplerianPropagator
Build a propagator from orbit and attitude provider.
FieldKeplerianPropagator(FieldOrbit<T>, AttitudeProvider, T) - Constructor for class org.orekit.propagation.analytical.FieldKeplerianPropagator
Build a propagator from orbit, attitude provider and central attraction coefficient μ.
FieldKeplerianPropagator(FieldOrbit<T>, AttitudeProvider, T, T) - Constructor for class org.orekit.propagation.analytical.FieldKeplerianPropagator
Build propagator from orbit, attitude provider, central attraction coefficient μ and mass.
FieldKeplerianPropagator(FieldOrbit<T>, T) - Constructor for class org.orekit.propagation.analytical.FieldKeplerianPropagator
Build a propagator from orbit and central attraction coefficient μ.
FieldKinematicTransform<T extends CalculusFieldElement<T>> - Interface in org.orekit.frames
A transform that only includes translation and rotation as well as their respective rates.
FieldLatitudeCrossingDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events
Detector for geographic latitude crossing.
FieldLatitudeCrossingDetector(Field<T>, OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.FieldLatitudeCrossingDetector
Build a new detector.
FieldLatitudeCrossingDetector(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>, OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.FieldLatitudeCrossingDetector
Protected constructor with full parameters.
FieldLatitudeCrossingDetector(T, T, OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.FieldLatitudeCrossingDetector
Build a detector.
FieldLatitudeRangeCrossingDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events
Detector for geographic latitude crossing.
FieldLatitudeRangeCrossingDetector(Field<T>, OneAxisEllipsoid, double, double) - Constructor for class org.orekit.propagation.events.FieldLatitudeRangeCrossingDetector
Build a new detector.
FieldLatitudeRangeCrossingDetector(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>, OneAxisEllipsoid, double, double) - Constructor for class org.orekit.propagation.events.FieldLatitudeRangeCrossingDetector
Private constructor with full parameters.
FieldLatitudeRangeCrossingDetector(T, T, OneAxisEllipsoid, double, double) - Constructor for class org.orekit.propagation.events.FieldLatitudeRangeCrossingDetector
Build a detector.
FieldLegendrePolynomials<T extends CalculusFieldElement<T>> - Class in org.orekit.utils
Computes the Pnm(t) coefficients.
FieldLegendrePolynomials(int, int, T) - Constructor for class org.orekit.utils.FieldLegendrePolynomials
Create Legendre polynomials for the given degree and order.
FieldLnsCoefficients<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities
Compute the Lns(γ).
FieldLnsCoefficients(int, int, T[][], SortedMap<CoefficientsFactory.NSKey, Double>, T, Field<T>) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FieldLnsCoefficients
Create a set of Lns(γ) coefficients.
FieldLongitudeCrossingDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events
Detector for geographic longitude crossing.
FieldLongitudeCrossingDetector(Field<T>, OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.FieldLongitudeCrossingDetector
Build a new detector.
FieldLongitudeCrossingDetector(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>, OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.FieldLongitudeCrossingDetector
Protected constructor with full parameters.
FieldLongitudeCrossingDetector(T, T, OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.FieldLongitudeCrossingDetector
Build a detector.
FieldLongitudeRangeCrossingDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events
Detector for geographic longitude crossing.
FieldLongitudeRangeCrossingDetector(Field<T>, OneAxisEllipsoid, double, double) - Constructor for class org.orekit.propagation.events.FieldLongitudeRangeCrossingDetector
Build a new detector.
FieldLongitudeRangeCrossingDetector(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>, OneAxisEllipsoid, double, double) - Constructor for class org.orekit.propagation.events.FieldLongitudeRangeCrossingDetector
Private constructor with full parameters.
FieldLongitudeRangeCrossingDetector(T, T, OneAxisEllipsoid, double, double) - Constructor for class org.orekit.propagation.events.FieldLongitudeRangeCrossingDetector
Build a detector.
FieldManeuverTriggersResetter<T extends CalculusFieldElement<T>> - Interface in org.orekit.forces.maneuvers.trigger
Resetter for maneuver triggers.
FieldMaxGapInterpolationGrid<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities
Interpolation grid where points obey a maximum time gap.
FieldMaxGapInterpolationGrid(Field<T>, T) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FieldMaxGapInterpolationGrid
Constructor.
fieldNaturalToProper(Gradient[], FieldTransform<Gradient>, Frame) - Static method in class org.orekit.estimation.measurements.modifiers.AberrationModifier
Natural to proper correction for aberration of light.
fieldNaturalToProper(Gradient[], FieldTransform<Gradient>, Frame, DataContext) - Static method in class org.orekit.estimation.measurements.modifiers.AberrationModifier
Natural to proper correction for aberration of light.
FieldNegateDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events
An event detector that negates the sign on another event detector's g function.
FieldNegateDetector(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>, FieldEventDetector<T>) - Constructor for class org.orekit.propagation.events.FieldNegateDetector
Private constructor.
FieldNegateDetector(FieldEventDetector<T>) - Constructor for class org.orekit.propagation.events.FieldNegateDetector
Create a new event detector that negates an existing event detector.
FieldNodeDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events
Finder for node crossing events.
FieldNodeDetector(FieldOrbit<T>, Frame) - Constructor for class org.orekit.propagation.events.FieldNodeDetector
Build a new instance.
FieldNodeDetector(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>, Frame) - Constructor for class org.orekit.propagation.events.FieldNodeDetector
Protected constructor with full parameters.
FieldNodeDetector(T, FieldOrbit<T>, Frame) - Constructor for class org.orekit.propagation.events.FieldNodeDetector
Build a new instance.
FieldNumericalPropagator<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.numerical
This class propagates orbits using numerical integration.
FieldNumericalPropagator(Field<T>, FieldODEIntegrator<T>) - Constructor for class org.orekit.propagation.numerical.FieldNumericalPropagator
Create a new instance of NumericalPropagator, based on orbit definition mu.
FieldNumericalPropagator(Field<T>, FieldODEIntegrator<T>, AttitudeProvider) - Constructor for class org.orekit.propagation.numerical.FieldNumericalPropagator
Create a new instance of NumericalPropagator, based on orbit definition mu.
FieldODEIntegratorBuilder<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation.conversion
This interface is the top-level abstraction to build first order integrators for propagators conversion.
FieldOfView - Interface in org.orekit.geometry.fov
Interface representing a spacecraft sensor Field Of View.
FieldOfViewDetector - Class in org.orekit.propagation.events
Finder for target entry/exit events with respect to a satellite sensor Field Of View.
FieldOfViewDetector(AdaptableInterval, double, int, EventHandler, PVCoordinatesProvider, double, VisibilityTrigger, FieldOfView) - Constructor for class org.orekit.propagation.events.FieldOfViewDetector
Protected constructor with full parameters.
FieldOfViewDetector(PVCoordinatesProvider, double, VisibilityTrigger, FieldOfView) - Constructor for class org.orekit.propagation.events.FieldOfViewDetector
Build a new instance.
FieldOfViewDetector(PVCoordinatesProvider, FieldOfView) - Constructor for class org.orekit.propagation.events.FieldOfViewDetector
Build a new instance.
FieldOrbit<T extends CalculusFieldElement<T>> - Class in org.orekit.orbits
This class handles orbital parameters.
FieldOrbit(Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldOrbit
Default constructor.
FieldOrbit(TimeStampedFieldPVCoordinates<T>, Frame, T) - Constructor for class org.orekit.orbits.FieldOrbit
Set the orbit from Cartesian parameters.
FieldOrbitBlender<KK extends CalculusFieldElement<KK>> - Class in org.orekit.orbits
Orbit blender.
FieldOrbitBlender(SmoothStepFactory.FieldSmoothStepFunction<KK>, FieldAbstractAnalyticalPropagator<KK>, Frame) - Constructor for class org.orekit.orbits.FieldOrbitBlender
Default constructor.
FieldOrbitHermiteInterpolator<KK extends CalculusFieldElement<KK>> - Class in org.orekit.orbits
Class using a Hermite interpolator to interpolate orbits.
FieldOrbitHermiteInterpolator(int, double, Frame, CartesianDerivativesFilter) - Constructor for class org.orekit.orbits.FieldOrbitHermiteInterpolator
Constructor.
FieldOrbitHermiteInterpolator(int, Frame) - Constructor for class org.orekit.orbits.FieldOrbitHermiteInterpolator
Constructor with : Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of position and two time derivatives during interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).
FieldOrbitHermiteInterpolator(int, Frame, CartesianDerivativesFilter) - Constructor for class org.orekit.orbits.FieldOrbitHermiteInterpolator
Constructor with default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s).
FieldOrbitHermiteInterpolator(Frame) - Constructor for class org.orekit.orbits.FieldOrbitHermiteInterpolator
Constructor with : Default number of interpolation points of DEFAULT_INTERPOLATION_POINTS Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of position and two time derivatives during interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).
FieldOrekitFixedStepHandler<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation.sampling
This interface is a space-dynamics aware fixed size step handler.
FieldOrekitStepHandler<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation.sampling
This interface is a space-dynamics aware step handler.
FieldOrekitStepInterpolator<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation.sampling
This interface is a space-dynamics aware step interpolator.
FieldOrekitStepNormalizer<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.sampling
This class wraps an object implementing OrekitFixedStepHandler into a OrekitStepHandler.
FieldOrekitStepNormalizer(T, FieldOrekitFixedStepHandler<T>) - Constructor for class org.orekit.propagation.sampling.FieldOrekitStepNormalizer
Simple constructor.
FieldParameterDrivenDateIntervalDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events
Detector for date intervals that may be offset thanks to parameter drivers.
FieldParameterDrivenDateIntervalDetector(Field<T>, String, AbsoluteDate, double) - Constructor for class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector
Build a new instance.
FieldParameterDrivenDateIntervalDetector(Field<T>, String, AbsoluteDate, AbsoluteDate) - Constructor for class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector
Build a new instance.
FieldParameterDrivenDateIntervalDetector(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>, DateDriver, DateDriver, DateDriver, ParameterDriver) - Constructor for class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector
Protected constructor with full parameters.
FieldPoleCorrection<T extends CalculusFieldElement<T>> - Class in org.orekit.frames
Simple container class for pole correction parameters.
FieldPoleCorrection(T, T) - Constructor for class org.orekit.frames.FieldPoleCorrection
Simple constructor.
FieldPressureTemperature<T extends CalculusFieldElement<T>> - Class in org.orekit.models.earth.weather
Container for pressure and temperature.
FieldPressureTemperature(Field<T>, PressureTemperatureHumidity) - Constructor for class org.orekit.models.earth.weather.FieldPressureTemperature
Simple constructor.
FieldPressureTemperature(T, T, T) - Constructor for class org.orekit.models.earth.weather.FieldPressureTemperature
Simple constructor.
FieldPressureTemperatureHumidity<T extends CalculusFieldElement<T>> - Class in org.orekit.models.earth.weather
Container for pressure, temperature, and humidity.
FieldPressureTemperatureHumidity(Field<T>, PressureTemperatureHumidity) - Constructor for class org.orekit.models.earth.weather.FieldPressureTemperatureHumidity
Simple constructor.
FieldPressureTemperatureHumidity(T, T, T, T, T, T) - Constructor for class org.orekit.models.earth.weather.FieldPressureTemperatureHumidity
Simple constructor.
FieldProbabilityOfCollision<T extends CalculusFieldElement<T>> - Class in org.orekit.ssa.metrics
Container for values relative to the probability of collision : Value of the probability of collision. Name of the method with which it was computed. Upper and lower limit of the value if the method provides them (such as Laas2015 for example). Flag defining if the probability was maximized in any way (such as Alfriend1999Max for example).
FieldProbabilityOfCollision(T, String) - Constructor for class org.orekit.ssa.metrics.FieldProbabilityOfCollision
Constructor with default values of 0 for the upper/lower limits and default false flag for maximum probability.
FieldProbabilityOfCollision(T, String, boolean) - Constructor for class org.orekit.ssa.metrics.FieldProbabilityOfCollision
Constructor with default values of 0 for the upper and lower limits.
FieldProbabilityOfCollision(T, T, T, String, boolean) - Constructor for class org.orekit.ssa.metrics.FieldProbabilityOfCollision
Constructor.
FieldPropagator<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation
This interface provides a way to propagate an orbit at any time.
fieldProperToNatural(Gradient[], FieldTransform<Gradient>, Frame) - Static method in class org.orekit.estimation.measurements.modifiers.AberrationModifier
Proper to natural correction for aberration of light.
fieldProperToNatural(Gradient[], FieldTransform<Gradient>, Frame, DataContext) - Static method in class org.orekit.estimation.measurements.modifiers.AberrationModifier
Proper to natural correction for aberration of light.
FieldPVCoordinates<T extends CalculusFieldElement<T>> - Class in org.orekit.utils
Simple container for Position/Velocity pairs, using CalculusFieldElement.
FieldPVCoordinates(double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Multiplicative constructor.
FieldPVCoordinates(double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Linear constructor.
FieldPVCoordinates(double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Linear constructor.
FieldPVCoordinates(double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Linear constructor.
FieldPVCoordinates(Field<T>, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates
Builds a FieldPVCoordinates from a field and a regular PVCoordinates.
FieldPVCoordinates(FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Builds a FieldPVCoordinates triplet with zero acceleration.
FieldPVCoordinates(FieldVector3D<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Builds a FieldPVCoordinates triplet.
FieldPVCoordinates(FieldVector3D<U>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Builds a FieldPVCoordinates triplet from a FieldVector3D<FieldDerivativeStructure>.
FieldPVCoordinates(FieldPVCoordinates<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Subtractive constructor.
FieldPVCoordinates(T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Multiplicative constructor.
FieldPVCoordinates(T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Linear constructor.
FieldPVCoordinates(T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Linear constructor.
FieldPVCoordinates(T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Linear constructor.
FieldPVCoordinates(T, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates
Multiplicative constructor.
FieldPVCoordinates(T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates
Linear constructor.
FieldPVCoordinates(T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates
Linear constructor.
FieldPVCoordinates(T, PVCoordinates, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates
Linear constructor.
FieldPVCoordinatesProvider<T extends CalculusFieldElement<T>> - Interface in org.orekit.utils
Interface for PV coordinates providers.
FieldRecallLastOccurrence<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events.handlers
Event handler wrapping another, arbitrary one whilst remembering date of last detection.
FieldRecallLastOccurrence(FieldEventHandler<T>) - Constructor for class org.orekit.propagation.events.handlers.FieldRecallLastOccurrence
Constructor.
FieldRecordAndContinue<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events.handlers
Handler that will record every time an event occurs and always return Action.CONTINUE.
FieldRecordAndContinue() - Constructor for class org.orekit.propagation.events.handlers.FieldRecordAndContinue
Create a new handler using an ArrayList to store events.
FieldRecordAndContinue(List<FieldRecordAndContinue.Event<T>>) - Constructor for class org.orekit.propagation.events.handlers.FieldRecordAndContinue
Create a handler using the given collection to store events.
FieldRecordAndContinue.Event<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events.handlers
A single event detected during propagation.
FieldRelativeDistanceDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events
Detector of specific value for the distance relative to another trajectory (using the Euclidean norm).
FieldRelativeDistanceDetector(FieldAdaptableInterval<T>, T, int, FieldEventHandler<T>, FieldPVCoordinatesProvider<T>, T) - Constructor for class org.orekit.propagation.events.FieldRelativeDistanceDetector
Deprecated.
as of 12.2
FieldRelativeDistanceDetector(FieldEventDetectionSettings<T>, FieldEventHandler<T>, FieldPVCoordinatesProvider<T>, T) - Constructor for class org.orekit.propagation.events.FieldRelativeDistanceDetector
Constructor.
FieldRelativeDistanceDetector(FieldPVCoordinatesProvider<T>, T) - Constructor for class org.orekit.propagation.events.FieldRelativeDistanceDetector
Constructor with default values.
FieldResetDerivativesOnEvent<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events.handlers
Event handler which will always return continue as a state.
FieldResetDerivativesOnEvent() - Constructor for class org.orekit.propagation.events.handlers.FieldResetDerivativesOnEvent
 
FieldSGP4<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical.tle
This class contains methods to compute propagated coordinates with the SGP4 model.
FieldSGP4(FieldTLE<T>, AttitudeProvider, T, Frame, T[]) - Constructor for class org.orekit.propagation.analytical.tle.FieldSGP4
Constructor for a unique initial TLE.
FieldSGP4(FieldTLE<T>, AttitudeProvider, T, T[]) - Constructor for class org.orekit.propagation.analytical.tle.FieldSGP4
Constructor for a unique initial TLE.
FieldShiftingPVCoordinatesProvider<T extends CalculusFieldElement<T>> - Class in org.orekit.utils
Provider using simple FieldPVCoordinates.shiftedBy(CalculusFieldElement) shiftedBy} and frame transforms for evolution.
FieldShiftingPVCoordinatesProvider(TimeStampedFieldPVCoordinates<T>, Frame) - Constructor for class org.orekit.utils.FieldShiftingPVCoordinatesProvider
Simple constructor.
FieldShortPeriodicsInterpolatedCoefficient<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities
Interpolated short periodics coefficients.
FieldShortPeriodicsInterpolatedCoefficient(int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FieldShortPeriodicsInterpolatedCoefficient
Simple constructor.
FieldShortPeriodTerms<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation.semianalytical.dsst.forces
Additive short period terms contributing to the mean to osculating orbit mapping.
FieldShortTermEncounter2DDefinition<T extends CalculusFieldElement<T>> - Class in org.orekit.ssa.collision.shorttermencounter.probability.twod
Defines the encounter between two collision object at time of closest approach assuming a short-term encounter model .
FieldShortTermEncounter2DDefinition(FieldOrbit<T>, FieldStateCovariance<T>, FieldOrbit<T>, FieldStateCovariance<T>, T) - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Constructor.
FieldShortTermEncounter2DDefinition(FieldOrbit<T>, FieldStateCovariance<T>, FieldOrbit<T>, FieldStateCovariance<T>, T, EncounterLOFType, double) - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Constructor.
FieldShortTermEncounter2DDefinition(FieldOrbit<T>, FieldStateCovariance<T>, T, FieldOrbit<T>, FieldStateCovariance<T>, T) - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Constructor.
FieldShortTermEncounter2DDefinition(FieldOrbit<T>, FieldStateCovariance<T>, T, FieldOrbit<T>, FieldStateCovariance<T>, T, EncounterLOFType, double) - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Constructor.
FieldSortedListTrimmer - Class in org.orekit.utils
A trimmer for externally stored chronologically sorted lists.
FieldSortedListTrimmer(int) - Constructor for class org.orekit.utils.FieldSortedListTrimmer
Create a new cache with the given neighbors size and data.
FieldSpacecraftState<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation
This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation.
FieldSpacecraftState(Field<T>, SpacecraftState) - Constructor for class org.orekit.propagation.FieldSpacecraftState
FieldSpacecraftState(FieldOrbit<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit only.
FieldSpacecraftState(FieldOrbit<T>, FieldAttitude<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit and attitude.
FieldSpacecraftState(FieldOrbit<T>, FieldAttitude<T>, FieldArrayDictionary<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit attitude and additional states.
FieldSpacecraftState(FieldOrbit<T>, FieldAttitude<T>, T) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit, attitude and mass.
FieldSpacecraftState(FieldOrbit<T>, FieldAttitude<T>, T, FieldArrayDictionary<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit, attitude, mass and additional states.
FieldSpacecraftState(FieldOrbit<T>, FieldAttitude<T>, T, FieldArrayDictionary<T>, FieldArrayDictionary<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit, attitude, mass, additional states and derivatives.
FieldSpacecraftState(FieldOrbit<T>, FieldArrayDictionary<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit and additional states.
FieldSpacecraftState(FieldOrbit<T>, T) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Create a new instance from orbit and mass.
FieldSpacecraftState(FieldOrbit<T>, T, FieldArrayDictionary<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Create a new instance from orbit, mass and additional states.
FieldSpacecraftState(FieldAbsolutePVCoordinates<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit only.
FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, FieldAttitude<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit and attitude.
FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, FieldAttitude<T>, FieldArrayDictionary<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit and attitude.
FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, FieldAttitude<T>, T) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit, attitude and mass.
FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, FieldAttitude<T>, T, FieldArrayDictionary<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit, attitude and mass.
FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, FieldAttitude<T>, T, FieldArrayDictionary<T>, FieldArrayDictionary<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit, attitude and mass.
FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, FieldArrayDictionary<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit only.
FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, T) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Create a new instance from orbit and mass.
FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, T, FieldArrayDictionary<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Create a new instance from orbit and mass.
FieldSpacecraftStateInterpolator<KK extends CalculusFieldElement<KK>> - Class in org.orekit.propagation
Generic class for spacecraft state interpolator.
FieldSpacecraftStateInterpolator(int, double, Frame) - Constructor for class org.orekit.propagation.FieldSpacecraftStateInterpolator
Constructor to create a customizable Hermite interpolator for every spacecraft state field.
FieldSpacecraftStateInterpolator(int, double, Frame, Frame) - Constructor for class org.orekit.propagation.FieldSpacecraftStateInterpolator
Constructor to create a customizable Hermite interpolator for every spacecraft state field.
FieldSpacecraftStateInterpolator(int, double, Frame, Frame, CartesianDerivativesFilter, AngularDerivativesFilter) - Constructor for class org.orekit.propagation.FieldSpacecraftStateInterpolator
Constructor.
FieldSpacecraftStateInterpolator(int, double, Frame, FieldTimeInterpolator<FieldOrbit<KK>, KK>, FieldTimeInterpolator<FieldAbsolutePVCoordinates<KK>, KK>, FieldTimeInterpolator<TimeStampedField<KK>, KK>, FieldTimeInterpolator<FieldAttitude<KK>, KK>, FieldTimeInterpolator<TimeStampedField<KK>, KK>) - Constructor for class org.orekit.propagation.FieldSpacecraftStateInterpolator
Constructor.
FieldSpacecraftStateInterpolator(int, Frame) - Constructor for class org.orekit.propagation.FieldSpacecraftStateInterpolator
Constructor to create a customizable Hermite interpolator for every spacecraft state field.
FieldSpacecraftStateInterpolator(int, Frame, Frame) - Constructor for class org.orekit.propagation.FieldSpacecraftStateInterpolator
Constructor to create a customizable Hermite interpolator for every spacecraft state field.
FieldSpacecraftStateInterpolator(Frame) - Constructor for class org.orekit.propagation.FieldSpacecraftStateInterpolator
Simplest constructor to create a default Hermite interpolator for every spacecraft state field.
FieldSpacecraftStateInterpolator(Frame, FieldTimeInterpolator<FieldOrbit<KK>, KK>, FieldTimeInterpolator<FieldAbsolutePVCoordinates<KK>, KK>, FieldTimeInterpolator<TimeStampedField<KK>, KK>, FieldTimeInterpolator<FieldAttitude<KK>, KK>, FieldTimeInterpolator<TimeStampedField<KK>, KK>) - Constructor for class org.orekit.propagation.FieldSpacecraftStateInterpolator
FieldStateCovariance<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation
This class is the representation of a covariance matrix at a given date.
FieldStateCovariance(FieldMatrix<T>, FieldAbsoluteDate<T>, Frame, OrbitType, PositionAngleType) - Constructor for class org.orekit.propagation.FieldStateCovariance
Constructor.
FieldStateCovariance(FieldMatrix<T>, FieldAbsoluteDate<T>, LOF) - Constructor for class org.orekit.propagation.FieldStateCovariance
Constructor.
FieldStateMapper<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.integration
This class maps between raw double elements and FieldSpacecraftState instances.
FieldStateMapper(FieldAbsoluteDate<T>, T, OrbitType, PositionAngleType, AttitudeProvider, Frame) - Constructor for class org.orekit.propagation.integration.FieldStateMapper
Simple constructor.
FieldStaticTransform<T extends CalculusFieldElement<T>> - Interface in org.orekit.frames
A transform that only includes translation and rotation.
FieldStepHandlerMultiplexer<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.sampling
This class gathers several OrekitStepHandler instances into one.
FieldStepHandlerMultiplexer() - Constructor for class org.orekit.propagation.sampling.FieldStepHandlerMultiplexer
Simple constructor.
FieldStopOnDecreasing<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events.handlers
Handle a detection event and choose what to do next.
FieldStopOnDecreasing() - Constructor for class org.orekit.propagation.events.handlers.FieldStopOnDecreasing
Empty constructor.
FieldStopOnEvent<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events.handlers
Event handler which will always return continue as a state.
FieldStopOnEvent() - Constructor for class org.orekit.propagation.events.handlers.FieldStopOnEvent
Empty constructor.
FieldStopOnIncreasing<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events.handlers
Handle a detection event and choose what to do next.
FieldStopOnIncreasing() - Constructor for class org.orekit.propagation.events.handlers.FieldStopOnIncreasing
Empty constructor.
FieldTimeDerivativesEquations<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation.numerical
Interface summing up the contribution of several forces into orbit and mass derivatives.
FieldTimeInterpolator<T extends FieldTimeStamped<KK>,​KK extends CalculusFieldElement<KK>> - Interface in org.orekit.time
This interface represents objects that can interpolate a time stamped value with respect to time.
FieldTimeShiftable<T extends FieldTimeShiftable<T,​KK>,​KK extends CalculusFieldElement<KK>> - Interface in org.orekit.time
This interface represents objects that can be shifted in time.
FieldTimeSpanMap<T,​D extends CalculusFieldElement<D>> - Class in org.orekit.utils
Container for objects that apply to spans of time.
FieldTimeSpanMap(T, Field<D>) - Constructor for class org.orekit.utils.FieldTimeSpanMap
Create a map containing a single object, initially valid throughout the timeline.
FieldTimeSpanMap.Transition<S,​D extends CalculusFieldElement<D>> - Class in org.orekit.utils
Local class holding transition times.
FieldTimeStamped<T extends CalculusFieldElement<T>> - Interface in org.orekit.time
This interface represents objects that have a AbsoluteDate date attached to them.
FieldTimeStampedCache<T extends FieldTimeStamped<KK>,​KK extends CalculusFieldElement<KK>> - Interface in org.orekit.utils
Interface for a data structure that can provide concurrent access to FieldTimeStamped data surrounding a given date.
FieldTimeStampedPair<F extends FieldTimeStamped<KK>,​S extends FieldTimeStamped<KK>,​KK extends CalculusFieldElement<KK>> - Class in org.orekit.time
Pair of time stamped values being defined at the same date.
FieldTimeStampedPair(F, S) - Constructor for class org.orekit.time.FieldTimeStampedPair
Constructor.
FieldTimeStampedPair(F, S, double) - Constructor for class org.orekit.time.FieldTimeStampedPair
Constructor.
FieldTLE<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical.tle
This class is a container for a single set of TLE data.
FieldTLE(int, char, int, int, String, int, int, FieldAbsoluteDate<T>, T, T, T, T, T, T, T, T, int, double) - Constructor for class org.orekit.propagation.analytical.tle.FieldTLE
Simple constructor from already parsed elements.
FieldTLE(int, char, int, int, String, int, int, FieldAbsoluteDate<T>, T, T, T, T, T, T, T, T, int, double, TimeScale) - Constructor for class org.orekit.propagation.analytical.tle.FieldTLE
Simple constructor from already parsed elements using the given time scale as UTC.
FieldTLE(Field<T>, String, String) - Constructor for class org.orekit.propagation.analytical.tle.FieldTLE
Simple constructor from unparsed two lines.
FieldTLE(Field<T>, String, String, TimeScale) - Constructor for class org.orekit.propagation.analytical.tle.FieldTLE
Simple constructor from unparsed two lines using the given time scale as UTC.
FieldTLEPropagator<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical.tle
This class provides elements to propagate TLE's.
FieldTLEPropagator(FieldTLE<T>, AttitudeProvider, T, Frame, T[]) - Constructor for class org.orekit.propagation.analytical.tle.FieldTLEPropagator
Protected constructor for derived classes.
FieldTLEPropagator(FieldTLE<T>, AttitudeProvider, T, T[]) - Constructor for class org.orekit.propagation.analytical.tle.FieldTLEPropagator
Protected constructor for derived classes.
FieldTrackingCoordinates<T extends CalculusFieldElement<T>> - Class in org.orekit.utils
Container for azimut/elevation/range coordinates as seen from a ground point.
FieldTrackingCoordinates(Field<T>, TrackingCoordinates) - Constructor for class org.orekit.utils.FieldTrackingCoordinates
Build a new instance from a TrackingCoordinates.
FieldTrackingCoordinates(T, T, T) - Constructor for class org.orekit.utils.FieldTrackingCoordinates
Simple constructor.
FieldTransform<T extends CalculusFieldElement<T>> - Class in org.orekit.frames
Transformation class in three-dimensional space.
FieldTransform(Field<T>, Transform) - Constructor for class org.orekit.frames.FieldTransform
Build a transform from a regular transform.
FieldTransform(FieldAbsoluteDate<T>, FieldRotation<T>) - Constructor for class org.orekit.frames.FieldTransform
Build a rotation transform.
FieldTransform(FieldAbsoluteDate<T>, FieldRotation<T>, FieldVector3D<T>) - Constructor for class org.orekit.frames.FieldTransform
Build a rotation transform.
FieldTransform(FieldAbsoluteDate<T>, FieldRotation<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.frames.FieldTransform
Build a rotation transform.
FieldTransform(FieldAbsoluteDate<T>, FieldVector3D<T>) - Constructor for class org.orekit.frames.FieldTransform
Build a translation transform.
FieldTransform(FieldAbsoluteDate<T>, FieldVector3D<T>, FieldRotation<T>) - Constructor for class org.orekit.frames.FieldTransform
Build a combined translation and rotation transform.
FieldTransform(FieldAbsoluteDate<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.frames.FieldTransform
Build a translation transform, with its first time derivative.
FieldTransform(FieldAbsoluteDate<T>, FieldVector3D<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.frames.FieldTransform
Build a translation transform, with its first and second time derivatives.
FieldTransform(FieldAbsoluteDate<T>, FieldTransform<T>, FieldTransform<T>) - Constructor for class org.orekit.frames.FieldTransform
Build a transform by combining two existing ones.
FieldTransform(FieldAbsoluteDate<T>, FieldAngularCoordinates<T>) - Constructor for class org.orekit.frames.FieldTransform
Build a rotation transform.
FieldTransform(FieldAbsoluteDate<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.frames.FieldTransform
Build a translation transform, with its first time derivative.
FieldTransformGenerator<T extends CalculusFieldElement<T>> - Class in org.orekit.frames
Generator to use field transforms in GenericTimeStampedCache.
FieldTransformGenerator(Field<T>, int, TransformProvider, double) - Constructor for class org.orekit.frames.FieldTransformGenerator
simple constructor.
FieldTroposphericDelay<T extends CalculusFieldElement<T>> - Class in org.orekit.models.earth.troposphere
Container for tropospheric delay.
FieldTroposphericDelay(T, T, T, T) - Constructor for class org.orekit.models.earth.troposphere.FieldTroposphericDelay
Simple constructor.
FieldViennaACoefficients<T extends CalculusFieldElement<T>> - Class in org.orekit.models.earth.troposphere
Container for the ViennaOne and ViennaThree coefficients ah and aw.
FieldViennaACoefficients(T, T) - Constructor for class org.orekit.models.earth.troposphere.FieldViennaACoefficients
Simple constructor.
FIFTIES_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Reference epoch for 1950 dates: 1950-01-01T00:00:00 Terrestrial Time.
FIFTIES_EPOCH - Static variable in class org.orekit.time.DateComponents
Reference epoch for 1950 dates: 1950-01-01.
FileFormat - Enum in org.orekit.files.ccsds.utils
Enumerate for file format.
FilesListCrawler - Class in org.orekit.data
Provider for data files in an explicit list.
FilesListCrawler(File...) - Constructor for class org.orekit.data.FilesListCrawler
Build a data classpath crawler.
fillHalfRow(double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit
Fill a Jacobian half row with a single vector.
fillHalfRow(double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit
Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit
Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit
Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit
Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit
Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit
Fill a Jacobian half row with a single vector.
fillHalfRow(T, FieldVector3D<T>, T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit
Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit
Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit
Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit
Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit
Fill a Jacobian half row with a linear combination of vectors.
fillHistory(IERSConventions.NutationCorrectionConverter, SortedSet<EOPEntry>) - Method in class org.orekit.files.sinex.SinexLoader
Load celestial body.
fillHistory(IERSConventions.NutationCorrectionConverter, SortedSet<EOPEntry>) - Method in interface org.orekit.frames.EopHistoryLoader
Load celestial body.
filter(boolean) - Method in class org.orekit.utils.ParameterDriversList
Filter parameters to keep only one type of selection status.
filter(DataSource) - Method in interface org.orekit.data.DataFilter
Filter the data source.
filter(DataSource) - Method in class org.orekit.data.GzipFilter
Filter the data source.
filter(DataSource) - Method in class org.orekit.data.TruncatingFilter
Filter the data source.
filter(DataSource) - Method in class org.orekit.data.UnixCompressFilter
Filter the data source.
filter(DataSource) - Method in class org.orekit.files.rinex.HatanakaCompressFilter
Filter the data source.
filter(DataSource) - Method in class org.orekit.files.sp3.NsgfV00Filter
Filter the data source.
filter(ObservedMeasurement<T>, SpacecraftState) - Method in class org.orekit.estimation.measurements.filtering.ElevationFilter
Apply a filter to an observed measurement.
filter(ObservedMeasurement<T>, SpacecraftState) - Method in interface org.orekit.estimation.measurements.filtering.MeasurementFilter
Apply a filter to an observed measurement.
filter(ObservedMeasurement<T>, SpacecraftState) - Method in class org.orekit.estimation.measurements.filtering.ResidualFilter
Apply a filter to an observed measurement.
FILTER_SMOOTHER - org.orekit.files.ccsds.definitions.AdMethodType
Method smoothing noisy processes.
filterData(ObservationData, ObservationData) - Method in class org.orekit.estimation.measurements.filtering.SingleFrequencyHatchFilter
This method filters the provided data given the state of the filter.
filterData(ObservationData, ObservationData, ObservationData) - Method in class org.orekit.estimation.measurements.filtering.DualFrequencyHatchFilter
This method filters the provided data given the state of the filter.
filterDataSet(List<ObservationDataSet>, SatelliteSystem, int, ObservationType) - Method in class org.orekit.estimation.measurements.filtering.SingleFrequencySmoother
Applies a Single Frequency Hatch filter to a list of ObservationDataSet.
filterDataSet(List<ObservationDataSet>, SatelliteSystem, int, ObservationType, ObservationType) - Method in class org.orekit.estimation.measurements.filtering.DualFrequencySmoother
Applies a Dual Frequency Hatch filter to a list of ObservationDataSet.
filterLine(int, String) - Method in class org.orekit.data.LineOrientedFilteringReader
Filter one line.
filterRelevant(ObservedMeasurement<?>, SpacecraftState[]) - Static method in class org.orekit.estimation.sequential.KalmanEstimatorUtil
Filter relevant states for a measurement.
FiltersManager - Class in org.orekit.data
Manager for data filters.
FiltersManager() - Constructor for class org.orekit.data.FiltersManager
Build an empty manager.
FilterType - Enum in org.orekit.propagation.events
Enumerate for filtering events.
finalizeData() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmParser
Finalize data after parsing.
finalizeData() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser
Finalize data after parsing.
finalizeData() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser
Finalize data after parsing.
finalizeData() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmParser
Finalize data after parsing.
finalizeData() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser
Finalize data after parsing.
finalizeData() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser
Finalize data after parsing.
finalizeData() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser
Finalize data after parsing.
finalizeData() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser
Finalize data after parsing.
finalizeData() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser
Finalize data after parsing.
finalizeData() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser
Finalize data after parsing.
finalizeEstimation(ObservedMeasurement<?>, ProcessEstimate) - Method in class org.orekit.estimation.sequential.KalmanModel
Finalize estimation.
finalizeEstimation(ObservedMeasurement<?>, ProcessEstimate) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Finalize estimation.
finalizeEstimation(ObservedMeasurement<?>, ProcessEstimate) - Method in interface org.orekit.estimation.sequential.SemiAnalyticalProcess
Finalize estimation.
finalizeEstimation(ObservedMeasurement<?>, ProcessEstimate) - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel
Finalize estimation.
finalizeEstimation(ObservedMeasurement<?>, ProcessEstimate) - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel
Finalize estimation.
finalizeHeader() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmParser
Finalize header after parsing.
finalizeHeader() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser
Finalize header after parsing.
finalizeHeader() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser
Finalize header after parsing.
finalizeHeader() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmParser
Finalize header after parsing.
finalizeHeader() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser
Finalize header after parsing.
finalizeHeader() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser
Finalize header after parsing.
finalizeHeader() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser
Finalize header after parsing.
finalizeHeader() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser
Finalize header after parsing.
finalizeHeader() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser
Finalize header after parsing.
finalizeHeader() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser
Finalize header after parsing.
finalizeMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmParser
Finalize metadata after parsing.
finalizeMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser
Finalize metadata after parsing.
finalizeMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser
Finalize metadata after parsing.
finalizeMetadata() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmParser
Finalize metadata after parsing.
finalizeMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser
Finalize metadata after parsing.
finalizeMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser
Finalize metadata after parsing.
finalizeMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser
Finalize metadata after parsing.
finalizeMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser
Finalize metadata after parsing.
finalizeMetadata() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser
Finalize metadata after parsing.
finalizeMetadata() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser
Finalize metadata after parsing.
finalizeMetadata(ContextBinding) - Method in class org.orekit.files.ccsds.ndm.odm.OdmCommonMetadata
Finalize the metadata.
finalizeOperationsObservationGrid() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Finalize estimation operations on the observation grid.
finalizeOperationsObservationGrid() - Method in interface org.orekit.estimation.sequential.SemiAnalyticalProcess
Finalize estimation operations on the observation grid.
finalizeOperationsObservationGrid() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel
Finalize estimation operations on the observation grid.
FIND_ROOT - org.orekit.errors.OrekitMessages
FIND_ROOT.
findByName(String) - Method in class org.orekit.utils.ParameterDriversList
Find a delegating driver by name.
findDelegatingSpanNameBySpanName(String) - Method in class org.orekit.utils.ParameterDriversList
Find a delegating driver by name.
findEOP(Frame) - Static method in class org.orekit.frames.FramesFactory
Retrieve EOP from a frame hierarchy.
findSatelliteAntenna(SatelliteSystem, int) - Method in class org.orekit.gnss.antenna.AntexLoader
Find the time map for a specific satellite antenna.
finish(List<SpacecraftState>) - Method in interface org.orekit.propagation.sampling.MultiSatFixedStepHandler
Finalize propagation.
finish(List<SpacecraftState>) - Method in interface org.orekit.propagation.sampling.MultiSatStepHandler
Finalize propagation.
finish(List<SpacecraftState>) - Method in class org.orekit.propagation.sampling.MultisatStepNormalizer
Finalize propagation.
finish(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldAdapterDetector
This method finalizes the event detector's job.
finish(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.events.FieldEventDetector
This method finalizes the event detector's job.
finish(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldEventState
This method finalizes the event detector's job.
finish(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.sampling.FieldOrekitFixedStepHandler
Finalize propagation.
finish(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.sampling.FieldOrekitStepHandler
Finalize propagation.
finish(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.sampling.FieldOrekitStepNormalizer
Finalize propagation.
finish(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.sampling.FieldStepHandlerMultiplexer
Finalize propagation.
finish(FieldSpacecraftState<T>, FieldEventDetector<T>) - Method in interface org.orekit.propagation.events.handlers.FieldEventHandler
This method finalize event handler at the end of a propagation.
finish(FieldSpacecraftState<T>, FieldEventDetector<T>) - Method in class org.orekit.propagation.events.handlers.FieldRecallLastOccurrence
This method finalize event handler at the end of a propagation.
finish(SpacecraftState) - Method in class org.orekit.files.ccsds.ndm.adm.aem.StreamingAemWriter.SegmentWriter
Finalize propagation.
finish(SpacecraftState) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.StreamingOcmWriter.BlockWriter
Finalize propagation.
finish(SpacecraftState) - Method in class org.orekit.files.ccsds.ndm.odm.oem.StreamingOemWriter.SegmentWriter
Finalize propagation.
finish(SpacecraftState) - Method in class org.orekit.files.ilrs.StreamingCpfWriter.Segment
Finalize propagation.
finish(SpacecraftState) - Method in class org.orekit.propagation.events.AdapterDetector
This method finalizes the event detector's job.
finish(SpacecraftState) - Method in interface org.orekit.propagation.events.EventDetector
This method finalizes the event detector's job.
finish(SpacecraftState) - Method in class org.orekit.propagation.events.EventState
This method finalizes the event detector's job.
finish(SpacecraftState) - Method in interface org.orekit.propagation.sampling.OrekitFixedStepHandler
Finalize propagation.
finish(SpacecraftState) - Method in interface org.orekit.propagation.sampling.OrekitStepHandler
Finalize propagation.
finish(SpacecraftState) - Method in class org.orekit.propagation.sampling.OrekitStepNormalizer
Finalize propagation.
finish(SpacecraftState) - Method in class org.orekit.propagation.sampling.StepHandlerMultiplexer
Finalize propagation.
finish(SpacecraftState, EventDetector) - Method in interface org.orekit.propagation.events.handlers.EventHandler
This method finalizes the event handler's job.
finish(SpacecraftState, EventDetector) - Method in class org.orekit.propagation.events.handlers.EventMultipleHandler
 
finish(SpacecraftState, EventDetector) - Method in class org.orekit.propagation.events.handlers.RecallLastOccurrence
This method finalizes the event handler's job.
finished(TaskEvent) - Method in class org.orekit.compiler.plugin.DefaultDataContextPlugin
 
FiniteDifferencePropagatorConverter - Class in org.orekit.propagation.conversion
Propagator converter using finite differences to compute the Jacobian.
FiniteDifferencePropagatorConverter(PropagatorBuilder, double, int) - Constructor for class org.orekit.propagation.conversion.FiniteDifferencePropagatorConverter
Simple constructor.
fit() - Method in class org.orekit.utils.SecularAndHarmonic
Fit parameters.
fit(EOPHistory) - Method in class org.orekit.frames.EOPFitter
Fit raw history.
fit(EOPHistory, ToDoubleFunction<EOPEntry>) - Method in class org.orekit.frames.SingleParameterFitter
Perform secular and harmonic fitting.
FIT - org.orekit.files.sp3.SP3OrbitType
fitted.
FIXED - org.orekit.files.stk.STKEphemerisFile.STKCoordinateSystem
Fixed frame.
FIXED_F10P7 - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey
Fixed (time invariant) value of the Solar Flux Unit daily proxy F10.7.
FIXED_F10P7_MEAN - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey
Fixed (time invariant) value of the Solar Flux Unit 81-day running center-average proxy F10.7.
FIXED_GEOMAG_AP - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey
Fixed (time invariant) value of the planetary 3-hour-range geomagnetic index aₚ.
FIXED_GEOMAG_DST - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey
Fixed (time invariant) value of the planetary 1-hour-range geomagnetic index Dst.
FIXED_GEOMAG_KP - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey
Fixed (time invariant) value of the planetary 3-hour-range geomagnetic index Kₚ.
FIXED_M10P7 - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey
Fixed (time invariant) value of the Solar Flux daily proxy M10.7.
FIXED_M10P7_MEAN - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey
Fixed (time invariant) value of the Solar Flux 81-day running center-average proxy M10.7.
FIXED_S10P7 - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey
Fixed (time invariant) value of the Solar Flux daily proxy S10.7.
FIXED_S10P7_MEAN - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey
Fixed (time invariant) value of the Solar Flux 81-day running center-average proxy S10.7.
FIXED_Y10P7 - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey
Fixed (time invariant) value of the Solar Flux daily proxy Y10.7.
FIXED_Y10P7_MEAN - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey
Fixed (time invariant) value of the Solar Flux 81-day running center-average proxy Y10.7.
FixedFrameBuilder - Class in org.orekit.attitudes
Builder that assumes angular coordinates are given in a fixed frame.
FixedFrameBuilder(Frame) - Constructor for class org.orekit.attitudes.FixedFrameBuilder
Creates new instance.
FixedNumberInterpolationGrid - Class in org.orekit.propagation.semianalytical.dsst.utilities
Interpolation grid where a fixed number of points are evenly spaced between the start and the end of the integration step.
FixedNumberInterpolationGrid(int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FixedNumberInterpolationGrid
Constructor.
FixedPanel - Class in org.orekit.forces
Class representing one panel of a satellite, fixed with respect to satellite body.
FixedPanel(Vector3D, double, boolean, double, double, double, double) - Constructor for class org.orekit.forces.FixedPanel
Simple constructor.
FixedPointOsculatingToAveragedConverter<T extends AveragedOrbitalState> - Class in org.orekit.propagation.conversion.averaging.converters
Abstract class for osculating-to-averaged converters based on a fixed-point algorithm.
FixedPointOsculatingToAveragedConverter(double, int) - Constructor for class org.orekit.propagation.conversion.averaging.converters.FixedPointOsculatingToAveragedConverter
Protected constructor.
FixedPointTleGenerationAlgorithm - Class in org.orekit.propagation.analytical.tle.generation
Fixed Point method to reverse SGP4 and SDP4 propagation algorithm and generate a usable TLE from a spacecraft state.
FixedPointTleGenerationAlgorithm() - Constructor for class org.orekit.propagation.analytical.tle.generation.FixedPointTleGenerationAlgorithm
Default constructor.
FixedPointTleGenerationAlgorithm(double, int, double) - Constructor for class org.orekit.propagation.analytical.tle.generation.FixedPointTleGenerationAlgorithm
Constructor.
FixedPointTleGenerationAlgorithm(double, int, double, TimeScale, Frame) - Constructor for class org.orekit.propagation.analytical.tle.generation.FixedPointTleGenerationAlgorithm
Constructor.
FixedRate - Class in org.orekit.attitudes
This class handles a simple attitude provider at constant rate around a fixed axis.
FixedRate(Attitude) - Constructor for class org.orekit.attitudes.FixedRate
Creates a new instance.
FixedStepSelector - Class in org.orekit.time
Selector generating a continuous stream of dates separated by a constant step.
FixedStepSelector(double, TimeScale) - Constructor for class org.orekit.time.FixedStepSelector
Simple constructor.
FixedTimeBoundaryOrbits - Class in org.orekit.control.indirect.shooting.boundary
Defines two-point boundary values for indirect shooting methods with Cartesian coordinates.
FixedTimeBoundaryOrbits(Orbit, Orbit) - Constructor for class org.orekit.control.indirect.shooting.boundary.FixedTimeBoundaryOrbits
Constructor.
FixedTimeCartesianBoundaryStates - Class in org.orekit.control.indirect.shooting.boundary
Defines two-point boundary values for indirect shooting methods with Cartesian coordinates.
FixedTimeCartesianBoundaryStates(AbsolutePVCoordinates, AbsolutePVCoordinates) - Constructor for class org.orekit.control.indirect.shooting.boundary.FixedTimeCartesianBoundaryStates
Constructor.
FixedTransformProvider - Class in org.orekit.frames
Transform provider using fixed transform.
FixedTransformProvider(Transform) - Constructor for class org.orekit.frames.FixedTransformProvider
Simple constructor.
FixedTroposphericDelay - Class in org.orekit.models.earth.troposphere
A static tropospheric model that interpolates the actual tropospheric delay based on values read from a configuration file (tropospheric-delay.txt) via the DataProvidersManager.
FixedTroposphericDelay(double[], double[], double[][]) - Constructor for class org.orekit.models.earth.troposphere.FixedTroposphericDelay
Creates a new FixedTroposphericDelay instance.
FixedTroposphericDelay(String) - Constructor for class org.orekit.models.earth.troposphere.FixedTroposphericDelay
Creates a new FixedTroposphericDelay instance, and loads the delay values from the given resource via the default data context.
FixedTroposphericDelay(String, DataProvidersManager) - Constructor for class org.orekit.models.earth.troposphere.FixedTroposphericDelay
Creates a new FixedTroposphericDelay instance, and loads the delay values from the given resource via the specified data manager.
fixIntegerAmbiguities(int, List<ParameterDriver>, RealMatrix) - Method in class org.orekit.estimation.measurements.gnss.AmbiguitySolver
Fix integer ambiguities.
FLOW_RATE - Static variable in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
Parameter name for flow rate.
FLOW_RATE_SCALE - Static variable in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
Flow rate scaling factor.
FootprintOverlapDetector - Class in org.orekit.propagation.events
Detector triggered by geographical region entering/leaving a spacecraft sensor Field Of View.
FootprintOverlapDetector(FieldOfView, OneAxisEllipsoid, SphericalPolygonsSet, double) - Constructor for class org.orekit.propagation.events.FootprintOverlapDetector
Build a new instance.
FootprintOverlapDetector(AdaptableInterval, double, int, EventHandler, FieldOfView, OneAxisEllipsoid, SphericalPolygonsSet, double, List<FootprintOverlapDetector.SamplingPoint>) - Constructor for class org.orekit.propagation.events.FootprintOverlapDetector
Protected constructor with full parameters.
ForceModel - Interface in org.orekit.forces
This interface represents a force modifying spacecraft motion.
ForceModelContext - Class in org.orekit.propagation.semianalytical.dsst.forces
Base class for dsst force models attributes containers.
ForceModelContext(AuxiliaryElements) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.ForceModelContext
Simple constructor.
forEach(Consumer<T>) - Method in class org.orekit.utils.TimeSpanMap
Performs an action for each non-null element of map.
format(double) - Static method in class org.orekit.utils.AccurateFormatter
Format a double number.
format(int, int, int, int, int, double) - Static method in class org.orekit.utils.AccurateFormatter
Format a date.
FORMAT_VERSION_KEY - Static variable in class org.orekit.files.ccsds.ndm.adm.acm.Acm
Key for format version.
FORMAT_VERSION_KEY - Static variable in class org.orekit.files.ccsds.ndm.adm.aem.Aem
Key for format version.
FORMAT_VERSION_KEY - Static variable in class org.orekit.files.ccsds.ndm.adm.apm.Apm
Key for format version.
FORMAT_VERSION_KEY - Static variable in class org.orekit.files.ccsds.ndm.cdm.Cdm
Key for format version.
FORMAT_VERSION_KEY - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.Ocm
Key for format version.
FORMAT_VERSION_KEY - Static variable in class org.orekit.files.ccsds.ndm.odm.oem.Oem
Key for format version.
FORMAT_VERSION_KEY - Static variable in class org.orekit.files.ccsds.ndm.odm.omm.Omm
Key for format version.
FORMAT_VERSION_KEY - Static variable in class org.orekit.files.ccsds.ndm.odm.opm.Opm
Key for format version.
FORMAT_VERSION_KEY - Static variable in class org.orekit.files.ccsds.ndm.tdm.Tdm
Key for format version.
formatIntegerOrNaN(int, int) - Static method in class org.orekit.files.ilrs.CRD
Format the integer value as a string, or the string VALUE_NOT_AVAILABLE.
formatUtcOffset() - Method in class org.orekit.time.TimeComponents
Get the UTC offset as a string in ISO8601 format.
formFieldRelativePosition(FieldAbsoluteDate<T>, T[], Frame) - Method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointNonCentralBodyTerm
Form relative position vector w.r.t.
formRelativePosition(AbsoluteDate, double[], Frame) - Method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointNonCentralBodyTerm
Form relative position vector w.r.t.
forwardSignalTimeOfFlight(TimeStampedFieldPVCoordinates<T>, FieldVector3D<T>, FieldAbsoluteDate<T>) - Static method in class org.orekit.estimation.measurements.TDOA
Compute propagation delay on a link leg (typically downlink or uplink).This differs from signalTimeOfFlight through advancing rather than delaying the emitter.
forwardSignalTimeOfFlight(TimeStampedPVCoordinates, Vector3D, AbsoluteDate) - Static method in class org.orekit.estimation.measurements.TDOA
Compute propagation delay on a link leg (typically downlink or uplink).
FOSTER_1992 - org.orekit.files.ccsds.definitions.PocMethodType
Foster 1992 method.
Frame - Class in org.orekit.frames
Tridimensional references frames class.
Frame(Frame, TransformProvider, String) - Constructor for class org.orekit.frames.Frame
Build a non-inertial frame from its transform with respect to its parent.
Frame(Frame, TransformProvider, String, boolean) - Constructor for class org.orekit.frames.Frame
Build a frame from its transform with respect to its parent.
Frame(Frame, Transform, String) - Constructor for class org.orekit.frames.Frame
Build a non-inertial frame from its transform with respect to its parent.
Frame(Frame, Transform, String, boolean) - Constructor for class org.orekit.frames.Frame
Build a frame from its transform with respect to its parent.
FRAME_ALREADY_ATTACHED - org.orekit.errors.OrekitMessages
FRAME_ALREADY_ATTACHED.
FRAME_ANCESTOR_OF_BOTH_FRAMES - org.orekit.errors.OrekitMessages
FRAME_ANCESTOR_OF_BOTH_FRAMES.
FRAME_ANCESTOR_OF_NEITHER_FRAME - org.orekit.errors.OrekitMessages
FRAME_ANCESTOR_OF_NEITHER_FRAME.
FRAME_NO_NTH_ANCESTOR - org.orekit.errors.OrekitMessages
FRAME_NO_NTH_ANCESTOR.
FRAME_NOT_ALLOWED - org.orekit.errors.OrekitMessages
FRAME_NOT_ALLOWED.
FRAME_NOT_ATTACHED - org.orekit.errors.OrekitMessages
FRAME_NOT_ATTACHED.
FrameAdapter - Class in org.orekit.utils
FrameAdapter(Frame) - Constructor for class org.orekit.utils.FrameAdapter
Simple constructor.
FrameAlignedProvider - Class in org.orekit.attitudes
This class handles an attitude provider aligned with a frame or a fixed offset to it.
FrameAlignedProvider(Rotation) - Constructor for class org.orekit.attitudes.FrameAlignedProvider
Creates new instance.
FrameAlignedProvider(Rotation, Frame) - Constructor for class org.orekit.attitudes.FrameAlignedProvider
Creates new instance with a fixed attitude in the given frame.
FrameAlignedProvider(Frame) - Constructor for class org.orekit.attitudes.FrameAlignedProvider
Creates new instance aligned with the given frame.
FrameAncestorException - Exception in org.orekit.errors
This class is the base class for exception thrown by the UpdatableFrame.updateTransform method.
FrameAncestorException(Localizable, Object...) - Constructor for exception org.orekit.errors.FrameAncestorException
Simple constructor.
FrameFacade - Class in org.orekit.files.ccsds.definitions
Facade in front of several frames types in CCSDS messages.
FrameFacade(Frame, CelestialBodyFrame, OrbitRelativeFrame, SpacecraftBodyFrame, String) - Constructor for class org.orekit.files.ccsds.definitions.FrameFacade
Simple constructor.
frameName(Frame) - Static method in class org.orekit.gnss.IGSUtils
Guess a frame name.
Frames - Interface in org.orekit.frames
A collection of commonly used Frames.
FRAMES_MISMATCH - org.orekit.errors.OrekitMessages
FRAMES_MISMATCH.
FramesFactory - Class in org.orekit.frames
Factory for predefined reference frames.
freeze() - Method in class org.orekit.frames.FieldTransform
Get a frozen transform.
freeze() - Method in class org.orekit.frames.Transform
Get a frozen transform.
freezeColumnsNames() - Method in class org.orekit.propagation.AbstractMatricesHarvester
Freeze the names of the Jacobian columns.
freezeColumnsNames() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester
Freeze the names of the Jacobian columns.
freezeColumnsNames() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester
Freeze the names of the Jacobian columns.
FREQ_OFFSET - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Frequency offset entry.
Frequency - Enum in org.orekit.gnss
Enumerate for GNSS frequencies.
FrequencyPattern - Class in org.orekit.gnss.antenna
Pattern for GNSS antenna model on one frequency.
FrequencyPattern(Vector3D, PhaseCenterVariationFunction) - Constructor for class org.orekit.gnss.antenna.FrequencyPattern
Simple constructor.
fromSeconds(int, double, double, int) - Static method in class org.orekit.time.TimeComponents
Build a time from the second number within the day.
fromSI(double) - Method in class org.orekit.utils.units.Unit
Convert a value from SI units.
fromSI(Double) - Method in class org.orekit.utils.units.Unit
Convert a value from SI units.
fromSI(T) - Method in class org.orekit.utils.units.Unit
Convert a value from SI units.
FrRangeMeasurement(AbsoluteDate, double, int, String, int, int, int, int, int) - Constructor for class org.orekit.files.ilrs.CRD.FrRangeMeasurement
Constructor.
FULL - org.orekit.files.ccsds.ndm.odm.ocm.Ordering
Full symmetric Matrix.
FULL_RATE - org.orekit.files.ilrs.CRDHeader.DataType
Full rate.
FUNCTION_NOT_IMPLEMENTED - org.orekit.errors.OrekitMessages
FUNCTION_NOT_IMPLEMENTED.
FunctionalDetector - Class in org.orekit.propagation.events
A detector that implements the FunctionalDetector.g(SpacecraftState) function using a lambda that can be set using FunctionalDetector.withFunction(ToDoubleFunction).
FunctionalDetector() - Constructor for class org.orekit.propagation.events.FunctionalDetector
Create an event detector with the default values.
FunctionalDetector(AdaptableInterval, double, int, EventHandler, ToDoubleFunction<SpacecraftState>) - Constructor for class org.orekit.propagation.events.FunctionalDetector
Private constructor.
FundamentalNutationArguments - Class in org.orekit.data
Class computing the fundamental arguments for nutation and tides.
FundamentalNutationArguments(IERSConventions, TimeScale, InputStream, String) - Constructor for class org.orekit.data.FundamentalNutationArguments
Build a model of fundamental arguments from an IERS table file.
FundamentalNutationArguments(IERSConventions, TimeScale, InputStream, String, TimeScales) - Constructor for class org.orekit.data.FundamentalNutationArguments
Build a model of fundamental arguments from an IERS table file.
FundamentalNutationArguments(IERSConventions, TimeScale, List<double[]>) - Constructor for class org.orekit.data.FundamentalNutationArguments
Build a model of fundamental arguments from an IERS table file.
FundamentalNutationArguments(IERSConventions, TimeScale, List<double[]>, TimeScales) - Constructor for class org.orekit.data.FundamentalNutationArguments
Build a model of fundamental arguments from an IERS table file.
FUTURE_INFINITY - Static variable in class org.orekit.time.AbsoluteDate
Dummy date at infinity in the future direction.

G

g(FieldSpacecraftState<T>) - Method in class org.orekit.forces.maneuvers.FieldImpulseManeuver
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldAdapterDetector
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldAltitudeDetector
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldApsideDetector
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldBetaAngleDetector
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldBooleanDetector
 
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldCylindricalShadowEclipseDetector
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldDateDetector
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldEclipseDetector
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldElevationDetector
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldElevationExtremumDetector
Compute the value of the detection function.
g(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.events.FieldEventDetector
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldEventEnablingPredicateFilter
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldEventSlopeFilter
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldExtremumApproachDetector
The g is positive when the primary object is getting further away from the secondary object and is negative when it is getting closer to it.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldFunctionalDetector
 
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldLatitudeCrossingDetector
Compute the value of the detection function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldLatitudeRangeCrossingDetector
Compute the value of the detection function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldLongitudeCrossingDetector
Compute the value of the detection function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldLongitudeRangeCrossingDetector
Compute the value of the detection function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldNegateDetector
 
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldNodeDetector
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldRelativeDistanceDetector
The g is positive when the relative distance is larger or equal than the threshold, non-positive otherwise.
g(SpacecraftState) - Method in class org.orekit.attitudes.AttitudesSequence.Switch
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.AdapterDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.AlignmentDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.AltitudeDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.AngularSeparationDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.AngularSeparationFromSatelliteDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.ApsideDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.BetaAngleDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.BooleanDetector
 
g(SpacecraftState) - Method in class org.orekit.propagation.events.CylindricalShadowEclipseDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.DateDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.EclipseDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.ElevationDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.ElevationExtremumDetector
Compute the value of the detection function.
g(SpacecraftState) - Method in interface org.orekit.propagation.events.EventDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.EventEnablingPredicateFilter
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.EventShifter
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.EventSlopeFilter
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.ExtremumApproachDetector
The g is positive when the primary object is getting further away from the secondary object and is negative when it is getting closer to it.
g(SpacecraftState) - Method in class org.orekit.propagation.events.FieldOfViewDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.FootprintOverlapDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.FunctionalDetector
 
g(SpacecraftState) - Method in class org.orekit.propagation.events.GeographicZoneDetector
Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.GroundAtNightDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.GroundFieldOfViewDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.HaloXZPlaneCrossingDetector
Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.InterSatDirectViewDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.LatitudeCrossingDetector
Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.LatitudeExtremumDetector
Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.LatitudeRangeCrossingDetector
Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.LongitudeCrossingDetector
Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.LongitudeExtremumDetector
Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.LongitudeRangeCrossingDetector
Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.MagneticFieldDetector
Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.NegateDetector
 
g(SpacecraftState) - Method in class org.orekit.propagation.events.NodeDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.PositionAngleDetector
Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.RelativeDistanceDetector
The g is positive when the relative distance is larger or equal than the threshold, non-positive otherwise.
G0_STANDARD_GRAVITY - Static variable in interface org.orekit.utils.Constants
Standard gravity constant, used in maneuvers definition: 9.80665 m/s².
G01 - org.orekit.gnss.Frequency
GPS L1 (1575.42 MHz).
G02 - org.orekit.gnss.Frequency
GPS L2 (1227.6 MHz).
G05 - org.orekit.gnss.Frequency
GPS L5 (1176.45 MHz).
GAGAN - org.orekit.files.rinex.navigation.SbasId
GPS Aided Geo Augmented Navigation.
GAL - org.orekit.files.rinex.navigation.IonosphericCorrectionType
Galileo.
GAL - org.orekit.files.rinex.navigation.UtcId
UTCGAL.
GAL - org.orekit.gnss.metric.ntrip.NavigationSystem
Galileo.
GAL - org.orekit.gnss.ObservationTimeScale
Galileo time scale.
Galileo - Class in org.orekit.gnss.attitude
Attitude providers for Galileo navigation satellites.
Galileo(double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.Galileo
Simple constructor.
GALILEO - org.orekit.files.sp3.SP3FileType
Galileo only file.
GALILEO - org.orekit.gnss.SatelliteSystem
Galileo system.
GALILEO - org.orekit.gnss.TimeSystem
GALILEO.
GALILEO_0A - org.orekit.gnss.antenna.SatelliteType
Galileo In-Orbit Validation Element A (GIOVE-A).
GALILEO_0B - org.orekit.gnss.antenna.SatelliteType
Galileo In-Orbit Validation Element B (GIOVE-B).
GALILEO_1 - org.orekit.gnss.antenna.SatelliteType
Galileo IOV : GSAT 0101-0104.
GALILEO_2 - org.orekit.gnss.antenna.SatelliteType
Galileo FOC : GSAT 0201-0222.
GALILEO_AV - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
Value of the earth's rotation rate in rad/s for Galileo user.
GALILEO_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Reference epoch for Galileo System Time: 1999-08-22T00:00:00 GST.
GALILEO_EPOCH - Static variable in class org.orekit.time.DateComponents
Reference epoch for Galileo System Time: 1999-08-22.
GALILEO_MU - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
Earth's universal gravitational parameter for Galileo user in m³/s².
GALILEO_WEEK_NB - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
Number of weeks in the Galileo cycle.
GalileoAlmanac - Class in org.orekit.propagation.analytical.gnss.data
Class for Galileo almanac.
GalileoAlmanac() - Constructor for class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac
Build a new almanac.
GalileoNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data
Container for data contained in a Galileo navigation message.
GalileoNavigationMessage() - Constructor for class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage
Constructor.
GalileoScale - Class in org.orekit.time
Galileo system time scale.
GammaMnsFunction - Class in org.orekit.propagation.semianalytical.dsst.utilities
Compute the Γmn,s(γ) function from equation 2.7.1-(13).
GammaMnsFunction(int, double, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.GammaMnsFunction
Simple constructor.
GatheringSubscriber - Class in org.orekit.estimation.measurements.generation
Subscriber that gather all generated measurements in a sorted set.
GatheringSubscriber() - Constructor for class org.orekit.estimation.measurements.generation.GatheringSubscriber
Simple constructor.
GCRF - org.orekit.files.ccsds.definitions.CelestialBodyFrame
Geocentric Celestial Reference Frame.
GCRF - org.orekit.frames.Predefined
GCRF frame.
GDOP - org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey
Generalize Dilution Of Precision.
GEGOUT - org.orekit.forces.gravity.potential.OceanLoadDeformationCoefficients
Coefficients computed by Pascal Gégout, CNRS / UMR5563 (GET).
generate(Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.AbstractScheduler
Generate a sequence of measurements.
generate(Map<ObservableSatellite, OrekitStepInterpolator>) - Method in interface org.orekit.estimation.measurements.generation.Scheduler
Generate a sequence of measurements.
generate(FieldSpacecraftState<T>, FieldTLE<T>) - Method in class org.orekit.propagation.analytical.tle.generation.FixedPointTleGenerationAlgorithm
Generate a TLE from a given spacecraft state and a template TLE.
generate(FieldSpacecraftState<T>, FieldTLE<T>) - Method in class org.orekit.propagation.analytical.tle.generation.LeastSquaresTleGenerationAlgorithm
Generate a TLE from a given spacecraft state and a template TLE.
generate(FieldSpacecraftState<T>, FieldTLE<T>) - Method in interface org.orekit.propagation.analytical.tle.generation.TleGenerationAlgorithm
Generate a TLE from a given spacecraft state and a template TLE.
generate(SpacecraftState, TLE) - Method in class org.orekit.propagation.analytical.tle.generation.FixedPointTleGenerationAlgorithm
Generate a TLE from a given spacecraft state and a template TLE.
generate(SpacecraftState, TLE) - Method in class org.orekit.propagation.analytical.tle.generation.LeastSquaresTleGenerationAlgorithm
Generate a TLE from a given spacecraft state and a template TLE.
generate(SpacecraftState, TLE) - Method in interface org.orekit.propagation.analytical.tle.generation.TleGenerationAlgorithm
Generate a TLE from a given spacecraft state and a template TLE.
generate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.estimation.measurements.generation.Generator
Generate measurements.
generate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.frames.FieldTransformGenerator
Generate a chronologically sorted list of entries to be cached.
generate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.frames.TransformGenerator
Generate a chronologically sorted list of entries to be cached.
generate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData.SolarActivityGenerator
Generate a chronologically sorted list of entries to be cached.
generate(AbsoluteDate, AbsoluteDate) - Method in interface org.orekit.utils.TimeStampedGenerator
Generate a chronologically sorted list of entries to be cached.
generateCartesianOrbit() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm
Generate a Cartesian orbit.
generateData(boolean, boolean, RotationOrder, boolean, TimeStampedAngularCoordinates) - Method in enum org.orekit.files.ccsds.ndm.adm.AttitudeType
Generate the attitude data corresponding to the attitude type.
generateDataFromEarliestToLatestDates(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData.SolarActivityGenerator
Generate a list of parameters between earliest and latest dates.
GeneratedMeasurementSubscriber - Interface in org.orekit.estimation.measurements.generation
Interface for subscribing to generated measurements events.
generateException(Exception) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Generate a parse exception for this entry.
generateKeplerianOrbit() - Method in class org.orekit.files.ccsds.ndm.odm.omm.Omm
Generate a keplerian orbit.
generateKeplerianOrbit() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm
Generate a keplerian orbit.
generateKeplerianOrbit(Frame) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Generate a keplerian orbit.
generateSpacecraftState() - Method in class org.orekit.files.ccsds.ndm.odm.omm.Omm
Generate spacecraft state from the CartesianOrbit generated by generateCartesianOrbit.
generateSpacecraftState() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm
Generate spacecraft state from the CartesianOrbit generated by generateCartesianOrbit.
generateTesseralPolynomials(int, int, int, int, int, int, PolynomialFunction[][], PolynomialFunction[][]) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities
Generate the polynomials needed in the linear transformation.
generateThirdBodyPolynomials(int, int, int, int, PolynomialFunction[][], PolynomialFunction[][]) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities
Generate the polynomials needed in the linear transformation.
generateTLE() - Method in class org.orekit.files.ccsds.ndm.odm.omm.Omm
Generate TLE from OMM file.
generateZonalPolynomials(int, int, int, int, int, PolynomialFunction[][], PolynomialFunction[][]) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities
Generate the polynomials needed in the linear transformation.
Generator - Class in org.orekit.estimation.measurements.generation
Main generator for observed measurements.
Generator - Interface in org.orekit.files.ccsds.utils.generation
Generation interface for CCSDS messages.
Generator() - Constructor for class org.orekit.estimation.measurements.generation.Generator
Build a generator with no sequences generator.
GenericGNSS - Class in org.orekit.gnss.attitude
Attitude providers for navigation satellites for which no specialized model is known.
GenericGNSS(AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.GenericGNSS
Simple constructor.
GenericTimeStampedCache<T extends TimeStamped> - Class in org.orekit.utils
Generic thread-safe cache for time-stamped data.
GenericTimeStampedCache(int, int, double, double, TimeStampedGenerator<T>) - Constructor for class org.orekit.utils.GenericTimeStampedCache
Simple constructor.
GenericTimeStampedCache(int, int, double, double, TimeStampedGenerator<T>, double) - Constructor for class org.orekit.utils.GenericTimeStampedCache
Simple constructor with overriding minimum step.
GEO - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCategory
Geosynchronous Earth Orbit, with i > 3°, 35586 < hp < 35986 km, 35586 < ha < 35986 km.
GEO - org.orekit.propagation.analytical.gnss.data.BeidouSatelliteType
Geostationary satellite.
GEODETIC - org.orekit.files.ccsds.ndm.odm.ocm.OrbitElementsType
Geodetic elements (λ, ΦGD, β, A, h, vre).
GeodeticPoint - Class in org.orekit.bodies
Point location relative to a 2D body surface.
GeodeticPoint(double, double, double) - Constructor for class org.orekit.bodies.GeodeticPoint
Build a new instance.
geodeticToIsometricLatitude(double) - Method in class org.orekit.bodies.OneAxisEllipsoid
Compute the isometric latitude corresponding to the provided latitude.
geodeticToIsometricLatitude(T) - Method in class org.orekit.bodies.OneAxisEllipsoid
Compute the isometric latitude corresponding to the provided latitude.
GeographicZoneDetector - Class in org.orekit.propagation.events
Detector for entry/exit of a zone defined by geographic boundaries.
GeographicZoneDetector(double, double, BodyShape, SphericalPolygonsSet, double) - Constructor for class org.orekit.propagation.events.GeographicZoneDetector
Build a detector.
GeographicZoneDetector(BodyShape, SphericalPolygonsSet, double) - Constructor for class org.orekit.propagation.events.GeographicZoneDetector
Build a new detector.
GeographicZoneDetector(AdaptableInterval, double, int, EventHandler, BodyShape, SphericalPolygonsSet, EnclosingBall<Sphere2D, S2Point>, double) - Constructor for class org.orekit.propagation.events.GeographicZoneDetector
Protected constructor with full parameters.
Geoid - Class in org.orekit.models.earth
A geoid is a level surface of the gravity potential of a body.
Geoid(NormalizedSphericalHarmonicsProvider, ReferenceEllipsoid) - Constructor for class org.orekit.models.earth.Geoid
Creates a geoid from the given geopotential, reference ellipsoid and the assumptions in the comment for Geoid.
GeoMagneticElements - Class in org.orekit.models.earth
Contains the elements to represent a magnetic field at a single point.
GeoMagneticElements(Vector3D) - Constructor for class org.orekit.models.earth.GeoMagneticElements
Construct a new element with the given field vector.
GeoMagneticField - Class in org.orekit.models.earth
Used to calculate the geomagnetic field at a given geodetic point on earth.
GeoMagneticField(String, double, int, int, double, double) - Constructor for class org.orekit.models.earth.GeoMagneticField
Create a new geomagnetic field model with the given parameters.
GeoMagneticFieldFactory - Class in org.orekit.models.earth
Factory for different GeoMagneticField models.
GeoMagneticFieldFactory.FieldModel - Enum in org.orekit.models.earth
The currently supported geomagnetic field models.
GeoMagneticFields - Interface in org.orekit.models.earth
Methods for obtaining geomagnetic fields.
GeoMagneticModelLoader - Class in org.orekit.models.earth
Loads geomagnetic field models from a given input stream.
GeoMagneticModelLoader() - Constructor for class org.orekit.models.earth.GeoMagneticModelLoader
Empty constructor.
GEOMETRY_FREE - org.orekit.estimation.measurements.gnss.CombinationType
Geometry-free combination.
GeometryFreeCombination - Class in org.orekit.estimation.measurements.gnss
Geometry-free combination.
GeometryFreeCycleSlipDetector - Class in org.orekit.estimation.measurements.gnss
Geometry free cycle slip detectors.
GeometryFreeCycleSlipDetector(double, double, int) - Constructor for class org.orekit.estimation.measurements.gnss.GeometryFreeCycleSlipDetector
Constructor.
get(String) - Method in class org.orekit.utils.DoubleArrayDictionary
Get the value corresponding to a key.
get(String) - Method in class org.orekit.utils.FieldArrayDictionary
Get the value corresponding to a key.
get(AbsoluteDate) - Method in class org.orekit.utils.TimeSpanMap
Get the entry valid at a specified date.
get(FieldAbsoluteDate<D>) - Method in class org.orekit.utils.FieldTimeSpanMap
Get the entry valid at a specified date.
get24HoursKp(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
Get the last 24H mean geomagnetic index.
get24HoursKp(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
The Kp index is derived from the Ap index.
get24HoursKp(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.DTM2000InputParameters
Get the last 24H mean geomagnetic index.
getA() - Method in class org.orekit.attitudes.FieldInertiaAxis
Get the inertia axis.
getA() - Method in class org.orekit.attitudes.InertiaAxis
Get the inertia axis.
getA() - Method in class org.orekit.bodies.Ellipse
Get the semi major axis.
getA() - Method in class org.orekit.bodies.Ellipsoid
Get the length of the first semi-axis.
getA() - Method in class org.orekit.bodies.FieldEllipse
Get the semi major axis.
getA() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Get the orbit semi-major axis.
getA() - Method in class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader
Returns the a coefficients array.
getA() - Method in class org.orekit.models.earth.weather.GlobalPressureTemperature2Model
Deprecated.
Returns the a coefficients array.
getA() - Method in class org.orekit.orbits.CartesianOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.CircularOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.FieldOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.KeplerianOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.Orbit
Get the semi-major axis.
getA() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the semi-major axis.
getA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTGravityContext
Getter for the a.
getA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext
Get A = sqrt(μ * a).
getA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext
Get A = sqrt(μ * a).
getA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTGravityContext
A = sqrt(μ * a).
getA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext
Get A = sqrt(μ * a).
getA() - Method in class org.orekit.propagation.SpacecraftState
Get the semi-major axis.
getA(FieldGeodeticPoint<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.ConstantViennaAProvider
Get coefficients array for VMF mapping function.
getA(FieldGeodeticPoint<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.models.earth.troposphere.ViennaAProvider
Get coefficients array for VMF mapping function.
getA(FieldGeodeticPoint<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.weather.AbstractGlobalPressureTemperature
Get coefficients array for VMF mapping function.
getA(GeodeticPoint, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.ConstantViennaAProvider
Get coefficients array for VMF mapping function.
getA(GeodeticPoint, AbsoluteDate) - Method in interface org.orekit.models.earth.troposphere.ViennaAProvider
Get coefficients array for VMF mapping function.
getA(GeodeticPoint, AbsoluteDate) - Method in class org.orekit.models.earth.weather.AbstractGlobalPressureTemperature
Get coefficients array for VMF mapping function.
getA0() - Method in class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage
Get the constant term of the offset.
getA0() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D
Get A0 field.
getA1() - Method in class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage
Get the linear term of the offset.
getA1() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D
Get A₁ field.
getA2() - Method in class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage
Get the quadratic term of the offset.
getA4() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTJ2SquaredClosedFormContext
Get the semi major axis to the power 4.
getA4() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTJ2SquaredClosedFormContext
Get the semi major axis to the power 4.
getAbscissaGrid() - Method in class org.orekit.utils.InterpolationTableLoader
Returns a copy of the abscissa grid for the interpolation function.
getAbsoluteDate() - Method in class org.orekit.utils.FieldTimeSpanMap.Transition
Get the transition field absolute date.
getAbsorption() - Method in class org.orekit.forces.Panel
Get radiation pressure absorption coefficient.
getAbsPVA() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the absolute position-velocity-acceleration.
getAbsPVA() - Method in class org.orekit.propagation.SpacecraftState
Get the absolute position-velocity-acceleration.
getAbsPVAInterpolator() - Method in class org.orekit.propagation.FieldSpacecraftStateInterpolator
Get absolute position-velocity-acceleration interpolator.
getAbsPVAInterpolator() - Method in class org.orekit.propagation.SpacecraftStateInterpolator
Get absolute position-velocity-acceleration interpolator.
getAcceleration() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Get acceleration.
getAcceleration() - Method in class org.orekit.frames.FieldTransform
Get the second time derivative of the translation.
getAcceleration() - Method in class org.orekit.frames.Transform
Get the second time derivative of the translation.
getAcceleration() - Method in class org.orekit.time.ClockOffset
Get acceleration.
getAcceleration() - Method in class org.orekit.time.FieldClockOffset
Get acceleration.
getAcceleration() - Method in class org.orekit.utils.FieldPVCoordinates
Gets the acceleration.
getAcceleration() - Method in class org.orekit.utils.PVCoordinates
Gets the acceleration.
getAcceleration(Transform, double[]) - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointInertialTerm
Evaluates the inertial acceleration vector.
getAcceleration(FieldSpacecraftState<T>, FieldAttitude<T>, T[]) - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel
Get the acceleration of the spacecraft during maneuver and in maneuver frame.
getAcceleration(FieldSpacecraftState<T>, FieldAttitude<T>, T[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
Get the acceleration of the spacecraft during maneuver and in maneuver frame.
getAcceleration(SpacecraftState, Attitude, double[]) - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel
Get the acceleration of the spacecraft during maneuver and in maneuver frame.
getAcceleration(SpacecraftState, Attitude, double[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
Get the acceleration of the spacecraft during maneuver and in maneuver frame.
getAcceleration(AbsoluteDate, double[], Frame) - Method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointEquationTerm
Compute the acceleration vector.
getAcceleration(AbsoluteDate, double[], Frame) - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointInertialTerm
Compute the acceleration vector.
getAcceleration(AbsoluteDate, double[], Frame) - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointJ2Term
Compute the acceleration vector.
getAcceleration(AbsoluteDate, double[], Frame) - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointKeplerianTerm
Compute the acceleration vector.
getAcceleration(AbsoluteDate, double[], Frame) - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointSingleBodyTerm
Compute the acceleration vector.
getAcceleration(AbsoluteDate, double[], Frame) - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointThirdBodyTerm
Compute the acceleration vector.
getAccelerationDirectionSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Get one σ angular off-nominal acceleration direction.
getAccelerationInterpolation() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Get interpolation mode between current and next acceleration line.
getAccelerationMagnitudeSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Get one σ percent error on acceleration magnitude.
getAccelerationModel(AbsoluteDate) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
Get the AccelerationModel model valid at a date.
getAccelerationModelSpan(AbsoluteDate) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
Get the AccelerationModel TimeSpanMap.Span containing a specified date.
getAccuracy() - Method in interface org.orekit.gnss.metric.messages.common.AccuracyProvider
Get the accuracy of the ephemeris data from an accuracy index.
getAccuracy() - Method in class org.orekit.gnss.metric.messages.common.GlonassUserRangeAccuracy
Get the accuracy of the ephemeris data from an accuracy index.
getAccuracy() - Method in class org.orekit.gnss.metric.messages.common.SignalInSpaceAccuracy
Get the accuracy of the ephemeris data from an accuracy index.
getAccuracy() - Method in class org.orekit.gnss.metric.messages.common.UserRangeAccuracy
Get the accuracy of the ephemeris data from an accuracy index.
getAccuracy(String) - Method in class org.orekit.files.sp3.SP3Header
Get the formal accuracy.
getAccuracyProvider() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.RtcmEphemerisData
Get the accuracy provider of the ephemeris message.
getAcmDataElements() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata
Get the list of elements of information data blocks included in this message.
getAction() - Method in class org.orekit.propagation.events.EventState.EventOccurrence
Get the user requested action.
getAction() - Method in class org.orekit.propagation.events.FieldEventState.EventOccurrence
Get the user requested action.
getActualOdSpan() - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters
Get the actual OD time based on the observations available and the RECOMMENDED_OD_SPAN.
getActualOdSpan() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get actual time span used for the OD of the object.
getActuatorUsed() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver
Get the actuator used.
getAdaptableInterval(TopocentricFrame, double, double) - Static method in class org.orekit.propagation.events.intervals.ElevationDetectionAdaptableIntervalFactory
Method providing a candidate AdaptableInterval for arbitrary elevation detection with forward propagation.
getAdaptedPropagator() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Get the adapted propagator.
getAdditionalCovMetadataBlock() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmData
Get the additional covariance metadata logical block.
getAdditionalDerivatives() - Method in class org.orekit.propagation.integration.CombinedDerivatives
Get the derivatives related to the additional state.
getAdditionalDerivatives() - Method in class org.orekit.propagation.integration.FieldCombinedDerivatives
Get the derivatives related to the additional state.
getAdditionalDerivativesProviders() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Get the list of additional equations.
getAdditionalDerivativesProviders() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get an unmodifiable list of providers for additional derivatives.
getAdditionalDerivativesProviders() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get an unmodifiable list of providers for additional derivatives.
getAdditionalParametersBlock() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmData
Get the additional parameters logical block.
getAdditionalState(String) - Method in class org.orekit.propagation.FieldSpacecraftState
Get an additional state.
getAdditionalState(String) - Method in class org.orekit.propagation.SpacecraftState
Get an additional state.
getAdditionalState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.FieldAbstractStateModifier
Get the additional state.
getAdditionalState(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.FieldAdditionalStateProvider
Get the additional state.
getAdditionalState(SpacecraftState) - Method in class org.orekit.forces.maneuvers.jacobians.Duration
Get the additional state.
getAdditionalState(SpacecraftState) - Method in class org.orekit.forces.maneuvers.jacobians.MedianDate
Get the additional state.
getAdditionalState(SpacecraftState) - Method in class org.orekit.forces.maneuvers.jacobians.TriggerDate
Get the additional state.
getAdditionalState(SpacecraftState) - Method in class org.orekit.propagation.AbstractStateModifier
Get the additional state.
getAdditionalState(SpacecraftState) - Method in interface org.orekit.propagation.AdditionalStateProvider
Get the additional state.
getAdditionalState(SpacecraftState) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester
Get the additional state.
getAdditionalState(SpacecraftState) - Method in class org.orekit.propagation.analytical.gnss.ClockCorrectionsProvider
Get the additional state.
getAdditionalState(SpacecraftState) - Method in class org.orekit.propagation.StateCovarianceMatrixProvider
Get the additional state.
getAdditionalStateDerivative(String) - Method in class org.orekit.propagation.FieldSpacecraftState
Get an additional state derivative.
getAdditionalStateDerivative(String) - Method in class org.orekit.propagation.SpacecraftState
Get an additional state derivative.
getAdditionalStateInterpolator() - Method in class org.orekit.propagation.FieldSpacecraftStateInterpolator
Get additional state interpolator.
getAdditionalStateInterpolator() - Method in class org.orekit.propagation.SpacecraftStateInterpolator
Get additional state interpolator.
getAdditionalStateProviders() - Method in class org.orekit.propagation.AbstractPropagator
Get an unmodifiable list of providers for additional state.
getAdditionalStateProviders() - Method in class org.orekit.propagation.FieldAbstractPropagator
Get an unmodifiable list of providers for additional state.
getAdditionalStateProviders() - Method in interface org.orekit.propagation.FieldPropagator
Get an unmodifiable list of providers for additional state.
getAdditionalStateProviders() - Method in interface org.orekit.propagation.Propagator
Get an unmodifiable list of providers for additional state.
getAdditionalStatesDerivatives() - Method in class org.orekit.propagation.FieldSpacecraftState
Get an unmodifiable map of additional states derivatives.
getAdditionalStatesDerivatives() - Method in class org.orekit.propagation.SpacecraftState
Get an unmodifiable map of additional states derivatives.
getAdditionalStatesValues() - Method in class org.orekit.propagation.FieldSpacecraftState
Get an unmodifiable map of additional states.
getAdditionalStatesValues() - Method in class org.orekit.propagation.SpacecraftState
Get an unmodifiable map of additional states.
getAdjointDimension() - Method in interface org.orekit.control.indirect.adjoint.cost.CartesianCost
Getter for adjoint vector dimension.
getAdjointDimension() - Method in class org.orekit.control.indirect.adjoint.cost.UnboundedCartesianEnergyNeglectingMass
Getter for adjoint vector dimension.
getAdjointDynamicsProvider() - Method in class org.orekit.control.indirect.shooting.propagation.ShootingPropagationSettings
Getter for adjoint dynamics provider.
getAdjointName() - Method in class org.orekit.control.indirect.adjoint.cost.AbstractCartesianEnergy
Getter for adjoint vector name.
getAdjointName() - Method in interface org.orekit.control.indirect.adjoint.cost.CartesianCost
Getter for adjoint vector name.
getAdjointName() - Method in interface org.orekit.control.indirect.shooting.propagation.AdjointDynamicsProvider
Getter for adjoint vector name.
getAdjointName() - Method in class org.orekit.control.indirect.shooting.propagation.CartesianAdjointDynamicsProvider
Getter for adjoint vector name.
getAdjointVelocityNorm(double[]) - Method in class org.orekit.control.indirect.adjoint.cost.AbstractCartesianEnergy
Computes the Euclidean norm of the adjoint velocity vector.
getAdmMessageLink() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the Unique identifier of Attitude Data Message linked to this Orbit Data Message.
getAdmMsgLink() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get the unique identifier of Attitude Data Message(s) that are linked (relevant) to this Conjunction Data Message.
getADot() - Method in class org.orekit.orbits.CartesianOrbit
Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.CircularOrbit
Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.FieldOrbit
Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.Orbit
Get the semi-major axis derivative.
getADot() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage
Getter for the change rate in semi-major axis.
getADot() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage
Getter for the change rate in semi-major axis.
getAe() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
Get the value of the central body reference radius.
getAe() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get the central body reference radius.
getAe() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider
Get the value of the central body reference radius.
getAf0() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Getter for the the SV Clock Bias Correction Coefficient.
getAf0() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSClockElements
Gets the Zeroth Order Clock Correction.
getAF0() - Method in class org.orekit.gnss.rflink.gps.SubFrame1
Get af₀.
getAF0() - Method in class org.orekit.gnss.rflink.gps.SubFrameAlmanac
Get af₀.
getAf1() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Getter for the SV Clock Drift Correction Coefficient.
getAf1() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSClockElements
Gets the First Order Clock Correction.
getAF1() - Method in class org.orekit.gnss.rflink.gps.SubFrame1
Get af₁.
getAF1() - Method in class org.orekit.gnss.rflink.gps.SubFrameAlmanac
Get af₁.
getAf2() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac
Getter for the Drift Rate Correction Coefficient.
getAf2() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Getter for the Drift Rate Correction Coefficient.
getAf2() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSClockElements
Gets the Second Order Clock Correction.
getAF2() - Method in class org.orekit.gnss.rflink.gps.SubFrame1
Get af₂.
getAfter() - Method in class org.orekit.utils.FieldTimeSpanMap.Transition
Get the entry valid after transition.
getAfter() - Method in class org.orekit.utils.TimeSpanMap.Transition
Get the entry valid after transition.
getAgency() - Method in class org.orekit.files.sp3.SP3Header
Returns the agency that prepared this SP3 file.
getAgencyName() - Method in class org.orekit.files.rinex.clock.RinexClock
Getter for the agency name.
getAgencyName() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Get name of the agency.
getAGf0() - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage
Gets the Zeroth Order Clock Correction.
getAGf0() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
Gets the Zeroth Order Clock Correction.
getAGf1() - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage
Gets the First Order Clock Correction.
getAGf1() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
Gets the First Order Clock Correction.
getAGoM() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
Get the SGP4-XP solar radiation pressure-like coefficient Aγ/m.
getAh() - Method in class org.orekit.models.earth.troposphere.FieldViennaACoefficients
Get hydrostatic coefficient.
getAh() - Method in class org.orekit.models.earth.troposphere.ViennaACoefficients
Get hydrostatic coefficient.
getAi0() - Method in class org.orekit.files.rinex.navigation.IonosphereNequickGMessage
Get aᵢ₀.
getAi1() - Method in class org.orekit.files.rinex.navigation.IonosphereNequickGMessage
Get aᵢ₁.
getAi2() - Method in class org.orekit.files.rinex.navigation.IonosphereNequickGMessage
Get aᵢ₂.
getAlbedoGridSize() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get albedo grid size.
getAlbedoModel() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get albedo model.
getAlert() - Method in class org.orekit.gnss.rflink.gps.SubFrame
Get alert flag.
getAlignAngle() - Method in class org.orekit.propagation.events.AlignmentDetector
Get the alignment angle (rad).
getAll() - Method in class org.orekit.utils.ImmutableFieldTimeStampedCache
Get all the data in this cache.
getAll() - Method in class org.orekit.utils.ImmutableTimeStampedCache
Get all of the data in this cache.
getAllAmbiguityDrivers() - Method in class org.orekit.estimation.measurements.gnss.AmbiguitySolver
Get all the ambiguity parameters drivers.
getAllForceModels() - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder
Get the list of all force models.
getAllForceModels() - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
Get the list of all force models.
getAllForceModels() - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Get all the force models, perturbing forces and Newtonian attraction included.
getAllForceModels() - Method in class org.orekit.propagation.numerical.NumericalPropagator
Get all the force models, perturbing forces and Newtonian attraction included.
getAllForceModels() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Get all the force models, perturbing forces and Newtonian attraction included.
getAllForceModels() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Get all the force models, perturbing forces and Newtonian attraction included.
getAlmanacs() - Method in class org.orekit.gnss.SEMParser
Gets all the GPS almanacs read from the file.
getAlmanacs() - Method in class org.orekit.gnss.YUMAParser
Gets all the GPS almanacs read from the file.
getAlpha() - Method in class org.orekit.files.rinex.navigation.IonosphereBDGIMMessage
Get the α coefficients.
getAlpha() - Method in class org.orekit.files.rinex.navigation.IonosphereKlobucharMessage
Get the α coefficients.
getAlpha() - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader
Returns the alpha coefficients array.
getAlpha() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTGravityContext
Get direction cosine α for central body.
getAlpha() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext
Get direction cosine α for central body.
getAlpha() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTGravityContext
Get direction cosine α for central body.
getAlpha() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext
Get direction cosine α for central body.
getAlpha() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Deprecated.
since 12.2, use DSSTGravityContext.getAlpha() instead
getAlpha() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Deprecated.
since 12.2, use FieldDSSTGravityContext.getAlpha() instead
getAlpha(PositionAngleType) - Method in class org.orekit.orbits.CircularOrbit
Get the latitude argument.
getAlpha(PositionAngleType) - Method in class org.orekit.orbits.FieldCircularOrbit
Get the latitude argument.
getAlpha0() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D
Get α₀ field.
getAlpha1() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D
Get α₁ field.
getAlpha2() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D
Get α₂ field.
getAlpha3() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D
Get α₃ field.
getAlpha4() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTJ2SquaredClosedFormContext
Get the equatorial radius of the central body to the power 4.
getAlpha4() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTJ2SquaredClosedFormContext
Get the equatorial radius of the central body to the power 4.
getAlphaDot(PositionAngleType) - Method in class org.orekit.orbits.CircularOrbit
Get the latitude argument derivative.
getAlphaDot(PositionAngleType) - Method in class org.orekit.orbits.FieldCircularOrbit
Get the latitude argument derivative.
getAlphaE() - Method in class org.orekit.orbits.CircularOrbit
Get the eccentric latitude argument.
getAlphaE() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the eccentric latitude argument.
getAlphaEDot() - Method in class org.orekit.orbits.CircularOrbit
Get the eccentric latitude argument derivative.
getAlphaEDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the eccentric latitude argument derivative.
getAlphaM() - Method in class org.orekit.orbits.CircularOrbit
Get the mean latitude argument.
getAlphaM() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the mean latitude argument.
getAlphaMDot() - Method in class org.orekit.orbits.CircularOrbit
Get the mean latitude argument derivative.
getAlphaMDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the mean latitude argument derivative.
getAlphaV() - Method in class org.orekit.orbits.CircularOrbit
Get the true latitude argument.
getAlphaV() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the true latitude argument.
getAlphaVDot() - Method in class org.orekit.orbits.CircularOrbit
Get the true latitude argument derivative.
getAlphaVDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the true latitude argument derivative.
getAltCovRefFrame() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get the value of ALT_COV_REF_FRAME as an Orekit Frame.
getAltCovType() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get the flag indicating the type of alternate covariance information provided.
getAlternateNames() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the alternate names for this space object.
getAltitude() - Method in class org.orekit.bodies.FieldGeodeticPoint
Get the altitude.
getAltitude() - Method in class org.orekit.bodies.GeodeticPoint
Get the altitude.
getAltitude() - Method in class org.orekit.bodies.Loxodrome
Get the altitude above the reference body.
getAltitude() - Method in class org.orekit.models.earth.weather.FieldPressureTemperature
Get altitude at which weather parameters have been computed.
getAltitude() - Method in class org.orekit.models.earth.weather.PressureTemperature
Get altitude at which weather parameters have been computed.
getAltitude() - Method in class org.orekit.propagation.events.AltitudeDetector
Get the threshold altitude value.
getAltitude() - Method in class org.orekit.propagation.events.FieldAltitudeDetector
Get the threshold altitude value.
getAmbiguity(String, String, double) - Method in class org.orekit.estimation.measurements.gnss.AmbiguityCache
Get a cached driver for ambiguity.
getAmbiguityDriver() - Method in class org.orekit.estimation.measurements.gnss.InterSatellitesPhase
Get the driver for phase ambiguity.
getAmbiguityDriver() - Method in class org.orekit.estimation.measurements.gnss.OneWayGNSSPhase
Get the driver for phase ambiguity.
getAmbiguityDriver() - Method in class org.orekit.estimation.measurements.gnss.Phase
Get the driver for phase ambiguity.
getAmplifierBandwidth() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Get the amplifier bandwidth.
getAmplifierGain() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Get the amplifier gain.
getAmplifierInUse() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Get the amplifier in use.
getAmplitude() - Method in class org.orekit.models.earth.displacement.PsdCorrection
Get amplitude.
getAnalysisCenterID() - Method in class org.orekit.files.rinex.clock.RinexClock
Getter for the analysis center ID.
getAnalysisCenterName() - Method in class org.orekit.files.rinex.clock.RinexClock
Getter for the analysis center name.
getAncestor(int) - Method in class org.orekit.frames.Frame
Get the nth ancestor of the frame.
getAngle() - Method in class org.orekit.propagation.events.PositionAngleDetector
Get the fixed angle to be crossed (radians).
getAngle() - Method in class org.orekit.utils.units.Unit
Get the angle exponent.
getAnglesData() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
Get the angles data for the data block.
getAngleType() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for angleType.
getAngular() - Method in class org.orekit.frames.FieldTransform
Get the underlying elementary angular part.
getAngular() - Method in class org.orekit.frames.Transform
Get the underlying elementary angular part.
getAngularCoordinates() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistory
Get an unmodifiable list of attitude data lines.
getAngularCoordinates() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemData
Get an unmodifiable view of the data points.
getAngularCoordinates() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSegment
Get an unmodifiable list of attitude data lines.
getAngularCoordinates() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.AttitudeEphemerisSegment
Get an unmodifiable list of attitude data lines.
getAngularCoordinates() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment
Get an unmodifiable list of attitude data lines.
getAngularDerivativesFilter() - Method in enum org.orekit.files.ccsds.ndm.adm.AttitudeType
Get the angular derivative filter corresponding to the attitude data.
getAngularInterpolator() - Method in class org.orekit.attitudes.AttitudeInterpolator
Get time stamped angular coordinates interpolator.
getAngularInterpolator() - Method in class org.orekit.attitudes.FieldAttitudeInterpolator
Get time stamped angular coordinates interpolator.
getAngularVelocity() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Getter for the mean angular velocity of the Earth for the GNSS model.
getAngularVelocity() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
Gets the mean angular velocity of the Earth of the GNSS model.
getAngularVelocity() - Method in class org.orekit.utils.FieldPVCoordinates
Get the angular velocity (spin) of this point as seen from the origin.
getAngularVelocity() - Method in class org.orekit.utils.PVCoordinates
Get the angular velocity (spin) of this point as seen from the origin.
getAngularVelocityBlock() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData
Get the angular velocity logical block.
getAngVelX() - Method in class org.orekit.files.ccsds.ndm.adm.apm.AngularVelocity
Get the angular velocity around X axis (rad/s).
getAngVelY() - Method in class org.orekit.files.ccsds.ndm.adm.apm.AngularVelocity
Get the angular velocity around Y axis (rad/s).
getAngVelZ() - Method in class org.orekit.files.ccsds.ndm.adm.apm.AngularVelocity
Get the angular velocity around Z axis (rad/s).
getAnomaly() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Get the orbit anomaly.
getAnomaly(PositionAngleType) - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the anomaly.
getAnomaly(PositionAngleType) - Method in class org.orekit.orbits.KeplerianOrbit
Get the anomaly.
getAnomalyDot(PositionAngleType) - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the anomaly derivative.
getAnomalyDot(PositionAngleType) - Method in class org.orekit.orbits.KeplerianOrbit
Get the anomaly derivative.
getAnomalyType() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Get the type of anomaly (true or mean).
getAntennaAzimuth() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Get the azimuth of the zero direction of a fixed antenna.
getAntennaBSight() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Get the antenna B.Sight.
getAntennaHeight() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Get the antenna height.
getAntennaNumber() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Get the number of the antenna.
getAntennaPhaseCenter() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Get the antenna phasecenter.
getAntennaReferencePoint() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Get the position of antenna reference point for antenna on vehicle.
getAntennaType() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Get the type of the antenna.
getAntennaType(AbsoluteDate) - Method in class org.orekit.files.sinex.Station
Get the antenna type for the given epoch.
getAntennaTypeTimeSpanMap() - Method in class org.orekit.files.sinex.Station
Get the TimeSpanMap of site antenna type.
getAntennaZeroDirection() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Get the zero direction of antenna.
getAntiSpoofing() - Method in class org.orekit.gnss.rflink.gps.SubFrame
Get anti-spoofing flag.
getAntiSpoofing(int) - Method in class org.orekit.gnss.rflink.gps.SubFrame4E
Get the anti-spoofing for a satellite.
getAODC() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouLegacyNavigationMessage
Getter for the Age Of Data Clock (AODC).
getAODE() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouLegacyNavigationMessage
Getter for the Age Of Data Ephemeris (AODE).
getAODO() - Method in class org.orekit.gnss.rflink.gps.SubFrame2
Get Age Of data Offset.
getAp() - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimationLoader.LineParameters
Get the Ap index.
getAp(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
Get the Ap geomagnetic indices.
getAp(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
Get the Ap geomagnetic indices.
getAp(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.NRLMSISE00InputParameters
Get the Ap geomagnetic indices.
getApAvg() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
Gets the arithmetic average of all eight Ap indices for the current entry.
getApoapsisAltitude() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Get the distance of the furthest point in the objects orbit above the equatorial radius of the central body.
getApplicableWavelength() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Get the applicable wavelength.
getAppliedEffects() - Method in class org.orekit.estimation.measurements.EstimatedMeasurementBase
Get the applied effects of modifiers.
getAppliedVoltage() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Get the applied voltage.
getApproachAngle() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the approach angle computed between Objects 1 and 2 in the RTN coordinate frame relative to object 1.
getApproxPos() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Get the Approximate Marker Position.
getAProvider() - Method in class org.orekit.models.earth.troposphere.AbstractVienna
Get provider for Vienna ah and aw coefficients.
getArbitraryEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Get an arbitrary date.
getArea() - Method in class org.orekit.forces.Panel
Get panel area.
getAreaDRG() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Get the effective area of the object exposed to atmospheric drag.
getAreaPC() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Get the actual area of the object.
getAreaPCMax() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Get the maximum area of the object to be used to compute the collision probability.
getAreaPCMin() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Set the minimum area of the object to be used to compute the collision probability.
getAreaSRP() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Get the effective area of the object exposed to solar radiation pressure.
getAstronomicalAmplitudesMap() - Method in class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader
Get astronomical amplitudes map.
getAtmosphere() - Method in class org.orekit.forces.drag.AbstractDragForceModel
Get the atmospheric model.
getAtmosphere() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Get the atmospheric model.
getAtmosphericModel() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get name of atmospheric model.
getAtmosphericModel() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get name of atmospheric model.
getAttBasis() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata
Get basis of this attitude state time history data.
getAttBasisID() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata
Get identification number of the orbit determination or simulation upon which this attitude is based.
getAttID() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata
Get attitude identification number.
getAttitude() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the attitude.
getAttitude() - Method in class org.orekit.propagation.SpacecraftState
Get the attitude.
getAttitude(Frame, PVCoordinatesProvider) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Apm
Get the attitude.
getAttitude(Frame, PVCoordinatesProvider) - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData
Get the attitude.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.AggregateBoundedAttitudeProvider
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.AlignedAndConstrained
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.attitudes.AttitudeProvider
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.AttitudesSequence
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.CelestialBodyPointed
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.FixedRate
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.FrameAlignedProvider
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.GroundPointing
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.LofOffset
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.SpinStabilized
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.TabulatedLofOffset
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.TabulatedProvider
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.TorqueFree
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawCompensation
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawSteering
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.AggregateBoundedAttitudeProvider
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.AlignedAndConstrained
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in interface org.orekit.attitudes.AttitudeProvider
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.AttitudesSequence
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.CelestialBodyPointed
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.FixedRate
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.FrameAlignedProvider
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.GroundPointing
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.LofOffset
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.SpinStabilized
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.TabulatedLofOffset
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.TabulatedProvider
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.TorqueFree
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawCompensation
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawSteering
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider
Compute the attitude corresponding to an orbital state.
getAttitudeActuatorType() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Get the type of actuator for attitude control.
getAttitudeBlocks() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmData
Get attitude state histories logical blocks.
getAttitudeControlAccuracy() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Get the accuracy of attitude control.
getAttitudeControlMode() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Get the attitude control mode.
getAttitudeDeterminationBlock() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmData
Get attitude determination logical block.
getAttitudeFromFrame(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider
Compute the attitude for DIRECTION_IN_FRAME or DIRECTION_IN_LOF types.
getAttitudeInterpolator() - Method in class org.orekit.propagation.FieldSpacecraftStateInterpolator
Get attitude interpolator.
getAttitudeInterpolator() - Method in class org.orekit.propagation.SpacecraftStateInterpolator
Get attitude interpolator.
getAttitudeKnowledgeAccuracy() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Get the accuracy of attitude knowledge.
getAttitudeOverride() - Method in class org.orekit.forces.maneuvers.FieldImpulseManeuver
Get the Attitude Provider to use during maneuver.
getAttitudeOverride() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
Get the Attitude Provider to use during maneuver.
getAttitudeOverride() - Method in class org.orekit.forces.maneuvers.Maneuver
Get the attitude override used for the maneuver.
getAttitudePointingAccuracy() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Get the overall accuracy of spacecraft to maintain attitude.
getAttitudeProvider() - Method in class org.orekit.control.indirect.shooting.propagation.ShootingPropagationSettings
Getter for the attitude provider.
getAttitudeProvider() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistory
Get the attitude provider for this attitude ephemeris segment.
getAttitudeProvider() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSegment
Get the attitude provider for this attitude ephemeris segment.
getAttitudeProvider() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.AttitudeEphemerisSegment
Get the attitude provider for this attitude ephemeris segment.
getAttitudeProvider() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.SatelliteAttitudeEphemeris
Get the attitude provider corresponding to this ephemeris, combining data from all segments.
getAttitudeProvider() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment
Get the attitude provider for this attitude ephemeris segment.
getAttitudeProvider() - Method in class org.orekit.propagation.AbstractPropagator
Get attitude provider.
getAttitudeProvider() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Get the attitude provider.
getAttitudeProvider() - Method in class org.orekit.propagation.FieldAbstractPropagator
Get attitude provider.
getAttitudeProvider() - Method in interface org.orekit.propagation.FieldPropagator
Get attitude provider.
getAttitudeProvider() - Method in class org.orekit.propagation.integration.FieldStateMapper
Get the attitude provider.
getAttitudeProvider() - Method in class org.orekit.propagation.integration.StateMapper
Get the attitude provider.
getAttitudeProvider() - Method in interface org.orekit.propagation.Propagator
Get attitude provider.
getAttitudeRotation(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.AggregateBoundedAttitudeProvider
Compute the attitude-related rotation corresponding to an orbital state.
getAttitudeRotation(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.AlignedAndConstrained
Compute the attitude-related rotation corresponding to an orbital state.
getAttitudeRotation(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.attitudes.AttitudeProvider
Compute the attitude-related rotation corresponding to an orbital state.
getAttitudeRotation(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.AttitudesSequence
 
getAttitudeRotation(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.CelestialBodyPointed
Compute the attitude-related rotation corresponding to an orbital state.
getAttitudeRotation(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.FixedRate
Compute the attitude-related rotation corresponding to an orbital state.
getAttitudeRotation(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.FrameAlignedProvider
Compute the attitude-related rotation corresponding to an orbital state.
getAttitudeRotation(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.GroundPointing
Compute the attitude-related rotation corresponding to an orbital state.
getAttitudeRotation(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.LofOffset
Compute the attitude-related rotation corresponding to an orbital state.
getAttitudeRotation(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing
Compute the attitude-related rotation corresponding to an orbital state.
getAttitudeRotation(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.SpinStabilized
Compute the attitude-related rotation corresponding to an orbital state.
getAttitudeRotation(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.AggregateBoundedAttitudeProvider
Compute the attitude-related rotation corresponding to an orbital state.
getAttitudeRotation(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.AlignedAndConstrained
Compute the attitude-related rotation corresponding to an orbital state.
getAttitudeRotation(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in interface org.orekit.attitudes.AttitudeProvider
Compute the attitude-related rotation corresponding to an orbital state.
getAttitudeRotation(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.AttitudesSequence
Compute the attitude-related rotation corresponding to an orbital state.
getAttitudeRotation(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.CelestialBodyPointed
Compute the attitude-related rotation corresponding to an orbital state.
getAttitudeRotation(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.FixedRate
Compute the attitude-related rotation corresponding to an orbital state.
getAttitudeRotation(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.FrameAlignedProvider
Compute the attitude-related rotation corresponding to an orbital state.
getAttitudeRotation(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.GroundPointing
Compute the attitude-related rotation corresponding to an orbital state.
getAttitudeRotation(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.LofOffset
Compute the attitude-related rotation corresponding to an orbital state.
getAttitudeRotation(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing
Compute the attitude-related rotation corresponding to an orbital state.
getAttitudeRotation(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.SpinStabilized
Compute the attitude-related rotation corresponding to an orbital state.
getAttitudeStates() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination
Get attitude states.
getAttitudeStates() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistory
Get the attitude states.
getAttitudeType() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeState
Get the type of the elements.
getAttitudeType() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata
Get attitude element set type.
getAttitudeType() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Get the format of the data lines in the message.
getAttPrevID() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata
Get identification number of previous attitude.
getAugmentedInitialState(int) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPMultipleShooter
Compute the additional state from the additionalEquations.
getAugmentedInitialState(int) - Method in class org.orekit.utils.AbstractMultipleShooting
Compute the additional state from the additionalEquations.
getAugmentedInitialState(int) - Method in class org.orekit.utils.MultipleShooter
Compute the additional state from the additionalEquations.
getAuthentication() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
Get the authentication method.
getAuthentication() - Method in class org.orekit.gnss.metric.ntrip.NetworkRecord
Get the authentication method.
getAuthentication(String) - Static method in enum org.orekit.gnss.metric.ntrip.Authentication
Get the authentication type corresponding to a keyword.
getAuxiliaryElements() - Method in class org.orekit.propagation.semianalytical.dsst.forces.ForceModelContext
Method to get the auxiliary elements related to the ForceModelContext.
getAvailableDerivatives() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeState
Get which derivatives of position are available in this state.
getAvailableDerivatives() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistory
Get which derivatives of angular data are available in this attitude ephemeris segment.
getAvailableDerivatives() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSegment
Get which derivatives of angular data are available in this attitude ephemeris segment.
getAvailableDerivatives() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryState
Get which derivatives of position are available in this state.
getAvailableDerivatives() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory
Get which derivatives of position are available in this ephemeris segment.
getAvailableDerivatives() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemData
Get the derivatives available in the block.
getAvailableDerivatives() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSegment
Get which derivatives of position are available in this ephemeris segment.
getAvailableDerivatives() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.AttitudeEphemerisSegment
Get which derivatives of angular data are available in this attitude ephemeris segment.
getAvailableDerivatives() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
Get which derivatives of position are available in this ephemeris segment.
getAvailableDerivatives() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment
Get which derivatives of angular data are available in this attitude ephemeris segment.
getAvailableDerivatives() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
Get which derivatives of position are available in this ephemeris segment.
getAvailableDerivatives() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris
Get which derivatives of position are available in this ephemeris segment.
getAvailableDerivatives() - Method in class org.orekit.files.sp3.SP3Ephemeris
Get the available derivatives.
getAvailableDerivatives() - Method in class org.orekit.files.sp3.SP3Segment
Get which derivatives of position are available in this ephemeris segment.
getAvailableDerivatives() - Method in class org.orekit.files.stk.STKEphemerisFile.STKEphemerisSegment
 
getAvailableObservationPairs() - Method in class org.orekit.files.sinex.Dcb
Get all available observation code pairs for the satellite.
getAvailableSatelliteSystems() - Method in class org.orekit.files.sinex.DcbStation
Get the satellite systems available for the station.
getAveragedCircularEx() - Method in class org.orekit.propagation.conversion.averaging.elements.AveragedCircularWithMeanAngle
Getter for averaged circular ex.
getAveragedCircularEy() - Method in class org.orekit.propagation.conversion.averaging.elements.AveragedCircularWithMeanAngle
Getter for averaged circular ey.
getAveragedEccentricity() - Method in class org.orekit.propagation.conversion.averaging.elements.AveragedKeplerianWithMeanAngle
Getter for the averaged eccentricity.
getAveragedElements() - Method in interface org.orekit.propagation.conversion.averaging.AveragedOrbitalState
Getter for the averaged orbital elements.
getAveragedElements() - Method in class org.orekit.propagation.conversion.averaging.BrouwerLyddaneOrbitalState
Getter for the averaged orbital elements.
getAveragedElements() - Method in class org.orekit.propagation.conversion.averaging.DSST6X0OrbitalState
Getter for the averaged orbital elements.
getAveragedElements() - Method in class org.orekit.propagation.conversion.averaging.EcksteinHechlerOrbitalState
Getter for the averaged orbital elements.
getAveragedElements() - Method in class org.orekit.propagation.conversion.averaging.SGP4OrbitalState
Getter for the averaged orbital elements.
getAveragedEquinoctialEx() - Method in class org.orekit.propagation.conversion.averaging.elements.AveragedEquinoctialWithMeanAngle
Getter for the averaged equinoctial ex.
getAveragedEquinoctialEy() - Method in class org.orekit.propagation.conversion.averaging.elements.AveragedEquinoctialWithMeanAngle
Getter for the averaged equinoctial ey.
getAveragedHx() - Method in class org.orekit.propagation.conversion.averaging.elements.AveragedEquinoctialWithMeanAngle
Getter for the averaged hx.
getAveragedHy() - Method in class org.orekit.propagation.conversion.averaging.elements.AveragedEquinoctialWithMeanAngle
Getter for the averaged hy.
getAveragedInclination() - Method in class org.orekit.propagation.conversion.averaging.elements.AveragedCircularWithMeanAngle
Getter for averaged inclination.
getAveragedInclination() - Method in class org.orekit.propagation.conversion.averaging.elements.AveragedKeplerianWithMeanAngle
Getter for the averaged inclination.
getAveragedMeanAnomaly() - Method in class org.orekit.propagation.conversion.averaging.elements.AveragedKeplerianWithMeanAngle
Getter for the averaged mean anomaly.
getAveragedMeanLatitudeArgument() - Method in class org.orekit.propagation.conversion.averaging.elements.AveragedCircularWithMeanAngle
Getter for averaged mean latitude argument.
getAveragedMeanLongitudeArgument() - Method in class org.orekit.propagation.conversion.averaging.elements.AveragedEquinoctialWithMeanAngle
Getter for the averaged mean longitude argument.
getAveragedPerigeeArgument() - Method in class org.orekit.propagation.conversion.averaging.elements.AveragedKeplerianWithMeanAngle
Getter for the averaged perigee argument.
getAveragedRightAscensionOfTheAscendingNode() - Method in class org.orekit.propagation.conversion.averaging.elements.AveragedCircularWithMeanAngle
Getter for averaged RAAN.
getAveragedRightAscensionOfTheAscendingNode() - Method in class org.orekit.propagation.conversion.averaging.elements.AveragedKeplerianWithMeanAngle
Getter for the averaged RAAN.
getAveragedSemiMajorAxis() - Method in class org.orekit.propagation.conversion.averaging.elements.AveragedCircularWithMeanAngle
Getter for averaged semi-major axis.
getAveragedSemiMajorAxis() - Method in class org.orekit.propagation.conversion.averaging.elements.AveragedEquinoctialWithMeanAngle
Getter for the averaged semi-major axis.
getAveragedSemiMajorAxis() - Method in class org.orekit.propagation.conversion.averaging.elements.AveragedKeplerianWithMeanAngle
Getter for the averaged semi-major axis.
getAverageFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
Get the value of the 81 day average of F10.7 solar flux centered on current day.
getAverageFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
 
getAverageFlux(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.NRLMSISE00InputParameters
Get the value of the 81 day average of F10.7 solar flux centered on current day.
getAw() - Method in class org.orekit.models.earth.troposphere.FieldViennaACoefficients
Get wet coefficient.
getAw() - Method in class org.orekit.models.earth.troposphere.ViennaACoefficients
Get wet coefficient.
getAx2oA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTGravityContext
Getter for the ax2oA.
getAx2oA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTGravityContext
Getter for the ax2oA.
getAxis() - Method in class org.orekit.models.earth.displacement.PsdCorrection
Get correction axis.
getAxisNormalToCollisionPlane() - Method in class org.orekit.frames.encounter.DefaultEncounterLOF
Get the axis normal to the collision plane (i, j or k) in this encounter local orbital frame.
getAxisNormalToCollisionPlane() - Method in interface org.orekit.frames.encounter.EncounterLOF
Get the axis normal to the collision plane (i, j or k) in this encounter local orbital frame.
getAxisNormalToCollisionPlane() - Method in class org.orekit.frames.encounter.ValsecchiEncounterFrame
Get the axis normal to the collision plane (i, j or k) in this encounter local orbital frame.
getAxisNormalToCollisionPlane(Field<T>) - Method in class org.orekit.frames.encounter.DefaultEncounterLOF
Get the axis normal to the collision plane (i, j or k) in this encounter local orbital frame.
getAxisNormalToCollisionPlane(Field<T>) - Method in interface org.orekit.frames.encounter.EncounterLOF
Get the axis normal to the collision plane (i, j or k) in this encounter local orbital frame.
getAxisNormalToCollisionPlane(Field<T>) - Method in class org.orekit.frames.encounter.ValsecchiEncounterFrame
Get the axis normal to the collision plane (i, j or k) in this encounter local orbital frame.
getAzimuth() - Method in class org.orekit.bodies.Loxodrome
Get the azimuth.
getAzimuth() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement
Get the azimuth angle.
getAzimuth() - Method in class org.orekit.utils.FieldTrackingCoordinates
Get the azimuth.
getAzimuth() - Method in class org.orekit.utils.TrackingCoordinates
Get the azimuth.
getAzimuth(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.TopocentricFrame
Get the azimuth of a point with regards to the topocentric frame center point.
getAzimuth(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame
Get the azimuth of a point with regards to the topocentric frame center point.
getAzimuthRate() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement
Get the azimuth rate.
getb() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext
Get b = 1 / (1 + sqrt(1 - e²)) = 1 / (1 + B).
getb() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext
Get b = 1 / (1 + sqrt(1 - e²)) = 1 / (1 + B).
getB() - Method in class org.orekit.bodies.Ellipse
Get the semi minor axis.
getB() - Method in class org.orekit.bodies.Ellipsoid
Get the length of the second semi-axis.
getB() - Method in class org.orekit.bodies.FieldEllipse
Get the semi minor axis.
getB() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get B = sqrt(1 - e²).
getB() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get B = sqrt(1 - e²).
getB1() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester
Get the Jacobian matrix B1 (B1 = ∂εη/∂Y).
getB2(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester
Get the Jacobian matrix B2 (B2 = ∂Y/∂Y₀).
getB3(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester
Get the Jacobian matrix B3 (B3 = ∂Y/∂P).
getB4() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester
Get the Jacobian matrix B4 (B4 = ∂εη/∂c).
getBackwardApoapsisDetectionAdaptableInterval() - Static method in class org.orekit.propagation.events.intervals.ApsideDetectionAdaptableIntervalFactory
Method providing a candidate AdaptableInterval for apoapsis detection with backward propagation.
getBackwardApsideDetectionAdaptableInterval() - Static method in class org.orekit.propagation.events.intervals.ApsideDetectionAdaptableIntervalFactory
Method providing a candidate AdaptableInterval for arbitrary apside detection with backward propagation.
getBackwardPeriapsisDetectionAdaptableInterval() - Static method in class org.orekit.propagation.events.intervals.ApsideDetectionAdaptableIntervalFactory
Method providing a candidate AdaptableInterval for periapsis detection with backward propagation.
getBase() - Method in class org.orekit.utils.units.PowerTerm
Get the base term.
getBaseDate() - Method in class org.orekit.utils.DateDriver
Get the base (unshifted) date.
getBaseEquipment() - Method in class org.orekit.files.ccsds.definitions.SpacecraftBodyFrame
Get the quipment on which the frame is located.
getBaseFrame() - Method in class org.orekit.estimation.measurements.GroundStation
Get the base frame associated with the station.
getBaseName(File) - Method in class org.orekit.data.FilesListCrawler
Get the base name of an input.
getBaseName(URL) - Method in class org.orekit.data.NetworkCrawler
Get the base name of an input.
getBaseName(T) - Method in class org.orekit.data.AbstractListCrawler
Get the base name of an input.
getBaseOffsets() - Method in class org.orekit.time.UTCScale
Get the base offsets.
getBaseProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get a time-independent provider containing base harmonics coefficients.
getBaseState(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.GroundPointingAttitudeModifier
Compute the base system state at given date, without modifications.
getBaseState(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.GroundPointingAttitudeModifier
Compute the base system state at given date, without modifications.
getBaseWeight() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Get the base weight associated with the measurement
getBaseWeight() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
Get the base weight associated with the measurement
getBaseWeight() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
Get the base weight associated with the measurement
getBasicDimension() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get state vector dimension without additional parameters.
getBasicDimension() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get state vector dimension without additional parameters.
getBB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext
Get B².
getBB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
Get B * B.
getBB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext
Get B².
getBB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
Get B * B.
getBBB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext
Get B³.
getBBB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext
Get B³.
getBDGIMMessages() - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Get the ionosphere BDGIM messages.
getBDT() - Method in class org.orekit.time.LazyLoadedTimeScales
 
getBDT() - Method in interface org.orekit.time.TimeScales
Get the BeiDou Navigation Satellite System time scale.
getBDT() - Static method in class org.orekit.time.TimeScalesFactory
Get the BeiDou Navigation Satellite System time scale.
getBeacon() - Method in class org.orekit.propagation.events.AngularSeparationDetector
Get the beacon at the center of the proximity zone.
getBeamDivergence() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
Get the beam divergence.
getBefore() - Method in class org.orekit.utils.FieldTimeSpanMap.Transition
Get the entry valid before transition.
getBefore() - Method in class org.orekit.utils.TimeSpanMap.Transition
Get the entry valid before transition.
getBeginDate(Frequency) - Method in class org.orekit.estimation.measurements.gnss.CycleSlipDetectorResults
Return the date of validity beginning of the detector.
getBeginTime() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver
Get start time of actual maneuver, relative to t₀.
getBeidouCivilianNavigationMessages() - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Get all the Beidou navigation messages contained in the file.
getBeidouCivilianNavigationMessages(String) - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Get the Beidou navigation messages for the given satellite Id.
getBeidouEpoch() - Method in class org.orekit.time.AbstractTimeScales
 
getBeidouEpoch() - Method in interface org.orekit.time.TimeScales
Reference epoch for BeiDou weeks: 2006-01-01T00:00:00 UTC.
getBeidouLegacyNavigationMessages() - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Get all the Beidou navigation messages contained in the file.
getBeidouLegacyNavigationMessages(String) - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Get the Beidou navigation messages for the given satellite Id.
getBeidouNavigationMessage() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1042Data
Get the Beidou navigation message corresponding to the current RTCM data.
getBeidouNavigationMessage(TimeScales) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1042Data
Get the Beidou navigation message corresponding to the current RTCM data.
getBeidouToc() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1042Data
Get the Beidou time of clock.
getBeta() - Method in class org.orekit.files.rinex.navigation.IonosphereKlobucharMessage
Get the β coefficients.
getBeta() - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader
Returns the beta coefficients array.
getBeta() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTGravityContext
Get direction cosine β for central body.
getBeta() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext
Get direction cosine β for central body.
getBeta() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTGravityContext
Get direction cosine β for central body.
getBeta() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext
Get direction cosine β for central body.
getBeta() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Deprecated.
since 12.2, use DSSTGravityContext.getBeta() instead
getBeta() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Deprecated.
since 12.2, use FieldDSSTGravityContext.getBeta() instead
getBeta0() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D
Get β₀ field.
getBeta1() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D
Get β₁ field.
getBeta2() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D
Get β₂ field.
getBeta3() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D
Get β₃ field.
getBetaAngleThreshold() - Method in class org.orekit.propagation.events.BetaAngleDetector
The beta angle threshold (radians).
getBetaAngleThreshold() - Method in class org.orekit.propagation.events.FieldBetaAngleDetector
The beta angle threshold (radians).
getBGDE1E5a() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage
Getter for the E1/E5a broadcast group delay.
getBGDE5bE1() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage
Getter for the the Broadcast Group Delay E5b/E1.
getBiasMode() - Method in class org.orekit.files.sinex.DcbDescription
Get the bias mode
getBinKurtosis() - Method in class org.orekit.files.ilrs.CRD.NptRangeMeasurement
Get the bin kurtosis from the mean of raw accepted time-of-flight values minus the trend function.
getBinPeakMinusMean() - Method in class org.orekit.files.ilrs.CRD.NptRangeMeasurement
Get the bin peak - mean value.
getBinRms() - Method in class org.orekit.files.ilrs.CRD.NptRangeMeasurement
Get the bin RMS from the mean of raw accepted time-of-flight values minus the trend function.
getBinSkew() - Method in class org.orekit.files.ilrs.CRD.NptRangeMeasurement
Get the bin skew from the mean of raw accepted time-of-flight values minus the trend function.
getBitRate() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
Get the bit rate.
getBN() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the GLONASS Bn Word.
getBoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTGravityContext
Get B / A.
getBoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext
Get B / A.
getBoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTGravityContext
Get B / A.
getBoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext
Get B / A.
getBoABpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTGravityContext
Get BoABpo = B / A(1 + B).
getBoABpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext
Get BoABpo = B / A(1 + B).
getBoABpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTGravityContext
Get BoABpo = B / A(1 + B).
getBoABpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext
Get BoABpo = B / A(1 + B).
getBody() - Method in class org.orekit.bodies.Loxodrome
Get the body on which the loxodrome is defined.
getBody() - Method in class org.orekit.files.ccsds.definitions.BodyFacade
Get the celestial body.
getBody() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory
Get central body.
getBody() - Method in class org.orekit.forces.gravity.AbstractBodyAttraction
Deprecated.
in next major release this shall be removed as the class will not have to use a CelestialBody
getBody() - Method in class org.orekit.propagation.events.FieldLatitudeCrossingDetector
Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.FieldLatitudeRangeCrossingDetector
Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.FieldLongitudeCrossingDetector
Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.FieldLongitudeRangeCrossingDetector
Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.FootprintOverlapDetector
Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.GeographicZoneDetector
Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.LatitudeCrossingDetector
Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.LatitudeExtremumDetector
Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.LatitudeRangeCrossingDetector
Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.LongitudeCrossingDetector
Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.LongitudeExtremumDetector
Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.LongitudeRangeCrossingDetector
Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Get third body.
getBody(String) - Method in interface org.orekit.bodies.CelestialBodies
Get a celestial body.
getBody(String) - Static method in class org.orekit.bodies.CelestialBodyFactory
Get a celestial body.
getBody(String) - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
Get a celestial body.
getBodyFixedToInertialTransform() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTGravityContext
Getter for the bodyFixedToInertialTransform.
getBodyFixedToInertialTransform() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTGravityContext
Getter for the bodyFixedToInertialTransform.
getBodyFrame() - Method in class org.orekit.attitudes.GroundPointing
Get the body frame.
getBodyFrame() - Method in interface org.orekit.bodies.BodyShape
Get body frame related to body shape.
getBodyFrame() - Method in class org.orekit.bodies.OneAxisEllipsoid
Get body frame related to body shape.
getBodyFrame() - Method in class org.orekit.models.earth.Geoid
 
getBodyName() - Method in class org.orekit.forces.gravity.AbstractBodyAttraction
Getter for the body's name.
getBodyOrientedFrame() - Method in interface org.orekit.bodies.CelestialBody
Get a body oriented, body centered frame.
getBodyPosition(AbsoluteDate, Frame) - Method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointNonCentralBodyTerm
Get body's position.
getBodyPosition(AbsoluteDate, Frame) - Method in class org.orekit.forces.gravity.AbstractBodyAttraction
Get the body's position vector.
getBodyPosition(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.forces.gravity.AbstractBodyAttraction
Get the body's position vector.
getBodyPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.forces.gravity.AbstractBodyAttraction
Get the body's position-velocity-acceleration vector.
getBodyPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.forces.gravity.AbstractBodyAttraction
Get the body's position-velocity-acceleration vector.
getBodyShape() - Method in class org.orekit.propagation.events.AltitudeDetector
Get the body shape.
getBodyShape() - Method in class org.orekit.propagation.events.FieldAltitudeDetector
Get the body shape.
getBolDv() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Get the total ΔV capability at beginning of life.
getBStar() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
Get the SGP/SGP4 drag-like coefficient.
getBStar() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get the ballistic coefficient.
getBStar() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the ballistic coefficient at tle date.
getBStar(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLE
Get the ballistic coefficient at a specific date.
getBTerm() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
Get the SGP4-XP drag-like coefficient.
getBufferedReader() - Method in class org.orekit.data.LineOrientedFilteringReader
Get the underlying line-oriented reader.
getBuilder() - Method in class org.orekit.estimation.measurements.generation.AbstractScheduler
Get the builder associated with this scheduler.
getBuilder() - Method in interface org.orekit.estimation.measurements.generation.Scheduler
Get the builder associated with this scheduler.
getBusModel() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Get the bus model name.
getC() - Method in class org.orekit.bodies.Ellipsoid
Get the length of the third semi-axis.
getC() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTJ2SquaredClosedFormContext
Get the cosine of the inclination.
getC() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTJ2SquaredClosedFormContext
Get the cosine of the inclination.
getC() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get C = 1 + p² + q².
getC() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get C = 1 + p² + q².
getC1cCodePhaseBias() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Get the code phase bias correction for GLONASS ObservationType.C1C signal.
getC1pCodePhaseBias() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Get the code phase bias correction for GLONASS ObservationType.C1P signal.
getC2cCodePhaseBias() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Get the code phase bias correction for GLONASS ObservationType.C2C signal.
getC2n0(int) - Method in class org.orekit.models.earth.ReferenceEllipsoid
Get the fully normalized coefficient C2n,0 for the normal gravity potential.
getC2pCodePhaseBias() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Get the code phase bias correction for GLONASS ObservationType.C2P signal.
getCache() - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData
Get underlying cache.
getCache() - Method in class org.orekit.time.SampledClockModel
Get the clock offsets cache.
getCachedPositionAngleType() - Method in class org.orekit.orbits.CircularOrbit
Get the cached PositionAngleType.
getCachedPositionAngleType() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the cached PositionAngleType.
getCachedPositionAngleType() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the cached PositionAngleType.
getCachedPositionAngleType() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the cached PositionAngleType.
getCachedPositionAngleType() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the cached PositionAngleType.
getCachedPositionAngleType() - Method in class org.orekit.orbits.KeplerianOrbit
Get the cached PositionAngleType.
getCachedPositionAngleType() - Method in interface org.orekit.orbits.PositionAngleBased
Get the cached PositionAngleType.
getCachedSamples() - Method in class org.orekit.time.AbstractFieldTimeInterpolator.InterpolationData
Deprecated.
This method appears to be unused and may be removed in Orekit 13.0. Please Comment on forum.orekit.org if you have a use case for this method.
getCachedSamples() - Method in class org.orekit.time.AbstractTimeInterpolator.InterpolationData
Deprecated.
This method appears to be unused and may be removed in Orekit 13.0. Please Comment on forum.orekit.org if you have a use case for this method.
getCacheSlotsNumber() - Static method in class org.orekit.utils.OrekitConfiguration
Get the number of slots to use in caches.
getCalendarWeek() - Method in class org.orekit.time.DateComponents
Get the calendar week number.
getCalibrationData() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
Get the calibration data for the data block.
getCalibrationDetailData() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
Get the calibration detail data for the data block.
getCalibrationDetailRecords() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
Get the CalibrationDetail record(s) related to the default system configuration id.
getCalibrationDetailRecords(String) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
Get the CalibrationDetail record(s) related to the given systemConfigurationId.
getCalibrationRecords() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
Get the Calibration record(s) related to the default system configuration id.
getCalibrationRecords(String) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
Get the Calibration record(s) related to the given systemConfigurationId.
getCalibrationTargetRecord() - Method in class org.orekit.files.ilrs.CRDConfiguration
Get the calibration target configuration record.
getCalibrationTargetRecord(CRDConfiguration.SystemConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration
Get calibration target configuration record related to the systemRecord.
getCalls() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get the number of calls to the differential equations computation method.
getCalls() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get the number of calls to the differential equations computation method.
getCaOrPFlag() - Method in class org.orekit.gnss.rflink.gps.SubFrame1
Get C/A or P flag.
getCapitalizedAbbreviation() - Method in enum org.orekit.time.Month
Get the capitalized three letters abbreviation.
getCapitalizedName() - Method in enum org.orekit.time.Month
Get the capitalized full name.
getCarrierPhase() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
Get the carrier phase.
getCarrierPhase(String) - Static method in enum org.orekit.gnss.metric.ntrip.CarrierPhase
Get the carrier phase corresponding to a code.
getCartesian() - Method in class org.orekit.frames.FieldTransform
Get the underlying elementary Cartesian part.
getCartesian() - Method in class org.orekit.frames.Transform
Get the underlying elementary Cartesian part.
getCartesianIntersectionPoint(FieldLine<T>, FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.bodies.OneAxisEllipsoid
Get the intersection point of a line with the surface of the body.
getCartesianIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.bodies.OneAxisEllipsoid
Get the intersection point of a line with the surface of the body.
getCartesianPoint() - Method in class org.orekit.frames.TopocentricFrame
Get the surface point defining the origin of the frame.
getCasters() - Method in class org.orekit.gnss.metric.ntrip.SourceTable
Get the casters records.
getCatalogName() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata
Get the specification of satellite catalog source.
getCatalogName() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get the satellite catalog used for the object.
getCatalogName() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the specification of satellite catalog source.
getCcsdsEpoch() - Method in class org.orekit.time.AbstractTimeScales
 
getCcsdsEpoch() - Method in interface org.orekit.time.TimeScales
Reference epoch for CCSDS Time Code Format (CCSDS 301.0-B-4): 1958-01-01T00:00:00 International Atomic Time (not UTC).
getCCSDSEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Reference epoch for CCSDS Time Code Format (CCSDS 301.0-B-4).
getCCSDSName() - Method in enum org.orekit.files.ccsds.definitions.PocMethodType
Get CCSDS compatible name.
getCCSDSType() - Method in enum org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethodType
Get the CCSDS type if used by the SANA registry.
getCDAreaOverMass() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Get the object’s Cd x A/m used to propagate the state vector and covariance to TCA.
getCdmMessageLink() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the Unique identifier of Conjunction Data Message linked to this Orbit Data Message.
getCdrgdrg() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [7,7] in covariance matrix (with index starting at 1).
getCdrgdrg() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the object [7,7] in covariance matrix (with index starting at 1).
getCdrgn() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [7,3] in covariance matrix (with index starting at 1).
getCdrgndot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [7,6] in covariance matrix (with index starting at 1).
getCdrgr() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [7,1] in covariance matrix (with index starting at 1).
getCdrgrdot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [7,4] in covariance matrix (with index starting at 1).
getCdrgt() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [7,2] in covariance matrix.
getCdrgtdot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [7,5] in covariance matrix (with index starting at 1).
getCdrgx() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the object [7,1] in covariance matrix (with index starting at 1).
getCdrgxdot() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the object [7,4] in covariance matrix (with index starting at 1).
getCdrgy() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the object [7,2] in covariance matrix.
getCdrgydot() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the object [7,5] in covariance matrix (with index starting at 1).
getCdrgz() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the object [7,3] in covariance matrix (with index starting at 1).
getCdrgzdot() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the object [7,6] in covariance matrix (with index starting at 1).
getCelestialBodies() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the instance of CelestialBodies that is called by the static methods in this class.
getCelestialBodies() - Method in class org.orekit.data.CompositeDataContext
 
getCelestialBodies() - Method in interface org.orekit.data.DataContext
Get a factory constructing CelestialBodys based on the auxiliary data in this context.
getCelestialBodies() - Method in class org.orekit.data.ExceptionalDataContext
 
getCelestialBodies() - Method in class org.orekit.data.LazyLoadedDataContext
 
getCelestialBody() - Method in enum org.orekit.files.ccsds.definitions.CenterName
Get the celestial body corresponding to the CCSDS constant.
getCelestialBody(CelestialBodies) - Method in enum org.orekit.files.ccsds.definitions.CenterName
Get the celestial body corresponding to the CCSDS constant.
getCelestialBodyProvider() - Method in class org.orekit.propagation.events.BetaAngleDetector
Coordinate provider for the celestial body.
getCelestialBodyProvider() - Method in class org.orekit.propagation.events.FieldBetaAngleDetector
Coordinate provider for the celestial body.
getCelestialSource() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the source and version of celestial body (e.g.
getCenter() - Method in class org.orekit.bodies.Ellipse
Get the center of the 2D ellipse.
getCenter() - Method in class org.orekit.bodies.FieldEllipse
Get the center of the 2D ellipse.
getCenter() - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata
Get the body at origin of reference frame.
getCenter() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Get the origin of reference frame.
getCenter() - Method in class org.orekit.files.ccsds.ndm.odm.OdmCommonMetadata
Get the origin of reference frame.
getCenter() - Method in class org.orekit.geometry.fov.SmoothFieldOfView
Get the direction of the FOV center, in spacecraft frame.
getCenter() - Method in class org.orekit.models.earth.tessellation.Tile
Get the center point.
getCenterMass() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Get the current center of mass of vehicle in body fixed coordinate system.
getCenterName() - Method in class org.orekit.files.ccsds.definitions.ModifiedFrame
Get the CCSDS center name.
getCenterOfCurvature(FieldVector2D<T>) - Method in class org.orekit.bodies.FieldEllipse
Find the center of curvature (point on the evolute) at the nadir of a point.
getCenterOfCurvature(Vector2D) - Method in class org.orekit.bodies.Ellipse
Find the center of curvature (point on the evolute) at the nadir of a point.
getCenterOfMassCorrection() - Method in class org.orekit.files.ilrs.CRD.RangeSupplement
Get the target center of mass.
getCenterOfMassOffset() - Method in class org.orekit.files.ilrs.CPFHeader
Get the approximate center of mass to reflector offset.
getCenterOfPressure() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalProperties
Get the location of center of pressure.
getCenterOfPressureReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalProperties
Get reference frame for center of pressure.
getCentralBody() - Method in class org.orekit.propagation.events.InterSatDirectViewDetector
Get the central body.
getCentralBodyRotation() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get central body angular rotation rate.
getCentralDate(AbsoluteDate) - Method in class org.orekit.time.AbstractTimeInterpolator.InterpolationData
Deprecated.
This method appears to be unused and may be removed in Orekit 13.0. Please Comment on forum.orekit.org if you have a use case for this method.
getCentralDate(AbsoluteDate, AbsoluteDate, AbsoluteDate, double) - Static method in class org.orekit.time.AbstractTimeInterpolator
Get the central date to use to find neighbors while taking into account extrapolation threshold.
getCentralDate(AbsoluteDate, ImmutableTimeStampedCache<T>, double) - Static method in class org.orekit.time.AbstractTimeInterpolator
Get the central date to use to find neighbors while taking into account extrapolation threshold.
getCentralDate(FieldAbsoluteDate<KK>) - Method in class org.orekit.time.AbstractFieldTimeInterpolator.InterpolationData
Deprecated.
This method appears to be unused and may be removed in Orekit 13.0. Please Comment on forum.orekit.org if you have a use case for this method.
getCentralDate(FieldAbsoluteDate<KK>, FieldAbsoluteDate<KK>, FieldAbsoluteDate<KK>, double) - Static method in class org.orekit.time.AbstractFieldTimeInterpolator
Get the central date to use to find neighbors while taking into account extrapolation threshold.
getCentralDate(FieldAbsoluteDate<KK>, ImmutableFieldTimeStampedCache<T, KK>, double) - Static method in class org.orekit.time.AbstractFieldTimeInterpolator
Get the central date to use to find neighbors while taking into account extrapolation threshold.
getChi() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTGravityContext
Getter for the chi.
getChi() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTGravityContext
Get Χ = 1 / sqrt(1 - e²) = 1 / B.
getChi2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTGravityContext
Getter for the chi2.
getChi2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTGravityContext
Get Χ².
getChi3() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
Getter for the Χ³.
getChi3() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
Deprecated.
getChildren() - Method in class org.orekit.frames.OrphanFrame
Get all children of the instance.
getCic() - Method in class org.orekit.gnss.rflink.gps.SubFrame3
Get Cic.
getCic() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac
Getter for the Cic parameter.
getCic() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Getter for the Cic parameter.
getCic() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
Gets the Amplitude of the Cosine Harmonic Correction Term to the Angle of Inclination.
getCij(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldFourierCjSjCoefficients
Get the coefficient Cij.
getCij(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FourierCjSjCoefficients
Get the coefficient Cij.
getCircularEx() - Method in class org.orekit.orbits.CircularOrbit
Get the first component of the circular eccentricity vector.
getCircularEx() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the first component of the circular eccentricity vector.
getCircularExDot() - Method in class org.orekit.orbits.CircularOrbit
Get the first component of the circular eccentricity vector derivative.
getCircularExDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the first component of the circular eccentricity vector derivative.
getCircularEy() - Method in class org.orekit.orbits.CircularOrbit
Get the second component of the circular eccentricity vector.
getCircularEy() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the second component of the circular eccentricity vector.
getCircularEyDot() - Method in class org.orekit.orbits.CircularOrbit
Get the second component of the circular eccentricity vector derivative.
getCircularEyDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the second component of the circular eccentricity vector derivative.
getCIRF(IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames
 
getCIRF(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames
Get the CIRF2000 reference frame.
getCIRF(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
Get the CIRF2000 reference frame.
getCis() - Method in class org.orekit.gnss.rflink.gps.SubFrame3
Get Cis.
getCis() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac
Getter for the Cis parameter.
getCis() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Getter for the Cis parameter.
getCis() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
Gets the Amplitude of the Sine Harmonic Correction Term to the Angle of Inclination.
getCj(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
Get the Cj coefficient.
getCj(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient
Get the Cj coefficient.
getCk0() - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Get the un-normalized zonal coefficients.
getCk0() - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Get the un-normalized zonal coefficients.
getClassification() - Method in class org.orekit.files.ccsds.section.Header
Get the classification/caveats.
getClassification() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get the classification.
getClassification() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the classification.
getClassificationType() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
Get the classification type.
getClkOffset() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Deprecated.
as of 12.1, replaced by #@link RinexObservationHeader.getClockOffsetApplied()
getClockAcceleration() - Method in class org.orekit.files.rinex.clock.RinexClock.ClockDataLine
Getter for the clock acceleration.
getClockAccelerationDriver() - Method in class org.orekit.estimation.measurements.GroundStation
Get a driver allowing to change station clock acceleration (which is related to measurement date).
getClockAccelerationDriver() - Method in class org.orekit.estimation.measurements.ObservableSatellite
Get the clock acceleration parameter driver.
getClockAccelerationSigma() - Method in class org.orekit.files.rinex.clock.RinexClock.ClockDataLine
Getter for the clock acceleration sigma.
getClockAccuracy() - Method in class org.orekit.files.sp3.SP3Coordinate
Get the clock accuracy.
getClockBase() - Method in class org.orekit.files.sp3.SP3Header
Get the base for clock/clock-rate accuracy.
getClockBias() - Method in class org.orekit.files.rinex.clock.RinexClock.ClockDataLine
Getter for the clock bias.
getClockBiasSigma() - Method in class org.orekit.files.rinex.clock.RinexClock.ClockDataLine
Getter for the clock bias sigma.
getClockConstraint() - Method in class org.orekit.files.rinex.clock.RinexClock.ReferenceClock
Getter for the clock constraint.
getClockCorrection() - Method in class org.orekit.files.sp3.SP3Coordinate
Get the clock correction value.
getClockCorrection() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmClockCorrectionData
Get the clock correction data.
getClockCorrection() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCombinedCorrectionData
Get the clock correction data.
getClockCorrection() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm02Data
Get the clock correction data.
getClockCorrection() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Data
Get the clock correction data.
getClockCount() - Method in class org.orekit.files.ccsds.utils.ContextBinding
Get clock count.
getClockData() - Method in class org.orekit.files.rinex.clock.RinexClock
Getter for an unmodifiable map of clock data.
getClockDataTypes() - Method in class org.orekit.files.rinex.clock.RinexClock
Getter for the different clock data types.
getClockDriftDriver() - Method in class org.orekit.estimation.measurements.GroundStation
Get a driver allowing to change station clock drift (which is related to measurement date).
getClockDriftDriver() - Method in class org.orekit.estimation.measurements.ObservableSatellite
Get the clock drift parameter driver.
getClockID() - Method in class org.orekit.files.rinex.clock.RinexClock.ReferenceClock
Getter for the clock ID.
getClockOffsetApplied() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Get the application flag for realtime-derived receiver clock offset.
getClockOffsetDriver() - Method in class org.orekit.estimation.measurements.GroundStation
Get a driver allowing to change station clock (which is related to measurement date).
getClockOffsetDriver() - Method in class org.orekit.estimation.measurements.ObservableSatellite
Get the clock offset parameter driver.
getClockRate() - Method in class org.orekit.files.ccsds.utils.ContextBinding
Get clock rate.
getClockRate() - Method in class org.orekit.files.rinex.clock.RinexClock.ClockDataLine
Getter for the clock rate.
getClockRateAccuracy() - Method in class org.orekit.files.sp3.SP3Coordinate
Get the clock rate accuracy.
getClockRateChange() - Method in class org.orekit.files.sp3.SP3Coordinate
Get the clock rate.
getClockRateSigma() - Method in class org.orekit.files.rinex.clock.RinexClock.ClockDataLine
Getter for the clock rate sigma.
getCndotn() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [6,3] in covariance matrix (with index starting at 1).
getCndotndot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [6,6] in covariance matrix (with index starting at 1).
getCndotr() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [6,1] in covariance matrix (with index starting at 1).
getCndotrdot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [6,4] in covariance matrix (with index starting at 1).
getCndott() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [6,2] in covariance matrix (with index starting at 1).
getCndottdot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [6,5] in covariance matrix (with index starting at 1).
getCnm() - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data
Get the cosine parameters of spherical harmonics expansion of degree N and order M.
getCnn() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [3,3] in covariance matrix (with index starting at 1).
getCnr() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [3,1] in covariance matrix (with index starting at 1).
getCnt() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [3,2] in covariance matrix (with index starting at 1).
getCo2AB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext
Get co2AB = C / 2AB.
getCo2AB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTGravityContext
Get Co2AB = C / 2AB.
getCo2AB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext
Get co2AB = C / 2AB.
getCo2AB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTGravityContext
Get Co2AB = C / 2AB.
getCodeBias() - Method in class org.orekit.gnss.metric.messages.common.CodeBias
Get the code bias associated to the signal ID.
getCodeBias(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm05Data
Get the code bias for a given signal ID.
getCodeBiases() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm05Data
Get the code biases for the current satellite.
getCoefficients() - Method in enum org.orekit.forces.gravity.potential.OceanLoadDeformationCoefficients
Get the load deformation coefficients for ocean tides.
getCoefficients(String) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficientsBLQFactory
Get the coefficients for a given site.
getCoefficients(AbsoluteDate, Set<String>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.GaussianShortPeriodicCoefficients
Computes the coefficients involved in the contributions.
getCoefficients(AbsoluteDate, Set<String>) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.ShortPeriodTerms
Computes the coefficients involved in the contributions.
getCoefficients(FieldAbsoluteDate<T>, Set<String>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldGaussianShortPeriodicCoefficients
Computes the coefficients involved in the contributions.
getCoefficients(FieldAbsoluteDate<T>, Set<String>) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.FieldShortPeriodTerms
Computes the coefficients involved in the contributions.
getCoefficientsKeyPrefix() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldGaussianShortPeriodicCoefficients
Get the prefix for short period coefficients keys.
getCoefficientsKeyPrefix() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.GaussianShortPeriodicCoefficients
Get the prefix for short period coefficients keys.
getCoefficientsKeyPrefix() - Method in interface org.orekit.propagation.semianalytical.dsst.forces.FieldShortPeriodTerms
Get the prefix for short period coefficients keys.
getCoefficientsKeyPrefix() - Method in interface org.orekit.propagation.semianalytical.dsst.forces.ShortPeriodTerms
Get the prefix for short period coefficients keys.
getCollisionPercentile() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the array of 1 to n elements indicating the percentile(s) for which estimates of the collision probability are provided in the COLLISION_PROBABILITY variable.
getCollisionProbability() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the probability (between 0.0 and 1.0) that Object1 and Object2 will collide.
getCollisionProbaMethod() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the method that was used to calculate the collision probability.
getCombinationType() - Method in class org.orekit.estimation.measurements.gnss.CombinedObservationData
Get the type of the combination of measurements used to build the instance.
getCombinedFrequency() - Method in class org.orekit.estimation.measurements.gnss.CombinedObservationData
Get the value of the combined frequency in MHz.
getCombinedFrequency(Frequency, Frequency) - Method in class org.orekit.estimation.measurements.gnss.AbstractDualFrequencyCombination
Get the combined frequency of two measurements.
getCombinedFrequency(Frequency, Frequency) - Method in class org.orekit.estimation.measurements.gnss.GeometryFreeCombination
Get the combined frequency of two measurements.
getCombinedFrequency(Frequency, Frequency) - Method in class org.orekit.estimation.measurements.gnss.IonosphereFreeCombination
Get the combined frequency of two measurements.
getCombinedFrequency(Frequency, Frequency) - Method in class org.orekit.estimation.measurements.gnss.NarrowLaneCombination
Get the combined frequency of two measurements.
getCombinedFrequency(Frequency, Frequency) - Method in class org.orekit.estimation.measurements.gnss.WideLaneCombination
Get the combined frequency of two measurements.
getCombinedMHzFrequency() - Method in class org.orekit.estimation.measurements.gnss.CombinedObservationData
Deprecated.
getCombinedProvider(TransformProvider, TransformProvider) - Static method in class org.orekit.frames.TransformProviderUtils
Combine two transform providers.
getCombinedRadius() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Get combined radius.
getCombinedRadius() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition
Get combined radius.
getCombinedValue(double, double) - Method in class org.orekit.estimation.measurements.gnss.AbstractSingleFrequencyCombination
Get the combined observed value of two measurements.
getCombinedValue(double, double) - Method in class org.orekit.estimation.measurements.gnss.GRAPHICCombination
Get the combined observed value of two measurements.
getCombinedValue(double, double) - Method in class org.orekit.estimation.measurements.gnss.PhaseMinusCodeCombination
Get the combined observed value of two measurements.
getCombinedValue(double, Frequency, double, Frequency) - Method in class org.orekit.estimation.measurements.gnss.AbstractDualFrequencyCombination
Get the combined observed value of two measurements.
getCombinedValue(double, Frequency, double, Frequency) - Method in class org.orekit.estimation.measurements.gnss.GeometryFreeCombination
Get the combined observed value of two measurements.
getCombinedValue(double, Frequency, double, Frequency) - Method in class org.orekit.estimation.measurements.gnss.IonosphereFreeCombination
Get the combined observed value of two measurements.
getCombinedValue(double, Frequency, double, Frequency) - Method in class org.orekit.estimation.measurements.gnss.NarrowLaneCombination
Get the combined observed value of two measurements.
getCombinedValue(double, Frequency, double, Frequency) - Method in class org.orekit.estimation.measurements.gnss.WideLaneCombination
Get the combined observed value of two measurements.
getComment() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get comment for relative metadata.
getComments() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData
Get the comments.
getComments() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmData
Get the comments.
getComments() - Method in class org.orekit.files.ccsds.ndm.Ndm
Get an unmodifiable view of the comments.
getComments() - Method in class org.orekit.files.ccsds.section.CommentsContainer
Get the comments.
getComments() - Method in class org.orekit.files.ilrs.CPF
Get the comments contained in the file.
getComments() - Method in class org.orekit.files.ilrs.CRD
Get the comments contained in the file.
getComments() - Method in class org.orekit.files.rinex.clock.RinexClock
Getter for the comments.
getComments() - Method in class org.orekit.files.rinex.RinexFile
Get an unmodifiable view of the comments.
getComments() - Method in class org.orekit.files.sp3.SP3Header
Get the comments.
getCompleteName(File) - Method in class org.orekit.data.FilesListCrawler
Get the complete name of a input.
getCompleteName(URL) - Method in class org.orekit.data.NetworkCrawler
Get the complete name of a input.
getCompleteName(T) - Method in class org.orekit.data.AbstractListCrawler
Get the complete name of a input.
getComponents() - Method in class org.orekit.files.ilrs.CRDConfiguration.SystemConfiguration
Get the components (config ids) for system configuration.
getComponents(int) - Method in class org.orekit.time.AbsoluteDate
Split the instance into date/time components for a local time.
getComponents(int) - Method in class org.orekit.time.FieldAbsoluteDate
Split the instance into date/time components for a local time.
getComponents(int, TimeScale) - Method in class org.orekit.time.AbsoluteDate
Split the instance into date/time components for a local time.
getComponents(int, TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate
Split the instance into date/time components for a local time.
getComponents(TimeZone) - Method in class org.orekit.time.AbsoluteDate
Split the instance into date/time components for a time zone.
getComponents(TimeZone) - Method in class org.orekit.time.FieldAbsoluteDate
Split the instance into date/time components for a time zone.
getComponents(TimeZone, TimeScale) - Method in class org.orekit.time.AbsoluteDate
Split the instance into date/time components for a time zone.
getComponents(TimeZone, TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate
Split the instance into date/time components for a time zone.
getComponents(TimeScale) - Method in class org.orekit.time.AbsoluteDate
Split the instance into date/time components.
getComponents(TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate
Split the instance into date/time components.
getCompressionEncryption() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
Get the compression/encryption algorithm applied.
getConditionChecker() - Method in class org.orekit.control.indirect.shooting.AbstractFixedBoundaryCartesianSingleShooting
Getter for the boundary condition checker.
getConfidence() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get confidence metric.
getConfiguration(String, int) - Method in class org.orekit.frames.ITRFVersionLoader
 
getConfiguration(String, int) - Method in interface org.orekit.frames.ItrfVersionProvider
Get the ITRF version configuration defined by a given file at specified date.
getConfigurationId() - Method in class org.orekit.files.ilrs.CRDConfiguration.BaseConfiguration
Get the configuration ID.
getConfigurationRecord(String) - Method in class org.orekit.files.ilrs.CRDConfiguration
Get configuration record corresponding to the configId.
getConfigurationRecordMap() - Method in class org.orekit.files.ilrs.CRDConfiguration
Get the configuration records map.
getConfigurationRecords() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
Get the system configuration records.
getConjunctionId() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the Originator’s ID that uniquely identifies the conjunction to which the message refers.
getConsiderN() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get number of consider parameters.
getConsiderParameters() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get description of consider parameters.
getConstantNormalizedProvider(int, int, AbsoluteDate) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Get the constant gravity field coefficients provider from the first supported file.
getConstantNormalizedProvider(int, int, AbsoluteDate) - Method in interface org.orekit.forces.gravity.potential.GravityFields
Get a constant gravity field normalized coefficients provider frozen at a given epoch.
getConstantNormalizedProvider(int, int, AbsoluteDate) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
Get a constant gravity field normalized coefficients provider frozen at a given epoch.
getConstantUnnormalizedProvider(int, int, AbsoluteDate) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Get the constant gravity field coefficients provider from the first supported file.
getConstantUnnormalizedProvider(int, int, AbsoluteDate) - Method in interface org.orekit.forces.gravity.potential.GravityFields
Get a constant gravity field unnormalized coefficients provider frozen at a given epoch.
getConstantUnnormalizedProvider(int, int, AbsoluteDate) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
Get a constant gravity field unnormalized coefficients provider frozen at a given epoch.
getConstellation() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the name of the constellation this space object belongs to.
getConstellation() - Method in class org.orekit.orbits.WalkerConstellationSlot
Get the constellation.
getConstituents() - Method in class org.orekit.files.ccsds.ndm.Ndm
Get an unmodifiable view of the constituents.
getConstraintsMap() - Method in class org.orekit.utils.AbstractMultipleShooting
Get the map of patch points components which are constrained.
getContentAsBoolean() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Get the content of the entry as a boolean.
getContentAsDouble() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Get the content of the entry as a double.
getContentAsEnum(Class<T>) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Get the content of the entry as an enum.
getContentAsEnumList(Class<T>) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Get the content of the entry as a list of enum.
getContentAsFreeTextList() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Get the content of the entry as a list of free-text strings.
getContentAsInt() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Get the content of the entry as an integer.
getContentAsNormalizedList() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Get the content of the entry as a list of normalized strings.
getContentAsNormalizedString() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Get the content of the entry.
getContentAsUppercaseCharacter() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Get the content of the entry as an uppercase character.
getContentAsUppercaseList() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Get the content of the entry as a list of normalized and uppercased strings.
getContentAsUppercaseString() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Get the content of the entry as normalized and uppercased.
getContentAsVector() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Get the content of the entry as a vector.
getContext() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter
Get the current context.
getContext() - Method in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter
Get the current context.
getControl3DVectorCostType() - Method in class org.orekit.forces.maneuvers.FieldImpulseManeuver
Get the control vector's cost type.
getControl3DVectorCostType() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
Get the control vector's cost type.
getControl3DVectorCostType() - Method in class org.orekit.forces.maneuvers.Maneuver
Get the control vector's cost type.
getControl3DVectorCostType() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the control vector's cost type.
getControl3DVectorCostType() - Method in class org.orekit.forces.maneuvers.propulsion.ProfileThrustPropulsionModel
Get the control vector's cost type.
getControl3DVectorCostType() - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel
Get the control vector's cost type.
getConventions() - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder
Get the IERS conventions.
getConventions() - Method in class org.orekit.files.ccsds.ndm.NdmConstituent
Get IERS conventions.
getConventions() - Method in class org.orekit.files.ccsds.utils.ContextBinding
Get IERS conventions.
getConventions() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser
Get IERS conventions.
getConventions() - Method in class org.orekit.frames.EOPHistory
Get the IERS conventions to which these EOP apply.
getConversionJacobian(SpacecraftState) - Method in class org.orekit.propagation.AbstractMatricesHarvester
Get the conversion Jacobian between state parameters and parameters used for derivatives.
getConverter(ContextBinding) - Method in enum org.orekit.files.ccsds.definitions.TimeSystem
Get associated TimeConverter.
getConverter(ITRFVersion, ITRFVersion) - Static method in enum org.orekit.frames.ITRFVersion
Find a converter between specified ITRF frames.
getConverter(ITRFVersion, ITRFVersion, TimeScale) - Static method in enum org.orekit.frames.ITRFVersion
Find a converter between specified ITRF frames.
getCoordinates() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory
Get the coordinates for this ephemeris segment in EphemerisFile.EphemerisSegment.getFrame().
getCoordinates() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemData
Get an unmodifiable view of the data points.
getCoordinates() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSegment
Get the coordinates for this ephemeris segment in EphemerisFile.EphemerisSegment.getFrame().
getCoordinates() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
Get the coordinates for this ephemeris segment in EphemerisFile.EphemerisSegment.getFrame().
getCoordinates() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
Get the coordinates for this ephemeris segment in EphemerisFile.EphemerisSegment.getFrame().
getCoordinates() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris
Get the coordinates for this ephemeris segment in EphemerisFile.EphemerisSegment.getFrame().
getCoordinates() - Method in class org.orekit.files.sp3.SP3Segment
Get the coordinates for this ephemeris segment in EphemerisFile.EphemerisSegment.getFrame().
getCoordinates() - Method in class org.orekit.files.stk.STKEphemerisFile.STKEphemerisSegment
 
getCoordinates(SpacecraftState, int, int) - Static method in class org.orekit.estimation.measurements.AbstractMeasurement
Get Cartesian coordinates as derivatives.
getCoordinateSystem() - Method in class org.orekit.files.sp3.SP3Header
Returns the coordinate system of the entries in this orbit file.
getCorrectedMeasurement() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the estimated measurement.
getCorrectedMeasurement() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Get the estimated measurement.
getCorrectedMeasurement() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel
Get the estimated measurement.
getCorrectedSpacecraftStates() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the corrected spacecraft states.
getCorrectedSpacecraftStates() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Get the corrected spacecraft states.
getCorrectedSpacecraftStates() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel
Get the corrected spacecraft states.
getCorrection() - Method in class org.orekit.files.rinex.observation.PhaseShiftCorrection
Get the Phase Shift Corrections.
getCorrection() - Method in class org.orekit.files.rinex.observation.ScaleFactorCorrection
Get the Scale Factor.
getCorrectionAberrationDiurnal() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the diurnal aberration correction.
getCorrectionAberrationYearly() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the yearly aberration correction.
getCorrectionAngle1() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the correctionAngle1.
getCorrectionAngle2() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the correctionAngle2.
getCorrectionDoppler() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the correctionDoppler.
getCorrectionMagnitude() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the magnitude correction.
getCorrectionRange(RangeUnitsConverter) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the raw correction for range in meters.
getCorrectionRcs() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the radar cross section correction.
getCorrectionReceive() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the correctionReceive.
getCorrectionsApplied() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the correctionApplied.
getCorrectionTransmit() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the correctionTransmit.
getCorrelationCoefficientsMatrix() - Method in class org.orekit.estimation.measurements.Position
Get the correlation coefficients matrix.
getCorrelationCoefficientsMatrix() - Method in class org.orekit.estimation.measurements.PV
Get the correlation coefficients matrix.
getCosparID() - Method in class org.orekit.gnss.antenna.SatelliteAntenna
Get COSPAR ID.
getCost() - Method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointDerivativesProvider
Getter for the cost.
getCount() - Method in class org.orekit.estimation.measurements.EstimatedMeasurementBase
Get the evaluations counter.
getCountry() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the name of the country where the space object owner is based.
getCountry() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord
Get the country.
getCountry() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
Get the country.
getCovariance() - Method in class org.orekit.estimation.sequential.MeasurementDecorator
getCovariance(AbsoluteDate) - Method in class org.orekit.propagation.analytical.Ephemeris
Get the covariance at given date.
getCovarianceBlock() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmData
Get the covariance matrix logical block.
getCovarianceBlock() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData
Get the covariance matrix logical block.
getCovarianceBlocks() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmData
Get covariance logical blocks.
getCovarianceBlocks() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmData
Get covariance logical blocks.
getCovarianceInterpolator() - Method in class org.orekit.propagation.analytical.Ephemeris
Get covariance interpolator.
getCovarianceMatrices() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemData
Get an unmodifiable view of Covariance Matrices.
getCovarianceMatrices() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSegment
Get an unmodifiable view of Covariance Matrices.
getCovarianceMatrix() - Method in class org.orekit.estimation.measurements.Position
Get the covariance matrix.
getCovarianceMatrix() - Method in class org.orekit.estimation.measurements.PV
Get the covariance matrix.
getCovarianceMatrix() - Method in class org.orekit.files.ccsds.ndm.odm.CartesianCovariance
Get the Position/Velocity covariance matrix.
getCovarianceMethod() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get the method name used to calculate covariance during OD.
getCovarianceOrbitType() - Method in class org.orekit.propagation.StateCovarianceMatrixProvider
Get the orbit type in which the covariance matrix is expressed.
getCovariances() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistory
Get the covariances.
getCovariances() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistory
Get the covariances.
getCovarianceSource() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get the source of the covariance data.
getCovarianceType() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination
Get type of attitude error state.
getCovBasis() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadata
Get basis of this covariance time history data.
getCovBasis() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata
Get basis of this covariance time history data.
getCovBasisID() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadata
Get identification number of the orbit determination or simulation upon which this covariance is based.
getCovBasisID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata
Get identification number of the orbit determination or simulation upon which this covariance is based.
getCovConfidence() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Get the measure of the confidence in the covariance errors matching reality.
getCovConfidence() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata
Get the measure of confidence in covariance error matching reality.
getCovConfidenceMethod() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Get the method used for the calculation of COV_CONFIDENCE.
getCovFrameEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata
Get epoch of the covariance reference frame.
getCovID() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadata
Get covariance identification number.
getCovID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata
Get covariance identification number.
getCovNextID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata
Get identification number of next covariance.
getCovOrdering() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata
Get covariance ordering.
getCovPrevID() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadata
Get identification number of previous covariance.
getCovPrevID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata
Get identification number of previous covariance.
getCovReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadata
Get reference frame of the covariance.
getCovReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata
Get reference frame of the covariance.
getCovScaleMax() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata
Get the maximum scale factor to apply to achieve realism.
getCovScaleMin() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata
Get the minimum scale factor to apply to achieve realism.
getCovType() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadata
Get covariance element set type.
getCovType() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata
Get covariance element set type.
getCovUnits() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata
Get covariance element set units.
getCr3bpSystem() - Method in class org.orekit.orbits.RichardsonExpansion
Get the considered CR3BP system.
getCRAreaOverMass() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Get the object’s Cr x A/m used to propagate the state vector and covariance to TCA.
getCrc() - Method in class org.orekit.gnss.rflink.gps.SubFrame3
Get Crc.
getCrc() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac
Getter for the Crc parameter.
getCrc() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Getter for the Crc parameter.
getCrc() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
Gets the Amplitude of the Cosine Harmonic Correction Term to the Orbit Radius.
getCrdotn() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [4, 3] in covariance matrix (with index starting at 1) .
getCrdotr() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [4,1] in covariance matrix (with index starting at 1).
getCrdotrdot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [4, 4] in covariance matrix (with index starting at 1).
getCrdott() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [4,2] in covariance matrix (with index starting at 1).
getCreationDate() - Method in class org.orekit.files.ccsds.section.Header
Get the message creation date and time in UTC.
getCreationDate() - Method in class org.orekit.files.rinex.clock.RinexClock
Getter for the creation date.
getCreationDate() - Method in class org.orekit.files.rinex.section.RinexBaseHeader
Getter for the creation date.
getCreationDate() - Method in class org.orekit.files.sinex.SinexLoader
Get the creation date of the parsed SINEX file.
getCreationDateComponents() - Method in class org.orekit.files.rinex.section.RinexBaseHeader
Getter for the creation date of the file as a string.
getCreationDateString() - Method in class org.orekit.files.rinex.clock.RinexClock
Getter for the creation date of the file as a string.
getCreationTimeString() - Method in class org.orekit.files.rinex.clock.RinexClock
Getter for the creation time of the file as a string.
getCreationTimeZone() - Method in class org.orekit.files.rinex.section.RinexBaseHeader
Getter for the creation time zone of the file as a string.
getCreationTimeZoneString() - Method in class org.orekit.files.rinex.clock.RinexClock
Getter for the creation time zone of the file as a string.
getCrr() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [1,1] in covariance matrix (with index starting at 1).
getCrs() - Method in class org.orekit.gnss.rflink.gps.SubFrame2
Get Crs.
getCrs() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac
Getter for the Crs parameter.
getCrs() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Getter for the Crs parameter.
getCrs() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
Gets the Amplitude of the Sine Harmonic Correction Term to the Orbit Radius.
getCrsIndicator() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01Header
Get the Global/Regional CRS Indicator.
getCrsIndicator() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Header
Get the Global/Regional CRS Indicator.
getcScaleFactor() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadata
Get the (median) suggested covariance scale factor.
getcScaleFactorMax() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadata
Get the maximum suggested covariance scale factor.
getcScaleFactorMin() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadata
Get the minimum suggested covariance scale factor.
getCsig3eigvec3() - Method in class org.orekit.files.ccsds.ndm.cdm.SigmaEigenvectorsCovariance
Get the Sigma/Eigenvectors Covariance data.
getCsrpdrg() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [8,7] in covariance matrix (with index starting at 1).
getCsrpdrg() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the object [8,7] in covariance matrix (with index starting at 1).
getCsrpn() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [8,3] in covariance matrix (with index starting at 1).
getCsrpndot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [8,6] in covariance matrix (with index starting at 1).
getCsrpr() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [8,1] in covariance matrix (with index starting at 1).
getCsrprdot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [8,4] in covariance matrix (with index starting at 1).
getCsrpsrp() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [8,8] in covariance matrix (with index starting at 1).
getCsrpsrp() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the object [8,8] in covariance matrix (with index starting at 1).
getCsrpt() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [8,2] in covariance matrix (with index starting at 1).
getCsrptdot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [8,5] in covariance matrix (with index starting at 1).
getCsrpx() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the object [8,1] in covariance matrix (with index starting at 1).
getCsrpxdot() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the object [8,4] in covariance matrix (with index starting at 1).
getCsrpy() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the object [8,2] in covariance matrix (with index starting at 1).
getCsrpydot() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the object [8,5] in covariance matrix (with index starting at 1).
getCsrpz() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the object [8,3] in covariance matrix (with index starting at 1).
getCsrpzdot() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the object [8,6] in covariance matrix (with index starting at 1).
getCtdotn() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [5,3] in covariance matrix (with index starting at 1).
getCtdotr() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [5, 1] in covariance matrix (with index starting at 1).
getCtdotrdot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [5,4] in covariance matrix (with index starting at 1).
getCtdott() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [5,2] in covariance matrix (with index starting at 1).
getCtdottdot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [5,5] in covariance matrix (with index starting at 1).
getCthrdrg() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [9,7] in covariance matrix (with index starting at 1).
getCthrdrg() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the object [9,7] in covariance matrix (with index starting at 1).
getCthrn() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [9,3] in covariance matrix (with index starting at 1).
getCthrndot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [9,6] in covariance matrix (with index starting at 1).
getCthrr() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [9,1] in covariance matrix (with index starting at 1).
getCthrrdot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [9,4] in covariance matrix (with index starting at 1).
getCthrsrp() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [9,8] in covariance matrix (with index starting at 1).
getCthrsrp() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the object [9,8] in covariance matrix (with index starting at 1).
getCthrt() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [9,2] in covariance matrix (with index starting at 1).
getCthrtdot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [9,5] in covariance matrix (with index starting at 1).
getCthrthr() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [9,9] in covariance matrix (with index starting at 1).
getCthrthr() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the object [9,9] in covariance matrix (with index starting at 1).
getCthrx() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the object [9,1] in covariance matrix (with index starting at 1).
getCthrxdot() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the object [9,4] in covariance matrix (with index starting at 1).
getCthry() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the object [9,2] in covariance matrix (with index starting at 1).
getCthrydot() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the object [9,5] in covariance matrix (with index starting at 1).
getCthrz() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the object [9,3] in covariance matrix (with index starting at 1).
getCthrzdot() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the object [9,6] in covariance matrix (with index starting at 1).
getCtr() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [2,1] in covariance matrix (with index starting at 1).
getCtr81Adj() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
Gets the centered 81-day arithmetic average of F10.7 (adjusted).
getCtr81Obs() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
Gets the centered 81-day arithmetic average of F10.7 (observed).
getCtt() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [2,2] in covariance matrix (with index starting at 1).
getCuc() - Method in class org.orekit.gnss.rflink.gps.SubFrame2
Get Cuc.
getCuc() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac
Getter for the Cuc parameter.
getCuc() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Getter for the Cuc parameter.
getCuc() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
Gets the Amplitude of the Cosine Harmonic Correction Term to the Argument of Latitude.
getCurrent() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser
Get the current processing state.
getCurrent() - Method in class org.orekit.utils.units.Unit
Get the current exponent.
getCurrentDate() - Method in class org.orekit.estimation.sequential.AbstractKalmanEstimator
Get the current date.
getCurrentDate() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the current date.
getCurrentDate() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Get the current date.
getCurrentDate() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel
Get the current date.
getCurrentMeasurementNumber() - Method in class org.orekit.estimation.sequential.AbstractKalmanEstimator
Get the current measurement number.
getCurrentMeasurementNumber() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the current measurement number.
getCurrentMeasurementNumber() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Get the current measurement number.
getCurrentMeasurementNumber() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel
Get the current measurement number.
getCurrentState() - Method in interface org.orekit.propagation.sampling.FieldOrekitStepInterpolator
Get the state at previous grid point date.
getCurrentState() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator
Get the state at current grid point date.
getCus() - Method in class org.orekit.gnss.rflink.gps.SubFrame2
Get Cus.
getCus() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac
Getter for the Cus parameter.
getCus() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Getter for the Cus parameter.
getCus() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
Gets the Amplitude of the Sine Harmonic Correction Term to the Argument of Latitude.
getCxdotx() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the object [4,1] in covariance matrix (with index starting at 1).
getCxdotxdot() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the object [4, 4] in covariance matrix (with index starting at 1).
getCxdoty() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the object [4,2] in covariance matrix (with index starting at 1).
getCxdotz() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the object [4, 3] in covariance matrix (with index starting at 1) .
getCXO2N2A2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
Get (C * χ) / ( 2 * n² * a² ).
getCXO2N2A2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
Get (C * χ) / ( 2 * n² * a² ).
getCxx() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the object [1,1] in covariance matrix (with index starting at 1).
getCycleDuration() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Getter for the duration of the GNSS cycle in seconds.
getCycleDuration() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSClockElements
Gets the duration of the GNSS cycle in seconds.
getCycleDuration() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
Gets the duration of the GNSS cycle in seconds.
getCycleSlipMap() - Method in class org.orekit.estimation.measurements.gnss.CycleSlipDetectorResults
Get the cycle slip Map with contains the results.
getCydotx() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the object [5, 1] in covariance matrix (with index starting at 1).
getCydotxdot() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the object [5,4] in covariance matrix (with index starting at 1).
getCydoty() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the object [5,2] in covariance matrix (with index starting at 1).
getCydotydot() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the object [5,5] in covariance matrix (with index starting at 1).
getCydotz() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the object [5,3] in covariance matrix (with index starting at 1).
getCyx() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the object [2,1] in covariance matrix (with index starting at 1).
getCyy() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the object [2,2] in covariance matrix (with index starting at 1).
getCzdotx() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the object [6,1] in covariance matrix (with index starting at 1).
getCzdotxdot() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the object [6,4] in covariance matrix (with index starting at 1).
getCzdoty() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the object [6,2] in covariance matrix (with index starting at 1).
getCzdotydot() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the object [6,5] in covariance matrix (with index starting at 1).
getCzdotz() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the object [6,3] in covariance matrix (with index starting at 1).
getCzdotzdot() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the object [6,6] in covariance matrix (with index starting at 1).
getCzx() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the object [3,1] in covariance matrix (with index starting at 1).
getCzy() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the object [3,2] in covariance matrix (with index starting at 1).
getCzz() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the object [3,3] in covariance matrix (with index starting at 1).
getD() - Method in class org.orekit.data.DelaunayArguments
Get the mean elongation of the Moon from the Sun.
getD() - Method in class org.orekit.data.FieldDelaunayArguments
Get the mean elongation of the Moon from the Sun.
getDailyFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
Get the value of the daily F10.7 solar flux for previous day.
getDailyFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
Get the value of the daily F10.7 solar flux for previous day.
getDailyFlux(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.NRLMSISE00InputParameters
Get the value of the daily F10.7 solar flux for previous day.
getDarkCount() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Get the dark count.
getData() - Method in class org.orekit.files.ccsds.ndm.adm.acm.Acm
Get the data from the single segment.
getData() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Apm
Get the file data.
getData() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Ocm
Get the data from the single segment.
getData() - Method in class org.orekit.files.ccsds.ndm.odm.omm.Omm
Get the file data.
getData() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm
Get the file data.
getData() - Method in class org.orekit.files.ccsds.section.Segment
Get the segment data.
getData() - Method in class org.orekit.files.ilrs.CRD.Meteo
Get an unmodifiable view of the tabulated meteorological data.
getData() - Method in class org.orekit.gnss.metric.messages.rtcm.RtcmMessage
Get the data.
getData() - Method in class org.orekit.gnss.metric.messages.ssr.SsrMessage
Get the data.
getData() - Method in class org.orekit.utils.DoubleArrayDictionary
Get an unmodifiable view of the dictionary entries.
getData() - Method in class org.orekit.utils.FieldArrayDictionary
Get an unmodifiable view of the dictionary entries.
getData() - Method in class org.orekit.utils.TimeSpanMap.Span
Get the data valid during this time span.
getDataBlocks() - Method in class org.orekit.files.ilrs.CRD
Get the data blocks contain in the file.
getDataContext() - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder
Get the data context.
getDataContext() - Method in class org.orekit.files.ccsds.ndm.NdmConstituent
Get the data context.
getDataContext() - Method in class org.orekit.files.ccsds.utils.ContextBinding
Get the data context used for getting frames, time scales, and celestial bodies.
getDataContext() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser
Get the data context used for getting frames, time scales, and celestial bodies.
getDataFormat(String) - Static method in enum org.orekit.gnss.metric.ntrip.DataFormat
Get the message type corresponding to a keyword.
getDataId() - Method in class org.orekit.gnss.rflink.gps.SubFrame45
Get data ID.
getDataMap() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionMessage
Get the all data parsed in the RTCM correction message.
getDataObject1() - Method in class org.orekit.files.ccsds.ndm.cdm.Cdm
Get the file data.
getDataObject2() - Method in class org.orekit.files.ccsds.ndm.cdm.Cdm
Get the file data.
getDataProvidersManager() - Method in class org.orekit.data.AbstractSelfFeedingLoader
Get the data provider manager.
getDataProvidersManager() - Method in class org.orekit.data.LazyLoadedDataContext
Get the provider of auxiliary data for this data context.
getDataProvidersManager() - Method in class org.orekit.frames.LazyLoadedEop
Get the data providers manager for this instance.
getDataQuality() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the dataQuality.
getDataQulityIndicator() - Method in class org.orekit.files.ilrs.CRD.SessionStatistics
Get the data quality assessment indicator 0=undefined or no comment 1=clear, easily filtered data, with little or no noise 2=clear data with some noise; filtering is slightly compromised by noise level 3=clear data with a significant amount of noise, or weak data with little noise.
getDataReleaseFlag() - Method in class org.orekit.files.ilrs.CRDHeader
Get the flag indicating the data release.
getDataSet() - Method in class org.orekit.estimation.measurements.filtering.SmoothedObservationDataSet
Get the original observation data set used to compute the smoothed observation data.
getDataSet() - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityDataLoader
Get the data set.
getDataSet() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader
Getter for the data set.
getDataSet() - Method in class org.orekit.models.earth.atmosphere.data.DtcDataLoader
Getter for the data set.
getDataSet() - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimationLoader
 
getDataSet() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader
Gets the data set.
getDataSource() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage
Getter for the the data source.
getDataStreams() - Method in class org.orekit.gnss.metric.ntrip.SourceTable
Get the data streams records.
getDataType() - Method in class org.orekit.files.ilrs.CRDHeader
Get the data type.
getDataType() - Method in class org.orekit.files.rinex.clock.RinexClock.ClockDataLine
Getter for the clock data type.
getDataType(int) - Static method in enum org.orekit.files.ilrs.CRDHeader.DataType
Get the data type for the given indicator.
getDataTypes() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get observation data types used.
getDataTypes() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the data types in the data section.
getDataUsed() - Method in class org.orekit.files.sp3.SP3Header
Returns the data used indicator from the SP3 file.
getDate() - Method in class org.orekit.attitudes.Attitude
Get the date of attitude parameters.
getDate() - Method in class org.orekit.attitudes.FieldAttitude
Get the date of attitude parameters.
getDate() - Method in class org.orekit.data.DelaunayArguments
Get the date.
getDate() - Method in class org.orekit.data.FieldDelaunayArguments
Get the date.
getDate() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Get the date.
getDate() - Method in class org.orekit.estimation.measurements.EstimatedMeasurementBase
Get the date.
getDate() - Method in class org.orekit.estimation.measurements.gnss.CombinedObservationDataSet
Get the date.
getDate() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovariance
Get the date.
getDate() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeState
Get the date.
getDate() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovariance
Get the date.
getDate() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Get the date.
getDate() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryState
Get the date.
getDate() - Method in class org.orekit.files.ccsds.ndm.odm.omm.Omm
Get the date.
getDate() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm
Get the date.
getDate() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement
Get the date.
getDate() - Method in class org.orekit.files.ilrs.CRD.Calibration
 
getDate() - Method in class org.orekit.files.ilrs.CRD.MeteorologicalMeasurement
Get the date.
getDate() - Method in class org.orekit.files.ilrs.CRD.RangeMeasurement
Get the date.
getDate() - Method in class org.orekit.files.ilrs.CRD.RangeSupplement
 
getDate() - Method in class org.orekit.files.rinex.observation.ObservationDataSet
Get the date.
getDate() - Method in class org.orekit.files.sinex.SinexEopEntry
Get the date.
getDate() - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
Get the date of the maneuver.
getDate() - Method in class org.orekit.frames.EOPEntry
Get the date.
getDate() - Method in class org.orekit.frames.FieldTransform
Get the date.
getDate() - Method in class org.orekit.frames.Transform
Get the date.
getDate() - Method in class org.orekit.gnss.DOP
Gets the calculation date of the DOP.
getDate() - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData.LocalSolarActivity
 
getDate() - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityDataLoader.LineParameters
 
getDate() - Method in class org.orekit.models.earth.atmosphere.data.DtcDataLoader.LineParameters
 
getDate() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader.LineParameters
 
getDate() - Method in class org.orekit.orbits.FieldOrbit
Get the date of orbital parameters.
getDate() - Method in class org.orekit.orbits.Orbit
Get the date of orbital parameters.
getDate() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Getter for the reference date of the ephemeris.
getDate() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Getter for the ephemeris reference date.
getDate() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
 
getDate() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
 
getDate() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get the TLE current date.
getDate() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the TLE current date.
getDate() - Method in class org.orekit.propagation.conversion.averaging.AbstractAveragedOrbitalState
Get the date.
getDate() - Method in interface org.orekit.propagation.conversion.averaging.AveragedOrbitalState
Get the date.
getDate() - Method in class org.orekit.propagation.events.DateDetector
Get the current event date according to the propagator.
getDate() - Method in class org.orekit.propagation.events.EventsLogger.LoggedEvent
Get the date.
getDate() - Method in class org.orekit.propagation.events.FieldDateDetector
Get the current event date according to the propagator.
getDate() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the date.
getDate() - Method in class org.orekit.propagation.FieldStateCovariance
Get the date.
getDate() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the date of the orbit.
getDate() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get the date of the orbit.
getDate() - Method in class org.orekit.propagation.SpacecraftState
Get the date.
getDate() - Method in class org.orekit.propagation.StateCovariance
Get the date.
getDate() - Method in class org.orekit.time.AbsoluteDate
Get the date.
getDate() - Method in class org.orekit.time.ClockOffset
Get the date.
getDate() - Method in class org.orekit.time.DateTimeComponents
Get the date component.
getDate() - Method in class org.orekit.time.FieldAbsoluteDate
Get the date.
getDate() - Method in class org.orekit.time.FieldClockOffset
Get the date.
getDate() - Method in interface org.orekit.time.FieldTimeStamped
Get the date.
getDate() - Method in class org.orekit.time.FieldTimeStampedPair
Get the date.
getDate() - Method in class org.orekit.time.GLONASSDate
 
getDate() - Method in class org.orekit.time.GNSSDate
Get the date.
getDate() - Method in interface org.orekit.time.TimeStamped
Get the date.
getDate() - Method in class org.orekit.time.TimeStampedDouble
Get the date.
getDate() - Method in class org.orekit.time.TimeStampedField
Get the date.
getDate() - Method in class org.orekit.time.TimeStampedPair
Get the date.
getDate() - Method in class org.orekit.time.UTCTAIOffset
Get the date of the start of the leap.
getDate() - Method in class org.orekit.utils.DateDriver
Get the shifted date.
getDate() - Method in class org.orekit.utils.FieldTimeSpanMap.Transition
Get the transition absolute date.
getDate() - Method in class org.orekit.utils.TimeSpanMap.Transition
Get the transition date.
getDate() - Method in class org.orekit.utils.TimeStampedAngularCoordinates
Get the date.
getDate() - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates
Get the date.
getDate() - Method in class org.orekit.utils.TimeStampedFieldPVCoordinates
Get the date.
getDate() - Method in class org.orekit.utils.TimeStampedPVCoordinates
Get the date.
getDateAndTime() - Method in class org.orekit.files.ilrs.CRDHeader
Get the date and time as the string value.
getDates() - Method in class org.orekit.propagation.events.DateDetector
Get all event dates currently managed, in chronological order.
getDates() - Method in class org.orekit.propagation.events.FieldDateDetector
Get all event field dates currently managed, in chronological order.
getDay() - Method in class org.orekit.time.DateComponents
Get the day.
getDayFraction() - Method in class org.orekit.files.sp3.SP3Header
Returns the day fraction for this SP3 file.
getDayNumber() - Method in class org.orekit.time.GLONASSDate
Get the number of the current day in a four year interval.
getDayOfWeek() - Method in class org.orekit.time.DateComponents
Get the day of week.
getDayOfYear() - Method in class org.orekit.time.DateComponents
Get the day number in year.
getDayOfYear(AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.AbstractVienna
Get day of year.
getDcb(String, String, AbsoluteDate) - Method in class org.orekit.files.sinex.Dcb
Get the value of the Differential Code Bias for a given observation pair and a at a given date.
getDcb(ObservationType, ObservationType, AbsoluteDate) - Method in class org.orekit.files.sinex.Dcb
Get the value of the Differential Code Bias for a given observation pair and a at a given date.
getDcbData() - Method in class org.orekit.files.sinex.DcbSatellite
Get the DCB data for the current satellite.
getDcbData(SatelliteSystem) - Method in class org.orekit.files.sinex.DcbStation
Get the DCB data for a given satellite system.
getDcBodyFrame() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Get spacecraft body frame in which OrbitManeuverHistoryMetadata.getDcBodyTrigger() is specified.
getDcBodyTrigger() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Get direction in body frame for triggering duty cycle.
getDcbSatellite(String) - Method in class org.orekit.files.sinex.SinexLoader
Get the DCB data for a given satellite identified by its PRN.
getDcbStation(String) - Method in class org.orekit.files.sinex.SinexLoader
Get the DCB data for a given station.
getDcExecStart() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Get the start time of initial duty cycle-based maneuver execution.
getDcExecStop() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Get the end time of final duty cycle-based maneuver execution.
getDcjDh(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
Get the dCj / dh coefficient.
getDcjDh(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient
Get the dCj / dh coefficient.
getDcjDk(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
Get the dCj / dk coefficient.
getDcjDk(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient
Get the dCj / dk coefficient.
getDcMaxCycles() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Get the maximum number of "ON" duty cycles.
getDcMinCycles() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Get the minimum number of "ON" duty cycles.
getDcPhaseStartAngle() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Get phase angle of pulse start.
getDcPhaseStopAngle() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Get phase angle of pulse stop.
getDcpSensitivityVectorPosition() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadata
Get the DCP sensitivity vector (position errors at TCA).
getDcpSensitivityVectorVelocity() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadata
Get the DCP sensitivity vector (velocity errors at TCA).
getDcRefDir() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Get reference direction for triggering duty cycle.
getDcRefTime() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Get duty cycle thrust reference time.
getDcTimePulseDuration() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Get duty cycle pulse "ON" duration.
getDcTimePulsePeriod() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Get duty cycle elapsed time between start of a pulse and start of next pulse.
getDcType() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Get type of duty cycle.
getDcWindowClose() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Get the end time of duty cycle-based maneuver window.
getDcWindowOpen() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Get the start time of duty cycle-based maneuver window.
getDdEps() - Method in class org.orekit.frames.EOPEntry
Get the correction for nutation in obliquity δΔε.
getDdim() - Method in class org.orekit.bodies.CR3BPSystem
Get the CR3BP distance between the two bodies.
getDDot() - Method in class org.orekit.data.DelaunayArguments
Get the mean elongation of the Moon from the Sun time derivative.
getDDot() - Method in class org.orekit.data.FieldDelaunayArguments
Get the mean elongation of the Moon from the Sun time derivative.
getDdPsi() - Method in class org.orekit.frames.EOPEntry
Get the correction for nutation in longitude δΔΨ.
getDecimalYear(int, int, int) - Static method in class org.orekit.models.earth.GeoMagneticField
Utility function to get a decimal year for a given day.
getDeclination() - Method in class org.orekit.models.earth.GeoMagneticElements
Returns the declination of the magnetic field in radians.
getDecorrelatedReference() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Get the reference decorrelated ambiguities.
getDecreasingTimeShift() - Method in class org.orekit.propagation.events.EventShifter
Get the decreasing events time shift.
getDefault() - Static method in interface org.orekit.data.DataContext
Get the default data context that is used to implement the static factories (TimeScalesFactory, FramesFactory, etc) and loaders that feed themselves (e.g.
getDefaultEclipseDetectionSettings() - Static method in class org.orekit.forces.radiation.ConicallyShadowedLightFluxModel
Define default detection settings for eclipses.
getDefaultEclipseDetectionSettings() - Static method in class org.orekit.forces.radiation.CylindricallyShadowedLightFluxModel
Define default detection settings for eclipses.
getDefaultEventDetectionSettings() - Static method in class org.orekit.propagation.events.EventDetectionSettings
Returns default settings for event detections.
getDefaultInterpolationDegree() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Get the default interpolation degree.
getDefaultLaw(Frames) - Static method in interface org.orekit.propagation.Propagator
Get a default law using the given frames.
getDefaultMass() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Get the default mass.
getDefaultModel() - Static method in class org.orekit.models.earth.troposphere.FixedTroposphericDelay
Returns the default model, loading delay values from the file "tropospheric-delay.txt" via the default data context.
getDefaultTleGenerationAlgorithm(TimeScale, Frame) - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator
Get the default TLE generation algorithm.
getDefaultVersion() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter
Get the default format version.
getDefaultVersion() - Method in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter
Get the default format version.
getDefaultYawRate(int) - Static method in class org.orekit.gnss.attitude.GPSBlockIIA
Get the default yaw rate for a satellite.
getDefinedTimeSystem() - Method in class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage
Get the time system defined by this message.
getDelaunayMultipliers() - Method in class org.orekit.models.earth.displacement.Tide
Get the multipliers for Delaunay arguments (l, l', F, D, Ω).
getDelay() - Method in class org.orekit.models.earth.troposphere.FieldTroposphericDelay
Get the total slanted delay (m).
getDelay() - Method in class org.orekit.models.earth.troposphere.TroposphericDelay
Get the total slanted delay (m).
getDelayShift() - Method in class org.orekit.files.ilrs.CRD.Calibration
Get the calibration delay shift.
getDeltaClockC0() - Method in class org.orekit.gnss.metric.messages.common.ClockCorrection
Get the delta clock C0.
getDeltaClockC1() - Method in class org.orekit.gnss.metric.messages.common.ClockCorrection
Get the delta clock C1.
getDeltaClockC2() - Method in class org.orekit.gnss.metric.messages.common.ClockCorrection
Get the delta clock C2.
getDeltai() - Method in class org.orekit.gnss.rflink.gps.SubFrameAlmanac
Get Δi.
getDeltaI() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
 
getDeltaI() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
Get the correction to the mean value of inclination.
getDeltaMass() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver
Get mass change during maneuver.
getDeltaMass() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Get mass change.
getDeltaMass() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver
Get mass change during maneuver (value is < 0).
getDeltaN() - Method in class org.orekit.gnss.rflink.gps.SubFrame2
Get Δn.
getDeltaN() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Getter for the delta of satellite mean motion.
getDeltaN0Dot() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage
Getter for change rate in Δn₀.
getDeltaN0Dot() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage
Getter for change rate in Δn₀.
getDeltaOrbitAlongTrack() - Method in class org.orekit.gnss.metric.messages.common.OrbitCorrection
Get the along-track orbit correction for broadcast ephemeris.
getDeltaOrbitCrossTrack() - Method in class org.orekit.gnss.metric.messages.common.OrbitCorrection
Get the cross-track orbit correction for broadcast ephemeris.
getDeltaOrbitRadial() - Method in class org.orekit.gnss.metric.messages.common.OrbitCorrection
Get the radial orbit correction for broadcast ephemeris.
getDeltaT() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
 
getDeltaT() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
Get the correction to the mean value of Draconian period.
getDeltaTDot() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
 
getDeltaTDot() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
Get the rate of change of Draconian period.
getDeltaTLs() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D
Get ΔtLS field.
getDeltaTLsf() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D
Get ΔtLSF field.
getDeltaTN() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the deltaTauN value.
getDeltaVSat() - Method in class org.orekit.forces.maneuvers.FieldImpulseManeuver
Get the velocity increment in satellite frame.
getDeltaVSat() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
Get the velocity increment in satellite frame.
getDensity(double, double, double, double, double, double, double, double, double, double, double, double, double, double, double) - Method in class org.orekit.models.earth.atmosphere.JB2008
Get the local density with initial entries.
getDensity(int) - Method in class org.orekit.models.earth.atmosphere.NRLMSISE00.FieldOutput
Get one of the stored densities.
getDensity(int, double, double, double, double, double, double, double, double) - Method in class org.orekit.models.earth.atmosphere.DTM2000
Get the local density with initial entries.
getDensity(int, T, T, T, T, double, double, double, double) - Method in class org.orekit.models.earth.atmosphere.DTM2000
Get the local density with initial entries.
getDensity(Vector3D, FieldVector3D<T>) - Method in class org.orekit.models.earth.atmosphere.HarrisPriester
Get the local density.
getDensity(Vector3D, Vector3D) - Method in class org.orekit.models.earth.atmosphere.HarrisPriester
Get the local density.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in interface org.orekit.models.earth.atmosphere.Atmosphere
Get the local density.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.models.earth.atmosphere.DTM2000
Get the local density.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.models.earth.atmosphere.HarrisPriester
Get the local density at some position.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.models.earth.atmosphere.JB2008
Get the local density.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.models.earth.atmosphere.NRLMSISE00
Get the local density.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.models.earth.atmosphere.SimpleExponentialAtmosphere
Get the local density.
getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in interface org.orekit.models.earth.atmosphere.Atmosphere
Get the local density.
getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.models.earth.atmosphere.DTM2000
Get the local density.
getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.models.earth.atmosphere.HarrisPriester
Get the local density at some position.
getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.models.earth.atmosphere.JB2008
Get the local density.
getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.models.earth.atmosphere.NRLMSISE00
Get the local density.
getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.models.earth.atmosphere.SimpleExponentialAtmosphere
 
getDensity(T, T, T, T, T, T, double, double, double, double, double, double, double, double, double) - Method in class org.orekit.models.earth.atmosphere.JB2008
Get the local density with initial entries.
getDensityForecastUncertainty() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadata
Get the atmospheric density forecast error.
getDeployDirSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Get one σ angular off-nominal deployment vector direction.
getDeployDv() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Get velocity increment of deployed "child" object.
getDeployDvCda() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Get typical (50th percentile) product of drag coefficient times cross-sectional area of deployed "child" object.
getDeployDvRatio() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Get ratio of child-to-host ΔV vectors.
getDeployDvSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Get one σ percent error on deployment ΔV magnitude.
getDeployId() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Get identifier of resulting "child" object deployed from this host.
getDeployMass() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Get decrement in host mass as a result of deployment.
getDepth() - Method in class org.orekit.frames.Frame
Get the depth of the frame.
getDerivative() - Method in class org.orekit.time.TimeStampedDoubleAndDerivative
Get time derivative.
getDerivative(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenTesseralLinear
Compute the value of the derivative dKj-n-1, s / de².
getDerivative(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenThirdBodyLinear
Compute the value of the Hansen coefficient dK₀n, s / dΧ.
getDerivative(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenZonalLinear
Get the dK₀-n-1,s / dΧ coefficient derivative.
getDerivative(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGammaMnsFunction
Get Γ function derivative.
getDerivative(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GammaMnsFunction
Get Γ function derivative.
getDerivative(int, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenTesseralLinear
Compute the value of the derivative dKj-n-1, s / de².
getDerivative(int, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenThirdBodyLinear
Compute the value of the Hansen coefficient dK₀n, s / dΧ.
getDerivative(int, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenZonalLinear
Get the dK₀-n-1,s / dΧ coefficient derivative.
getDerivative2TargetDirection(ExtendedPositionProvider, OneAxisEllipsoid, TimeStampedFieldPVCoordinates<T>, Frame) - Method in class org.orekit.attitudes.GroundPointTarget
Get a target vector.
getDerivative2TargetDirection(ExtendedPositionProvider, OneAxisEllipsoid, TimeStampedFieldPVCoordinates<T>, Frame) - Method in interface org.orekit.attitudes.TargetProvider
Get a target vector.
getDerivative2TargetDirection(ExtendedPositionProvider, OneAxisEllipsoid, TimeStampedPVCoordinates, Frame) - Method in class org.orekit.attitudes.GroundPointTarget
Get a target vector.
getDerivative2TargetDirection(ExtendedPositionProvider, OneAxisEllipsoid, TimeStampedPVCoordinates, Frame) - Method in interface org.orekit.attitudes.TargetProvider
Get a target vector.
getDerivativesDrivers() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Get all the drivers with set derivatives.
getDerivativesToEpoch(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.ThirdBodyAttractionEpoch
Compute derivatives of the state w.r.t epoch.
getDescription() - Method in class org.orekit.files.sinex.DcbSatellite
Get the data contained in "DCB/DESCRIPTION" block of the Sinex file.
getDescription() - Method in class org.orekit.files.sinex.DcbStation
Get the data contained in "DCB/DESCRIPTION" block of the Sinex file.
getDesignator() - Method in class org.orekit.files.rinex.clock.RinexClock.Receiver
Getter for the designator.
getDestination() - Method in enum org.orekit.frames.HelmertTransformation.Predefined
Get the destination ITRF.
getDestination() - Method in class org.orekit.frames.ITRFVersion.Converter
Get the destination ITRF.
getDetectionSettings() - Method in class org.orekit.propagation.events.AbstractDetector
Getter for the settings.
getDetectionSettings() - Method in class org.orekit.propagation.events.AdapterDetector
Getter for the settings.
getDetectionSettings() - Method in interface org.orekit.propagation.events.EventDetector
Getter for the settings.
getDetectionSettings() - Method in class org.orekit.propagation.events.FieldAbstractDetector
Getter for the settings.
getDetectionSettings() - Method in class org.orekit.propagation.events.FieldAdapterDetector
Getter for the settings.
getDetectionSettings() - Method in interface org.orekit.propagation.events.FieldEventDetector
Getter for the settings.
getDetector() - Method in class org.orekit.propagation.events.AdapterDetector
Get the wrapped detector.
getDetector() - Method in class org.orekit.propagation.events.EventEnablingPredicateFilter
Get the wrapped raw detector.
getDetector() - Method in class org.orekit.propagation.events.EventShifter
Get the detector for the raw unshifted event.
getDetector() - Method in class org.orekit.propagation.events.EventSlopeFilter
Get the wrapped raw detector.
getDetector() - Method in class org.orekit.propagation.events.FieldAdapterDetector
Get the wrapped detector.
getDetector() - Method in class org.orekit.propagation.events.FieldEventEnablingPredicateFilter
Get the wrapped raw detector.
getDetector() - Method in class org.orekit.propagation.events.FieldEventSlopeFilter
Get the wrapped raw detector.
getDetector() - Method in class org.orekit.propagation.events.handlers.FieldRecordAndContinue.Event
Get the detector.
getDetector() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue.Event
Get the detector.
getDetectorChannel() - Method in class org.orekit.files.ilrs.CRD.Calibration
Get the detector channel.
getDetectorChannel() - Method in class org.orekit.files.ilrs.CRD.FrRangeMeasurement
Get the detector channel.
getDetectorChannel() - Method in class org.orekit.files.ilrs.CRD.NptRangeMeasurement
Get the detector channel.
getDetectorId() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Get the detector configuration ID.
getDetectorRecord() - Method in class org.orekit.files.ilrs.CRDConfiguration
Get the detector configuration record.
getDetectorRecord(CRDConfiguration.SystemConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration
Get detector configuration record related to the systemRecord.
getDetectors() - Method in class org.orekit.propagation.events.BooleanDetector
Get the list of original detectors.
getDetectors() - Method in class org.orekit.propagation.events.FieldBooleanDetector
Get the list of original detectors.
getDetectorType() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Get the detector type.
getDeterminationMethod() - Method in class org.orekit.files.sinex.DcbDescription
Get the determination mode used to generate the bias results.
getdGjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dGjs / dα coefficient.
getdGjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dGjs / dα coefficient.
getdGjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dGjs / dβ coefficient.
getdGjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dGjs / dβ coefficient.
getdGjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dGjs / dh coefficient.
getdGjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dGjs / dh coefficient.
getdGjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dGjs / dk coefficient.
getdGjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dGjs / dk coefficient.
getdGmsdAlpha(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials
Get the dGmsj / dα coefficient.
getdGmsdAlpha(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dGmsj / dα coefficient.
getdGmsdBeta(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials
Get the dGmsj / dβ coefficient.
getdGmsdBeta(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dGmsj / dβ coefficient.
getdGmsdh(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials
Get the dGmsj / dh coefficient.
getdGmsdh(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dGmsj / dh coefficient.
getdGmsdk(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials
Get the dGmsj / dk coefficient.
getdGmsdk(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dGmsj / dk coefficient.
getdHjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dHjs / dα coefficient.
getdHjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dHjs / dα coefficient.
getdHjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dHjs / dβ coefficient.
getdHjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dHjs / dβ coefficient.
getdHjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dHjs / dh coefficient.
getdHjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dHjs / dh coefficient.
getdHjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dHjs / dk coefficient.
getdHjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dHjs / dk coefficient.
getdHmsdAlpha(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials
Get the dHmsj / dα coefficient.
getdHmsdAlpha(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dHmsj / dα coefficient.
getdHmsdBeta(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials
Get the dHmsj / dβ coefficient.
getdHmsdBeta(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dHmsj / dβ coefficient.
getdHmsdh(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials
Get the dHmsj / dh coefficient.
getdHmsdh(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dHmsj / dh coefficient.
getdHmsdk(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials
Get the dHmsj / dk coefficient.
getdHmsdk(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dHmsj / dk coefficient.
getDiagReference() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Get a reference to the diagonal matrix of the decomposition.
getdIjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dIjs / dα coefficient.
getdIjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dIjs / dα coefficient.
getdIjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dIjs / dβ coefficient.
getdIjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dIjs / dβ coefficient.
getdIjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dIjs / dh coefficient.
getdIjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dIjs / dh coefficient.
getdIjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dIjs / dk coefficient.
getdIjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dIjs / dk coefficient.
getDimension() - Method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointDerivativesProvider
Getter for the dimension.
getDimension() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Get the dimension of the measurement.
getDimension() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
Get the dimension of the measurement.
getDimension() - Method in class org.orekit.forces.maneuvers.jacobians.MassDepletionDelay
Get the dimension of the generated column.
getDimension() - Method in interface org.orekit.propagation.integration.AdditionalDerivativesProvider
Get the dimension of the generated derivative.
getDimension() - Method in interface org.orekit.propagation.integration.FieldAdditionalDerivativesProvider
Get the dimension of the generated derivative.
getDimension() - Method in class org.orekit.propagation.numerical.cr3bp.STMEquations
Get the dimension of the generated derivative.
getDimension() - Method in class org.orekit.propagation.numerical.EpochDerivativesEquations
Get the dimension of the generated derivative.
getDirection() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Get the direction.
getDirection() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the thrust direction in S/C frame.
getDirection(SpacecraftState) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
Get the thrust direction in spacecraft frame.
getDirection(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Get the direction.
getDirection(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the thrust direction in S/C frame.
getDirectionFlag() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement
Get the direction flag (0 = transmit & receive ; 1 = transmit ; 2 = receive).
getDiscontinuityCounter() - Method in class org.orekit.gnss.metric.messages.common.PhaseBias
Get the signal phase discontinuity counter.
getDisplacements() - Method in class org.orekit.estimation.measurements.GroundStation
Get the displacement models.
getDistance() - Method in class org.orekit.bodies.LoxodromeArc
Compute the distance of the arc along the surface of the ellipsoid.
getDistanceThreshold() - Method in class org.orekit.propagation.events.FieldRelativeDistanceDetector
Get the relative distance threshold.
getDistanceThreshold() - Method in class org.orekit.propagation.events.RelativeDistanceDetector
Get the relative distance threshold.
getdJjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dJjs / dα coefficient.
getdJjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dJjs / dα coefficient.
getdJjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dJjs / dβ coefficient.
getdJjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dJjs / dβ coefficient.
getdJjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dJjs / dh coefficient.
getdJjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dJjs / dh coefficient.
getdJjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dJjs / dk coefficient.
getdJjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dJjs / dk coefficient.
getdLnsdGamma(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldLnsCoefficients
Get the value of dLns / dγ (γ).
getdLnsdGamma(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.LnsCoefficients
Get the value of dLns / dγ (γ).
getDn() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D
Get DN field.
getDnl(double, double, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.UpperBounds
Get the upper bound value Dnl(Χ).
getDnl(T, T, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.UpperBounds
Get the upper bound value Dnl(Χ).
getDockedWith() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Get the other space objects this object is docked to.
getDoi() - Method in class org.orekit.files.rinex.section.RinexBaseHeader
Getter for the Digital Object Information.
getDomes() - Method in class org.orekit.files.sinex.Station
Get the site DOMES number.
getDoodson() - Method in class org.orekit.forces.gravity.potential.OceanTidesWave
Get the Doodson number for the wave.
getDoodsonMultipliers() - Method in class org.orekit.models.earth.displacement.Tide
Get the multipliers for Doodson arguments (τ, s, h, p, N', ps).
getDoodsonNumber() - Method in class org.orekit.models.earth.displacement.Tide
Get the Doodson number.
getDopplerCountBias() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Get the Doppler count bias.
getDopplerCountScale() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Get the Doppler count scale.
getDotOrbitDeltaAlongTrack() - Method in class org.orekit.gnss.metric.messages.common.OrbitCorrection
Get the velocity of along-track orbit correction for broadcast ephemeris.
getDotOrbitDeltaCrossTrack() - Method in class org.orekit.gnss.metric.messages.common.OrbitCorrection
Get the velocity of cross-track orbit correction for broadcast ephemeris.
getDotOrbitDeltaRadial() - Method in class org.orekit.gnss.metric.messages.common.OrbitCorrection
Get the velocity of radial orbit correction for broadcast ephemeris.
getDrag() - Method in class org.orekit.forces.Panel
Get drag coefficient.
getDrag() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Get drag force.
getDragArea() - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters
Get the drag area.
getDragCoeff() - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters
Get the drag coefficient.
getDragCoefficient() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalProperties
Get the drag coefficient.
getDragCoefficient() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Get the nominal drag coefficient.
getDragConstantArea() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Get the attitude-independent drag cross-sectional area, not already into attitude-dependent area along OEB.
getDragParametersDrivers() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Get the drivers for supported parameters.
getDragParametersDrivers() - Method in interface org.orekit.forces.drag.DragSensitive
Get the drivers for supported parameters.
getDragParametersDrivers() - Method in class org.orekit.forces.drag.IsotropicDrag
Get the drivers for supported parameters.
getDragSensitive(AbsoluteDate) - Method in class org.orekit.forces.drag.TimeSpanDragForce
Deprecated.
Get the DragSensitive model valid at a date.
getDragSensitiveSpan(AbsoluteDate) - Method in class org.orekit.forces.drag.TimeSpanDragForce
Deprecated.
Get the DragSensitive TimeSpanMap.Span containing a specified date.
getDragUncertainty() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Get the drag coefficient 1σ uncertainty.
getDrivers() - Method in class org.orekit.estimation.measurements.modifiers.AbstractAmbiguityModifier
Deprecated.
Get the drivers for this modifier.
getDrivers() - Method in class org.orekit.utils.ParameterDriversList
Get delegating drivers for all parameters.
getDrivers(double, Orbit, PositionAngleType) - Method in enum org.orekit.orbits.OrbitType
Get parameters drivers initialized from a reference orbit.
getDryMass() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalProperties
Get the mass without propellant.
getDryMass() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Get the mass without propellant.
getDSDensityWrtState(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>) - Method in class org.orekit.forces.drag.AbstractDragForceModel
Compute density and its derivatives.
getDSDensityWrtStateUsingFiniteDifferences(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>) - Method in class org.orekit.forces.drag.AbstractDragForceModel
Compute density and its derivatives.
getDsjDh(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
Get the dSj / dh coefficient.
getDsjDh(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient
Get the dSj / dh coefficient.
getDsjDk(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
Get the dSj / dk coefficient.
getDsjDk(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient
Get the dSj / dk coefficient.
getDSTDTC() - Method in class org.orekit.models.earth.atmosphere.data.DtcDataLoader.LineParameters
Get the DSTDTC parameter.
getDSTDTC(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData
Get the temperature change computed from Dst index.
getDSTDTC(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters
Get the temperature change computed from Dst index.
getDuration() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver
Get duration.
getDuration() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver
Get duration (value is 0 for impulsive maneuver).
getDuration() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Get duration.
getDuration() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver
Get duration (value is 0 for impulsive maneuver).
getDuration() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Get the duration of the maneuver (s).
getDuration() - Method in class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers
Get the duration of the maneuver (s).
getDurationDriver() - Method in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector
Get the driver for duration.
getDurationDriver() - Method in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector
Get the driver for duration.
getDut1() - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage
Get the ΔUT₁.
getDUT1() - Method in class org.orekit.frames.EOPFittedModel
Get the fitted secular and harmonics model for DUT1/LOD.
getDut1Dot() - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage
Get the ΔUT₁ first derivative.
getDut1DotDot() - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage
Get the ΔUT₁ second derivative.
getDv() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Get velocity increment.
getDV() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver
Get velocity increment.
getDvDirSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Get one σ angular off-nominal ΔV direction.
getDvMagSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Get one σ percent error on ΔV magnitude.
getDx() - Method in class org.orekit.frames.EOPEntry
Get the correction for Celestial Intermediate Pole (CIP) coordinates.
getDx() - Method in class org.orekit.frames.EOPFittedModel
Get the fitted secular and harmonics model for nutation x component.
getDy() - Method in class org.orekit.frames.EOPEntry
Get the correction for Celestial Intermediate Pole (CIP) coordinates.
getDy() - Method in class org.orekit.frames.EOPFittedModel
Get the fitted secular and harmonics model for nutation y component.
getE() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Get the orbit eccentricity.
getE() - Method in class org.orekit.gnss.rflink.gps.SubFrame2
Get e.
getE() - Method in class org.orekit.gnss.rflink.gps.SubFrameAlmanac
Get eccentricity.
getE() - Method in class org.orekit.orbits.CartesianOrbit
Get the eccentricity.
getE() - Method in class org.orekit.orbits.CircularOrbit
Get the eccentricity.
getE() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the eccentricity.
getE() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the eccentricity.
getE() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the eccentricity.
getE() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the eccentricity.
getE() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the eccentricity.
getE() - Method in class org.orekit.orbits.FieldOrbit
Get the eccentricity.
getE() - Method in class org.orekit.orbits.KeplerianOrbit
Get the eccentricity.
getE() - Method in class org.orekit.orbits.Orbit
Get the eccentricity.
getE() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Getter for the eccentricity.
getE() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
 
getE() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
Get the Eccentricity.
getE() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
Gets the Eccentricity.
getE() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get the eccentricity.
getE() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the eccentricity.
getE() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the eccentricity.
getE() - Method in class org.orekit.propagation.SpacecraftState
Get the eccentricity.
getE2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext
Get ecc².
getE2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext
Get ecc².
getEarliest() - Method in interface org.orekit.utils.FieldTimeStampedCache
Get the earliest entry in this cache.
getEarliest() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the earliest entry in this cache.
getEarliest() - Method in class org.orekit.utils.ImmutableFieldTimeStampedCache
Get the earliest entry in this cache.
getEarliest() - Method in class org.orekit.utils.ImmutableTimeStampedCache
Get the earliest entry in this cache.
getEarliest() - Method in interface org.orekit.utils.TimeStampedCache
Get the earliest entry in this cache.
getEarliestEpoch() - Method in class org.orekit.files.rinex.clock.RinexClock
Get earliest epoch from the clock data.
getEarth() - Method in interface org.orekit.bodies.CelestialBodies
Get the Earth singleton body.
getEarth() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Earth singleton body.
getEarth() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
 
getEarth() - Method in class org.orekit.forces.gravity.DeSitterRelativity
Get the Earth model used to compute De Sitter effect.
getEarthMoonBarycenter() - Method in interface org.orekit.bodies.CelestialBodies
Get the Earth-Moon barycenter singleton bodies pair.
getEarthMoonBarycenter() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Earth-Moon barycenter singleton bodies pair.
getEarthMoonBarycenter() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
 
getEarthMoonBarycenterSemiMajorAxis(AbsoluteDate, TimeScale) - Static method in class org.orekit.propagation.numerical.cr3bp.CR3BPConstants
Get the Earth-Moon barycenter semi-major axis.
getEarthMoonCR3BP() - Static method in class org.orekit.bodies.CR3BPFactory
Get the Earth-Moon CR3BP singleton bodies pair.
getEarthOrientationAngleFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions
Get the function computing the raw Earth Orientation Angle.
getEarthOrientationAngleFunction(TimeScale, TimeScale) - Method in enum org.orekit.utils.IERSConventions
Get the function computing the raw Earth Orientation Angle.
getEarthOrientationParameters() - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Get the Earth orientation parameters.
getEarthquakeDate() - Method in class org.orekit.models.earth.displacement.PsdCorrection
Get earthquake date.
getEarthTides() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get Enum YesNoUnknown that indicates if Earth and ocean tides are taken into account or not.
getEast() - Method in class org.orekit.bodies.FieldGeodeticPoint
Get the direction to the east of point, expressed in parent shape frame.
getEast() - Method in class org.orekit.bodies.GeodeticPoint
Get the direction to the east of point, expressed in parent shape frame.
getEast() - Method in class org.orekit.frames.TopocentricFrame
Get the east direction of topocentric frame, expressed in parent shape frame.
getEastLongitudeDegrees() - Method in class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElementsPropagator
Get the computed satellite's east longitude.
getEastLongitudeDegrees() - Method in class org.orekit.propagation.analytical.intelsat.IntelsatElevenElementsPropagator
Get the computed satellite's east longitude.
getEastOffsetDriver() - Method in class org.orekit.estimation.measurements.GroundStation
Get a driver allowing to change station position along East axis.
getEcc() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the eccentricity.
getEcc() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get the eccentricity.
getEccentricAnomaly() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the eccentric anomaly.
getEccentricAnomaly() - Method in class org.orekit.orbits.KeplerianOrbit
Get the eccentric anomaly.
getEccentricAnomalyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the eccentric anomaly derivative.
getEccentricAnomalyDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the eccentric anomaly derivative.
getEccentricities() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Get the eccentricities of antenna center.
getEccentricities() - Method in class org.orekit.gnss.antenna.FrequencyPattern
Get the phase center eccentricities.
getEccentricities(Frequency) - Method in class org.orekit.gnss.antenna.Antenna
Get the phase center eccentricities.
getEccentricities(AbsoluteDate) - Method in class org.orekit.files.sinex.Station
Get the station antenna eccentricities for the given epoch.
getEccentricitiesTimeSpanMap() - Method in class org.orekit.files.sinex.Station
Get the TimeSpanMap of site antenna eccentricities.
getEccentricity() - Method in class org.orekit.bodies.OneAxisEllipsoid
Get the first eccentricity of the ellipsoid: e = sqrt(f * (2.0 - f)).
getEccentricitySquared() - Method in class org.orekit.bodies.OneAxisEllipsoid
Get the first eccentricity squared of the ellipsoid: e^2 = f * (2.0 - f).
getEccRefSystem() - Method in class org.orekit.files.sinex.Station
Get the reference system used to define the eccentricity vector (local or cartesian).
getEccRefSystem(String) - Static method in enum org.orekit.files.sinex.Station.ReferenceSystem
Get the eccentricity reference system corresponding to the given value.
getECEF() - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator
Gets the Earth Centered Earth Fixed frame used to propagate GLONASS orbits.
getECEF() - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator
Gets the Earth Centered Earth Fixed frame used to propagate GNSS orbits according to the Interface Control Document.
getECEF() - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator
Gets the Earth Centered Earth Fixed frame used to propagate GNSS orbits.
getECI() - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator
Gets the Earth Centered Inertial frame used to propagate the orbit.
getECI() - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator
Gets the Earth Centered Inertial frame used to propagate the orbit.
getECI() - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator
Gets the Earth Centered Inertial frame used to propagate the orbit.
getEclipseConditionsDetector() - Method in class org.orekit.forces.radiation.ConicallyShadowedLightFluxModel
Retrieve detectors finding entries and exits in different eclipse zones.
getEclipseConditionsDetector() - Method in class org.orekit.forces.radiation.CylindricallyShadowedLightFluxModel
Retrieve detectors finding entries and exits in different eclipse zones.
getEclipseConditionsDetector() - Method in interface org.orekit.forces.radiation.LightFluxModel
Retrieve detectors finding entries and exits in different eclipse zones.
getEcliptic(IERSConventions) - Method in class org.orekit.frames.AbstractFrames
 
getEcliptic(IERSConventions) - Method in interface org.orekit.frames.Frames
Get the ecliptic frame.
getEcliptic(IERSConventions) - Static method in class org.orekit.frames.FramesFactory
Get the ecliptic frame.
getEDot() - Method in class org.orekit.orbits.CartesianOrbit
Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.CircularOrbit
Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.FieldOrbit
Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.Orbit
Get the eccentricity derivative.
getEffects() - Method in class org.orekit.propagation.analytical.AdapterPropagator
Get the differential effects.
getElem(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix
Get the value of an element.
getElementNumber() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get the element number.
getElementNumber() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the element number.
getElements() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeState
Get attitude elements.
getElements() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryState
Get trajectory elements.
getElementSetNumber() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
Get the element set number for this satellite.
getElevation() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement
Get the elevation angle.
getElevation() - Method in class org.orekit.utils.FieldTrackingCoordinates
Get the elevation.
getElevation() - Method in class org.orekit.utils.TrackingCoordinates
Get the elevation.
getElevation(double) - Method in class org.orekit.utils.ElevationMask
Get the interpolated elevation for a given azimuth according to the mask.
getElevation(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.TopocentricFrame
Get the elevation of a point with regards to the local point.
getElevation(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame
Get the elevation of a point with regards to the local point.
getElevation(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldElevationExtremumDetector
Get the elevation value.
getElevation(SpacecraftState) - Method in class org.orekit.propagation.events.ElevationExtremumDetector
Get the elevation value.
getElevationMask() - Method in class org.orekit.gnss.DOPComputer
Get the elevation mask.
getElevationMask() - Method in class org.orekit.propagation.events.ElevationDetector
Returns the currently configured elevation mask.
getElevationMask() - Method in class org.orekit.propagation.events.FieldElevationDetector
Returns the currently configured elevation mask.
getElevationRate() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement
Get the elevation rate.
getEllipsoid() - Method in interface org.orekit.models.earth.EarthShape
Get the underlying ellipsoid model that defines latitude and longitude.
getEllipsoid() - Method in class org.orekit.models.earth.Geoid
 
getEllipsoid() - Method in class org.orekit.models.earth.ReferenceEllipsoid
 
getEME2000() - Method in class org.orekit.frames.AbstractFrames
 
getEME2000() - Method in interface org.orekit.frames.Frames
Get the unique EME2000 frame.
getEME2000() - Static method in class org.orekit.frames.FramesFactory
Get the unique EME2000 frame.
getEmitter() - Method in class org.orekit.estimation.measurements.gnss.AmbiguityDriver
Get emitter id.
getEmitterStation() - Method in class org.orekit.estimation.measurements.BistaticRange
Get the emitter ground station.
getEmitterStation() - Method in class org.orekit.estimation.measurements.BistaticRangeRate
Get the emitter ground station.
getEn() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the GLONASS En Word.
getEncounterFrame() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Get encounter local orbital frame.
getEncounterFrame() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition
Get encounter local orbital frame.
getEnd() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
Get the end of the measurements time span.
getEnd() - Method in class org.orekit.utils.TimeSpanMap.Span
Get the end of this time span.
getEndDate() - Method in class org.orekit.files.rinex.clock.RinexClock.ReferenceClock
Getter for the validity period end date.
getEndDate() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Get the end date.
getEndDate() - Method in class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers
Get the end date.
getEndDate() - Method in class org.orekit.frames.EOPHistory
Get the date of the last available Earth Orientation Parameters.
getEndDate(Frequency) - Method in class org.orekit.estimation.measurements.gnss.CycleSlipDetectorResults
Return the end date at the given frequency.
getEndEpoch() - Method in class org.orekit.files.ilrs.ILRSHeader
Get the ending epoch (UTC).
getEndpoints() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination
Get the endpoints (i.e.
getEndpoints() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata
Get the endpoints (i.e.
getEndpoints() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Get the endpoints (i.e.
getEndpoints() - Method in class org.orekit.files.ccsds.ndm.adm.apm.AngularVelocity
Get the endpoints (i.e.
getEndpoints() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternion
Get the endpoints (i.e.
getEndpoints() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler
Get the endpoints (i.e.
getEndpoints() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
Get the endpoints (i.e.
getEndTime() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver
Get end time of actual maneuver, relative to t₀.
getEndTransition() - Method in class org.orekit.utils.TimeSpanMap.Span
Get the transition at end of this time span.
getEntries() - Method in class org.orekit.frames.EOPHistory
Get a non-modifiable view of the EOP entries.
getEntries() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the total number of entries cached.
getEntry(String) - Method in class org.orekit.utils.DoubleArrayDictionary
Get a complete entry.
getEntry(String) - Method in class org.orekit.utils.FieldArrayDictionary
Get a complete entry.
getEnum(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.Maneuvrable
Get the enum entry corresponding to the given String.
getEopHistory(IERSConventions, boolean) - Method in class org.orekit.time.AbstractTimeScales
Get the EOP history for the given conventions.
getEopHistory(IERSConventions, boolean) - Method in class org.orekit.time.LazyLoadedTimeScales
 
getEOPHistory() - Method in interface org.orekit.frames.EOPBasedTransformProvider
Get the EOP history.
getEOPHistory() - Method in class org.orekit.frames.GTODProvider
Get the EOP history.
getEOPHistory() - Method in class org.orekit.time.UT1Scale
Get the EOP history.
getEOPHistory(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames
Get Earth Orientation Parameters history.
getEOPHistory(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
Get Earth Orientation Parameters history.
getEOPHistory(IERSConventions, boolean) - Method in class org.orekit.frames.LazyLoadedFrames
Get Earth Orientation Parameters history.
getEOPHistory(IERSConventions, boolean, TimeScales) - Method in class org.orekit.frames.LazyLoadedEop
Get Earth Orientation Parameters history.
getEOPHistoryWithoutCachedTidalCorrection() - Method in class org.orekit.frames.EOPHistory
Get version of the instance that does not cache tidal correction.
getEopSource() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the source and version of Earth Orientation Parameters.
getEOPTidalCorrection() - Method in enum org.orekit.utils.IERSConventions
Get the function computing tidal corrections for Earth Orientation Parameters.
getEOPTidalCorrection(TimeScales) - Method in enum org.orekit.utils.IERSConventions
Get the function computing tidal corrections for Earth Orientation Parameters.
getEphemeridesDataLines() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemData
Get the list of Ephemerides data lines.
getEphemeridesDataLines() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris
Get the list of Ephemerides data lines.
getEphemeris(int) - Method in class org.orekit.files.sp3.SP3
Get an ephemeris.
getEphemeris(String) - Method in class org.orekit.files.sp3.SP3
Get an ephemeris.
getEphemerisData() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.RtcmEphemerisMessage
Get the ephemeris data contain in the ephemeris message.
getEphemerisGenerator() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Set up an ephemeris generator that will monitor the propagation for building an ephemeris from it once completed.
getEphemerisGenerator() - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Set up an ephemeris generator that will monitor the propagation for building an ephemeris from it once completed.
getEphemerisGenerator() - Method in interface org.orekit.propagation.FieldPropagator
Set up an ephemeris generator that will monitor the propagation for building an ephemeris from it once completed.
getEphemerisGenerator() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Set up an ephemeris generator that will monitor the propagation for building an ephemeris from it once completed.
getEphemerisGenerator() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Set up an ephemeris generator that will monitor the propagation for building an ephemeris from it once completed.
getEphemerisGenerator() - Method in interface org.orekit.propagation.Propagator
Set up an ephemeris generator that will monitor the propagation for building an ephemeris from it once completed.
getEphemerisNames() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for external ephemeris names for participants.
getEphemerisType() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
Get the ephemeris type.
getEphemerisType() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get the type of ephemeris.
getEphemerisType() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the type of ephemeris.
getEphemName() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get the unique name of the external ephemeris used for OD.
getEpoch() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData
Get the epoch of the data.
getEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.CartesianCovariance
Get matrix epoch.
getEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Get epoch of state vector, Keplerian elements and covariance matrix data.
getEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get time tag for orbit determination solved-for state.
getEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.StateVector
Get epoch of state vector, Keplerian elements and covariance matrix data.
getEpoch() - Method in class org.orekit.files.ccsds.ndm.tdm.Observation
Getter for the epoch.
getEpoch() - Method in class org.orekit.files.rinex.clock.RinexClock.ClockDataLine
Get data line epoch.
getEpoch() - Method in class org.orekit.files.sinex.Station
Get the coordinates reference epoch.
getEpoch() - Method in class org.orekit.files.sp3.SP3Header
Returns the start epoch of the orbit file.
getEpoch() - Method in class org.orekit.frames.HelmertTransformation
Get the reference epoch of the transform.
getEpoch() - Method in class org.orekit.models.earth.GeoMagneticField
Returns the epoch for this magnetic field model.
getEpoch() - Method in class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElements
Get the elements epoch.
getEpoch() - Method in class org.orekit.propagation.analytical.intelsat.IntelsatElevenElements
Get the elements epoch.
getEpoch(TimeScale) - Method in class org.orekit.files.rinex.clock.RinexClock.ClockDataLine
Get data line epoch.
getEpochDelayCorrection() - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration
Get the epoch delay correction.
getEpochEigenInt() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get positional error ellipsoid 1σ intermediate eigenvalue at the epoch of OD.
getEpochEigenMaj() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get positional error ellipsoid 1σ major eigenvalue at the epoch of OD.
getEpochEigenMin() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get positional error ellipsoid 1σ minor eigenvalue at the epoch of OD.
getEpochEvent() - Method in class org.orekit.files.ilrs.CRD.RangeMeasurement
Get the indicator for the time event reference.
getEpochIdentifier() - Method in class org.orekit.files.ilrs.CRDHeader
Get the epoch identifier.
getEpochIgnition() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver
Get epoch ignition.
getEpochInterval() - Method in class org.orekit.files.sp3.SP3Header
Returns the time interval between epochs (in seconds).
getEpochStart() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver
Get epoch start.
getEpochT0() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata
Get the epoch to which all relative times are referenced in data blocks.
getEpochT0() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the epoch to which all relative times are referenced in data blocks.
getEpochTime1s() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionHeader
Get the Epoch Time 1s.
getEpochToc() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Getter for the time of clock epoch.
getEpochToc() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Getter for the time of clock epoch.
getEpsilon() - Method in class org.orekit.propagation.conversion.averaging.converters.FixedPointOsculatingToAveragedConverter
Getter for the convergence threshold.
getEquatorialRadius() - Method in class org.orekit.bodies.OneAxisEllipsoid
Get the equatorial radius of the body.
getEquatorialRadius() - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder
Get the central body equatorial radius.
getEquatorialRadius() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmWriter
Get the central body equatorial radius.
getEquatorialRadius() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get oblate spheroid equatorial radius of central body.
getEquatorialRadius() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Get the central body equatorial radius.
getEquinoctialEx() - Method in class org.orekit.orbits.CartesianOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.CircularOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.FieldOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.KeplerianOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.Orbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the first component of the eccentricity vector (as per equinoctial parameters).
getEquinoctialEx() - Method in class org.orekit.propagation.SpacecraftState
Get the first component of the eccentricity vector (as per equinoctial parameters).
getEquinoctialExDot() - Method in class org.orekit.orbits.CartesianOrbit
Get the first component of the equinoctial eccentricity vector derivative.
getEquinoctialExDot() - Method in class org.orekit.orbits.CircularOrbit
Get the first component of the equinoctial eccentricity vector derivative.
getEquinoctialExDot() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the first component of the equinoctial eccentricity vector derivative.
getEquinoctialExDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the first component of the equinoctial eccentricity vector derivative.
getEquinoctialExDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the first component of the equinoctial eccentricity vector derivative.
getEquinoctialExDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the first component of the equinoctial eccentricity vector derivative.
getEquinoctialExDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the first component of the equinoctial eccentricity vector derivative.
getEquinoctialExDot() - Method in class org.orekit.orbits.FieldOrbit
Get the first component of the equinoctial eccentricity vector derivative.
getEquinoctialExDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the first component of the equinoctial eccentricity vector derivative.
getEquinoctialExDot() - Method in class org.orekit.orbits.Orbit
Get the first component of the equinoctial eccentricity vector derivative.
getEquinoctialEy() - Method in class org.orekit.orbits.CartesianOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.CircularOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.FieldOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.KeplerianOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.Orbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the second component of the eccentricity vector (as per equinoctial parameters).
getEquinoctialEy() - Method in class org.orekit.propagation.SpacecraftState
Get the second component of the eccentricity vector (as per equinoctial parameters).
getEquinoctialEyDot() - Method in class org.orekit.orbits.CartesianOrbit
Get the second component of the equinoctial eccentricity vector derivative.
getEquinoctialEyDot() - Method in class org.orekit.orbits.CircularOrbit
Get the second component of the equinoctial eccentricity vector derivative.
getEquinoctialEyDot() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the second component of the equinoctial eccentricity vector derivative.
getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the second component of the equinoctial eccentricity vector derivative.
getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the second component of the equinoctial eccentricity vector derivative.
getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the second component of the equinoctial eccentricity vector derivative.
getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the second component of the equinoctial eccentricity vector derivative.
getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldOrbit
Get the second component of the equinoctial eccentricity vector derivative.
getEquinoctialEyDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the second component of the equinoctial eccentricity vector derivative.
getEquinoctialEyDot() - Method in class org.orekit.orbits.Orbit
Get the second component of the equinoctial eccentricity vector derivative.
getEquinoxNutationCorrection(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory
Get the correction to the nutation parameters for equinox-based paradigm.
getEquinoxNutationCorrection(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EOPHistory
Get the correction to the nutation parameters for equinox-based paradigm.
getERD(int) - Method in class org.orekit.gnss.rflink.gps.SubFrame4C
Get an Estimated Range Deviation.
getEstimate() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Get the current corrected estimate.
getEstimate() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel
Get the current corrected estimate.
getEstimatedEarthFrame() - Method in class org.orekit.estimation.measurements.GroundStation
Get the estimated Earth frame, including the estimated linear models for pole and prime meridian.
getEstimatedMeasurement(int) - Method in interface org.orekit.estimation.measurements.EstimationsProvider
Get one estimated measurement.
getEstimatedMeasurements() - Method in class org.orekit.estimation.measurements.MultiplexedMeasurement
Get the underlying estimated measurements.
getEstimatedMeasurementsParameters() - Method in class org.orekit.estimation.sequential.AbstractKalmanEstimator
Get the list of estimated measurements parameters.
getEstimatedMeasurementsParameters() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the list of estimated measurements parameters.
getEstimatedMeasurementsParameters() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Get the list of estimated measurements parameters.
getEstimatedMeasurementsParameters() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel
Get the list of estimated measurements parameters.
getEstimatedMeasurementsWithoutDerivatives() - Method in class org.orekit.estimation.measurements.MultiplexedMeasurement
Get the underlying estimated measurements without derivatives.
getEstimatedOrbitalParameters() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the list of estimated orbital parameters.
getEstimatedOrbitalParameters() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Get the list of estimated orbital parameters.
getEstimatedOrbitalParameters() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel
Get the list of estimated orbital parameters.
getEstimatedPropagationParameters() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the list of estimated propagation parameters.
getEstimatedPropagationParameters() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Get the list of estimated propagation parameters.
getEstimatedPropagationParameters() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel
Get the list of estimated propagation parameters.
getEstimatedPropagator() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Get the propagator estimated with the values set in the propagator builder.
getEstimatedPropagator() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel
Get the propagator estimated with the values set in the propagator builder.
getEstimatedUT1() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
Get the estimated UT1 time scale.
getEstimatedUT1() - Method in class org.orekit.estimation.measurements.GroundStation
Get the estimated UT1 scale, including the estimated linear models for prime meridian.
getEstimatedValue() - Method in class org.orekit.estimation.measurements.EstimatedMeasurementBase
Get the estimated value.
getEta() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTJ2SquaredClosedFormContext
Get the eta value.
getEta() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTJ2SquaredClosedFormContext
Get the eta value.
getEulerBlock() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData
Get the Euler angles logical block.
getEulerRotSeq() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination
Get the rotation order for Euler angles.
getEulerRotSeq() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata
Get the rotation order for Euler angles.
getEulerRotSeq() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Get the rotation order of Euler angles.
getEulerRotSeq() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler
Get the rotation order of Euler angles.
getEvaluations() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Get the number of objective function evaluations.
getEvaluationsCount() - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel
Get the evaluations count.
getEvaluationsCount() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Get the number of evaluations used for last estimation.
getEventDate() - Method in class org.orekit.propagation.events.EventState
Get the occurrence time of the event triggered in the current step.
getEventDate() - Method in class org.orekit.propagation.events.FieldEventState
Get the occurrence time of the event triggered in the current step.
getEventDetectionSettings() - Method in class org.orekit.forces.radiation.AbstractSolarLightFluxModel
Getter for eclipse event detection settings used for eclipses.
getEventDetector() - Method in class org.orekit.propagation.events.EventsLogger.LoggedEvent
Get the event detector triggered.
getEventDetector() - Method in class org.orekit.propagation.events.EventState
Get the underlying event detector.
getEventDetector() - Method in class org.orekit.propagation.events.FieldEventsLogger.FieldLoggedEvent
Get the event detector triggered.
getEventDetector() - Method in class org.orekit.propagation.events.FieldEventState
Get the underlying event detector.
getEventDetectors() - Method in class org.orekit.control.indirect.adjoint.cost.BoundedCartesianEnergy
Get the discrete events related to the model.
getEventDetectors() - Method in class org.orekit.control.indirect.adjoint.cost.UnboundedCartesianEnergy
Get the discrete events related to the model.
getEventDetectors() - Method in class org.orekit.control.indirect.adjoint.cost.UnboundedCartesianEnergyNeglectingMass
Get the discrete events related to the model.
getEventDetectors() - Method in class org.orekit.forces.drag.TimeSpanDragForce
Deprecated.
Get the discrete events related to the model.
getEventDetectors() - Method in class org.orekit.forces.empirical.ParametricAcceleration
Get the discrete events related to the model.
getEventDetectors() - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
Get the discrete events related to the model.
getEventDetectors() - Method in interface org.orekit.forces.ForceModel
Get the discrete events related to the model.
getEventDetectors() - Method in class org.orekit.forces.gravity.OceanTides
Get the discrete events related to the model.
getEventDetectors() - Method in class org.orekit.forces.gravity.SolidTides
Get the discrete events related to the model.
getEventDetectors() - Method in class org.orekit.forces.maneuvers.Maneuver
Get the discrete events related to the model.
getEventDetectors() - Method in class org.orekit.forces.maneuvers.propulsion.ProfileThrustPropulsionModel
Get the discrete events related to the model.
getEventDetectors() - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel
Get the discrete events related to the model.
getEventDetectors() - Method in class org.orekit.forces.maneuvers.trigger.IntervalEventTrigger
Get the discrete events related to the model.
getEventDetectors() - Method in class org.orekit.forces.maneuvers.trigger.StartStopEventsTrigger
Get the discrete events related to the model.
getEventDetectors() - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel
Get the discrete events related to the model.
getEventDetectors() - Method in class org.orekit.forces.radiation.RadiationPressureModel
Get the discrete events related to the model.
getEventDetectors() - Method in interface org.orekit.propagation.events.EventDetectorsProvider
Get the discrete events related to the model.
getEventDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Get the discrete events related to the model.
getEventDetectors() - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Get the discrete events related to the model.
getEventDetectors(List<ParameterDriver>) - Method in interface org.orekit.propagation.events.EventDetectorsProvider
Get the discrete events related to the model from a list of ParameterDriver
getEventFlag() - Method in class org.orekit.files.rinex.observation.ObservationDataSet
Get the event flag.
getEvents() - Method in class org.orekit.propagation.events.handlers.FieldRecordAndContinue
Get the events passed to this handler.
getEvents() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue
Get the events passed to this handler.
getEventsDetectors() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Get all the events detectors that have been added.
getEventsDetectors() - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Get all the events detectors that have been added.
getEventsDetectors() - Method in interface org.orekit.propagation.FieldPropagator
Get all the events detectors that have been added.
getEventsDetectors() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get all the events detectors that have been added.
getEventsDetectors() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get all the events detectors that have been added.
getEventsDetectors() - Method in interface org.orekit.propagation.Propagator
Get all the events detectors that have been added.
getEvolution() - Method in class org.orekit.models.earth.displacement.PsdCorrection
Get time evolution.
getEvolution(double, RealVector[], MeasurementDecorator) - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel
getEvolution(double, RealVector[], MeasurementDecorator) - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel
getEvolution(double, RealVector, MeasurementDecorator) - Method in class org.orekit.estimation.sequential.KalmanModel
getEvolution(double, RealVector, MeasurementDecorator) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
getException() - Method in class org.orekit.gnss.metric.ntrip.StreamMonitor
Retrieve exception caught during monitoring.
getExponent() - Method in class org.orekit.utils.units.PowerTerm
Get the fractional exponent.
getExternalClockReference() - Method in class org.orekit.files.rinex.clock.RinexClock
Getter for the external clock reference.
getExternalFrame() - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints
Get the external frame.
getExternalSignalProcessing() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Get the external signal processing.
getExtrapolationThreshold() - Method in class org.orekit.time.AbstractFieldTimeInterpolator
Get the extrapolation threshold.
getExtrapolationThreshold() - Method in class org.orekit.time.AbstractTimeInterpolator
Get the extrapolation threshold.
getExtrapolationThreshold() - Method in interface org.orekit.time.FieldTimeInterpolator
Get the extrapolation threshold.
getExtrapolationThreshold() - Method in interface org.orekit.time.TimeInterpolator
Get the extrapolation threshold.
getF() - Method in class org.orekit.data.DelaunayArguments
Get L - Ω where L is the mean longitude of the Moon.
getF() - Method in class org.orekit.data.FieldDelaunayArguments
Get L - Ω where L is the mean longitude of the Moon.
getF() - Method in class org.orekit.orbits.WalkerConstellation
Get the phasing parameter.
getF10() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader.LineParameters
Get the value of the instantaneous solar flux index (1e-22*Watt/(m²*Hertz)).
getF10(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData
Get the value of the instantaneous solar flux index (1e-22*Watt/(m²*Hertz)).
getF10(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters
Get the value of the instantaneous solar flux index (1e-22*Watt/(m²*Hertz)).
getF107() - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimationLoader.LineParameters
Get the F10.0 flux.
getF107Adj() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
Gets the 10.7-cm Solar Radio Flux (F10.7) Adjusted to 1 AU.
getF107Obs() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
Gets the observed (unadjusted) value of F10.7.
getF10B() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader.LineParameters
Get the value of the mean solar flux.
getF10B(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData
Get the value of the mean solar flux.
getF10B(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters
Get the value of the mean solar flux.
getFactoryKey() - Method in class org.orekit.frames.FactoryManagedFrame
Get the key of the frame within the factory.
getFallbackHostOrIPAddress() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord
Get the fallback host or IP address.
getFallbackPort() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord
Get the fallback port number.
getFDot() - Method in class org.orekit.data.DelaunayArguments
Get L - Ω where L is the mean longitude of the Moon time derivative.
getFDot() - Method in class org.orekit.data.FieldDelaunayArguments
Get L - Ω where L is the mean longitude of the Moon time derivative.
getField() - Method in class org.orekit.orbits.FieldOrbit
Getter for Field.
getField() - Method in class org.orekit.propagation.FieldAbstractPropagator
Field getter.
getField() - Method in class org.orekit.time.AbstractFieldTimeInterpolator.InterpolationData
Get field.
getField() - Method in class org.orekit.time.FieldAbsoluteDate
Get the field.
getField() - Method in class org.orekit.utils.FieldArrayDictionary
Get the field to which elements belong.
getField(int) - Method in class org.orekit.gnss.metric.ntrip.Record
Get one field from the parsed sourcetable.
getField(int) - Method in class org.orekit.gnss.rflink.gps.SubFrame
Get a field.
getField(GeoMagneticFieldFactory.FieldModel, double) - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory
Get the GeoMagneticField for the given model type and year.
getField(GeoMagneticFieldFactory.FieldModel, double) - Method in interface org.orekit.models.earth.GeoMagneticFields
Get the GeoMagneticField for the given model type and year.
getField(GeoMagneticFieldFactory.FieldModel, double) - Method in class org.orekit.models.earth.LazyLoadedGeoMagneticFields
 
getFieldAcceleration(FieldAbsoluteDate<T>, T[], Frame) - Method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointEquationTerm
Compute the acceleration vector.
getFieldAcceleration(FieldAbsoluteDate<T>, T[], Frame) - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointInertialTerm
Compute the acceleration vector.
getFieldAcceleration(FieldAbsoluteDate<T>, T[], Frame) - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointJ2Term
Compute the acceleration vector.
getFieldAcceleration(FieldAbsoluteDate<T>, T[], Frame) - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointKeplerianTerm
Compute the acceleration vector.
getFieldAcceleration(FieldAbsoluteDate<T>, T[], Frame) - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointSingleBodyTerm
Compute the acceleration vector.
getFieldAcceleration(FieldAbsoluteDate<T>, T[], Frame) - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointThirdBodyTerm
Compute the acceleration vector.
getFieldAdjointVelocityNorm(T[]) - Method in class org.orekit.control.indirect.adjoint.cost.AbstractCartesianEnergy
Computes the Euclidean norm of the adjoint velocity vector.
getFieldAuxiliaryElements() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldForceModelContext
Method to get the auxiliary elementsrelated to the ForceModelContext.
getFieldBodyPosition(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointNonCentralBodyTerm
Get body's position.
getFieldDate() - Method in interface org.orekit.frames.FieldStaticTransform
Get the Field date.
getFieldDate() - Method in class org.orekit.frames.FieldTransform
Get the date.
getFieldDensity(FieldSpacecraftState<T>) - Method in class org.orekit.forces.drag.AbstractDragForceModel
Evaluate the Field density.
getFieldEclipseConditionsDetector(Field<T>) - Method in class org.orekit.forces.radiation.ConicallyShadowedLightFluxModel
Retrieve Field detectors finding entries and exits in different eclipse zones.
getFieldEclipseConditionsDetector(Field<T>) - Method in class org.orekit.forces.radiation.CylindricallyShadowedLightFluxModel
Retrieve Field detectors finding entries and exits in different eclipse zones.
getFieldEclipseConditionsDetector(Field<T>) - Method in interface org.orekit.forces.radiation.LightFluxModel
Retrieve Field detectors finding entries and exits in different eclipse zones.
getFieldEventDetectors(Field<S>) - Method in class org.orekit.forces.maneuvers.trigger.IntervalEventTrigger
Get the discrete events related to the model.
getFieldEventDetectors(Field<S>) - Method in class org.orekit.forces.maneuvers.trigger.StartStopEventsTrigger
Get the discrete events related to the model.
getFieldEventDetectors(Field<T>) - Method in class org.orekit.control.indirect.adjoint.cost.BoundedCartesianEnergy
Get the discrete events related to the model.
getFieldEventDetectors(Field<T>) - Method in class org.orekit.control.indirect.adjoint.cost.UnboundedCartesianEnergy
Get the discrete events related to the model.
getFieldEventDetectors(Field<T>) - Method in class org.orekit.control.indirect.adjoint.cost.UnboundedCartesianEnergyNeglectingMass
Get the discrete events related to the model.
getFieldEventDetectors(Field<T>) - Method in class org.orekit.forces.drag.TimeSpanDragForce
Deprecated.
Get the discrete events related to the model.
getFieldEventDetectors(Field<T>) - Method in class org.orekit.forces.empirical.ParametricAcceleration
Get the discrete events related to the model.
getFieldEventDetectors(Field<T>) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
Get the discrete events related to the model.
getFieldEventDetectors(Field<T>) - Method in interface org.orekit.forces.ForceModel
Get the discrete events related to the model.
getFieldEventDetectors(Field<T>) - Method in class org.orekit.forces.gravity.OceanTides
Get the discrete events related to the model.
getFieldEventDetectors(Field<T>) - Method in class org.orekit.forces.gravity.SolidTides
Get the discrete events related to the model.
getFieldEventDetectors(Field<T>) - Method in class org.orekit.forces.maneuvers.Maneuver
Get the discrete events related to the model.
getFieldEventDetectors(Field<T>) - Method in class org.orekit.forces.maneuvers.propulsion.ProfileThrustPropulsionModel
Get the discrete events related to the model.
getFieldEventDetectors(Field<T>) - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel
Get the discrete events related to the model.
getFieldEventDetectors(Field<T>) - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel
Get the discrete events related to the model.
getFieldEventDetectors(Field<T>) - Method in class org.orekit.forces.radiation.RadiationPressureModel
Get the discrete events related to the model.
getFieldEventDetectors(Field<T>) - Method in interface org.orekit.propagation.events.EventDetectorsProvider
Get the discrete events related to the model.
getFieldEventDetectors(Field<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Get the discrete events related to the model.
getFieldEventDetectors(Field<T>) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Get the discrete events related to the model.
getFieldEventDetectors(Field<T>, List<ParameterDriver>) - Method in interface org.orekit.propagation.events.EventDetectorsProvider
Get the discrete events related to the model from a list of ParameterDriver
getFieldHamiltonianContribution(FieldAbsoluteDate<T>, T[], T[], Frame) - Method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointEquationTerm
Computes the contribution to the Hamiltonian.
getFieldHamiltonianContribution(FieldAbsoluteDate<T>, T[], T[], Frame) - Method in interface org.orekit.control.indirect.adjoint.CartesianAdjointEquationTerm
Computes the contribution to the Hamiltonian.
getFieldHamiltonianContribution(T[], T) - Method in interface org.orekit.control.indirect.adjoint.cost.CartesianCost
Computes the Hamiltonian contribution of the cost function.
getFieldHamiltonianContribution(T[], T) - Method in class org.orekit.control.indirect.adjoint.cost.UnboundedCartesianEnergyNeglectingMass
Computes the Hamiltonian contribution of the cost function.
getFieldIntegratorBuilder(Field<T>) - Method in class org.orekit.control.indirect.shooting.propagation.ClassicalRungeKuttaIntegrationSettings
Returns a Field ODE integrator builder.
getFieldIntegratorBuilder(Field<T>) - Method in class org.orekit.control.indirect.shooting.propagation.DormandPrince54IntegrationSettings
Returns a Field ODE integrator builder.
getFieldIntegratorBuilder(Field<T>) - Method in interface org.orekit.control.indirect.shooting.propagation.ShootingIntegrationSettings
Returns a Field ODE integrator builder.
getFieldNewtonianAcceleration(T[]) - Method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointNewtonianTerm
Compute the Newtonian acceleration.
getFieldNewtonianVelocityAdjointContribution(T[], T[]) - Method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointNewtonianTerm
Computes the generic term of a Newtonian attraction (central or not).
getFieldOther(Field<T>) - Method in class org.orekit.frames.encounter.AbstractEncounterLOF
Get the field version of other's position and velocity coordinates.
getFieldOther(Field<T>) - Method in interface org.orekit.frames.encounter.EncounterLOF
Get other's position and velocity coordinates.
getFieldRatesContribution(FieldAbsoluteDate<T>, T[], T[], Frame) - Method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointEquationTerm
Computes the contribution to the rates of the adjoint variables.
getFieldRatesContribution(FieldAbsoluteDate<T>, T[], T[], Frame) - Method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointGravitationalTerm
Computes the contribution to the rates of the adjoint variables.
getFieldRatesContribution(FieldAbsoluteDate<T>, T[], T[], Frame) - Method in interface org.orekit.control.indirect.adjoint.CartesianAdjointEquationTerm
Computes the contribution to the rates of the adjoint variables.
getFieldRatesContribution(FieldAbsoluteDate<T>, T[], T[], Frame) - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointInertialTerm
Computes the contribution to the rates of the adjoint variables.
getFieldsNumber() - Method in class org.orekit.gnss.metric.ntrip.Record
Get the number of fields.
getFieldStep(Field<T>) - Method in class org.orekit.propagation.conversion.AbstractFixedStepFieldIntegratorBuilder
Get "fielded" step size (s).
getFieldThrustAccelerationVector(T[], T) - Method in interface org.orekit.control.indirect.adjoint.cost.CartesianCost
Computes the thrust acceleration vector in propagation frame from the adjoint variables and the mass.
getFieldThrustAccelerationVector(T[], T) - Method in class org.orekit.control.indirect.adjoint.cost.UnboundedCartesianEnergyNeglectingMass
Computes the thrust acceleration vector in propagation frame from the adjoint variables and the mass.
getFieldThrustForceNorm(T[], T) - Method in class org.orekit.control.indirect.adjoint.cost.BoundedCartesianEnergy
Computes the Euclidean norm of the thrust force.
getFieldThrustForceNorm(T[], T) - Method in class org.orekit.control.indirect.adjoint.cost.UnboundedCartesianEnergy
Computes the Euclidean norm of the thrust force.
getFieldVector() - Method in class org.orekit.models.earth.GeoMagneticElements
Returns the magnetic field vector in Tesla.
getFiftiesEpoch() - Method in class org.orekit.time.AbstractTimeScales
 
getFiftiesEpoch() - Method in interface org.orekit.time.TimeScales
Reference epoch for 1950 dates: 1950-01-01T00:00:00 Terrestrial Time.
getFiftiesEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Reference epoch for 1950 dates: 1950-01-01T00:00:00 Terrestrial Time.
getFileDate() - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimationLoader.LineParameters
Get the file date.
getFileDate(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
Get the date of the file from which data at the specified date comes from.
getFileEpochEndTime() - Method in class org.orekit.files.sinex.SinexLoader
Get the file epoch end time.
getFileEpochStartTime() - Method in class org.orekit.files.sinex.SinexLoader
Get the file epoch start time.
getFileFormat() - Method in interface org.orekit.files.ccsds.utils.lexical.MessageParser
Get the file format of the last message parsed.
getFileFormat() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser
Get the file format of the last message parsed.
getFileName() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Get the name of the file.
getFileType() - Method in class org.orekit.files.rinex.section.RinexBaseHeader
Get the file type.
getFilter() - Method in class org.orekit.files.sp3.SP3Header
Get the derivatives filter.
getFilter() - Method in class org.orekit.propagation.events.EventSlopeFilter
Get filter type.
getFilter() - Method in class org.orekit.propagation.StateCovarianceKeplerianHermiteInterpolator
Get Filter defining if only the state covariance value are used or if first or/and second Keplerian derivatives should be used.
getFilter() - Method in class org.orekit.utils.AbsolutePVCoordinatesHermiteInterpolator
Get the filter for derivatives from the sample to use in interpolation.
getFilter() - Method in class org.orekit.utils.FieldAbsolutePVCoordinatesHermiteInterpolator
Get filter for derivatives from the sample to use in interpolation.
getFilter() - Method in class org.orekit.utils.TimeStampedAngularCoordinatesHermiteInterpolator
Get filter for derivatives from the sample to use in interpolation.
getFilter() - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinatesHermiteInterpolator
Get filter for derivatives from the sample to use in interpolation.
getFilter() - Method in class org.orekit.utils.TimeStampedFieldPVCoordinatesHermiteInterpolator
filter for derivatives from the sample to use in interpolation.
getFilter() - Method in class org.orekit.utils.TimeStampedPVCoordinatesHermiteInterpolator
Get filter for derivatives from the sample to use in interpolation.
getFilter(int) - Static method in enum org.orekit.utils.AngularDerivativesFilter
Get the filter corresponding to a maximum derivation order.
getFilter(int) - Static method in enum org.orekit.utils.CartesianDerivativesFilter
Get the filter corresponding to a maximum derivation order.
getFilteredDataMap() - Method in class org.orekit.estimation.measurements.filtering.DualFrequencySmoother
Get the map of the filtered data.
getFilteredDataMap() - Method in class org.orekit.estimation.measurements.filtering.SingleFrequencySmoother
Get the map of the filtered data.
getFilterFlag() - Method in class org.orekit.files.ilrs.CRD.FrRangeMeasurement
Get the filter flag.
getFilters() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Get the filters to apply to parse tokens.
getFiltersManager() - Method in class org.orekit.data.DataProvidersManager
Get the manager for filters.
getFinalPoint() - Method in class org.orekit.bodies.LoxodromeArc
Get the final point of the arc.
getFiringIntervalDetector() - Method in class org.orekit.forces.maneuvers.trigger.IntervalEventTrigger
Getter for the firing interval detector.
getFirings() - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers
Get the firings detected during last propagation.
getFirst() - Method in class org.orekit.time.FieldTimeStampedPair
Get first time stamped value.
getFirst() - Method in class org.orekit.time.TimeStampedPair
Get first time stamped value.
getFirstFrequencyPhaseHistory() - Method in class org.orekit.estimation.measurements.filtering.DualFrequencyHatchFilter
Get the history of phase values of the first frequency.
getFirstKnownLeapSecond() - Method in class org.orekit.time.UTCScale
Get the date of the first known leap second.
getFirstNonNullSpan() - Method in class org.orekit.utils.TimeSpanMap
Get the first (earliest) span with non-null data.
getFirstSpan() - Method in class org.orekit.forces.drag.TimeSpanDragForce
Deprecated.
Get the first time span of the drag sensitive time span map.
getFirstSpan() - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
Get the first time span of the acceleration model time span map.
getFirstSpan() - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedModel
Get the first time span of the tropospheric model time span map.
getFirstSpan() - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
Deprecated.
Get the first time span of the tropospheric model time span map.
getFirstSpan() - Method in class org.orekit.utils.TimeSpanMap
Get the first (earliest) span.
getFirstTransition() - Method in class org.orekit.utils.TimeSpanMap
Get the first (earliest) transition.
getFitInterval() - Method in class org.orekit.gnss.rflink.gps.SubFrame2
Get fit interval.
getFitInterval() - Method in class org.orekit.propagation.analytical.gnss.data.LegacyNavigationMessage
Getter for the fit interval.
getFittedParameters() - Method in class org.orekit.utils.SecularAndHarmonic
Get a copy of the last fitted parameters.
getFixedF10P7() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get fixed (time invariant) value of the Solar Flux Unit daily proxy F10.7.
getFixedF10P7Mean() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get fixed (time invariant) value of the Solar Flux Unit 81-day running center-average proxy F10.7.
getFixedGeomagneticAp() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get fixed (time invariant) value of the planetary 3-hour-range geomagnetic index aₚ.
getFixedGeomagneticDst() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get fixed (time invariant) value of the planetary 1-hour-range geomagnetic index Dst.
getFixedGeomagneticKp() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get fixed (time invariant) value of the planetary 3-hour-range geomagnetic index Kₚ.
getFixedM10P7() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get fixed (time invariant) value of the Solar Flux daily proxy M10.7.
getFixedM10P7Mean() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get fixed (time invariant) value of the Solar Flux 81-day running center-average proxy M10.7.
getFixedS10P7() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get fixed (time invariant) value of the Solar Flux daily proxy S10.7.
getFixedS10P7Mean() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get fixed (time invariant) value of the Solar Flux 81-day running center-average proxy S10.7.
getFixedStepHandler() - Method in class org.orekit.propagation.sampling.FieldOrekitStepNormalizer
Get the underlying fixed step handler.
getFixedStepHandler() - Method in class org.orekit.propagation.sampling.MultisatStepNormalizer
Get the underlying fixed step handler.
getFixedStepHandler() - Method in class org.orekit.propagation.sampling.OrekitStepNormalizer
Get the underlying fixed step handler.
getFixedTimeStep() - Method in class org.orekit.propagation.sampling.FieldOrekitStepNormalizer
Get the fixed time step.
getFixedTimeStep() - Method in class org.orekit.propagation.sampling.MultisatStepNormalizer
Get the fixed time step.
getFixedTimeStep() - Method in class org.orekit.propagation.sampling.OrekitStepNormalizer
Get the fixed time step.
getFixedY10P7() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get fixed (time invariant) value of the Solar Flux daily proxy Y10.7.
getFixedY10P7Mean() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get fixed (time invariant) value of the Solar Flux 81-day running center-average proxy Y10.7.
getFlags() - Method in class org.orekit.files.rinex.navigation.IonosphereNequickGMessage
Get the disturbance flags.
getFlattening() - Method in class org.orekit.bodies.OneAxisEllipsoid
Get the flattening of the body: f = (a-b)/a.
getFlattening() - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder
Get the central body flattening.
getFlattening() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmWriter
Get the central body flattening.
getFlowRate() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Get the flow rate.
getFlowRate() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate() - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate() - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate(double[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate(double[]) - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate(double[]) - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.maneuvers.propulsion.ProfileThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate(SpacecraftState) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate(SpacecraftState) - Method in class org.orekit.forces.maneuvers.propulsion.ProfileThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate(SpacecraftState) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate(SpacecraftState, double[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate(SpacecraftState, double[]) - Method in class org.orekit.forces.maneuvers.propulsion.ProfileThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate(SpacecraftState, double[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Get the flow rate at given date.
getFlowRate(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate(T[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate(T[]) - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate(T[]) - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel
Get the flow rate (kg/s).
getFluxQualifier() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
Gets the Flux Qualifier.
getFocus1() - Method in class org.orekit.geometry.fov.EllipticalFieldOfView
Get first focus in spacecraft frame.
getFocus2() - Method in class org.orekit.geometry.fov.EllipticalFieldOfView
Get second focus in spacecraft frame.
getFootprint(Transform, OneAxisEllipsoid, double) - Method in interface org.orekit.geometry.fov.FieldOfView
Get the footprint of the Field Of View on ground.
getFootprint(Transform, OneAxisEllipsoid, double) - Method in class org.orekit.geometry.fov.PolygonalFieldOfView
Get the footprint of the Field Of View on ground.
getFootprint(Transform, OneAxisEllipsoid, double) - Method in class org.orekit.geometry.fov.SmoothFieldOfView
Get the footprint of the Field Of View on ground.
getForceModels() - Method in class org.orekit.control.indirect.shooting.propagation.ShootingPropagationSettings
Getter for the force models.
getFormat() - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Get the generated file format.
getFormat() - Method in class org.orekit.files.ccsds.utils.generation.KvnGenerator
Get the generated file format.
getFormat() - Method in class org.orekit.files.ccsds.utils.generation.XmlGenerator
Get the generated file format.
getFormat() - Method in class org.orekit.files.ilrs.ILRSHeader
Get the file format.
getFormat() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
Get the data format.
getFormatDetails() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
Get the format details.
getFormatVersion() - Method in class org.orekit.files.ccsds.section.Header
Get the CCSDS NDM (ADM, ODM or TDM) format version.
getFormatVersion() - Method in class org.orekit.files.rinex.clock.RinexClock
Getter for the format version.
getFormatVersion() - Method in class org.orekit.files.rinex.section.RinexBaseHeader
Getter for the format version.
getFormatVersionKey() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter
Get key for format version.
getFormatVersionKey() - Method in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter
Get key for format version.
getFormatVersionKey() - Method in interface org.orekit.files.ccsds.utils.generation.MessageWriter
Get key for format version.
getFormatVersionKey() - Method in interface org.orekit.files.ccsds.utils.lexical.MessageParser
Get the key for format version.
getFormatVersionKey() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser
Get the key for format version.
getForwardApoapsisDetectionAdaptableInterval() - Static method in class org.orekit.propagation.events.intervals.ApsideDetectionAdaptableIntervalFactory
Method providing a candidate AdaptableInterval for apoapsis detection with forward propagation.
getForwardApsideDetectionAdaptableInterval() - Static method in class org.orekit.propagation.events.intervals.ApsideDetectionAdaptableIntervalFactory
Method providing a candidate AdaptableInterval for arbitrary apside detection with forward propagation.
getForwardPeriapsisDetectionAdaptableInterval() - Static method in class org.orekit.propagation.events.intervals.ApsideDetectionAdaptableIntervalFactory
Method providing a candidate AdaptableInterval for periapsis detection with forward propagation.
getFOV() - Method in class org.orekit.propagation.events.FieldOfViewDetector
Get the Field Of View.
getFOV() - Method in class org.orekit.propagation.events.FootprintOverlapDetector
Get the Field Of View.
getFOV() - Method in class org.orekit.propagation.events.GroundFieldOfViewDetector
Get the Field Of View.
getFrame() - Method in class org.orekit.bodies.Ellipse
Get the defining frame.
getFrame() - Method in class org.orekit.bodies.Ellipsoid
Get the ellipsoid central frame.
getFrame() - Method in class org.orekit.bodies.FieldEllipse
Get the defining frame.
getFrame() - Method in class org.orekit.files.ccsds.ndm.adm.apm.AngularVelocity
Get frame in which angular velocities are specified.
getFrame() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Inertia
Get frame in which inertia is specified.
getFrame() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver
Get Coordinate system for the torque vector.
getFrame() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get the reference frame in which data are given: used for state vector and Keplerian elements data (and for the covariance reference frame if none is given).
getFrame() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory
Get the reference frame for this ephemeris segment.
getFrame() - Method in class org.orekit.files.ccsds.ndm.odm.OdmCommonMetadata
Get the reference frame in which data are given: used for state vector and Keplerian elements data (and for the covariance reference frame if none is given).
getFrame() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSegment
Get the reference frame for this ephemeris segment.
getFrame() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
Get the reference frame for this ephemeris segment.
getFrame() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
Get the reference frame for this ephemeris segment.
getFrame() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris
Get the reference frame for this ephemeris segment.
getFrame() - Method in class org.orekit.files.rinex.clock.RinexClock
Get the reference frame for the station positions.
getFrame() - Method in class org.orekit.files.sp3.SP3Ephemeris
Get the reference frame.
getFrame() - Method in class org.orekit.files.sp3.SP3Segment
Get the reference frame for this ephemeris segment.
getFrame() - Method in class org.orekit.files.stk.STKEphemerisFile.STKEphemerisSegment
 
getFrame() - Method in class org.orekit.forces.gravity.J2OnlyPerturbation
Getter for frame.
getFrame() - Method in class org.orekit.frames.OrphanFrame
Get the associated frame.
getFrame() - Method in interface org.orekit.models.earth.atmosphere.Atmosphere
Get the frame of the central body.
getFrame() - Method in class org.orekit.models.earth.atmosphere.DTM2000
Get the frame of the central body.
getFrame() - Method in class org.orekit.models.earth.atmosphere.HarrisPriester
Get the frame of the central body.
getFrame() - Method in class org.orekit.models.earth.atmosphere.JB2008
Get the frame of the central body.
getFrame() - Method in class org.orekit.models.earth.atmosphere.NRLMSISE00
Get the frame of the central body.
getFrame() - Method in class org.orekit.models.earth.atmosphere.SimpleExponentialAtmosphere
Get the frame of the central body.
getFrame() - Method in class org.orekit.orbits.FieldOrbit
Get the frame in which the orbital parameters are defined.
getFrame() - Method in class org.orekit.orbits.Orbit
Get the frame in which the orbital parameters are defined.
getFrame() - Method in class org.orekit.propagation.AbstractPropagator
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.analytical.Ephemeris
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElementsPropagator
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.analytical.intelsat.IntelsatElevenElementsPropagator
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Get the frame of the initial state.
getFrame() - Method in class org.orekit.propagation.conversion.averaging.AbstractAveragedOrbitalState
Getter for the reference frame.
getFrame() - Method in interface org.orekit.propagation.conversion.averaging.AveragedOrbitalState
Getter for the reference frame.
getFrame() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.events.FieldNodeDetector
Get the frame in which the equator is defined.
getFrame() - Method in class org.orekit.propagation.events.GroundFieldOfViewDetector
Get the sensor reference frame.
getFrame() - Method in class org.orekit.propagation.events.NodeDetector
Get the frame in which the equator is defined.
getFrame() - Method in class org.orekit.propagation.FieldAbstractPropagator
Get the frame in which the orbit is propagated.
getFrame() - Method in interface org.orekit.propagation.FieldPropagator
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the defining frame.
getFrame() - Method in class org.orekit.propagation.FieldStateCovariance
Get the covariance frame.
getFrame() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
 
getFrame() - Method in class org.orekit.propagation.integration.FieldStateMapper
Get the inertial frame.
getFrame() - Method in class org.orekit.propagation.integration.IntegratedEphemeris
 
getFrame() - Method in class org.orekit.propagation.integration.StateMapper
Get the inertial frame.
getFrame() - Method in interface org.orekit.propagation.Propagator
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the definition frame of the orbit.
getFrame() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get the definition frame of the orbit.
getFrame() - Method in class org.orekit.propagation.SpacecraftState
Get the defining frame.
getFrame() - Method in class org.orekit.propagation.StateCovariance
Get the covariance frame.
getFrame() - Method in class org.orekit.utils.AbsolutePVCoordinates
Get the frame in which the coordinates are defined.
getFrame() - Method in class org.orekit.utils.FieldAbsolutePVCoordinates
Get the frame in which the coordinates are defined.
getFrame(Predefined) - Method in class org.orekit.frames.AbstractFrames
 
getFrame(Predefined) - Method in interface org.orekit.frames.Frames
Get one of the predefined frames.
getFrame(Predefined) - Static method in class org.orekit.frames.FramesFactory
Get one of the predefined frames.
getFrame(FieldPVCoordinates<T>) - Method in enum org.orekit.frames.encounter.EncounterLOFType
Get encounter local orbital frame associated to this enum.
getFrame(IERSConventions, boolean, DataContext) - Method in enum org.orekit.files.ccsds.definitions.CelestialBodyFrame
Get the frame corresponding to the CCSDS constant.
getFrame(PVCoordinates) - Method in enum org.orekit.frames.encounter.EncounterLOFType
Get encounter local orbital frame associated to this enum.
getFrameA() - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints
Get frame A.
getFrameAngvelFrame() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Get frame in which angular velocities are specified.
getFrameB() - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints
Get frame B.
getFrameEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.OdmCommonMetadata
Get epoch of reference frame, if not intrinsic to the definition of the reference frame.
getFrameName() - Method in class org.orekit.files.rinex.clock.RinexClock
Getter for the frame name.
getFrames() - Method in class org.orekit.data.CompositeDataContext
 
getFrames() - Method in interface org.orekit.data.DataContext
Get a factory constructing Frames based on the auxiliary data in this context.
getFrames() - Method in class org.orekit.data.ExceptionalDataContext
 
getFrames() - Method in class org.orekit.data.LazyLoadedDataContext
 
getFrames() - Static method in class org.orekit.frames.FramesFactory
Get the instance of Frames that is called by the static methods in this class.
getFreeAmbiguityDrivers() - Method in class org.orekit.estimation.measurements.gnss.AmbiguitySolver
Get the ambiguity parameters drivers that have not been fixed yet.
getFreeAmbiguityIndirection(int, List<ParameterDriver>) - Method in class org.orekit.estimation.measurements.gnss.AmbiguitySolver
Get ambiguity indirection array for ambiguity parameters drivers that have not been fixed yet.
getFreeCompsMap() - Method in class org.orekit.utils.AbstractMultipleShooting
Get the map of free state components.
getFreeStateParameters() - Method in class org.orekit.propagation.integration.AbstractGradientConverter
Get the number of free state parameters.
getFreqOffset() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the freqOffset.
getFrequencies() - Method in class org.orekit.gnss.antenna.Antenna
Get supported frequencies.
getFrequency() - Method in enum org.orekit.gnss.Frequency
Get the value of the frequency in Hz.
getFrequency() - Method in interface org.orekit.gnss.RadioWave
Get the value of the frequency in Hz.
getFrequency(SatelliteSystem) - Method in enum org.orekit.gnss.ObservationType
Get the frequency for a specified satellite system.
getFrequencyChannel() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
Get the frequency channel.
getFrequencyNumber() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage
Getter for the frequency number.
getFrequencySource() - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration
Get the frequency source.
getFrom() - Method in class org.orekit.utils.units.UnitsConverter
Get the source unit.
getFromLatitude() - Method in class org.orekit.propagation.events.FieldLatitudeRangeCrossingDetector
Get the fixed latitude range to be crossed (radians), lower boundary.
getFromLatitude() - Method in class org.orekit.propagation.events.LatitudeRangeCrossingDetector
Get the fixed latitude range to be crossed (radians), lower boundary.
getFromLongitude() - Method in class org.orekit.propagation.events.FieldLongitudeRangeCrossingDetector
Get the fixed longitude range to be crossed (radians), lower boundary.
getFromLongitude() - Method in class org.orekit.propagation.events.LongitudeRangeCrossingDetector
Get the fixed longitude range to be crossed (radians), lower boundary.
getFrozenAttitudeProvider(AttitudeProvider) - Static method in interface org.orekit.attitudes.AttitudeProviderModifier
Wrap the input provider with a new one always returning attitudes with zero rotation rate and acceleration.
getFrozenFrame(Frame, AbsoluteDate, String) - Method in class org.orekit.frames.Frame
Get a new version of the instance, frozen with respect to a reference frame.
getFT() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the GLONASS FT Word.
getFunction() - Method in class org.orekit.propagation.events.FieldFunctionalDetector
Get the switching function.
getFunction() - Method in class org.orekit.propagation.events.FunctionalDetector
Get the switching function.
getFutureInfinity() - Method in class org.orekit.time.AbstractTimeScales
 
getFutureInfinity() - Method in interface org.orekit.time.TimeScales
Dummy date at infinity in the future direction.
getFutureInfinity(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Dummy date at infinity in the future direction.
getGalileoDataValidityStatus() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1045Data
Get the Galileo data validity status.
getGalileoEpoch() - Method in class org.orekit.time.AbstractTimeScales
 
getGalileoEpoch() - Method in interface org.orekit.time.TimeScales
Reference epoch for Galileo System Time: 1999-08-22T00:00:00 GST.
getGalileoEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Reference epoch for Galileo System Time: 1999-08-22T00:00:00 UTC.
getGalileoNavigationMessage() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1045Data
Get the Galileo navigation message corresponding to the current RTCM data.
getGalileoNavigationMessage(TimeScales) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1045Data
Get the Galileo navigation message corresponding to the current RTCM data.
getGalileoNavigationMessages() - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Get all the Galileo navigation messages contained in the file.
getGalileoNavigationMessages(String) - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Get the Galileo navigation messages for the given satellite Id.
getGalileoToc() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1045Data
Get the Galileo time of clock.
getGamma() - Method in class org.orekit.data.DelaunayArguments
Get the tide parameter γ = GMST + π.
getGamma() - Method in class org.orekit.data.FieldDelaunayArguments
Get the tide parameter γ = GMST + π.
getGamma() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTGravityContext
Get direction cosine γ for central body.
getGamma() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext
Get direction cosine γ for central body.
getGamma() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTGravityContext
Get direction cosine γ for central body.
getGamma() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext
Get direction cosine γ for central body.
getGamma() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Deprecated.
since 12.2, use DSSTGravityContext.getGamma() instead
getGamma() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Deprecated.
since 12.2, use FieldDSSTGravityContext.getGamma() instead
getGamma(LagrangianPoints) - Method in class org.orekit.bodies.CR3BPSystem
Get the position of the Lagrangian point in the CR3BP Rotating frame.
getGammaDot() - Method in class org.orekit.data.DelaunayArguments
Get the tide parameter γ = GMST + π time derivative.
getGammaDot() - Method in class org.orekit.data.FieldDelaunayArguments
Get the tide parameter γ = GMST + π time derivative.
getGammaN() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage
Get the relative deviation of predicted satellite carrier frequency from nominal value.
getGammaN() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
Get the relative deviation of predicted satellite carrier frequency from nominal value.
getGASTFunction(TimeScale, EOPHistory) - Method in enum org.orekit.utils.IERSConventions
Get the function computing Greenwich apparent sidereal time, in radians.
getGASTFunction(TimeScale, EOPHistory, TimeScales) - Method in enum org.orekit.utils.IERSConventions
Get the function computing Greenwich apparent sidereal time, in radians.
getGCRF() - Method in class org.orekit.frames.AbstractFrames
 
getGCRF() - Method in interface org.orekit.frames.Frames
Get the unique GCRF frame.
getGCRF() - Static method in class org.orekit.frames.FramesFactory
Get the unique GCRF frame.
getGdop() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get generalize Dilution Of Precision.
getGdop() - Method in class org.orekit.gnss.DOP
Gets the geometric dilution of precision.
getGeh() - Method in class org.orekit.models.earth.troposphere.AzimuthalGradientCoefficients
Get East hydrostatic coefficient.
getGeh() - Method in class org.orekit.models.earth.troposphere.FieldAzimuthalGradientCoefficients
Get East hydrostatic coefficient.
getGeneralEclipseAngles(FieldVector3D<T>, FieldVector3D<T>, T, FieldVector3D<T>, T) - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel
Get the useful angles for eclipse computation.
getGeneralEclipseAngles(Vector3D, Vector3D, double, Vector3D, double) - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel
Get the useful angles for eclipse computation.
getGenerateCalls() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the number of calls to the generate method.
getGeneratedEphemeris() - Method in interface org.orekit.propagation.EphemerisGenerator
Get the ephemeris generated during the propagation.
getGeneratedEphemeris() - Method in interface org.orekit.propagation.FieldEphemerisGenerator
Get the ephemeris generated during the propagation.
getGeneratedMeasurements() - Method in class org.orekit.estimation.measurements.generation.GatheringSubscriber
Get generated measurements.
getGenerator() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
Get the hardware or software generator.
getGenerator() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the generator.
getGeocentricLatitudeDegrees() - Method in class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElementsPropagator
Get the computed satellite's geocentric latitude.
getGeocentricLatitudeDegrees() - Method in class org.orekit.propagation.analytical.intelsat.IntelsatElevenElementsPropagator
Get the computed satellite's geocentric latitude.
getGeoMagneticFields() - Method in class org.orekit.data.CompositeDataContext
 
getGeoMagneticFields() - Method in interface org.orekit.data.DataContext
Get a factory constructing GeoMagneticFields based on the auxiliary data in this context.
getGeoMagneticFields() - Method in class org.orekit.data.ExceptionalDataContext
 
getGeoMagneticFields() - Method in class org.orekit.data.LazyLoadedDataContext
 
getGeoMagneticFields() - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory
Get the instance of GeoMagneticFields that is called by methods in this class.
getGeometryFreeCombination(SatelliteSystem) - Static method in class org.orekit.estimation.measurements.gnss.MeasurementCombinationFactory
Get the Geometry-Free combination of measurements.
getGetNeighborsCalls() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the number of calls to the TimeStampedCache.getNeighbors(AbsoluteDate) method.
getGew() - Method in class org.orekit.models.earth.troposphere.AzimuthalGradientCoefficients
Get East wet coefficient.
getGew() - Method in class org.orekit.models.earth.troposphere.FieldAzimuthalGradientCoefficients
Get East wet coefficient.
getGjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the Gjs coefficient.
getGjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the Gjs coefficient.
getGlo2UTC() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
Get the correction from GLONASS to UTC.
getGLONASS() - Method in class org.orekit.time.LazyLoadedTimeScales
 
getGLONASS() - Method in interface org.orekit.time.TimeScales
Get the GLObal NAvigation Satellite System time scale.
getGLONASS() - Static method in class org.orekit.time.TimeScalesFactory
Get the GLObal NAvigation Satellite System time scale.
getGlonassChannels() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Get the list of GLONASS satellite/channel associations.
getGlonassEpoch() - Method in class org.orekit.time.AbstractTimeScales
 
getGlonassEpoch() - Method in interface org.orekit.time.TimeScales
Reference epoch for GLONASS four-year interval number: 1996-01-01T00:00:00 GLONASS time.
getGlonassNavigationMessage() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the Glonass navigation message corresponding to the current RTCM data.
getGlonassNavigationMessage(TimeScales) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the Glonass navigation message corresponding to the current RTCM data.
getGlonassNavigationMessages() - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Get all the Glonass navigation messages contained in the file.
getGlonassNavigationMessages(String) - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Get the Glonass navigation messages for the given satellite Id.
getGLONASSOrbitalElements() - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator
Gets the underlying GLONASS orbital elements.
getGLONASSOrbitalElements() - Method in class org.orekit.propagation.numerical.GLONASSNumericalPropagator
Gets the underlying GLONASS orbital elements.
getGloOffset() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
Get the correction of time relative to GLONASS system time.
getGm() - Method in class org.orekit.estimation.measurements.modifiers.AbstractRelativisticClockOnBoardRangeRateModifier
Get gravitational constant for main body in signal path vicinity.
getGm() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get gravitational coefficient of attracting body.
getGM() - Method in interface org.orekit.bodies.CelestialBody
Get the attraction coefficient of the body.
getGM() - Method in class org.orekit.models.earth.ReferenceEllipsoid
Gets the gravitational parameter that is part of the definition of the reference ellipsoid.
getGM() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttractionContext
Get standard gravitational parameter μ for the body in m³/s².
getGM() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTNewtonianAttractionContext
Get standard gravitational parameter μ for the body in m³/s².
getGmsj(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials
Get the Gmsj coefficient.
getGmsj(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the Gmsj coefficient.
getGMST() - Method in class org.orekit.time.GLONASSDate
Get the Greenwich Mean Sidereal Time.
getGMST(IERSConventions, boolean) - Method in class org.orekit.time.AbstractTimeScales
 
getGMST(IERSConventions, boolean) - Method in class org.orekit.time.LazyLoadedTimeScales
 
getGMST(IERSConventions, boolean) - Method in interface org.orekit.time.TimeScales
Get the Greenwich Mean Sidereal Time scale.
getGMST(IERSConventions, boolean) - Static method in class org.orekit.time.TimeScalesFactory
Get the Greenwich Mean Sidereal Time scale.
getGMSTFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions
Get the function computing Greenwich mean sidereal time, in radians.
getGMSTFunction(TimeScale, TimeScales) - Method in enum org.orekit.utils.IERSConventions
Get the function computing Greenwich mean sidereal time, in radians.
getGMSTRateFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions
Get the function computing Greenwich mean sidereal time rate, in radians per second.
getGMSTRateFunction(TimeScale, TimeScales) - Method in enum org.orekit.utils.IERSConventions
Get the function computing Greenwich mean sidereal time rate, in radians per second.
getGnh() - Method in class org.orekit.models.earth.troposphere.AzimuthalGradientCoefficients
Get North hydrostatic coefficient.
getGnh() - Method in class org.orekit.models.earth.troposphere.FieldAzimuthalGradientCoefficients
Get North hydrostatic coefficient.
getGnssIod() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCombinedCorrectionData
Get the GNSS IOD.
getGnssIod() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmOrbitCorrectionData
Get the GNSS IOD.
getGnssIod() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01Data
Get the GNSS IOD.
getGnssIod() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Data
Get the GNSS IOD.
getGnssNb() - Method in class org.orekit.gnss.DOP
Gets the number of GNSS satellites taken into account for DOP computation.
getGnw() - Method in class org.orekit.models.earth.troposphere.AzimuthalGradientCoefficients
Get North wet coefficient.
getGnw() - Method in class org.orekit.models.earth.troposphere.FieldAzimuthalGradientCoefficients
Get North wet coefficient.
getGPS() - Method in class org.orekit.time.LazyLoadedTimeScales
 
getGPS() - Method in interface org.orekit.time.TimeScales
Get the Global Positioning System scale.
getGPS() - Static method in class org.orekit.time.TimeScalesFactory
Get the Global Positioning System scale.
getGPS2Glo() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
Get the correction to GPS time relative GLONASS.
getGPSCivilianNavigationMessages() - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Get all the GPS civilian navigation messages contained in the file.
getGPSCivilianNavigationMessages(String) - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Get the GPS civilian navigation messages for the given satellite Id.
getGpsCodeOnL2() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data
Get the GPS code on L2.
getGpsEpoch() - Method in class org.orekit.time.AbstractTimeScales
 
getGpsEpoch() - Method in interface org.orekit.time.TimeScales
Reference epoch for GPS weeks: 1980-01-06T00:00:00 GPS time.
getGPSEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Reference epoch for GPS weeks: 1980-01-06T00:00:00 GPS time.
getGpsFitInterval() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data
Get the GPS fit interval.
getGpsL2PDataFlag() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data
Get the GPS L2 P-Code data flag.
getGPSLegacyNavigationMessages() - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Get all the GPS legacy navigation messages contained in the file.
getGPSLegacyNavigationMessages(String) - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Get the GPS legacy navigation messages for the given satellite Id.
getGpsNavigationMessage() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data
Get the GPS navigation message corresponding to the current RTCM data.
getGpsNavigationMessage(TimeScales) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data
Get the GPS navigation message corresponding to the current RTCM data.
getGpsToc() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data
Get the GPS time of clock.
getGpsWeek() - Method in class org.orekit.files.sp3.SP3Header
Returns the GPS week as contained in the SP3 file.
getGradientCoefficients(FieldGeodeticPoint<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.models.earth.troposphere.AzimuthalGradientProvider
Get azimuthal asymmetry gradients.
getGradientCoefficients(FieldGeodeticPoint<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.ConstantAzimuthalGradientProvider
Get azimuthal asymmetry gradients.
getGradientCoefficients(FieldGeodeticPoint<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.weather.AbstractGlobalPressureTemperature
Get azimuthal asymmetry gradients.
getGradientCoefficients(GeodeticPoint, AbsoluteDate) - Method in interface org.orekit.models.earth.troposphere.AzimuthalGradientProvider
Get azimuthal asymmetry gradients.
getGradientCoefficients(GeodeticPoint, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.ConstantAzimuthalGradientProvider
Get azimuthal asymmetry gradients.
getGradientCoefficients(GeodeticPoint, AbsoluteDate) - Method in class org.orekit.models.earth.weather.AbstractGlobalPressureTemperature
Get azimuthal asymmetry gradients.
getGradientConverter() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester
Get the gradient converter related to the analytical orbit propagator.
getGradientDensityWrtState(AbsoluteDate, Frame, FieldVector3D<Gradient>) - Method in class org.orekit.forces.drag.AbstractDragForceModel
Compute density and its derivatives.
getGradientDensityWrtStateUsingFiniteDifferences(AbsoluteDate, Frame, FieldVector3D<Gradient>) - Method in class org.orekit.forces.drag.AbstractDragForceModel
Compute density and its derivatives.
getGRAPHICCombination(SatelliteSystem) - Static method in class org.orekit.estimation.measurements.gnss.MeasurementCombinationFactory
Get the GRAPHIC combination of measurements.
getGravitationalAssist() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Get the origin of gravitational assist.
getGravityDegree() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get degree of the gravity model.
getGravityDegree() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get degree of the gravity model.
getGravityFields() - Method in class org.orekit.data.CompositeDataContext
 
getGravityFields() - Method in interface org.orekit.data.DataContext
Get a factory constructing gravity fields based on the auxiliary data in this context.
getGravityFields() - Method in class org.orekit.data.ExceptionalDataContext
 
getGravityFields() - Method in class org.orekit.data.LazyLoadedDataContext
 
getGravityFields() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Get the instance of GravityFields that is called by the static methods of this class.
getGravityModel() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get gravity model name.
getGravityModel() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get gravity model name.
getGravityOrder() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get order of the gravity model.
getGravityOrder() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get order of the gravity model.
getGridPoints() - Method in class org.orekit.frames.InterpolatingTransformProvider
Get the number of interpolation grid points.
getGridPoints() - Method in class org.orekit.frames.ShiftingTransformProvider
Get the number of interpolation grid points.
getGridPoints(double, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FixedNumberInterpolationGrid
Get grid points that are within the current step.
getGridPoints(double, double) - Method in interface org.orekit.propagation.semianalytical.dsst.utilities.InterpolationGrid
Get grid points that are within the current step.
getGridPoints(double, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.MaxGapInterpolationGrid
Get grid points that are within the current step.
getGridPoints(T, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldFixedNumberInterpolationGrid
Get grid points that are within the current step.
getGridPoints(T, T) - Method in interface org.orekit.propagation.semianalytical.dsst.utilities.FieldInterpolationGrid
Get grid points that are within the current step.
getGridPoints(T, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldMaxGapInterpolationGrid
Get grid points that are within the current step.
getGroundStationCoordinates(Frame) - Method in class org.orekit.estimation.measurements.GroundReceiverMeasurement
Get the station coordinates for a given frame.
getGroundStationPosition(Frame) - Method in class org.orekit.estimation.measurements.GroundReceiverMeasurement
Get the station position for a given frame.
getGroupDelayDifference() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage
Get group delay difference.
getGrs80(Frame) - Static method in class org.orekit.models.earth.ReferenceEllipsoid
Get the GRS80 ellipsoid, attached to the given body frame.
getGST() - Method in class org.orekit.time.LazyLoadedTimeScales
 
getGST() - Method in interface org.orekit.time.TimeScales
Get the Galileo System Time scale.
getGST() - Static method in class org.orekit.time.TimeScalesFactory
Get the Galileo System Time scale.
getGTOD(boolean) - Method in class org.orekit.frames.AbstractFrames
 
getGTOD(boolean) - Method in interface org.orekit.frames.Frames
Get the GTOD reference frame.
getGTOD(boolean) - Static method in class org.orekit.frames.FramesFactory
Get the GTOD reference frame.
getGTOD(IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames
 
getGTOD(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames
Get the GTOD reference frame.
getGTOD(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
Get the GTOD reference frame.
getH() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the y component of eccentricity vector.
getH() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get the y component of eccentricity vector.
getH1CrdString() - Method in class org.orekit.files.ilrs.CRDHeader
Get a string representation of the H1 in the CRD format.
getH2CrdString() - Method in class org.orekit.files.ilrs.CRDHeader
Get a string representation of the H2 in the CRD format.
getH3CrdString() - Method in class org.orekit.files.ilrs.CRDHeader
Get a string representation of the H3 in the CRD format.
getH4CrdString() - Method in class org.orekit.files.ilrs.CRDHeader
Get a string representation of the H4 in the CRD format.
getH5CrdString() - Method in class org.orekit.files.ilrs.CRDHeader
Get a string representation of the H5 in the CRD format.
getHalfAperture() - Method in class org.orekit.geometry.fov.CircularFieldOfView
get the FOV half aperture angle.
getHalfApertureAlongX() - Method in class org.orekit.geometry.fov.EllipticalFieldOfView
get the FOV half aperture angle for spreading along Xell (i.e.
getHalfApertureAlongY() - Method in class org.orekit.geometry.fov.EllipticalFieldOfView
get the FOV half aperture angle for spreading along Yell (i.e.
getHaloOrbitalPeriod(double) - Method in class org.orekit.orbits.RichardsonExpansion
Return the orbital period of the Halo Orbit.
getHamiltonianContribution(double[], double) - Method in interface org.orekit.control.indirect.adjoint.cost.CartesianCost
Computes the Hamiltonian contribution of the cost function.
getHamiltonianContribution(double[], double) - Method in class org.orekit.control.indirect.adjoint.cost.UnboundedCartesianEnergyNeglectingMass
Computes the Hamiltonian contribution of the cost function.
getHamiltonianContribution(AbsoluteDate, double[], double[], Frame) - Method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointEquationTerm
Computes the contribution to the Hamiltonian.
getHamiltonianContribution(AbsoluteDate, double[], double[], Frame) - Method in interface org.orekit.control.indirect.adjoint.CartesianAdjointEquationTerm
Computes the contribution to the Hamiltonian.
getHandler() - Method in class org.orekit.attitudes.AttitudesSequence.Switch
Get the handler.
getHandler() - Method in class org.orekit.propagation.events.AbstractDetector
Get the handler.
getHandler() - Method in class org.orekit.propagation.events.AdapterDetector
Get the handler.
getHandler() - Method in interface org.orekit.propagation.events.EventDetector
Get the handler.
getHandler() - Method in class org.orekit.propagation.events.FieldAbstractDetector
Get the handler.
getHandler() - Method in class org.orekit.propagation.events.FieldAdapterDetector
Get the handler.
getHandler() - Method in interface org.orekit.propagation.events.FieldEventDetector
Get the handler.
getHandlers() - Method in class org.orekit.propagation.events.handlers.EventMultipleHandler
Retrieve managed handlers list.
getHandlers() - Method in class org.orekit.propagation.sampling.FieldStepHandlerMultiplexer
Get an unmodifiable view of all handlers.
getHandlers() - Method in class org.orekit.propagation.sampling.StepHandlerMultiplexer
Get an unmodifiable view of all handlers.
getHarmonicAmplitude() - Method in class org.orekit.utils.SecularAndHarmonic
Get an upper bound of the fitted harmonic amplitude.
getHarvester() - Method in class org.orekit.propagation.AbstractPropagator
Get the harvester.
getHarvester() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Get the harvester.
getHasCreatableBody() - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata
Get boolean testing whether the body corresponding to the centerName attribute can be created through the CelestialBodies.
getHbr() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Get the object hard body radius.
getHdop() - Method in class org.orekit.gnss.DOP
Gets the horizontal dilution of precision.
getHeader() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmParser
Get file header to fill.
getHeader() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser
Get file header to fill.
getHeader() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser
Get file header to fill.
getHeader() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmParser
Get file header to fill.
getHeader() - Method in class org.orekit.files.ccsds.ndm.NdmConstituent
Get the header.
getHeader() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser
Get file header to fill.
getHeader() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser
Get file header to fill.
getHeader() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser
Get file header to fill.
getHeader() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser
Get file header to fill.
getHeader() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser
Get file header to fill.
getHeader() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser
Get file header to fill.
getHeader() - Method in class org.orekit.files.ilrs.CPF
Get the CPF file header.
getHeader() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
Get the header of the current data block.
getHeader() - Method in class org.orekit.files.rinex.RinexFile
Get the header.
getHeader() - Method in class org.orekit.files.sp3.SP3
Get the header.
getHeader() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionMessage
Get the header.
getHeader() - Method in class org.orekit.gnss.metric.messages.ssr.SsrMessage
Get the header.
getHealth() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Getter for the health status.
getHealth() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouAlmanac
Gets the Health status.
getHealth() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage
Getter for health.
getHealth() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
Get the Health status.
getHealth() - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac
Gets the Health status.
getHealth() - Method in class org.orekit.propagation.analytical.gnss.data.QZSSAlmanac
Gets the Health status.
getHealthE1() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac
Gets the E1-B/C signal health status.
getHealthE5a() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac
Gets the E5a signal health status.
getHealthE5b() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac
Gets the E5b signal health status.
getHealthFlags() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage
Get health flags.
getHeightIonosphericLayer() - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data
Get the height of the ionospheric layer.
getHighRateClockCorrection() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm04Data
Get the high rate clock correction to be added to the polynomial clock correction.
getHjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the Hjs coefficient.
getHjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the Hjs coefficient.
getHK() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
Get h * k.
getHK() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
Get h * k.
getHmsj(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials
Get the Hmsj coefficient.
getHmsj(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the Hmsj coefficient.
getHorizontalIntensity() - Method in class org.orekit.models.earth.GeoMagneticElements
Returns the horizontal intensity of the magnetic field (= norm of the vector in the plane spanned by the x/y components of the field vector).
getHost() - Method in class org.orekit.gnss.metric.ntrip.NtripClient
Get the caster host.
getHostOrIPAddress() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord
Get the host or IP address.
getHour() - Method in class org.orekit.time.TimeComponents
Get the hour number.
getHumidity() - Method in class org.orekit.files.ilrs.CRD.MeteorologicalMeasurement
Get the relative humidity at the surface.
getHumiSensorManufacturer() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
Get the humidity sensor manufacturer.
getHumiSensorModel() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
Get the humidity sensor model.
getHumiSensorSerialNumber() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
Get the humidity sensor serial number.
getHx() - Method in class org.orekit.orbits.CartesianOrbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.CircularOrbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.FieldOrbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.KeplerianOrbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.Orbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the first component of the inclination vector (as per equinoctial parameters).
getHx() - Method in class org.orekit.propagation.SpacecraftState
Get the first component of the inclination vector (as per equinoctial parameters).
getHxDot() - Method in class org.orekit.orbits.CartesianOrbit
Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.CircularOrbit
Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.FieldOrbit
Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.Orbit
Get the first component of the inclination vector derivative.
getHXXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext
Get hXXX = h * Χ³.
getHXXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext
Get hXXX = h * Χ³.
getHy() - Method in class org.orekit.orbits.CartesianOrbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.CircularOrbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.FieldOrbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.KeplerianOrbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.Orbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the second component of the inclination vector (as per equinoctial parameters).
getHy() - Method in class org.orekit.propagation.SpacecraftState
Get the second component of the inclination vector (as per equinoctial parameters).
getHyDot() - Method in class org.orekit.orbits.CartesianOrbit
Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.CircularOrbit
Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.FieldOrbit
Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.Orbit
Get the second component of the inclination vector derivative.
getI() - Method in class org.orekit.attitudes.FieldInertiaAxis
Get the moment of inertia.
getI() - Method in class org.orekit.attitudes.InertiaAxis
Get the moment of inertia.
getI() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Get the orbit inclination.
getI() - Method in class org.orekit.orbits.CartesianOrbit
Get the inclination.
getI() - Method in class org.orekit.orbits.CircularOrbit
Get the inclination.
getI() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the inclination.
getI() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the inclination.
getI() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the inclination.
getI() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the inclination.
getI() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the inclination.
getI() - Method in class org.orekit.orbits.FieldOrbit
Get the inclination.
getI() - Method in class org.orekit.orbits.KeplerianOrbit
Get the inclination.
getI() - Method in class org.orekit.orbits.Orbit
Get the inclination.
getI() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get the inclination.
getI() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the inclination.
getI() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the inclination.
getI() - Method in class org.orekit.propagation.SpacecraftState
Get the inclination.
getI0() - Method in class org.orekit.gnss.rflink.gps.SubFrame3
Get i₀.
getI0() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Getter for the inclination angle at reference time.
getI0() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
Gets the Inclination Angle at Reference Time.
getICRF() - Method in class org.orekit.frames.AbstractFrames
 
getICRF() - Method in interface org.orekit.frames.Frames
Get the unique ICRF frame.
getICRF() - Static method in class org.orekit.frames.FramesFactory
Get the unique ICRF frame.
getId() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmSatelliteEphemeris
Get the satellite ID.
getId() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination
Get identification number.
getId() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSatelliteEphemeris
Get the satellite ID.
getId() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmSatelliteEphemeris
Get the satellite ID.
getId() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get identification number.
getId() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSatelliteEphemeris
Get the satellite ID.
getId() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.SatelliteAttitudeEphemeris
Get the satellite ID.
getId() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris
Get the satellite ID.
getId() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitSatelliteAttitudeEphemeris
Get the satellite ID.
getId() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
Get the satellite ID.
getId() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris
Get the satellite ID.
getId() - Method in class org.orekit.files.sp3.SP3Ephemeris
Get the satellite ID.
getId() - Method in class org.orekit.files.stk.STKEphemerisFile.STKEphemeris
 
getId() - Method in class org.orekit.gnss.metric.ntrip.StreamedMessage
Get message id.
getId() - Method in class org.orekit.gnss.rflink.gps.SubFrame
Get sub-frame id.
getID() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver
Get maneuver identification number.
getIdentifier() - Method in enum org.orekit.files.ilrs.StreamingCpfWriter.HeaderLineWriter
Get the regular expression for identifying line.
getIdentity() - Static method in interface org.orekit.frames.KinematicTransform
Get the identity kinematic transform.
getIdentity() - Static method in interface org.orekit.frames.StaticTransform
Get the identity static transform.
getIdentity(Field<T>) - Static method in interface org.orekit.frames.FieldKinematicTransform
Get the identity kinematic transform.
getIdentity(Field<T>) - Static method in interface org.orekit.frames.FieldStaticTransform
Get the identity static transform.
getIdentity(Field<T>) - Static method in class org.orekit.frames.FieldTransform
Get the identity transform.
getIdentity(Field<T>) - Static method in class org.orekit.utils.FieldAngularCoordinates
Fixed orientation parallel with reference frame (identity rotation, zero rotation rate and acceleration).
getIDot() - Method in class org.orekit.gnss.rflink.gps.SubFrame3
Get dot(i).
getIDot() - Method in class org.orekit.orbits.CartesianOrbit
Get the inclination derivative.
getIDot() - Method in class org.orekit.orbits.CircularOrbit
Get the inclination derivative.
getIDot() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the inclination derivative.
getIDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the inclination derivative.
getIDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the inclination derivative.
getIDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the inclination derivative.
getIDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the inclination derivative.
getIDot() - Method in class org.orekit.orbits.FieldOrbit
Get the inclination derivative.
getIDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the inclination derivative.
getIDot() - Method in class org.orekit.orbits.Orbit
Get the inclination derivative.
getIDot() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac
Getter for the rate of inclination angle.
getIDot() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Getter for the rate of inclination angle.
getIDot() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
Gets the Rate of Inclination Angle.
getIers2003(Frame) - Static method in class org.orekit.models.earth.ReferenceEllipsoid
Get the IERS2003 ellipsoid, attached to the given body frame.
getIers2010(Frame) - Static method in class org.orekit.models.earth.ReferenceEllipsoid
Get the IERS2010 ellipsoid, attached to the given body frame.
getIers96(Frame) - Static method in class org.orekit.models.earth.ReferenceEllipsoid
Get the IERS96 ellipsoid, attached to the given body frame.
getIGRF(double) - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory
Get the IGRF model for the given year.
getIGRF(double) - Method in interface org.orekit.models.earth.GeoMagneticFields
Get the IGRF model for the given year.
getIGRF(double) - Method in class org.orekit.models.earth.LazyLoadedGeoMagneticFields
 
getIjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the Ijs coefficient.
getIjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the Ijs coefficient.
getIlrsSatelliteId() - Method in class org.orekit.files.ilrs.ILRSHeader
Get the IRLS satellite ID (based on COSPAR ID).
getImaginary(int, int) - Method in class org.orekit.utils.LoveNumbers
Get the imaginary part of a nominal Love numbers.
getImpulseManeuvers() - Method in class org.orekit.propagation.conversion.AbstractAnalyticalPropagatorBuilder
Protected getter for the impulse maneuvers.
getInclination() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Get the angle between the objects orbit plane and the orbit centers equatorial plane.
getInclination() - Method in class org.orekit.models.earth.GeoMagneticElements
Returns the inclination of the magnetic field in radians.
getIncreasingTimeShift() - Method in class org.orekit.propagation.events.EventShifter
Get the increasing events time shift.
getIndicator() - Method in enum org.orekit.files.ilrs.CRDHeader.DataType
Get the data type indicator.
getIndicator() - Method in enum org.orekit.files.ilrs.CRDHeader.RangeType
Get the range type indicator.
getIndices() - Method in class org.orekit.estimation.measurements.CommonParametersWithDerivatives
Get derivatives indices map.
getInertia() - Method in class org.orekit.attitudes.TorqueFree
Get the spacecraft inertia.
getInertiaAxis1() - Method in class org.orekit.attitudes.FieldInertia
Get inertia along first axis.
getInertiaAxis1() - Method in class org.orekit.attitudes.Inertia
Get inertia along first axis.
getInertiaAxis2() - Method in class org.orekit.attitudes.FieldInertia
Get inertia along second axis.
getInertiaAxis2() - Method in class org.orekit.attitudes.Inertia
Get inertia along second axis.
getInertiaAxis3() - Method in class org.orekit.attitudes.FieldInertia
Get inertia along third axis.
getInertiaAxis3() - Method in class org.orekit.attitudes.Inertia
Get inertia along third axis.
getInertiaBlock() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData
Get the inertia logical block.
getInertialDV() - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
Get the inertial velocity increment of the maneuver.
getInertialFrame() - Method in class org.orekit.attitudes.LofOffset
Get the inertial frame.
getInertialFrame() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSegment
Get the inertial reference frame for this ephemeris segment.
getInertialFrame() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
Get the inertial reference frame for this ephemeris segment.
getInertialFrame() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
Get the inertial reference frame for this ephemeris segment.
getInertialFrame() - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
Get the inertial frame in which the velocity increment is defined.
getInertialFrame() - Method in class org.orekit.frames.LocalMagneticFieldFrame
Get interlai frame.
getInertialFrame() - Method in class org.orekit.propagation.events.BetaAngleDetector
The inertial frame in which beta angle is computed.
getInertialFrame() - Method in class org.orekit.propagation.events.FieldBetaAngleDetector
The inertial frame in which beta angle is computed.
getInertiallyOrientedFrame() - Method in interface org.orekit.bodies.CelestialBody
Get an inertially oriented, body centered frame.
getInertiaMatrix() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalProperties
Get the inertia matrix.
getInertiaMatrix() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Inertia
Get the inertia matrix.
getInertiaMatrix() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Get the inertia matrix.
getInertiaReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalProperties
Get reference frame for inertia.
getInitialAttitude() - Method in class org.orekit.attitudes.TorqueFree
Get the initial attitude.
getInitialCartesianState() - Method in class org.orekit.control.indirect.shooting.boundary.FixedTimeCartesianBoundaryStates
Getter for the initial Cartesian condition.
getInitialCovarianceMatrix(SpacecraftState) - Method in class org.orekit.estimation.sequential.AbstractCovarianceMatrixProvider
Get the initial covariance matrix.
getInitialCovarianceMatrix(SpacecraftState) - Method in interface org.orekit.estimation.sequential.CovarianceMatrixProvider
Get the initial covariance matrix.
getInitialFlowRate() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the initial flow rate.
getInitialIntegrationState() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get the initial state for integration.
getInitialIntegrationState() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get the initial state for integration.
getInitialIntegrationState() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Get the initial state for integration.
getInitialIntegrationState() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Get the initial state for integration.
getInitialJacobianColumn(String) - Method in class org.orekit.propagation.AbstractMatricesHarvester
Get the initial column of Jacobian matrix with respect to named parameter.
getInitialOrbit() - Method in class org.orekit.control.indirect.shooting.boundary.FixedTimeBoundaryOrbits
Getter for the initial condition.
getInitialOrbitDate() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Get the date of the initial orbit.
getInitialOrbitDate() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
Get the date of the initial orbit.
getInitialPV() - Method in class org.orekit.orbits.LibrationOrbit
Return the initialPV on the libration orbit.
getInitialState() - Method in class org.orekit.control.indirect.shooting.ShootingBoundaryOutput
Getter for the initial state.
getInitialState() - Method in class org.orekit.files.general.EphemerisSegmentPropagator
 
getInitialState() - Method in class org.orekit.propagation.AbstractPropagator
Get the propagator initial state.
getInitialState() - Method in class org.orekit.propagation.analytical.AdapterPropagator
Get the propagator initial state.
getInitialState() - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
 
getInitialState() - Method in class org.orekit.propagation.analytical.Ephemeris
Get the propagator initial state.
getInitialState() - Method in class org.orekit.propagation.FieldAbstractPropagator
Get the propagator initial state.
getInitialState() - Method in interface org.orekit.propagation.FieldPropagator
Get the propagator initial state.
getInitialState() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
Get the propagator initial state.
getInitialState() - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Get the propagator initial state.
getInitialState() - Method in interface org.orekit.propagation.Propagator
Get the propagator initial state.
getInitialStateTransitionMatrix() - Method in class org.orekit.propagation.AbstractMatricesHarvester
Get the initial State Transition Matrix.
getInitialThrustVector() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the initial thrust vector.
getInitialWetMass() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Get the total mass at beginning of life.
getInnovation(MeasurementDecorator, NonLinearEvolution, RealMatrix) - Method in class org.orekit.estimation.sequential.KalmanModel
getInnovation(MeasurementDecorator, NonLinearEvolution, RealMatrix) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
getInnovation(MeasurementDecorator, RealVector, RealVector, RealMatrix) - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel
getInnovation(MeasurementDecorator, RealVector, RealVector, RealMatrix) - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel
getInputs() - Method in class org.orekit.data.AbstractListCrawler
Get the list of inputs supported by the instance.
getInstantFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
Get the value of the instantaneous solar flux.
getInstantFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
Get the value of the instantaneous solar flux.
getInstantFlux(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.DTM2000InputParameters
Get the value of the instantaneous solar flux.
getIntegrationInterval() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the integrationInterval.
getIntegrationRef() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the integrationRef.
getIntegrationSettings() - Method in class org.orekit.control.indirect.shooting.propagation.ShootingPropagationSettings
Getter for the integration settings.
getIntegrator() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get the integrator used by the propagator.
getIntegrator() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get the integrator used by the propagator.
getIntegratorBuilder() - Method in class org.orekit.control.indirect.shooting.propagation.ClassicalRungeKuttaIntegrationSettings
Returns an ODE integrator builder.
getIntegratorBuilder() - Method in class org.orekit.control.indirect.shooting.propagation.DormandPrince54IntegrationSettings
Returns an ODE integrator builder.
getIntegratorBuilder() - Method in interface org.orekit.control.indirect.shooting.propagation.ShootingIntegrationSettings
Returns an ODE integrator builder.
getIntegratorBuilder() - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder
Get the integrator builder.
getIntegratorBuilder() - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
Get the integrator builder.
getIntegratorName() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get the integrator's name.
getIntegratorName() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get the integrator's name.
getIntegrityFlags() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage
Getter for B1C integrity flags.
getIntegrityStatus() - Method in class org.orekit.gnss.rflink.gps.SubFrame
Get integrity status flag.
getIntelsatElevenElements() - Method in class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElementsPropagator
Get the Intelsat's 11 elements used by the propagator.
getIntelsatElevenElements() - Method in class org.orekit.propagation.analytical.intelsat.IntelsatElevenElementsPropagator
Get the Intelsat's 11 elements used by the propagator.
getInternationalDes() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get the international designator for the object.
getInternationalDesignator() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata
Get the international designator for the object.
getInternationalDesignator() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the international designator for the object.
getInterpMethodEOP() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the interpolation method for Earth Orientation Parameters.
getInterpMethodSW() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get the interpolation method for Space Weather data.
getInterpolatedPoint(double, double) - Method in class org.orekit.models.earth.tessellation.Tile
Get an interpolated point inside the tile.
getInterpolatedState(AbsoluteDate) - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator
Get the state at interpolated date.
getInterpolatedState(FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.sampling.FieldOrekitStepInterpolator
Get the state at interpolated date.
getInterpolationDate() - Method in class org.orekit.time.AbstractFieldTimeInterpolator.InterpolationData
Get interpolation date.
getInterpolationDate() - Method in class org.orekit.time.AbstractTimeInterpolator.InterpolationData
Get interpolation date.
getInterpolationDegree() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Get the interpolation degree.
getInterpolationDegree() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Get the interpolation degree.
getInterpolationDegree() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata
Get the interpolation degree.
getInterpolationDegree() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Get the interpolation degree.
getInterpolationDegree() - Method in class org.orekit.frames.EOPHistory
Get interpolation degree.
getInterpolationMethod() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistory
Get the interpolation method to be used.
getInterpolationMethod() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Get the interpolation method to be used.
getInterpolationMethod() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSegment
Get the interpolation method to be used.
getInterpolationMethod() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Get the interpolation method to be used.
getInterpolationMethod() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata
Get the interpolation method to be used.
getInterpolationMethod() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Get the interpolation method to be used.
getInterpolationMethod() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.AttitudeEphemerisSegment
Get the interpolation method to be used.
getInterpolationMethod() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment
Get the interpolation method to be used.
getInterpolationSamples() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistory
Get the number of samples to use in interpolation.
getInterpolationSamples() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Get the number of samples to use in interpolation.
getInterpolationSamples() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSegment
Get the number of samples to use in interpolation.
getInterpolationSamples() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory
Get the number of samples to use in interpolation.
getInterpolationSamples() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSegment
Get the number of samples to use in interpolation.
getInterpolationSamples() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.AttitudeEphemerisSegment
Get the number of samples to use in interpolation.
getInterpolationSamples() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
Get the number of samples to use in interpolation.
getInterpolationSamples() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment
Get the number of samples to use in interpolation.
getInterpolationSamples() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
Get the number of samples to use in interpolation.
getInterpolationSamples() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris
Get the number of samples to use in interpolation.
getInterpolationSamples() - Method in class org.orekit.files.sp3.SP3Ephemeris
Get the number of points to use for interpolation.
getInterpolationSamples() - Method in class org.orekit.files.sp3.SP3Segment
Get the number of samples to use in interpolation.
getInterpolationSamples() - Method in class org.orekit.files.stk.STKEphemerisFile.STKEphemerisSegment
 
getIntersectionPoint(FieldLine<T>, FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.BodyShape
Get the intersection point of a line with the surface of the body.
getIntersectionPoint(FieldLine<T>, FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.bodies.OneAxisEllipsoid
Get the intersection point of a line with the surface of the body.
getIntersectionPoint(FieldLine<T>, FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.Geoid
Get the intersection point of a line with the surface of the body.
getIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in interface org.orekit.bodies.BodyShape
Get the intersection point of a line with the surface of the body.
getIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.bodies.OneAxisEllipsoid
Get the intersection point of a line with the surface of the body.
getIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.models.earth.Geoid
Get the intersection point of a line with the surface of the body.
getInterval() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Get the observation interval in seconds.
getIntervalNumber() - Method in class org.orekit.time.GLONASSDate
Get the number of the current four year interval.
getIntrackThrust() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get Enum YesNoUnknown that indicates if intrack thrust modeling was into account or not.
getInverse() - Method in interface org.orekit.frames.FieldKinematicTransform
Get the inverse transform of the instance.
getInverse() - Method in interface org.orekit.frames.FieldStaticTransform
Get the inverse transform of the instance.
getInverse() - Method in class org.orekit.frames.FieldTransform
Get the inverse transform of the instance.
getInverse() - Method in interface org.orekit.frames.KinematicTransform
Get the inverse transform of the instance.
getInverse() - Method in interface org.orekit.frames.StaticTransform
Get the inverse transform of the instance.
getInverse() - Method in class org.orekit.frames.Transform
Get the inverse transform of the instance.
getIOD() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac
Gets the Issue of Data (IOD).
getIOD() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
Gets the GLONASS Issue Of Data (IOD).
getIODC() - Method in class org.orekit.gnss.rflink.gps.SubFrame1
Get IODC.
getIODC() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage
Getter for the Issue Of Data Clock (IODC).
getIODC() - Method in class org.orekit.propagation.analytical.gnss.data.LegacyNavigationMessage
Getter for the Issue Of Data Clock (IODC).
getIODE() - Method in class org.orekit.gnss.rflink.gps.SubFrame2
Get Issue Of Data (ephemeris).
getIODE() - Method in class org.orekit.gnss.rflink.gps.SubFrame3
Get Issue Of Data (ephemeris).
getIODE() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage
Getter for the Issue Of Data Ephemeris (IODE).
getIODE() - Method in class org.orekit.propagation.analytical.gnss.data.LegacyNavigationMessage
Getter for the Issue Of Data Ephemeris (IODE).
getIODEC() - Method in class org.orekit.propagation.analytical.gnss.data.IRNSSNavigationMessage
Getter for the Issue Of Data Ephemeris and Clock (IODEC).
getIODN() - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage
Gets the Issue Of Data Navigation (IODN).
getIODN() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
Gets the Issue Of Data Navigation (IODN).
getIODNav() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage
Getter for the the Issue Of Data (IOD).
getIodSsr() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionHeader
Get the IOD SSR.
getIodSsr() - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader
Get the IOD SSR.
getIonoModel() - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeIonosphericDelayModifier
Get the ionospheric delay model.
getIonoModel() - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeRateIonosphericDelayModifier
Get the ionospheric delay model.
getIonosphereFreeCombination(SatelliteSystem) - Static method in class org.orekit.estimation.measurements.gnss.MeasurementCombinationFactory
Get the Ionosphere-Free combination of measurements.
getIonosphericCorrectionType() - Method in class org.orekit.files.rinex.navigation.RinexNavigationHeader
Getter for the ionospheric correction type.
getIonosphericModel() - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201
Get the ionospheric model adapted to the current IM201 message.
getIRNSS() - Method in class org.orekit.time.LazyLoadedTimeScales
 
getIRNSS() - Method in interface org.orekit.time.TimeScales
Get the Indian Regional Navigation Satellite System time scale.
getIRNSS() - Static method in class org.orekit.time.TimeScalesFactory
Get the Indian Regional Navigation Satellite System time scale.
getIrnssEpoch() - Method in class org.orekit.time.AbstractTimeScales
 
getIrnssEpoch() - Method in interface org.orekit.time.TimeScales
Reference epoch for IRNSS weeks: 1999-08-22T00:00:00 IRNSS time.
getIRNSSNavigationMessages() - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Get all the IRNSS navigation messages contained in the file.
getIRNSSNavigationMessages(String) - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Get the IRNSS navigation messages for the given satellite Id.
getIscB1CD() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage
Getter for inter Signal Delay for B1 CD.
getIscB1CP() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage
Getter for inter Signal Delay for B1 CP.
getIscB2AD() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage
Getter for inter Signal Delay for B2 AD.
getIscL1CA() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage
Getter for inter Signal Delay for L1 C/A.
getIscL1CD() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage
Getter for inter Signal Delay for L1 CD.
getIscL1CP() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage
Getter for inter Signal Delay for L1 CP.
getIscL2C() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage
Getter for inter Signal Delay for L2 C.
getIscL5I5() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage
Getter for inter Signal Delay for L5I.
getIscL5Q5() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage
Getter for inter Signal Delay for L5Q.
getIsp() - Method in class org.orekit.forces.maneuvers.ConfigurableLowThrustManeuver
Get the specific impulse.
getIsp() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Get the specific impulse.
getIsp() - Method in class org.orekit.forces.maneuvers.FieldImpulseManeuver
Get the specific impulse.
getIsp() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
Get the specific impulse.
getIsp() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the specific impulse.
getIsp(SpacecraftState) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
Get the specific impulse (s).
getIsp(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.ConfigurableLowThrustManeuver
Get the specific impulse.
getIsp(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Get the specific impulse at given date.
getIsp(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the specific impulse at given date.
getIteration() - Method in class org.orekit.estimation.measurements.EstimatedMeasurementBase
Get the iteration number.
getIterationCount() - Method in class org.orekit.control.indirect.shooting.ShootingBoundaryOutput
Getter for the iteration number.
getIterationsCount() - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel
Get the iterations count.
getIterationsCount() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Get the number of iterations used for last estimation.
getITRF(ITRFVersion, IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames
 
getITRF(ITRFVersion, IERSConventions, boolean) - Method in interface org.orekit.frames.Frames
Get an specific International Terrestrial Reference Frame.
getITRF(ITRFVersion, IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
Get a specific International Terrestrial Reference Frame.
getITRF(IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames
 
getITRF(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames
Get an unspecified International Terrestrial Reference Frame.
getITRF(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
Get an unspecified International Terrestrial Reference Frame.
getITRFEquinox(IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames
 
getITRFEquinox(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames
Get the equinox-based ITRF reference frame.
getITRFEquinox(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
Get the equinox-based ITRF reference frame.
getITRFType() - Method in class org.orekit.frames.EOPEntry
Get the ITRF version this entry defines.
getITRFVersion() - Method in class org.orekit.files.sinex.SinexLoader
Get the ITRF version used for the EOP entries processing.
getITRFVersion() - Method in class org.orekit.frames.VersionedITRF
Get the ITRF version.
getITRFVersion(int) - Static method in enum org.orekit.frames.ITRFVersion
Find an ITRF version from its reference year.
getITRFVersion(String) - Static method in enum org.orekit.frames.ITRFVersion
Find an ITRF version from its name.
getITRFVersion(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory
Get the ITRF version.
getJ2() - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointJ2Term
Getter for J2.
getJ2(AbsoluteDate) - Method in class org.orekit.forces.gravity.J2OnlyPerturbation
Return J2 at requested date.
getJ2(FieldAbsoluteDate<T>) - Method in class org.orekit.forces.gravity.J2OnlyPerturbation
Return J2 at requested date (Field version).
getJ2000Day() - Method in class org.orekit.time.DateComponents
Get the day number with respect to J2000 epoch.
getJ2000Epoch() - Method in class org.orekit.time.AbstractTimeScales
 
getJ2000Epoch() - Method in interface org.orekit.time.TimeScales
J2000.0 Reference epoch: 2000-01-01T12:00:00 Terrestrial Time (not UTC).
getJ2000Epoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
J2000.0 Reference epoch: 2000-01-01T12:00:00 Terrestrial Time (not UTC).
getJacobian(Orbit, PositionAngleType, double[][]) - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
Compute the Jacobian of the orbit with respect to maneuver parameters.
getJacobian(CartesianDerivativesFilter, double[][]) - Method in class org.orekit.frames.Transform
Compute the Jacobian of the Transform.transformPVCoordinates(PVCoordinates) method of the transform.
getJacobian(CartesianDerivativesFilter, T[][]) - Method in class org.orekit.frames.FieldTransform
Compute the Jacobian of the FieldTransform.transformPVCoordinates(FieldPVCoordinates) method of the transform.
getJacobiansColumnsNames() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester
Get the names of the parameters in the matrix returned by MatricesHarvester.getParametersJacobian(org.orekit.propagation.SpacecraftState).
getJacobiansColumnsNames() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Get the names of the parameters in the matrix returned by MatricesHarvester.getParametersJacobian(org.orekit.propagation.SpacecraftState).
getJacobiansColumnsNames() - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Get the names of the parameters in the matrix returned by MatricesHarvester.getParametersJacobian(org.orekit.propagation.SpacecraftState).
getJacobiansColumnsNames() - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
Get the names of the parameters in the matrix returned by MatricesHarvester.getParametersJacobian(org.orekit.propagation.SpacecraftState).
getJacobiansColumnsNames() - Method in interface org.orekit.propagation.MatricesHarvester
Get the names of the parameters in the matrix returned by MatricesHarvester.getParametersJacobian(org.orekit.propagation.SpacecraftState).
getJacobiansColumnsNames() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester
Get the names of the parameters in the matrix returned by MatricesHarvester.getParametersJacobian(org.orekit.propagation.SpacecraftState).
getJacobiansColumnsNames() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Get the names of the parameters in the matrix returned by MatricesHarvester.getParametersJacobian(org.orekit.propagation.SpacecraftState).
getJacobianWrtCartesian(PositionAngleType, double[][]) - Method in class org.orekit.orbits.Orbit
Compute the Jacobian of the orbital parameters with respect to the Cartesian parameters.
getJacobianWrtCartesian(PositionAngleType, T[][]) - Method in class org.orekit.orbits.FieldOrbit
Compute the Jacobian of the orbital parameters with respect to the Cartesian parameters.
getJacobianWrtParameters(PositionAngleType, double[][]) - Method in class org.orekit.orbits.Orbit
Compute the Jacobian of the Cartesian parameters with respect to the orbital parameters.
getJacobianWrtParameters(PositionAngleType, T[][]) - Method in class org.orekit.orbits.FieldOrbit
Compute the Jacobian of the Cartesian parameters with respect to the orbital parameters.
getJavaEpoch() - Method in class org.orekit.time.AbstractTimeScales
 
getJavaEpoch() - Method in interface org.orekit.time.TimeScales
Java Reference epoch: 1970-01-01T00:00:00 Universal Time Coordinate.
getJavaEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Java Reference epoch: 1970-01-01T00:00:00 Universal Time Coordinate.
getJD() - Method in class org.orekit.time.AbsoluteDate
Return the given date as a Julian Date expressed in UTC.
getJD() - Method in class org.orekit.time.FieldAbsoluteDate
Return the given date as a Julian Date expressed in UTC.
getJD(TimeScale) - Method in class org.orekit.time.AbsoluteDate
Return the given date as a Julian Date expressed in given timescale.
getJD(TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate
Return the given date as a Julian Date expressed in given timescale.
getJD0() - Method in class org.orekit.time.GLONASSDate
Get the current Julian date JD0.
getJjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the Jjs coefficient.
getJjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the Jjs coefficient.
getJulianEpoch() - Method in class org.orekit.time.AbstractTimeScales
 
getJulianEpoch() - Method in interface org.orekit.time.TimeScales
Reference epoch for julian dates: -4712-01-01T12:00:00 Terrestrial Time.
getJulianEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Reference epoch for julian dates: -4712-01-01T12:00:00 Terrestrial Time.
getJupiter() - Method in interface org.orekit.bodies.CelestialBodies
Get the Jupiter singleton body.
getJupiter() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Jupiter singleton body.
getJupiter() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
 
getJupiterSemiMajorAxis(AbsoluteDate, TimeScale) - Static method in class org.orekit.propagation.numerical.cr3bp.CR3BPConstants
Get the Jupiter semi-major axis.
getK() - Method in class org.orekit.files.rinex.observation.GlonassSatelliteChannel
Get the channel frequency multiplier.
getK() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the x component of eccentricity vector.
getK() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get the x component of eccentricity vector.
getK2MH2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
Get k² - h².
getK2MH2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
Get k² - h².
getK2MH2O2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
Get (k² - h²) / 2.
getK2MH2O2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
Get (k² - h²) / 2.
getKalmanEstimation() - Method in class org.orekit.estimation.sequential.AbstractKalmanEstimator
Get the provider for kalman filter estimations.
getKalmanEstimation() - Method in class org.orekit.estimation.sequential.KalmanEstimator
Get the provider for kalman filter estimations.
getKalmanEstimation() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimator
Get the provider for kalman filter estimations.
getKalmanEstimation() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanEstimator
Get the provider for kalman filter estimations.
getKalmanEstimation() - Method in class org.orekit.estimation.sequential.UnscentedKalmanEstimator
Get the provider for kalman filter estimations.
getKeplerianElementsBlock() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmData
Get the Keplerian elements logical block.
getKeplerianElementsBlock() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData
Get the Keplerian elements logical block.
getKeplerianMeanMotion() - Method in class org.orekit.orbits.FieldOrbit
Get the Keplerian mean motion.
getKeplerianMeanMotion() - Method in class org.orekit.orbits.Orbit
Get the Keplerian mean motion.
getKeplerianMeanMotion() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the Keplerian mean motion.
getKeplerianMeanMotion() - Method in class org.orekit.propagation.SpacecraftState
Get the Keplerian mean motion.
getKeplerianPeriod() - Method in class org.orekit.orbits.FieldOrbit
Get the Keplerian period.
getKeplerianPeriod() - Method in class org.orekit.orbits.Orbit
Get the Keplerian period.
getKeplerianPeriod() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the Keplerian period.
getKeplerianPeriod() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the Keplerian period.
getKeplerianPeriod() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get the Keplerian period.
getKeplerianPeriod() - Method in class org.orekit.propagation.SpacecraftState
Get the Keplerian period.
getKey() - Method in enum org.orekit.files.rinex.clock.RinexClock.ClockDataType
Get the key for the system.
getKey() - Method in enum org.orekit.files.sp3.DataUsed
Get the key for the data used.
getKey() - Method in enum org.orekit.files.sp3.SP3FileType
Get the key for the file type.
getKey() - Method in enum org.orekit.gnss.SatelliteSystem
Get the key for the system.
getKey() - Method in enum org.orekit.gnss.TimeSystem
Get the 3 letters key of the time system.
getKey() - Method in class org.orekit.utils.DoubleArrayDictionary.Entry
Get the entry key.
getKey() - Method in class org.orekit.utils.FieldArrayDictionary.Entry
Get the entry key.
getKinematicTransform(AbsoluteDate) - Method in class org.orekit.frames.GTODProvider
Get a transform for position and velocity, not acceleration.
getKinematicTransform(AbsoluteDate) - Method in class org.orekit.frames.ITRFVersion.Converter
Get a transform for position and velocity, not acceleration.
getKinematicTransform(AbsoluteDate) - Method in interface org.orekit.frames.TransformProvider
Get a transform for position and velocity, not acceleration.
getKinematicTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.GTODProvider
Get a transform for position and velocity, not acceleration.
getKinematicTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.ITRFVersion.Converter
Get a transform for position and velocity, not acceleration.
getKinematicTransform(FieldAbsoluteDate<T>) - Method in interface org.orekit.frames.TransformProvider
Get a transform for position and velocity, not acceleration.
getKinematicTransformTo(Frame, AbsoluteDate) - Method in class org.orekit.frames.Frame
Get the kinematic portion of the transform from the instance to another frame.
getKinematicTransformTo(Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.Frame
Get the kinematic portion of the transform from the instance to another frame.
getKlobucharAlpha() - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Get the "alpha" ionospheric parameters.
getKlobucharBeta() - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Get the "beta" ionospheric parameters.
getKlobucharMessages() - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Get the ionosphere Klobuchar messages.
getKpSum() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
Gets the sum of all eight Kp indices for the current entry.
getKurtosis() - Method in class org.orekit.files.ilrs.CRD.Calibration
Get the kurtosis of raw system delay values from the mean.
getKurtosis() - Method in class org.orekit.files.ilrs.CRD.SessionStatistics
Get the session kurtosis from the mean of raw accepted time-of-flight values minus the trend function.
getKXXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext
Get kXXX = h * Χ³.
getKXXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext
Get kXXX = h * Χ³.
getL() - Method in class org.orekit.data.DelaunayArguments
Get the mean anomaly of the Moon.
getL() - Method in class org.orekit.data.FieldDelaunayArguments
Get the mean anomaly of the Moon.
getL(PositionAngleType) - Method in class org.orekit.orbits.EquinoctialOrbit
Get the longitude argument.
getL(PositionAngleType) - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the longitude argument.
getL2PDataFlag() - Method in class org.orekit.gnss.rflink.gps.SubFrame1
Get L2 P data flag.
getLabel() - Method in class org.orekit.files.ccsds.definitions.SpacecraftBodyFrame
Get the frame label.
getLabel() - Method in enum org.orekit.files.rinex.section.RinexLabels
Get the first label.
getLabel(String) - Static method in class org.orekit.files.rinex.utils.parsing.RinexUtils
Get the trimmed label from a header line.
getLagrangianPoint() - Method in class org.orekit.orbits.RichardsonExpansion
Get the considered lagrangian point.
getLambda() - Method in class org.orekit.models.earth.weather.FieldPressureTemperatureHumidity
Get water vapor decrease factor.
getLambda() - Method in class org.orekit.models.earth.weather.PressureTemperatureHumidity
Get water vapor decrease factor.
getLambda() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
 
getLambda() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
Get the longitude of ascending node of orbit.
getLaserId() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
Get the laser configuration ID.
getLaserRecord() - Method in class org.orekit.files.ilrs.CRDConfiguration
Get the laser configuration record.
getLaserRecord(CRDConfiguration.SystemConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration
Get laser configuration record related to the systemRecord.
getLaserType() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
Get the laser type.
getLast() - Static method in enum org.orekit.frames.ITRFVersion
Get last supported ITRF version.
getLastDailyPredictedDate() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader
Gets the day (at data start) of the last daily data entry.
getLastEstimations() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Get the last estimations performed.
getLastKnownLeapSecond() - Method in class org.orekit.time.UTCScale
Get the date of the last known leap second.
getLastNonNullSpan() - Method in class org.orekit.utils.TimeSpanMap
Get the last (latest) span with non-null data.
getLastObservedDate() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader
Gets the day (at data start) of the last observed data entry.
getLastOccurrence() - Method in class org.orekit.propagation.events.handlers.FieldRecallLastOccurrence
Getter for last occurrence.
getLastOccurrence() - Method in class org.orekit.propagation.events.handlers.RecallLastOccurrence
Getter for last occurrence.
getLastSpan() - Method in class org.orekit.utils.TimeSpanMap
Get the last (latest) span.
getLastSystemRecord() - Method in class org.orekit.files.ilrs.CRDConfiguration
Get the system configuration record.
getLastTransition() - Method in class org.orekit.utils.TimeSpanMap
Get the last (latest) transition.
getLatC() - Method in class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElements
Get the latitude oscillation-amplitude for the cosine term.
getLatC() - Method in class org.orekit.propagation.analytical.intelsat.IntelsatElevenElements
Get the latitude oscillation-amplitude for the cosine term.
getLatC1() - Method in class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElements
Get the rate of change of latitude, for the cosine term.
getLatC1() - Method in class org.orekit.propagation.analytical.intelsat.IntelsatElevenElements
Get the rate of change of latitude, for the cosine term.
getLatest() - Method in interface org.orekit.utils.FieldTimeStampedCache
Get the latest entry in this cache.
getLatest() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the latest entry in this cache.
getLatest() - Method in class org.orekit.utils.ImmutableFieldTimeStampedCache
Get the latest entry in this cache.
getLatest() - Method in class org.orekit.utils.ImmutableTimeStampedCache
Get the latest entry in this cache.
getLatest() - Method in interface org.orekit.utils.TimeStampedCache
Get the latest entry in this cache.
getLatestEpoch() - Method in class org.orekit.files.rinex.clock.RinexClock
Get latest epoch from the clock data.
getLatitude() - Method in class org.orekit.bodies.FieldGeodeticPoint
Get the latitude.
getLatitude() - Method in class org.orekit.bodies.GeodeticPoint
Get the latitude.
getLatitude() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord
Get the latitude.
getLatitude() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
Get the latitude.
getLatitude() - Method in class org.orekit.propagation.events.FieldLatitudeCrossingDetector
Get the fixed latitude to be crossed (radians).
getLatitude() - Method in class org.orekit.propagation.events.LatitudeCrossingDetector
Get the fixed latitude to be crossed (radians).
getLatS() - Method in class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElements
Get the latitude oscillation-amplitude for the sine term.
getLatS() - Method in class org.orekit.propagation.analytical.intelsat.IntelsatElevenElements
Get the latitude oscillation-amplitude for the sine term.
getLatS1() - Method in class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElements
Get the rate of change of latitude, for the sine term.
getLatS1() - Method in class org.orekit.propagation.analytical.intelsat.IntelsatElevenElements
Get the rate of change of latitude, for the sine term.
getLaunchNumber() - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata
Get the launch number.
getLaunchNumber() - Method in class org.orekit.files.ccsds.ndm.odm.OdmCommonMetadata
Get the launch number.
getLaunchNumber() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get the launch number.
getLaunchNumber() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the launch number.
getLaunchNumber(String) - Method in class org.orekit.files.ccsds.section.Metadata
Get the launch number.
getLaunchPiece() - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata
Get the piece of launch.
getLaunchPiece() - Method in class org.orekit.files.ccsds.ndm.odm.OdmCommonMetadata
Get the piece of launch.
getLaunchPiece() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get the launch piece.
getLaunchPiece() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the launch piece.
getLaunchPiece(String) - Method in class org.orekit.files.ccsds.section.Metadata
Get the piece of launch.
getLaunchYear() - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata
Get the launch year.
getLaunchYear() - Method in class org.orekit.files.ccsds.ndm.odm.OdmCommonMetadata
Get the launch year.
getLaunchYear() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get the launch year.
getLaunchYear() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the launch year.
getLaunchYear(String) - Method in class org.orekit.files.ccsds.section.Metadata
Get the launch year.
getLDot() - Method in class org.orekit.data.DelaunayArguments
Get the mean anomaly of the Moon time derivative.
getLDot() - Method in class org.orekit.data.FieldDelaunayArguments
Get the mean anomaly of the Moon time derivative.
getLDot(PositionAngleType) - Method in class org.orekit.orbits.EquinoctialOrbit
Get the longitude argument derivative.
getLDot(PositionAngleType) - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the longitude argument derivative.
getLe() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get the eccentric longitude.
getLE() - Method in class org.orekit.data.BodiesElements
Get the mean Earth longitude.
getLE() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Earth longitude.
getLE() - Method in class org.orekit.orbits.CartesianOrbit
Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.CircularOrbit
Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.FieldOrbit
Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.KeplerianOrbit
Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.Orbit
Get the eccentric longitude argument.
getLE() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the eccentric latitude argument (as per equinoctial parameters).
getLE() - Method in class org.orekit.propagation.SpacecraftState
Get the eccentric latitude argument (as per equinoctial parameters).
getLeap() - Method in class org.orekit.files.ilrs.CPF.CPFCoordinate
Get the leap second flag (= 0 or the value of the new leap second).
getLeap() - Method in class org.orekit.time.UTCTAIOffset
Get the value of the leap at offset validity start (in seconds).
getLeap(AbsoluteDate) - Method in class org.orekit.time.GLONASSScale
Get the value of the previous leap.
getLeap(AbsoluteDate) - Method in interface org.orekit.time.TimeScale
Get the value of the previous leap.
getLeap(AbsoluteDate) - Method in class org.orekit.time.UTCScale
Get the value of the previous leap.
getLeap(FieldAbsoluteDate<T>) - Method in class org.orekit.time.GLONASSScale
Get the value of the previous leap.
getLeap(FieldAbsoluteDate<T>) - Method in interface org.orekit.time.TimeScale
Get the value of the previous leap.
getLeap(FieldAbsoluteDate<T>) - Method in class org.orekit.time.UTCScale
Get the value of the previous leap.
getLeapSeconds() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Get the Number of leap seconds since 6-Jan-1980.
getLeapSecondsDayNum() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Get the respective leap second day number.
getLeapSecondsFuture() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Get the future or past leap seconds.
getLeapSecondsWeekNum() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Get the respective leap second week number.
getLEDot() - Method in class org.orekit.data.BodiesElements
Get the mean Earth longitude time derivative.
getLEDot() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Earth longitude time derivative.
getLEDot() - Method in class org.orekit.orbits.CartesianOrbit
Get the eccentric longitude argument derivative.
getLEDot() - Method in class org.orekit.orbits.CircularOrbit
Get the eccentric longitude argument derivative.
getLEDot() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the eccentric longitude argument derivative.
getLEDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the eccentric longitude argument derivative.
getLEDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the eccentric longitude argument derivative.
getLEDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the eccentric longitude argument derivative.
getLEDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the eccentric longitude argument derivative.
getLEDot() - Method in class org.orekit.orbits.FieldOrbit
Get the eccentric longitude argument derivative.
getLEDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the eccentric longitude argument derivative.
getLEDot() - Method in class org.orekit.orbits.Orbit
Get the eccentric longitude argument derivative.
getLength() - Method in class org.orekit.utils.units.Unit
Get the length exponent.
getLf() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the eccentric longitude.
getLicense() - Method in class org.orekit.files.rinex.section.RinexBaseHeader
Getter for the license of use.
getLiftRatio() - Method in class org.orekit.forces.Panel
Get drag lift ratio.
getLightFluxModel() - Method in class org.orekit.forces.radiation.RadiationPressureModel
Getter for light flux model.
getLightFluxVector(FieldSpacecraftState<T>) - Method in class org.orekit.forces.radiation.AbstractLightFluxModel
Get the light flux vector in the state's frame.
getLightFluxVector(FieldSpacecraftState<T>) - Method in interface org.orekit.forces.radiation.LightFluxModel
Get the light flux vector in the state's frame.
getLightFluxVector(SpacecraftState) - Method in class org.orekit.forces.radiation.AbstractLightFluxModel
Get the light flux vector in the state's frame.
getLightFluxVector(SpacecraftState) - Method in interface org.orekit.forces.radiation.LightFluxModel
Get the light flux vector in the state's frame.
getLightingRatio(FieldVector3D<T>, FieldVector3D<T>) - Method in class org.orekit.forces.radiation.AbstractLightFluxModel
Get the lighting ratio ([0-1]).
getLightingRatio(FieldVector3D<T>, FieldVector3D<T>) - Method in class org.orekit.forces.radiation.ConicallyShadowedLightFluxModel
Get the lighting ratio ([0-1]).
getLightingRatio(FieldVector3D<T>, FieldVector3D<T>) - Method in class org.orekit.forces.radiation.CylindricallyShadowedLightFluxModel
Get the lighting ratio ([0-1]).
getLightingRatio(Vector3D, Vector3D) - Method in class org.orekit.forces.radiation.AbstractLightFluxModel
Get the lighting ratio ([0-1]).
getLightingRatio(Vector3D, Vector3D) - Method in class org.orekit.forces.radiation.ConicallyShadowedLightFluxModel
Get the lighting ratio ([0-1]).
getLightingRatio(Vector3D, Vector3D) - Method in class org.orekit.forces.radiation.CylindricallyShadowedLightFluxModel
Get the lighting ratio ([0-1]).
getLightingRatio(FieldSpacecraftState<T>) - Method in class org.orekit.forces.radiation.AbstractLightFluxModel
Get the lighting ratio ([0-1]).
getLightingRatio(FieldSpacecraftState<T>) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Get the lighting ratio ([0-1]).
getLightingRatio(SpacecraftState) - Method in class org.orekit.forces.radiation.AbstractLightFluxModel
Get the lighting ratio ([0-1]).
getLightingRatio(SpacecraftState) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Get the lighting ratio ([0-1]).
getLimbRadius() - Method in class org.orekit.utils.OccultationEngine.FieldOccultationAngles
Get limb radius in occulting/occulted plane.
getLimbRadius() - Method in class org.orekit.utils.OccultationEngine.OccultationAngles
Get limb radius in occulting/occulted plane.
getLine1() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get the first line.
getLine1() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the first line.
getLine2() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get the second line.
getLine2() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the second line.
getLinearInterpolation(AbstractSolarActivityData.LocalSolarActivity, Function<L, Double>) - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData
Performs a linear interpolation between two values The weights are computed from the time delta between previous date, current date, next date.
getLinearInterpolation(AbsoluteDate, Function<L, Double>) - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData
Performs a linear interpolation between two values The weights are computed from the time delta between previous date, current date, next date.
getLineNumber() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Get the number of the line in the CCSDS data message.
getLineNumber() - Method in class org.orekit.files.rinex.section.RinexComment
Get the line number.
getListAppliedDCBS() - Method in class org.orekit.files.rinex.clock.RinexClock
Getter for the applied differential code bias corrections.
getListAppliedDCBS() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Get the list of applied differential code bias corrections.
getListAppliedPCVS() - Method in class org.orekit.files.rinex.clock.RinexClock
Getter for the applied phase center variations.
getListAppliedPCVS() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Get the list of antenna center variation corrections.
getLJu() - Method in class org.orekit.data.BodiesElements
Get the mean Jupiter longitude.
getLJu() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Jupiter longitude.
getLJuDot() - Method in class org.orekit.data.BodiesElements
Get the mean Jupiter longitude time derivative.
getLJuDot() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Jupiter longitude time derivative.
getLLimits(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Compute the limits in L, the true longitude, for integration.
getLLimits(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Compute the limits in L, the true longitude, for integration.
getLLimits(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Compute the limits in L, the true longitude, for integration.
getLLimits(SpacecraftState, AuxiliaryElements) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Compute the limits in L, the true longitude, for integration.
getLLimits(SpacecraftState, AuxiliaryElements) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Compute the limits in L, the true longitude, for integration.
getLLimits(SpacecraftState, AuxiliaryElements) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Compute the limits in L, the true longitude, for integration.
getLM() - Method in class org.orekit.orbits.CartesianOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.CircularOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.FieldOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.KeplerianOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.Orbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the mean longitude argument (as per equinoctial parameters).
getLM() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the mean longitude.
getLM() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get the mean longitude.
getLM() - Method in class org.orekit.propagation.SpacecraftState
Get the mean longitude argument (as per equinoctial parameters).
getLm0() - Method in class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElements
Get the mean longitude (East of Greenwich).
getLm0() - Method in class org.orekit.propagation.analytical.intelsat.IntelsatElevenElements
Get the mean longitude (East of Greenwich).
getLm1() - Method in class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElements
Get the drift rate.
getLm1() - Method in class org.orekit.propagation.analytical.intelsat.IntelsatElevenElements
Get the drift rate.
getLm2() - Method in class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElements
Get the drift acceleration.
getLm2() - Method in class org.orekit.propagation.analytical.intelsat.IntelsatElevenElements
Get the drift acceleration.
getLMa() - Method in class org.orekit.data.BodiesElements
Get the mean Mars longitude.
getLMa() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Mars longitude.
getLMaDot() - Method in class org.orekit.data.BodiesElements
Get the mean Mars longitude time derivative.
getLMaDot() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Mars longitude time derivative.
getLMDot() - Method in class org.orekit.orbits.CartesianOrbit
Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.CircularOrbit
Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.FieldOrbit
Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.Orbit
Get the mean longitude argument derivative.
getLMe() - Method in class org.orekit.data.BodiesElements
Get the mean Mercury longitude.
getLMe() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Mercury longitude.
getLMeDot() - Method in class org.orekit.data.BodiesElements
Get the mean Mercury longitude time derivative.
getLMeDot() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Mercury longitude time derivative.
getLNe() - Method in class org.orekit.data.BodiesElements
Get the mean Neptune longitude.
getLNe() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Neptune longitude.
getLNeDot() - Method in class org.orekit.data.BodiesElements
Get the mean Neptune longitude time derivative.
getLNeDot() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Neptune longitude time derivative.
getLNFifthString() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the GLONASS ln Word extracted from fifth string of the subframe.
getLns(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldLnsCoefficients
Get the value of Lns(γ).
getLns(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.LnsCoefficients
Get the value of Lns(γ).
getLNThirdString() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the GLONASS ln Word extracted from third string of the subframe.
getLoadedAstronomicalUnit() - Method in class org.orekit.bodies.JPLEphemeridesLoader
Get astronomical unit.
getLoadedConstant(String...) - Method in class org.orekit.bodies.JPLEphemeridesLoader
Get a constant defined in the ephemerides headers.
getLoadedDataNames() - Method in class org.orekit.data.DataProvidersManager
Get an unmodifiable view of the set of data file names that have been loaded.
getLoadedEarthMoonMassRatio() - Method in class org.orekit.bodies.JPLEphemeridesLoader
Get Earth/Moon mass ratio.
getLoadedGravitationalCoefficient(JPLEphemeridesLoader.EphemerisType) - Method in class org.orekit.bodies.JPLEphemeridesLoader
Get the gravitational coefficient of a body.
getLocalizedMessage() - Method in exception org.orekit.errors.OrekitException
getLocalizedMessage() - Method in exception org.orekit.errors.OrekitIllegalArgumentException
getLocalizedMessage() - Method in exception org.orekit.errors.OrekitIllegalStateException
getLocalizedMessage() - Method in exception org.orekit.errors.OrekitInternalError
getLocalizedMessage() - Method in exception org.orekit.errors.OrekitIOException
getLocalizedMessage() - Method in exception org.orekit.errors.OrekitParseException
getLocalizedString(Locale) - Method in enum org.orekit.errors.OrekitMessages
getLocalOffset() - Method in class org.orekit.estimation.measurements.gnss.OnBoardCommonParametersWithDerivatives
Get local clock offset.
getLocalOffset() - Method in class org.orekit.estimation.measurements.gnss.OnBoardCommonParametersWithoutDerivatives
Get local clock offset.
getLocalRate() - Method in class org.orekit.estimation.measurements.gnss.OnBoardCommonParametersWithDerivatives
Get local clock rate.
getLocalRate() - Method in class org.orekit.estimation.measurements.gnss.OnBoardCommonParametersWithoutDerivatives
Get local clock rate.
getLocalTimingId() - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration
Get the local timing system configuration ID.
getLocation() - Method in class org.orekit.gnss.DOP
Gets the location with respect to the Earth where DOP was calculated.
getLod() - Method in class org.orekit.files.sinex.SinexEopEntry
Get the length of day.
getLOD() - Method in class org.orekit.frames.EOPEntry
Get the LoD (Length of Day) value.
getLOD(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory
Get the LoD (Length of Day) value.
getLOD(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EOPHistory
Get the LoD (Length of Day) value.
getLof() - Method in class org.orekit.attitudes.LofOffset
Get the local orbital frame.
getLOF() - Method in class org.orekit.propagation.FieldStateCovariance
Get the covariance LOF type.
getLOF() - Method in class org.orekit.propagation.StateCovariance
Get the covariance LOF type.
getLofCartesianOrbitalParametersEvolution() - Method in class org.orekit.estimation.sequential.UnivariateProcessNoise
Getter for the lofCartesianOrbitalParametersEvolution.
getLofType() - Method in class org.orekit.estimation.sequential.UnivariateProcessNoise
Getter for the lofType.
getLofType() - Method in enum org.orekit.files.ccsds.definitions.OrbitRelativeFrame
Get the type of Local Orbital frame.
getLoggedEvents() - Method in class org.orekit.propagation.events.EventsLogger
Get an immutable copy of the logged events.
getLoggedEvents() - Method in class org.orekit.propagation.events.FieldEventsLogger
Get an immutable copy of the logged events.
getLonC() - Method in class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElements
Get the longitude oscillation-amplitude for the cosine term.
getLonC() - Method in class org.orekit.propagation.analytical.intelsat.IntelsatElevenElements
Get the longitude oscillation-amplitude for the cosine term.
getLonC1() - Method in class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElements
Get the rate of change of longitude, for the cosine term.
getLonC1() - Method in class org.orekit.propagation.analytical.intelsat.IntelsatElevenElements
Get the rate of change of longitude, for the cosine term.
getLongitude() - Method in class org.orekit.bodies.FieldGeodeticPoint
Get the longitude.
getLongitude() - Method in class org.orekit.bodies.GeodeticPoint
Get the longitude.
getLongitude() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord
Get the longitude.
getLongitude() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
Get the longitude.
getLongitude() - Method in class org.orekit.propagation.events.FieldLongitudeCrossingDetector
Get the fixed longitude to be crossed (radians).
getLongitude() - Method in class org.orekit.propagation.events.LongitudeCrossingDetector
Get the fixed longitude to be crossed (radians).
getLonS() - Method in class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElements
Get the longitude oscillation-amplitude for the sine term.
getLonS() - Method in class org.orekit.propagation.analytical.intelsat.IntelsatElevenElements
Get the longitude oscillation-amplitude for the sine term.
getLonS1() - Method in class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElements
Get the rate of change of longitude, for the sine term.
getLonS1() - Method in class org.orekit.propagation.analytical.intelsat.IntelsatElevenElements
Get the rate of change of longitude, for the sine term.
getLossOfLockIndicator() - Method in class org.orekit.files.rinex.observation.ObservationData
Get the Loss of Lock Indicator.
getLoveNumbers() - Method in enum org.orekit.utils.IERSConventions
Get the Love numbers.
getLowElevationThreshold() - Method in class org.orekit.models.earth.troposphere.CanonicalSaastamoinenModel
Get the low elevation threshold value for path delay computation.
getLowElevationThreshold() - Method in class org.orekit.models.earth.troposphere.ModifiedSaastamoinenModel
Get the low elevation threshold value for path delay computation.
getLowerCaseAbbreviation() - Method in enum org.orekit.time.Month
Get the lower case three letters abbreviation.
getLowerCaseName() - Method in enum org.orekit.time.Month
Get the lower case full name.
getLowercaseOmega() - Method in class org.orekit.gnss.rflink.gps.SubFrame3
Get ω.
getLowercaseOmega() - Method in class org.orekit.gnss.rflink.gps.SubFrameAlmanac
Get ω.
getLowerLimit() - Method in class org.orekit.ssa.metrics.FieldProbabilityOfCollision
Get lower limit of the probability of collision value.
getLowerLimit() - Method in class org.orekit.ssa.metrics.ProbabilityOfCollision
Get lower limit of the probability of collision value.
getLowReference() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Get a reference to the lower triangular matrix of the decomposition.
getLPosition(LagrangianPoints) - Method in class org.orekit.bodies.CR3BPSystem
Get the position of the Lagrangian point in the CR3BP Rotating frame.
getLPrime() - Method in class org.orekit.data.DelaunayArguments
Get the mean anomaly of the Sun.
getLPrime() - Method in class org.orekit.data.FieldDelaunayArguments
Get the mean anomaly of the Sun.
getLPrimeDot() - Method in class org.orekit.data.DelaunayArguments
Get the mean anomaly of the Sun time derivative.
getLPrimeDot() - Method in class org.orekit.data.FieldDelaunayArguments
Get the mean anomaly of the Sun time derivative.
getLSa() - Method in class org.orekit.data.BodiesElements
Get the mean Saturn longitude.
getLSa() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Saturn longitude.
getLSaDot() - Method in class org.orekit.data.BodiesElements
Get the mean Saturn longitude time derivative.
getLSaDot() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Saturn longitude time derivative.
getLst81Adj() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
Gets the last 81-day arithmetic average of F10.7 (adjusted).
getLst81Obs() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
Gets the last 81-day arithmetic average of F10.7 (observed).
getLUr() - Method in class org.orekit.data.BodiesElements
Get the mean Uranus longitude.
getLUr() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Uranus longitude.
getLUrDot() - Method in class org.orekit.data.BodiesElements
Get the mean Uranus longitude time derivative.
getLUrDot() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Uranus longitude time derivative.
getLv() - Method in class org.orekit.orbits.CartesianOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.CircularOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.FieldOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.KeplerianOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.Orbit
Get the true longitude argument.
getLv() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the true latitude argument (as per equinoctial parameters).
getLv() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the true longitude.
getLv() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get the true longitude.
getLv() - Method in class org.orekit.propagation.SpacecraftState
Get the true latitude argument (as per equinoctial parameters).
getLvDot() - Method in class org.orekit.orbits.CartesianOrbit
Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.CircularOrbit
Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.FieldOrbit
Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.Orbit
Get the true longitude argument derivative.
getLVe() - Method in class org.orekit.data.BodiesElements
Get the mean Venus longitude.
getLVe() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Venus longitude.
getLVeDot() - Method in class org.orekit.data.BodiesElements
Get the mean Venus longitude time derivative.
getLVeDot() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Venus longitude time derivative.
getLyapunovOrbitalPeriod(double) - Method in class org.orekit.orbits.RichardsonExpansion
Return the orbital period of the Halo Orbit.
getM() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the GLONASS M Word.
getM0() - Method in class org.orekit.gnss.rflink.gps.SubFrame2
Get M₀.
getM0() - Method in class org.orekit.gnss.rflink.gps.SubFrameAlmanac
Get M₀.
getM0() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Getter for the mean anomaly at reference time.
getM0() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
Gets the Mean Anomaly at Reference Time.
getM2() - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Get the value of the M2 drag parameter.
getM2() - Method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Get the value of the M2 drag parameter.
getM2(AbsoluteDate) - Method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Get the value of the M2 drag parameter.
getM2aoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext
Get m2aoA = -2 * a / A.
getM2aoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
Deprecated.
since 12.2 Use -getAx2oA()() instead
getM2aoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext
Get m2aoA = -2 * a / A.
getM2aoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
Deprecated.
since 12.2 Use -getAx2oA()() instead
getM2Value() - Method in class org.orekit.propagation.conversion.BrouwerLyddanePropagatorBuilder
Get the value of the M2 parameter.
getMagneticField() - Method in class org.orekit.frames.LocalMagneticFieldFrame
Get geomagnetid field.
getMahalanobisDistance() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the Mahalanobis Distance.
getMainStateDerivativesIncrements() - Method in class org.orekit.propagation.integration.CombinedDerivatives
Get the derivatives increments related to the main state.
getMainStateDerivativesIncrements() - Method in class org.orekit.propagation.integration.FieldCombinedDerivatives
Get the derivatives increments related to the main state.
getMainStateEquations(FieldODEIntegrator<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get the differential equations to integrate (for main state only).
getMainStateEquations(FieldODEIntegrator<T>) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Get the differential equations to integrate (for main state only).
getMainStateEquations(FieldODEIntegrator<T>) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Get the differential equations to integrate (for main state only).
getMainStateEquations(ODEIntegrator) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get the differential equations to integrate (for main state only).
getMainStateEquations(ODEIntegrator) - Method in class org.orekit.propagation.numerical.GLONASSNumericalPropagator
 
getMainStateEquations(ODEIntegrator) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Get the differential equations to integrate (for main state only).
getMainStateEquations(ODEIntegrator) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Get the differential equations to integrate (for main state only).
getManagedAdditionalStates() - Method in class org.orekit.propagation.AbstractPropagator
Get all the names of all managed states.
getManagedAdditionalStates() - Method in class org.orekit.propagation.analytical.Ephemeris
Get all the names of all managed states.
getManagedAdditionalStates() - Method in class org.orekit.propagation.FieldAbstractPropagator
Get all the names of all managed states.
getManagedAdditionalStates() - Method in interface org.orekit.propagation.FieldPropagator
Get all the names of all managed states.
getManagedAdditionalStates() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get all the names of all managed states.
getManagedAdditionalStates() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get all the names of all managed states.
getManagedAdditionalStates() - Method in interface org.orekit.propagation.Propagator
Get all the names of all managed states.
getManBasis() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Get basis of this maneuver history data.
getManBasisID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Get identification number of the orbit determination or simulation upon which this maneuver is based.
getManComposition() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Get maneuver elements of information.
getManDeviceID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Get identifier of the device used for this maneuver.
getManeuver(int) - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData
Get a maneuver.
getManeuver(int) - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm
Get a maneuver.
getManeuver(int) - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData
Get a maneuver.
getManeuverable() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get the ability of object to maneuver or not.
getManeuverAttitudeProvider() - Method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider
Attitude provider to use.
getManeuverBlocks() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmData
Get maneuvers logical blocks.
getManeuverBlocks() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmData
Get maneuvers logical blocks.
getManeuvers() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData
Get a list of all maneuvers.
getManeuvers() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistory
Get the maneuvers.
getManeuvers() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm
Get a list of all maneuvers.
getManeuvers() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData
Get a list of all maneuvers.
getManeuversFrequency() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Get the average frequency of orbit or attitude maneuvers (in SI units, hence per second).
getManeuversPerYear() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Get the average number of orbit or attitude maneuvers per year.
getManeuverTriggers() - Method in class org.orekit.forces.maneuvers.Maneuver
Get the maneuver triggers.
getManeuverTriggersParameters(double[]) - Method in class org.orekit.forces.maneuvers.Maneuver
Extract maneuver triggers' parameters from the parameters' array called in by the ForceModel interface.
getManeuverTriggersParameters(T[]) - Method in class org.orekit.forces.maneuvers.Maneuver
Extract maneuver triggers' parameters from the parameters' array called in by the ForceModel interface.
getManFrameEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Get epoch of the maneuver reference frame.
getManID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Get maneuver identification number.
getManifolds(SpacecraftState, boolean) - Method in class org.orekit.orbits.LibrationOrbit
Return a manifold direction from one position on a libration Orbit.
getManNextEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Get start time of next maneuver.
getManNextID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Get identification number of next maneuver.
getManPredSource() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Get prediction source on which this maneuver is based.
getManPrevEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Get completion time of previous maneuver.
getManPrevID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Get identification number of previous maneuver.
getManPurpose() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver
Get purpose of maneuver.
getManPurpose() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Get the purposes of the maneuver.
getManReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Get reference frame of the maneuver.
getManufacturer() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Get manufacturer name.
getManUnits() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Get maneuver elements of information units.
getMapFilters() - Method in class org.orekit.estimation.measurements.filtering.DualFrequencySmoother
Get the map storing the filters for each observation type.
getMapFilters() - Method in class org.orekit.estimation.measurements.filtering.SingleFrequencySmoother
Get the map storing the filters for each observation type.
getMargin() - Method in class org.orekit.geometry.fov.AbstractFieldOfView
Get the angular margin to apply (radians).
getMargin() - Method in interface org.orekit.geometry.fov.FieldOfView
Get the angular margin to apply (radians).
getMargin() - Method in class org.orekit.propagation.events.EclipseDetector
Get the angular margin used for eclipse detection.
getMargin() - Method in class org.orekit.propagation.events.FieldEclipseDetector
Get the angular margin used for eclipse detection.
getMargin() - Method in class org.orekit.propagation.events.GeographicZoneDetector
Get the angular margin to apply (radians).
getMarkerName() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Get name of the antenna marker.
getMarkerNumber() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Get number of the antenna marker.
getMarkerType() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Get type of the antenna marker.
getMars() - Method in interface org.orekit.bodies.CelestialBodies
Get the Mars singleton body.
getMars() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Mars singleton body.
getMars() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
 
getMass() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Get the mass of the object.
getMass() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmData
Get the mass.
getMass() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData
Get the mass.
getMass() - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters
Get the spacecraft mass.
getMass() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Get the mass.
getMass() - Method in class org.orekit.propagation.FieldSpacecraftState
Gets the current mass.
getMass() - Method in class org.orekit.propagation.SpacecraftState
Gets the current mass.
getMass() - Method in class org.orekit.utils.units.Unit
Get the mass exponent.
getMass(AbsoluteDate) - Method in class org.orekit.files.general.EphemerisSegmentPropagator
 
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AdapterPropagator
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
 
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.Ephemeris
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.intelsat.IntelsatElevenElementsPropagator
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.KeplerianPropagator
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Get the mass.
getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Get the mass.
getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Get the mass.
getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Get the mass.
getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldKeplerianPropagator
Get the mass.
getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElementsPropagator
Get the mass.
getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
Get the mass.
getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
Get the mass.
getMassDepletionDelay() - Method in class org.orekit.forces.maneuvers.jacobians.TriggerDate
Get the mass depletion effect processor.
getMassDerivatives(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel
Get the mass derivative (i.e.
getMassDerivatives(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
Get the mass derivative (i.e.
getMassDerivatives(SpacecraftState, double[]) - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel
Get the mass derivative (i.e.
getMassDerivatives(SpacecraftState, double[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
Get the mass derivative (i.e.
getMassFlowRateFactor() - Method in class org.orekit.control.indirect.adjoint.cost.AbstractCartesianEnergy
Getter for mass flow rate factor.
getMassFlowRateFactor() - Method in interface org.orekit.control.indirect.adjoint.cost.CartesianCost
Getter for mass flow rate factor.
getMassFlowRateFactor() - Method in class org.orekit.control.indirect.adjoint.cost.UnboundedCartesianEnergyNeglectingMass
Getter for mass flow rate factor.
getMassInterpolator() - Method in class org.orekit.propagation.FieldSpacecraftStateInterpolator
Get mass interpolator.
getMassInterpolator() - Method in class org.orekit.propagation.SpacecraftStateInterpolator
Get mass interpolator.
getMassRatio() - Method in class org.orekit.bodies.CR3BPSystem
Get the CR3BP mass ratio of the system mu2/(mu1+mu2).
getMatrix() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovariance
Get the covariance matrix.
getMatrix() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovariance
Get the covariance matrix.
getMatrix() - Method in class org.orekit.propagation.FieldStateCovariance
Get the covariance matrix.
getMatrix() - Method in class org.orekit.propagation.StateCovariance
Get the covariance matrix.
getMatrixLine(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix
Get a line of the matrix.
getMaxAlt() - Method in class org.orekit.models.earth.atmosphere.HarrisPriester
Get the maximal altitude for the model.
getMaxAR3Pow() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyStaticContext
Get the value of max power for a/R3 in the serie expansion.
getMaxAreaForCollisionProbability() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Get the maximum cross-sectional area for collision probability estimation purposes.
getMaxAvailableDegree() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Get the maximal degree available in the last file parsed.
getMaxAvailableDegree() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get the maximal degree available in the last file parsed.
getMaxAvailableOrder() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Get the maximal order available in the last file parsed.
getMaxAvailableOrder() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get the maximal order available in the last file parsed.
getMaxCheckInterval() - Method in class org.orekit.attitudes.AttitudesSequence.Switch
Get maximal time interval between switching function checks.
getMaxCheckInterval() - Method in class org.orekit.propagation.events.AbstractDetector
Get maximal time interval between switching function checks.
getMaxCheckInterval() - Method in class org.orekit.propagation.events.AdapterDetector
Get maximal time interval between switching function checks.
getMaxCheckInterval() - Method in class org.orekit.propagation.events.EventDetectionSettings
Getter for adaptable interval.
getMaxCheckInterval() - Method in interface org.orekit.propagation.events.EventDetector
Get maximal time interval between switching function checks.
getMaxCheckInterval() - Method in class org.orekit.propagation.events.FieldAbstractDetector
Get maximal time interval between switching function checks.
getMaxCheckInterval() - Method in class org.orekit.propagation.events.FieldAdapterDetector
Get maximal time interval between switching function checks.
getMaxCheckInterval() - Method in class org.orekit.propagation.events.FieldEventDetectionSettings
Getter for adaptable interval.
getMaxCheckInterval() - Method in interface org.orekit.propagation.events.FieldEventDetector
Get maximal time interval between switching function checks.
getMaxChunksDuration() - Method in class org.orekit.bodies.JPLEphemeridesLoader
Get the maximal chunks duration.
getMaxCollisionProbability() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get max collision probability.
getMaxCollisionProbabilityMethod() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get max collision probability method.
getMaxDate() - Method in class org.orekit.attitudes.AggregateBoundedAttitudeProvider
Get the last date of the range.
getMaxDate() - Method in interface org.orekit.attitudes.BoundedAttitudeProvider
Get the last date of the range.
getMaxDate() - Method in class org.orekit.attitudes.TabulatedLofOffset
Get the last date of the range.
getMaxDate() - Method in class org.orekit.attitudes.TabulatedProvider
Get the last date of the range.
getMaxDate() - Method in class org.orekit.files.general.EphemerisSegmentPropagator
 
getMaxDate() - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData
Gets the available data range maximum date.
getMaxDate() - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityDataLoader
Gets the available data range maximum date.
getMaxDate() - Method in class org.orekit.models.earth.atmosphere.data.DtcDataLoader
Gets the available data range maximum date.
getMaxDate() - Method in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData
Gets the available data range maximum date.
getMaxDate() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader
Gets the available data range maximum date.
getMaxDate() - Method in interface org.orekit.models.earth.atmosphere.DTM2000InputParameters
Gets the available data range maximum date.
getMaxDate() - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters
Gets the available data range maximum date.
getMaxDate() - Method in interface org.orekit.models.earth.atmosphere.NRLMSISE00InputParameters
Gets the available data range maximum date.
getMaxDate() - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
 
getMaxDate() - Method in class org.orekit.propagation.analytical.Ephemeris
Get the last date of the range.
getMaxDate() - Method in interface org.orekit.propagation.BoundedPropagator
Get the last date of the range.
getMaxDate() - Method in interface org.orekit.propagation.FieldBoundedPropagator
Get the last date of the range.
getMaxDate() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
Get the last date of the range.
getMaxDate() - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Get the last date of the range.
getMaxDate() - Method in class org.orekit.utils.AggregatedPVCoordinatesProvider
Get the last date of the range.
getMaxDegree() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
Get the maximal supported degree.
getMaxDegree() - Method in class org.orekit.forces.gravity.potential.OceanTidesWave
Get the maximum supported degree.
getMaxDegree() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider
Get the maximal supported degree.
getMaxDistance() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Get the maximum of distance among the solutions found.
getMaxEccPow() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyStaticContext
Get the value of max power for e in the serie expansion.
getMaxFreqF() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyStaticContext
Get the value of max frequency of F.
getMaximumIterationCount() - Method in interface org.orekit.control.indirect.shooting.boundary.CartesianBoundaryConditionChecker
Returns the maximum number of iterations.
getMaximumIterationCount() - Method in class org.orekit.control.indirect.shooting.boundary.NormBasedCartesianConditionChecker
Returns the maximum number of iterations.
getMaximumObsGap() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get maximum time between observations in the OD of the object.
getMaximumValidDateForObservationPair(String, String) - Method in class org.orekit.files.sinex.Dcb
Get the maximum valid date for a given observation pair.
getMaximumValidDateForObservationPair(ObservationType, ObservationType) - Method in class org.orekit.files.sinex.Dcb
Get the maximum valid date for a given observation pair.
getMaxIterationCount() - Method in class org.orekit.attitudes.AttitudesSequence.Switch
Get maximal number of iterations in the event time search.
getMaxIterationCount() - Method in class org.orekit.propagation.events.AbstractDetector
Get maximal number of iterations in the event time search.
getMaxIterationCount() - Method in class org.orekit.propagation.events.AdapterDetector
Get maximal number of iterations in the event time search.
getMaxIterationCount() - Method in class org.orekit.propagation.events.EventDetectionSettings
Getter for max iter.
getMaxIterationCount() - Method in interface org.orekit.propagation.events.EventDetector
Get maximal number of iterations in the event time search.
getMaxIterationCount() - Method in class org.orekit.propagation.events.FieldAbstractDetector
Get maximal number of iterations in the event time search.
getMaxIterationCount() - Method in class org.orekit.propagation.events.FieldAdapterDetector
Get maximal number of iterations in the event time search.
getMaxIterationCount() - Method in class org.orekit.propagation.events.FieldEventDetectionSettings
Getter for max iter.
getMaxIterationCount() - Method in interface org.orekit.propagation.events.FieldEventDetector
Get maximal number of iterations in the event time search.
getMaxIterations() - Method in class org.orekit.propagation.conversion.averaging.converters.FixedPointOsculatingToAveragedConverter
Getter for the maximum number of iterations.
getMaxNeighborsSize() - Method in interface org.orekit.utils.FieldTimeStampedCache
Get the fixed size of the lists returned by FieldTimeStampedCache.getNeighbors(FieldAbsoluteDate).
getMaxNeighborsSize() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the maximum size of the lists returned by TimeStampedCache.getNeighbors(AbsoluteDate, int).
getMaxNeighborsSize() - Method in class org.orekit.utils.ImmutableFieldTimeStampedCache
Get the fixed size of the lists returned by FieldTimeStampedCache.getNeighbors(FieldAbsoluteDate).
getMaxNeighborsSize() - Method in class org.orekit.utils.ImmutableTimeStampedCache
Get the maximum size of the lists returned by TimeStampedCache.getNeighbors(AbsoluteDate, int).
getMaxNeighborsSize() - Method in interface org.orekit.utils.TimeStampedCache
Get the maximum size of the lists returned by TimeStampedCache.getNeighbors(AbsoluteDate, int).
getMaxOrder() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
Get the maximal supported order.
getMaxOrder() - Method in class org.orekit.forces.gravity.potential.OceanTidesWave
Get the maximum supported order.
getMaxOrder() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider
Get the maximal supported order.
getMaxOrder() - Method in enum org.orekit.utils.AngularDerivativesFilter
Get the maximum derivation order.
getMaxOrder() - Method in enum org.orekit.utils.CartesianDerivativesFilter
Get the maximum derivation order.
getMaxParseDegree() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Get the degree limit for the next file parsing.
getMaxParseDegree() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get the degree limit for the next file parsing.
getMaxParseOrder() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Get the order limit for the next file parsing.
getMaxParseOrder() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get the order limit for the next file parsing.
getMaxPredictedEigenMaj() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get maximum predicted major eigenvalue of 1σ positional error ellipsoid over entire time span of the OCM.
getMaxRcs() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties
Get the maximum radar cross-section.
getMaxSigma() - Method in class org.orekit.estimation.measurements.modifiers.OutlierFilter
Get the value of the outlier detection limit.
getMaxSlots() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the maximum number of independent cached time slots.
getMaxSolution() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Get the maximum number of solutions seeked.
getMaxSpan() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the maximum duration span in seconds of one slot.
getMaxThrust() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Get the maximum composite thrust the spacecraft can accomplish.
getMaxTimeBeetween2Measurement() - Method in class org.orekit.estimation.measurements.gnss.AbstractCycleSlipDetector
Get the maximum time lapse between 2 measurements without considering a cycle-slip has occurring between both.
getMaxValue() - Method in class org.orekit.utils.ParameterDriver
Get maximum parameter value.
getMCo2AB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext
Get mCo2AB = -C / 2AB.
getMCo2AB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
Deprecated.
since 12.2 Use -getCo2AB()() instead
getMCo2AB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext
Get mCo2AB = -C / 2AB.
getMCo2AB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
Deprecated.
since 12.2 Use -getCo2AB()() instead
getMeanAnomaly() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the mean anomaly.
getMeanAnomaly() - Method in class org.orekit.orbits.KeplerianOrbit
Get the mean anomaly.
getMeanAnomaly() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get the mean anomaly.
getMeanAnomaly() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the mean anomaly.
getMeanAnomalyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the mean anomaly derivative.
getMeanAnomalyDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the mean anomaly derivative.
getMeanAnomalyDotWrtA() - Method in class org.orekit.orbits.FieldOrbit
Get the derivative of the mean anomaly with respect to the semi major axis.
getMeanAnomalyDotWrtA() - Method in class org.orekit.orbits.Orbit
Get the derivative of the mean anomaly with respect to the semi major axis.
getMeanElementRate(FieldSpacecraftState<T>, AbstractGaussianContribution.GaussQuadrature, T, T, FieldAbstractGaussianContributionContext<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTJ2SquaredClosedForm
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(SpacecraftState, AbstractGaussianContribution.GaussQuadrature, double, double, AbstractGaussianContributionContext, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTJ2SquaredClosedForm
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Computes the mean equinoctial elements rates dai / dt.
getMeanElementTheory() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmMetadata
Get the description of the Mean Element Theory.
getMeanFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
Get the value of the mean solar flux.
getMeanFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
Get the value of the mean solar flux.
getMeanFlux(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.DTM2000InputParameters
Get the value of the mean solar flux.
getMeanMotion() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Get the orbit mean motion.
getMeanMotion() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac
Getter for the mean motion.
getMeanMotion() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Getter for the mean motion.
getMeanMotion() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
Gets the Mean Motion.
getMeanMotion() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get the mean motion.
getMeanMotion() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the mean motion.
getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext
Get the Keplerian mean motion.
getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTGravityContext
Get the Keplerian mean motion.
getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext
Get the Keplerian mean motion.
getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext
Get the Keplerian mean motion.
getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTGravityContext
Get the Keplerian mean motion.
getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext
Get the Keplerian mean motion.
getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the Keplerian mean motion.
getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get the Keplerian mean motion.
getMeanMotionDot() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
Get the first time derivative of the mean motion.
getMeanMotionDotDot() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
Get the second time derivative of the mean motion.
getMeanMotionFirstDerivative() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get the mean motion first derivative.
getMeanMotionFirstDerivative() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the mean motion first derivative.
getMeanMotionSecondDerivative() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get the mean motion second derivative.
getMeanMotionSecondDerivative() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the mean motion second derivative.
getMeanObliquityFunction() - Method in enum org.orekit.utils.IERSConventions
Get the function computing mean obliquity of the ecliptic.
getMeanObliquityFunction(TimeScales) - Method in enum org.orekit.utils.IERSConventions
Get the function computing mean obliquity of the ecliptic.
getMeasurement() - Method in class org.orekit.files.ccsds.ndm.tdm.Observation
Getter for the measurement.
getMeasurements() - Method in class org.orekit.estimation.measurements.MultiplexedMeasurement
Get the underlying measurements.
getMeasurementsParametersDrivers(boolean) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Get the measurements parameters supported by this estimator (including measurements and modifiers).
getMeasurementsParametersEvolution() - Method in class org.orekit.estimation.sequential.UnivariateProcessNoise
Getter for the measurementsParametersEvolution.
getMeasurementType() - Method in class org.orekit.estimation.measurements.gnss.CombinedObservationData
Get the measurement type.
getMeasurementType() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
Get the type of measurement.
getMeasurementType() - Method in enum org.orekit.gnss.ObservationType
Get the measurement type.
getMedianDriver() - Method in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector
Get the driver for median date.
getMedianDriver() - Method in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector
Get the driver for median date.
getMelbourneWubbenaCombination(SatelliteSystem) - Static method in class org.orekit.estimation.measurements.gnss.MeasurementCombinationFactory
Get the Melbourne-Wübbena combination of measurements.
getMercury() - Method in interface org.orekit.bodies.CelestialBodies
Get the Mercury singleton body.
getMercury() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Mercury singleton body.
getMercury() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
 
getMergedFiles() - Method in class org.orekit.files.rinex.navigation.RinexNavigationHeader
Getter for the number of merged files.
getMessage() - Method in exception org.orekit.errors.OrekitException
getMessage() - Method in exception org.orekit.errors.OrekitIllegalArgumentException
getMessage() - Method in exception org.orekit.errors.OrekitIllegalStateException
getMessage() - Method in exception org.orekit.errors.OrekitInternalError
getMessage() - Method in exception org.orekit.errors.OrekitIOException
getMessage() - Method in exception org.orekit.errors.OrekitParseException
getMessage() - Method in class org.orekit.gnss.rflink.gps.SubFrame
Get telemetry message.
getMessage(Locale) - Method in interface org.orekit.errors.LocalizedException
Gets the message in a specified locale.
getMessage(Locale) - Method in exception org.orekit.errors.OrekitException
Gets the message in a specified locale.
getMessage(Locale) - Method in exception org.orekit.errors.OrekitIllegalArgumentException
Gets the message in a specified locale.
getMessage(Locale) - Method in exception org.orekit.errors.OrekitIllegalStateException
Gets the message in a specified locale.
getMessage(Locale) - Method in exception org.orekit.errors.OrekitInternalError
Gets the message in a specified locale.
getMessage(Locale) - Method in exception org.orekit.errors.OrekitIOException
Gets the message in a specified locale.
getMessage(Locale) - Method in exception org.orekit.errors.OrekitParseException
Gets the message in a specified locale.
getMessageFor() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmHeader
Get the spacecraft name for which the CDM is provided stored in MESSAGE_FOR key.
getMessageId() - Method in class org.orekit.files.ccsds.section.Header
Get the ID that uniquely identifies a message from a given originator.
getMessageType(String) - Method in class org.orekit.gnss.metric.parser.IgsSsrMessagesParser
Get the message type corresponding to the message number.
getMessageType(String) - Static method in enum org.orekit.gnss.metric.parser.IgsSsrMessageType
Get the message type corresponding to a message number.
getMessageType(String) - Method in class org.orekit.gnss.metric.parser.MessagesParser
Get the message type corresponding to the message number.
getMessageType(String) - Method in class org.orekit.gnss.metric.parser.RtcmMessagesParser
Get the message type corresponding to the message number.
getMessageType(String) - Static method in enum org.orekit.gnss.metric.parser.RtcmMessageType
Get the message type corresponding to a message number.
getMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.acm.Acm
Get the metadata from the single segment.
getMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistory
Get metadata.
getMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistory
Get metadata.
getMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Apm
Get the file metadata.
getMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Ocm
Get the metadata from the single segment.
getMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistory
Get metadata.
getMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistory
Get metadata.
getMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory
Get metadata.
getMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.omm.Omm
Get the file metadata.
getMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm
Get the file metadata.
getMetadata() - Method in class org.orekit.files.ccsds.section.Segment
Get the segment metadata.
getMetadataObject1() - Method in class org.orekit.files.ccsds.ndm.cdm.Cdm
Get the file metadata.
getMetadataObject2() - Method in class org.orekit.files.ccsds.ndm.cdm.Cdm
Get the file metadata.
getMeteo(AbsoluteDate) - Method in class org.orekit.files.ilrs.CRD.Meteo
Get the meteorological parameters at a given date.
getMeteoData() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
Get the meteorological data for the data block.
getMeteorologicalId() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
Get the meteorological configuration ID.
getMeteorologicalRecord() - Method in class org.orekit.files.ilrs.CRDConfiguration
Get the meteorological record.
getMeteorologicalRecord(CRDConfiguration.SystemConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration
Get meteorological configuration record related to the systemRecord.
getMethod() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination
Get attitude determination method.
getMethod() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get orbit determination method.
getMethod() - Method in enum org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethodType
Get probability of collision method.
getMethodType() - Method in enum org.orekit.files.ccsds.definitions.PocMethodType
Get a probability of collision computing method type based on the short term encounter model.
getMHzFrequency() - Method in enum org.orekit.gnss.Frequency
Deprecated.
as of 12.1 replaced by Frequency.getFrequency()
getMilliInWeek() - Method in class org.orekit.time.GNSSDate
Get the number of milliseconds since week start.
getMinAlt() - Method in class org.orekit.models.earth.atmosphere.HarrisPriester
Get the minimal altitude for the model.
getMinAreaForCollisionProbability() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Get the minimum cross-sectional area for collision probability estimation purposes.
getMinDate() - Method in class org.orekit.attitudes.AggregateBoundedAttitudeProvider
 
getMinDate() - Method in interface org.orekit.attitudes.BoundedAttitudeProvider
Get the first date of the range.
getMinDate() - Method in class org.orekit.attitudes.TabulatedLofOffset
Get the first date of the range.
getMinDate() - Method in class org.orekit.attitudes.TabulatedProvider
Get the first date of the range.
getMinDate() - Method in class org.orekit.files.general.EphemerisSegmentPropagator
 
getMinDate() - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData
Gets the available data range minimum date.
getMinDate() - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityDataLoader
Gets the available data range minimum date.
getMinDate() - Method in class org.orekit.models.earth.atmosphere.data.DtcDataLoader
Gets the available data range minimum date.
getMinDate() - Method in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData
Gets the available data range minimum date.
getMinDate() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader
Gets the available data range minimum date.
getMinDate() - Method in interface org.orekit.models.earth.atmosphere.DTM2000InputParameters
Gets the available data range minimum date.
getMinDate() - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters
Gets the available data range minimum date.
getMinDate() - Method in interface org.orekit.models.earth.atmosphere.NRLMSISE00InputParameters
Gets the available data range minimum date.
getMinDate() - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
 
getMinDate() - Method in class org.orekit.propagation.analytical.Ephemeris
Get the first date of the range.
getMinDate() - Method in interface org.orekit.propagation.BoundedPropagator
Get the first date of the range.
getMinDate() - Method in interface org.orekit.propagation.FieldBoundedPropagator
Get the first date of the range.
getMinDate() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
Get the first date of the range.
getMinDate() - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Get the first date of the range.
getMinDate() - Method in class org.orekit.utils.AggregatedPVCoordinatesProvider
Get the first date of the range.
getMinElevation() - Method in class org.orekit.gnss.DOPComputer
Get the minimum elevation.
getMinElevation() - Method in class org.orekit.propagation.events.ElevationDetector
Returns the currently configured minimum valid elevation value.
getMinElevation() - Method in class org.orekit.propagation.events.FieldElevationDetector
Returns the currently configured minimum valid elevation value.
getMinimumValidDateForObservationPair(String, String) - Method in class org.orekit.files.sinex.Dcb
Get the minimum valid date for a given observation pair.
getMinimumValidDateForObservationPair(ObservationType, ObservationType) - Method in class org.orekit.files.sinex.Dcb
Get the minimum valid date for a given observation pair.
getMinMeasurementNumber() - Method in class org.orekit.estimation.measurements.gnss.AbstractCycleSlipDetector
Get the minimum number of measurement needed before being able to figure out cycle-slip occurrence.
getMinPredictedEigenMin() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get minimum predicted minor eigenvalue of 1σ positional error ellipsoid over entire time span of the OCM.
getMinRcs() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties
Get the minimum radar cross-section.
getMinute() - Method in class org.orekit.time.TimeComponents
Get the minute number.
getMinutesFromUTC() - Method in class org.orekit.time.TimeComponents
Get the offset between the specified date and UTC.
getMinValue() - Method in class org.orekit.utils.ParameterDriver
Get minimum parameter value.
getMisc() - Method in class org.orekit.gnss.metric.ntrip.Record
Get miscellaneous information.
getMissDistance() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the norm of relative position vector at TCA.
getMissionReferenceDate() - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder
Get the mission reference date or Mission Elapsed Time or Mission Relative Time time systems.
getMissionReferenceDate() - Method in class org.orekit.files.ccsds.ndm.adm.AdmParser
Get reference date for Mission Elapsed Time and Mission Relative Time time systems.
getMissionReferenceDate() - Method in class org.orekit.files.ccsds.ndm.odm.OdmParser
Get reference date for Mission Elapsed Time and Mission Relative Time time systems.
getMjd() - Method in class org.orekit.frames.EOPEntry
Get the entry date (modified julian day, 00h00 UTC scale).
getMJD() - Method in class org.orekit.time.AbsoluteDate
Return the given date as a Modified Julian Date expressed in UTC.
getMJD() - Method in class org.orekit.time.DateComponents
Get the modified julian day.
getMJD() - Method in class org.orekit.time.FieldAbsoluteDate
Return the given date as a Modified Julian Date expressed in UTC.
getMJD() - Method in class org.orekit.time.UTCTAIOffset
Get the date of the start of the leap as Modified Julian Day.
getMJD(TimeScale) - Method in class org.orekit.time.AbsoluteDate
Return the given date as a Modified Julian Date expressed in given timescale.
getMJD(TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate
Return the given date as a Modified Julian Date expressed in given timescale.
getMJDRef() - Method in class org.orekit.time.OffsetModel
Get the reference date of the linear model as a modified julian day.
getMoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext
Deprecated.
since 12.2 Use getMuoa() instead
getMoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext
Deprecated.
since 12.2 Use getMuoa() instead
getMOD(boolean) - Method in class org.orekit.frames.AbstractFrames
 
getMOD(boolean) - Method in interface org.orekit.frames.Frames
Get the MOD reference frame.
getMOD(boolean) - Static method in class org.orekit.frames.FramesFactory
Get the MOD reference frame.
getMOD(IERSConventions) - Method in class org.orekit.frames.AbstractFrames
 
getMOD(IERSConventions) - Method in interface org.orekit.frames.Frames
Get the MOD reference frame.
getMOD(IERSConventions) - Static method in class org.orekit.frames.FramesFactory
Get the MOD reference frame.
getMode() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the mode.
getModel() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Get the Jacobian of the function computing position/velocity at sample points.
getModel() - Method in class org.orekit.propagation.conversion.FiniteDifferencePropagatorConverter
Get the Jacobian of the function computing position/velocity at sample points.
getModel() - Method in class org.orekit.propagation.conversion.JacobianPropagatorConverter
Get the Jacobian of the function computing position/velocity at sample points.
getModelName() - Method in class org.orekit.models.earth.GeoMagneticField
Returns the model name.
getModels() - Method in class org.orekit.models.earth.GeoMagneticModelLoader
Returns a Collection of the GeoMagneticField models that have been successfully loaded.
getModels() - Method in class org.orekit.time.AggregatedClockModel
Get the underlying models.
getModifiedJulianDay() - Method in class org.orekit.files.sp3.SP3Header
Returns the modified julian day for this SP3 file.
getModifiedJulianEpoch() - Method in class org.orekit.time.AbstractTimeScales
 
getModifiedJulianEpoch() - Method in interface org.orekit.time.TimeScales
Reference epoch for modified julian dates: 1858-11-17T00:00:00 Terrestrial Time.
getModifiedJulianEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Reference epoch for modified julian dates: 1858-11-17T00:00:00 Terrestrial Time.
getModifiedRodrigues(double) - Method in class org.orekit.utils.AngularCoordinates
Convert rotation, rate and acceleration to modified Rodrigues vector and derivatives.
getModifiedRodrigues(double) - Method in class org.orekit.utils.FieldAngularCoordinates
Convert rotation, rate and acceleration to modified Rodrigues vector and derivatives.
getModifiers() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Get the modifiers that apply to a measurement.
getModifiers() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
Get the modifiers that apply to a measurement.
getModifiers() - Method in interface org.orekit.estimation.measurements.generation.MeasurementBuilder
Get the modifiers that apply to a measurement.
getModifiers() - Method in class org.orekit.estimation.measurements.generation.MultiplexedMeasurementBuilder
Get the modifiers that apply to a measurement.
getModifiers() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
Get the modifiers that apply to a measurement.
getMomentum() - Method in class org.orekit.utils.FieldPVCoordinates
Gets the momentum.
getMomentum() - Method in class org.orekit.utils.PVCoordinates
Gets the momentum.
getMomentumAlpha() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
Get the right ascension of angular momentum vector (rad).
getMomentumDelta() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
Get the declination of the angular momentum vector (rad).
getMonth() - Method in class org.orekit.time.DateComponents
Get the month.
getMonth(int) - Static method in enum org.orekit.time.Month
Get the month corresponding to a number.
getMonthEnum() - Method in class org.orekit.time.DateComponents
Get the month as an enumerate.
getMoon() - Method in interface org.orekit.bodies.CelestialBodies
Get the Moon singleton body.
getMoon() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Moon singleton body.
getMoon() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
 
getMoonSemiMajorAxis() - Static method in class org.orekit.propagation.numerical.cr3bp.CR3BPConstants
Get the Moon semi-major axis.
getMountPoint() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
Get the mount point.
getMu() - Method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointGravitationalTerm
Getter for the gravitational constant.
getMu() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Get the gravitational coefficient.
getMu() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmSatelliteEphemeris
Get the standard gravitational parameter for the satellite.
getMu() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory
Get the standard gravitational parameter for the satellite.
getMu() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSatelliteEphemeris
Get the standard gravitational parameter for the satellite.
getMu() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSegment
Get the standard gravitational parameter for the satellite.
getMu() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Get the gravitational coefficient.
getMu() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
Get the standard gravitational parameter for the satellite.
getMu() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris
Get the standard gravitational parameter for the satellite.
getMu() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
Get the standard gravitational parameter for the satellite.
getMu() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
Get the standard gravitational parameter for the satellite.
getMu() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris
Get the standard gravitational parameter for the satellite.
getMu() - Method in class org.orekit.files.sp3.SP3Ephemeris
Get the standard gravitational parameter for the satellite.
getMu() - Method in class org.orekit.files.sp3.SP3Segment
Get the standard gravitational parameter for the satellite.
getMu() - Method in class org.orekit.files.stk.STKEphemerisFile.STKEphemeris
 
getMu() - Method in class org.orekit.files.stk.STKEphemerisFile.STKEphemerisSegment
 
getMu() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Get the central attraction coefficient μ.
getMu() - Method in class org.orekit.forces.gravity.J2OnlyPerturbation
Getter for mu.
getMu() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
Get the central body attraction coefficient.
getMu() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get the central body attraction coefficient.
getMu() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider
Get the central body attraction coefficient.
getMu() - Method in class org.orekit.orbits.FieldOrbit
Get the central attraction coefficient used for position and velocity conversions (m³/s²).
getMu() - Method in class org.orekit.orbits.Orbit
Get the central acceleration constant.
getMu() - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Get the central attraction coefficient μ.
getMu() - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Get the central attraction coefficient μ.
getMu() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Getter for the Earth's universal gravitational parameter.
getMu() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
Gets the Earth's universal gravitational parameter.
getMu() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Get the central attraction coefficient (µ - m³/s²) value.
getMu() - Method in interface org.orekit.propagation.conversion.averaging.AveragedOrbitalState
Getter for the central body's gravitational constant.
getMu() - Method in class org.orekit.propagation.conversion.averaging.SGP4OrbitalState
Getter for the central body's gravitational constant.
getMu() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
Get the central attraction coefficient (µ - m³/s²) value.
getMu() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the central attraction coefficient.
getMu() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get the central attraction coefficient μ.
getMu() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get the central attraction coefficient μ.
getMu() - Method in class org.orekit.propagation.integration.FieldStateMapper
Get the central attraction coefficient μ.
getMu() - Method in class org.orekit.propagation.integration.StateMapper
Get the central attraction coefficient μ.
getMu() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext
Get central attraction coefficient.
getMu() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext
Get central attraction coefficient.
getMu() - Method in class org.orekit.propagation.SpacecraftState
Get the central attraction coefficient.
getMu(Field<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.forces.gravity.NewtonianAttraction
Get the central attraction coefficient μ.
getMu(AbsoluteDate) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Get the central attraction coefficient μ.
getMu(AbsoluteDate) - Method in class org.orekit.forces.gravity.NewtonianAttraction
Get the central attraction coefficient μ.
getMu(AbsoluteDate) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction
Get the central attraction coefficient μ at specific date.
getMU() - Static method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator
Get the Earth gravity coefficient used for GLONASS propagation.
getMU() - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator
Gets the Earth gravity coefficient used for GNSS propagation.
getMU() - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator
Get the Earth gravity coefficient used for SBAS propagation.
getMU() - Static method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
Get the Earth gravity coefficient used for TLE propagation.
getMU() - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator
Get the Earth gravity coefficient used for TLE propagation.
getMultipleMessageIndicator() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionHeader
Get the Multiple Message Indicator.
getMultiplexer() - Method in class org.orekit.propagation.AbstractPropagator
Get the multiplexer holding all step handlers.
getMultiplexer() - Method in class org.orekit.propagation.FieldAbstractPropagator
Get the multiplexer holding all step handlers.
getMultiplexer() - Method in interface org.orekit.propagation.FieldPropagator
Get the multiplexer holding all step handlers.
getMultiplexer() - Method in interface org.orekit.propagation.Propagator
Get the multiplexer holding all step handlers.
getMuoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTGravityContext
Get μ / a.
getMuoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTGravityContext
Get muoa = μ / a.
getMuoR3() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext
Get muoR3 = mu3 / R3.
getMuoR3() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext
Get muoR3 = mu3 / R3.
getMuSet() - Method in class org.orekit.files.ccsds.ndm.odm.OdmParser
Get the gravitational coefficient set at construction.
getN() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey
Get n.
getN4() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the four-year interval number starting from 1996.
getN4() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
 
getN4() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
 
getN4() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
Get the number of the current four year interval.
getNa() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
 
getNa() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
 
getNa() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
Get the number of the current day in a four year interval.
getNA() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the GLONASS NA Word.
getNadir() - Method in class org.orekit.bodies.FieldGeodeticPoint
Get the direction below the point, expressed in parent shape frame.
getNadir() - Method in class org.orekit.bodies.GeodeticPoint
Get the direction below the point, expressed in parent shape frame.
getNadir() - Method in class org.orekit.frames.TopocentricFrame
Get the nadir direction of topocentric frame, expressed in parent shape frame.
getName() - Method in interface org.orekit.bodies.CelestialBody
Get the name of the body.
getName() - Method in class org.orekit.bodies.CR3BPSystem
Get the name of the CR3BP system.
getName() - Method in class org.orekit.compiler.plugin.DefaultDataContextPlugin
 
getName() - Method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointDerivativesProvider
Getter for the name.
getName() - Method in class org.orekit.data.DataSource
Get the name of the data.
getName() - Method in class org.orekit.estimation.measurements.gnss.AbstractDualFrequencyCombination
Get the name of the combination of measurements.
getName() - Method in class org.orekit.estimation.measurements.gnss.AbstractSingleFrequencyCombination
Get the name of the combination of measurements.
getName() - Method in enum org.orekit.estimation.measurements.gnss.CombinationType
Get the name of the combination of measurements.
getName() - Method in interface org.orekit.estimation.measurements.gnss.MeasurementCombination
Get the name of the combination of measurements.
getName() - Method in class org.orekit.estimation.measurements.gnss.MelbourneWubbenaCombination
Get the name of the combination of measurements.
getName() - Method in class org.orekit.estimation.measurements.ObservableSatellite
Build a name for the satellite.
getName() - Method in class org.orekit.files.ccsds.definitions.BodyFacade
Get the CCSDS name for the body.
getName() - Method in enum org.orekit.files.ccsds.definitions.CelestialBodyFrame
Get the name of celestial body frame.
getName() - Method in class org.orekit.files.ccsds.definitions.FrameFacade
Get the CCSDS name for the frame.
getName() - Method in class org.orekit.files.ccsds.definitions.OdMethodFacade
Get the name of the method.
getName() - Method in class org.orekit.files.ccsds.definitions.PocMethodFacade
Get the name of the method.
getName() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Get the name of the block or entry.
getName() - Method in class org.orekit.files.ilrs.ILRSHeader
Get the satellite target name.
getName() - Method in class org.orekit.files.rinex.clock.RinexClock.ClockDataLine
Getter for the receiver/satellite name.
getName() - Method in enum org.orekit.files.sinex.Station.ReferenceSystem
Get the name used to define the reference system in SINEX file.
getName() - Method in class org.orekit.forces.maneuvers.jacobians.Duration
Get the name of the additional state.
getName() - Method in class org.orekit.forces.maneuvers.jacobians.MassDepletionDelay
Get the name of the additional derivatives (which will become state once integrated).
getName() - Method in class org.orekit.forces.maneuvers.jacobians.MedianDate
Get the name of the additional state.
getName() - Method in class org.orekit.forces.maneuvers.jacobians.TriggerDate
Get the name of the additional state.
getName() - Method in class org.orekit.forces.maneuvers.Maneuver
Get the name of the maneuver.
getName() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the maneuver name.
getName() - Method in class org.orekit.forces.maneuvers.propulsion.ProfileThrustPropulsionModel
Get the maneuver name.
getName() - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel
Get the maneuver name.
getName() - Method in class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers
Get the maneuver name.
getName() - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggers
Get the maneuver name.
getName() - Method in class org.orekit.frames.encounter.DefaultEncounterLOF
Get name of the local orbital frame.
getName() - Method in class org.orekit.frames.encounter.ValsecchiEncounterFrame
Get name of the local orbital frame.
getName() - Method in class org.orekit.frames.Frame
Get the name.
getName() - Method in enum org.orekit.frames.ITRFVersion
Get the name the frame version.
getName() - Method in class org.orekit.frames.LocalMagneticFieldFrame
Get name of the local orbital frame.
getName() - Method in interface org.orekit.frames.LOF
Get name of the local orbital frame.
getName() - Method in enum org.orekit.frames.LOFType
Get name of the local orbital frame.
getName() - Method in enum org.orekit.frames.Predefined
Get the name of the frame.
getName() - Method in enum org.orekit.gnss.antenna.SatelliteType
Get the IGS name for the antenna code.
getName() - Method in enum org.orekit.gnss.Frequency
Get the RINEX name for the frequency.
getName() - Method in class org.orekit.propagation.AbstractStateModifier
Get the name of the additional state.
getName() - Method in interface org.orekit.propagation.AdditionalStateProvider
Get the name of the additional state.
getName() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester
Get the name of the additional state.
getName() - Method in class org.orekit.propagation.analytical.gnss.ClockCorrectionsProvider
Get the name of the additional state.
getName() - Method in class org.orekit.propagation.FieldAbstractStateModifier
Get the name of the additional state.
getName() - Method in interface org.orekit.propagation.FieldAdditionalStateProvider
Get the name of the additional state.
getName() - Method in interface org.orekit.propagation.integration.AdditionalDerivativesProvider
Get the name of the additional derivatives (which will become state once integrated).
getName() - Method in interface org.orekit.propagation.integration.FieldAdditionalDerivativesProvider
Get the name of the additional derivatives (which will become state once integrated).
getName() - Method in class org.orekit.propagation.numerical.cr3bp.STMEquations
Get the name of the additional derivatives (which will become state once integrated).
getName() - Method in class org.orekit.propagation.numerical.EpochDerivativesEquations
Get the name of the additional derivatives (which will become state once integrated).
getName() - Method in class org.orekit.propagation.StateCovarianceMatrixProvider
Get the name of the additional state.
getName() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter2DPOCMethod
Get name of the method.
getName() - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod
Get name of the method.
getName() - Method in class org.orekit.time.ClockTimeScale
Get the name time scale.
getName() - Method in class org.orekit.time.ConstantOffsetTimeScale
Get the name time scale.
getName() - Method in class org.orekit.time.GLONASSScale
Get the name time scale.
getName() - Method in class org.orekit.time.GMSTScale
Get the name time scale.
getName() - Method in class org.orekit.time.SatelliteClockScale
Get the name time scale.
getName() - Method in class org.orekit.time.TCBScale
Get the name time scale.
getName() - Method in class org.orekit.time.TCGScale
Get the name time scale.
getName() - Method in class org.orekit.time.TDBScale
Get the name time scale.
getName() - Method in interface org.orekit.time.TimeScale
Get the name time scale.
getName() - Method in class org.orekit.time.UT1Scale
Get the name time scale.
getName() - Method in class org.orekit.time.UTCScale
Get the name time scale.
getName() - Method in class org.orekit.utils.ParameterDriver
Get parameter driver general name.
getName() - Method in class org.orekit.utils.units.Unit
Get the name of the unit.
getName(double) - Method in enum org.orekit.files.ccsds.ndm.adm.AttitudeType
Get the type name for a given format version.
getNameSpan(AbsoluteDate) - Method in class org.orekit.utils.ParameterDriver
Get name of the parameter span for a specific date.
getNamesSpanMap() - Method in class org.orekit.utils.ParameterDriver
Get current name span map of the parameterDriver, cut in interval in accordance with value span map and validity period.
getNarrowLaneCombination(SatelliteSystem) - Static method in class org.orekit.estimation.measurements.gnss.MeasurementCombinationFactory
Get the Narrow-Lane combination of measurements.
getNavigationMessageType() - Method in class org.orekit.files.rinex.navigation.TypeSvMessage
Get navigation message type.
getNavigationSystem(String) - Static method in enum org.orekit.gnss.metric.ntrip.NavigationSystem
Get the navigation system corresponding to a keyword.
getNavigationSystems() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
Get the navigation systems.
getNbInterpolationPoints() - Method in class org.orekit.time.AbstractFieldTimeInterpolator
Get the number of interpolation points.
getNbInterpolationPoints() - Method in class org.orekit.time.AbstractTimeInterpolator
Get the number of interpolation points.
getNbInterpolationPoints() - Method in interface org.orekit.time.FieldTimeInterpolator
Get the number of interpolation points.
getNbInterpolationPoints() - Method in interface org.orekit.time.TimeInterpolator
Get the number of interpolation points.
getNbManeuvers() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData
Get the number of maneuvers present in the APM.
getNbManeuvers() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm
Get the number of maneuvers present in the OPM.
getNbManeuvers() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData
Get the number of maneuvers present in the APM.
getNbObsPerSat() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Get an unmodifiable view of the map of number of observations per satellites.
getNBodyPerturbations() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get n-body perturbation bodies.
getNBodyPerturbations() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get n-body perturbation bodies.
getNbOfValues() - Method in class org.orekit.utils.ParameterDriver
Get the number of values to estimate that is to say the number.
getNbParametersDriversValue() - Method in interface org.orekit.utils.ParameterDriversProvider
Get total number of spans for all the parameters driver.
getNbParams() - Method in class org.orekit.utils.ParameterDriversList
Get the number of parameters with different names.
getNbSat() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Get number of satellites.
getNbSensorNoiseCovariance() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationSensor
Get number of noise elements for sensor.
getNbSpecies() - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
Get the number of species.
getNbStates() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination
getNbStates() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata
Get the number of data states included (attitude components plus rates components).
getNbTides(int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
Get the number of tides for one species.
getNbValuesToEstimate() - Method in class org.orekit.utils.ParameterDriversList
Get the number of values to estimate for parameters with different names.
getNdFilterValue() - Method in class org.orekit.files.ilrs.CRD.RangeSupplement
Get the neutral density (ND) filter value.
getNeighborList() - Method in class org.orekit.time.AbstractFieldTimeInterpolator.InterpolationData
Get neighbor list.
getNeighborList() - Method in class org.orekit.time.AbstractTimeInterpolator.InterpolationData
Get neighbor list.
getNeighbors(AbsoluteDate) - Method in interface org.orekit.utils.TimeStampedCache
Get the entries surrounding a central date.
getNeighbors(AbsoluteDate, int) - Method in class org.orekit.frames.EOPHistory
Get the entries surrounding a central date.
getNeighbors(AbsoluteDate, int) - Method in class org.orekit.utils.GenericTimeStampedCache
Get the entries surrounding a central date.
getNeighbors(AbsoluteDate, int) - Method in class org.orekit.utils.ImmutableTimeStampedCache
Get the entries surrounding a central date.
getNeighbors(AbsoluteDate, int) - Method in interface org.orekit.utils.TimeStampedCache
Get the entries surrounding a central date.
getNeighbors(FieldAbsoluteDate<KK>) - Method in interface org.orekit.utils.FieldTimeStampedCache
Get the entries surrounding a central date.
getNeighbors(FieldAbsoluteDate<KK>, int) - Method in interface org.orekit.utils.FieldTimeStampedCache
Get the entries surrounding a central date.
getNeighbors(FieldAbsoluteDate<KK>, int) - Method in class org.orekit.utils.ImmutableFieldTimeStampedCache
Get the entries surrounding a central date.
getNeighborsSize() - Method in class org.orekit.utils.FieldSortedListTrimmer
getNeighborsSize() - Method in class org.orekit.utils.SortedListTrimmer
getNeighborsSubList(AbsoluteDate, List<T>) - Method in class org.orekit.utils.SortedListTrimmer
Get the entries surrounding a central date.
getNeighborsSubList(FieldAbsoluteDate<K>, List<T>) - Method in class org.orekit.utils.FieldSortedListTrimmer
Get the entries surrounding a central date.
getNeptune() - Method in interface org.orekit.bodies.CelestialBodies
Get the Neptune singleton body.
getNeptune() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Neptune singleton body.
getNeptune() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
 
getNeQuickAlpha() - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Get the "alpha" ionospheric parameters.
getNequickGMessages() - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Get the ionosphere Nequick-G messages.
getNetwork() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
Get the network.
getNetworkIdentifier() - Method in class org.orekit.gnss.metric.ntrip.NetworkRecord
Get the network identifier.
getNetworkInfoAddress() - Method in class org.orekit.gnss.metric.ntrip.NetworkRecord
Get the web address for network information.
getNetworks() - Method in class org.orekit.gnss.metric.ntrip.SourceTable
Get the networks records.
getNewSlotQuantumGap() - Method in class org.orekit.utils.GenericTimeStampedCache
Get quantum gap above which a new slot is created instead of extending an existing one.
getNewState() - Method in class org.orekit.propagation.events.EventState.EventOccurrence
Get the new state for a reset action.
getNewState() - Method in class org.orekit.propagation.events.FieldEventState.EventOccurrence
Get the new state for a reset action.
getNewtonianAcceleration(double[]) - Method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointNewtonianTerm
Compute the Newtonian acceleration.
getNewtonianVelocityAdjointContribution(double[], double[]) - Method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointNewtonianTerm
Computes the generic term of a Newtonian attraction (central or not).
getNextLeapEpoch() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata
Get the epoch of next leap second.
getNextLeapEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the epoch of next leap second.
getNextLeapTaimutc() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata
Get the difference (TAI – UTC) in seconds incorporated at epoch AcmMetadata.getNextLeapEpoch().
getNextLeapTaimutc() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the difference (TAI – UTC) in seconds incorporated at epoch OcmMetadata.getNextLeapEpoch().
getNextMessageEpoch() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get Scheduled UTC epoch of the next CDM associated with the event identified by CONJUNCTION_ID.
getNextMessageEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the creation date of next message from a given originator.
getNextMessageID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the unique ID identifying next message from a given originator.
getNextParam() - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData.LocalSolarActivity
 
getNode(AbsoluteDate) - Method in interface org.orekit.bodies.IAUPole
Get the body Q Node direction in ICRF frame.
getNode(FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.IAUPole
Get the body Q Node direction in ICRF frame.
getNoise() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
Generate a noise vector.
getNominalFireRate() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
Get the nominal fire rate.
getNominalTidalDisplacement() - Method in enum org.orekit.utils.IERSConventions
Get the nominal values of the displacement numbers.
getNonInterpolatingProvider() - Method in interface org.orekit.frames.EOPBasedTransformProvider
Get a version of the provider that does not cache tidal corrections.
getNonInterpolatingProvider() - Method in class org.orekit.frames.GTODProvider
Get a version of the provider that does not cache tidal corrections.
getNonInterpolatingTransform(Frame, Frame, AbsoluteDate) - Static method in class org.orekit.frames.FramesFactory
Get the transform between two frames, suppressing all interpolation.
getNonInterpolatingTransform(Frame, Frame, FieldAbsoluteDate<T>) - Static method in class org.orekit.frames.FramesFactory
Get the transform between two frames, suppressing all interpolation.
getNonPolynomialSize() - Method in class org.orekit.data.PoissonSeries
Get the number of different terms in the non-polynomial part.
getNonRotatinOriginNutationCorrection(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory
Get the correction to the nutation parameters for Non-Rotating Origin paradigm.
getNonRotatinOriginNutationCorrection(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EOPHistory
Get the correction to the nutation parameters for Non-Rotating Origin paradigm.
getNoradId() - Method in class org.orekit.files.ilrs.ILRSHeader
Get the satellite NORAD ID (i.e.
getNoradID() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
Get the NORAD Catalog Number ("Satellite Number").
getNormal(FieldSpacecraftState<T>) - Method in class org.orekit.forces.FixedPanel
Get panel normal in spacecraft frame.
getNormal(FieldSpacecraftState<T>) - Method in class org.orekit.forces.Panel
Get panel normal in spacecraft frame.
getNormal(FieldSpacecraftState<T>) - Method in class org.orekit.forces.PointingPanel
Get panel normal in spacecraft frame.
getNormal(FieldSpacecraftState<T>) - Method in class org.orekit.forces.SlewingPanel
Get panel normal in spacecraft frame.
getNormal(SpacecraftState) - Method in class org.orekit.forces.FixedPanel
Get panel normal in spacecraft frame.
getNormal(SpacecraftState) - Method in class org.orekit.forces.Panel
Get panel normal in spacecraft frame.
getNormal(SpacecraftState) - Method in class org.orekit.forces.PointingPanel
Get panel normal in spacecraft frame.
getNormal(SpacecraftState) - Method in class org.orekit.forces.SlewingPanel
Get panel normal in spacecraft frame.
getNormalGravity(double) - Method in class org.orekit.models.earth.ReferenceEllipsoid
Gets the normal gravity, that is gravity just due to the reference ellipsoid's potential.
getNormalizedC20(AbsoluteDate) - Method in interface org.orekit.forces.gravity.potential.NormalizedSphericalHarmonicsProvider
Get the normalized coefficient of degree 2 and order 0 at a specific instance in time.
getNormalizedCnm(int, int) - Method in interface org.orekit.forces.gravity.potential.NormalizedSphericalHarmonicsProvider.NormalizedSphericalHarmonics
Get a spherical harmonic cosine coefficient.
getNormalizedProvider(double, double, TideSystem, double[][], double[][]) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Create a time-independent NormalizedSphericalHarmonicsProvider from canonical coefficients.
getNormalizedProvider(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Get the gravity field coefficients provider from the first supported file.
getNormalizedProvider(int, int) - Method in interface org.orekit.forces.gravity.potential.GravityFields
Get a gravity field normalized coefficients provider.
getNormalizedProvider(int, int) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
Get a gravity field normalized coefficients provider.
getNormalizedProvider(UnnormalizedSphericalHarmonicsProvider) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
getNormalizedSnm(int, int) - Method in interface org.orekit.forces.gravity.potential.NormalizedSphericalHarmonicsProvider.NormalizedSphericalHarmonics
Get a spherical harmonic sine coefficient.
getNormalizedValue() - Method in class org.orekit.utils.ParameterDriver
Get normalized value.
getNormalizedValue(AbsoluteDate) - Method in class org.orekit.utils.ParameterDriver
Get normalized value at specific date.
getNorth() - Method in class org.orekit.bodies.FieldGeodeticPoint
Get the direction to the north of point, expressed in parent shape frame.
getNorth() - Method in class org.orekit.bodies.GeodeticPoint
Get the direction to the north of point, expressed in parent shape frame.
getNorth() - Method in class org.orekit.frames.TopocentricFrame
Get the north direction of topocentric frame, expressed in parent shape frame.
getNorthOffsetDriver() - Method in class org.orekit.estimation.measurements.GroundStation
Get a driver allowing to change station position along North axis.
getNt() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the current date.
getNtripFlags() - Method in class org.orekit.gnss.metric.ntrip.SourceTable
Get the flags set by server.
getNumber() - Method in interface org.orekit.estimation.measurements.EstimationsProvider
Get the number of evaluations available.
getNumber() - Method in enum org.orekit.time.Month
Get the month number.
getNumberOfBiasesProcessed() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm05Data
Get the number of biases processed for the current satellite.
getNumberOfBiasesProcessed() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data
Get the number of biases processed for the current satellite.
getNumberOfClockDataTypes() - Method in class org.orekit.files.rinex.clock.RinexClock
Get the number of different clock data types in the file.
getNumberOfConstraints() - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPMultipleShooter
Get the total number of constraints.
getNumberOfConstraints() - Method in class org.orekit.utils.AbstractMultipleShooting
Get the total number of constraints.
getNumberOfEpochs() - Method in class org.orekit.files.sp3.SP3Header
Returns the number of epochs contained in this orbit file.
getNumberOfFreeComponents() - Method in class org.orekit.utils.AbstractMultipleShooting
Get the number of free state components.
getNumberOfIonosphericLayers() - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Header
Get the number of ionospheric layers.
getNumberOfLeapSeconds() - Method in class org.orekit.files.rinex.clock.RinexClock
Getter for the number of leap seconds.
getNumberOfLeapSeconds() - Method in class org.orekit.files.rinex.navigation.RinexNavigationHeader
Getter for the current number of leap seconds.
getNumberOfLeapSecondsGNSS() - Method in class org.orekit.files.rinex.clock.RinexClock
Getter for the number of leap second for GNSS time scales.
getNumberOfPointsRecorded() - Method in class org.orekit.files.ilrs.CRD.Calibration
Get the number of data points recorded.
getNumberOfPointsUsed() - Method in class org.orekit.files.ilrs.CRD.Calibration
Get the number of data points used.
getNumberOfRawRanges() - Method in class org.orekit.files.ilrs.CRD.NptRangeMeasurement
Get the umber of raw ranges (after editing) compressed into the normal point.
getNumberOfReceivers() - Method in class org.orekit.files.rinex.clock.RinexClock
Get the number of receivers that are considered in the file.
getNumberOfSatellites() - Method in class org.orekit.files.rinex.clock.RinexClock
Get the number of satellites that are considered in the file.
getNumberOfSatellites() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionHeader
Get the number of satellites for the current IGM message.
getNumberOfSatellites() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgmHeader
Get the number of satellites for the current IGM message.
getNumberOfValues() - Method in class org.orekit.files.rinex.clock.RinexClock.ClockDataLine
Getter for the number of values to follow.
getNumberSelectedMeasurementDrivers() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel
Get the number of estimated measurement parameters.
getNumberSelectedOrbitalDrivers() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel
Get the number of estimated orbital parameters.
getNumberSelectedPropagationDrivers() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel
Get the number of estimated propagation parameters.
getNutation() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
Get the nutation angle of spin axis (rad).
getNutationArguments(TimeScale) - Method in enum org.orekit.utils.IERSConventions
Get the fundamental nutation arguments.
getNutationArguments(TimeScale, TimeScales) - Method in enum org.orekit.utils.IERSConventions
Get the fundamental nutation arguments.
getNutationArguments(TimeScales) - Method in enum org.orekit.utils.IERSConventions
Get the fundamental nutation arguments.
getNutationCorrectionConverter() - Method in enum org.orekit.utils.IERSConventions
Create a function converting nutation corrections between δX/δY and δΔψ/δΔε.
getNutationCorrectionConverter(TimeScales) - Method in enum org.orekit.utils.IERSConventions
Create a function converting nutation corrections between δX/δY and δΔψ/δΔε.
getNutationFunction() - Method in enum org.orekit.utils.IERSConventions
Get the function computing the nutation angles.
getNutationFunction(TimeScales) - Method in enum org.orekit.utils.IERSConventions
Get the function computing the nutation angles.
getNutationPeriod() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
Get the body nutation period of the spin axis (s).
getNutationPhase() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
Get the inertial nutation phase (rad).
getNutationReferenceEpoch() - Method in enum org.orekit.utils.IERSConventions
Get the reference epoch for fundamental nutation arguments.
getNutationReferenceEpoch(TimeScales) - Method in enum org.orekit.utils.IERSConventions
Get the reference epoch for fundamental nutation arguments.
getNutationVel() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
Get the angular velocity of spin vector around angular momentum vector.
getNutLn() - Method in class org.orekit.files.sinex.SinexEopEntry
Get the nutation correction in longitude.
getNutOb() - Method in class org.orekit.files.sinex.SinexEopEntry
Get the nutation correction in obliquity.
getNutX() - Method in class org.orekit.files.sinex.SinexEopEntry
Get the nutation correction X.
getNutY() - Method in class org.orekit.files.sinex.SinexEopEntry
Get the nutation correction Y.
getObject() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get the object name for which metadata are given.
getObjectDesignator() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata
Get the unique satellite identification designator for the object.
getObjectDesignator() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get the object satellite catalog designator for which metadata are given.
getObjectDesignator() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the unique satellite identification designator for the object.
getObjectID() - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata
Get the spacecraft ID for which the attitude data are provided.
getObjectID() - Method in class org.orekit.files.ccsds.ndm.odm.OdmCommonMetadata
Get the spacecraft ID for which the orbit state is provided.
getObjectiveFunction() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Get the function computing position/velocity at sample points.
getObjectiveFunction() - Method in class org.orekit.propagation.conversion.FiniteDifferencePropagatorConverter
Get the function computing position/velocity at sample points.
getObjectiveFunction() - Method in class org.orekit.propagation.conversion.JacobianPropagatorConverter
Get the function computing position/velocity at sample points.
getObjectName() - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata
Get the spacecraft name for which the attitude data are provided.
getObjectName() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get the spacecraft name for the object.
getObjectName() - Method in class org.orekit.files.ccsds.ndm.odm.OdmMetadata
Get the spacecraft name for which the orbit state is provided.
getObjectOrbitFromCdm(CdmRelativeMetadata, CdmData, CdmMetadata, DataContext) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter2DPOCMethod
Extract collision object spacecraft state from given Conjunction Data Message data.
getObjectStateCovarianceFromCdm(CdmRelativeMetadata, CdmData) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter2DPOCMethod
Get collision object state covariance from given Conjunction Data Message data.
getObjectType() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get the type of object.
getObjectType() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the type of object.
getOblateFlattening() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get central body oblate spheroid oblateness.
getObsAvailable() - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters
Get the number of observations available for the OD of the object.
getObsAvailable() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get number of observations available within the actual OD span.
getObsBeforeNextMessage() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get the flag indicating whether new tracking observations are anticipated prior to the issue of the next CDM associated with the event specified by CONJUNCTION_ID.
getObservationCode() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Get the observation code of the average phasecenter position w/r to antenna reference point.
getObservationData() - Method in class org.orekit.estimation.measurements.gnss.CombinedObservationDataSet
Get list of observation data.
getObservationData() - Method in class org.orekit.files.rinex.observation.ObservationDataSet
Get list of observation data.
getObservationDataSets() - Method in class org.orekit.files.rinex.observation.RinexObservation
Get an unmodifiable view of the observations.
getObservations() - Method in class org.orekit.files.ccsds.ndm.tdm.ObservationsBlock
Get the list of Observations data lines.
getObservationSampling() - Method in class org.orekit.files.sinex.DcbDescription
Get the observation sampling interval used for data analysis.
getObservationTimeScale() - Method in enum org.orekit.gnss.SatelliteSystem
Get observation time scale for satellite system.
getObservationType() - Method in class org.orekit.files.rinex.observation.ObservationData
Get the observation type.
getObservedLineOfSight(Frame) - Method in class org.orekit.estimation.measurements.AngularAzEl
Calculate the Line Of Sight of the given measurement.
getObservedLineOfSight(Frame) - Method in class org.orekit.estimation.measurements.AngularRaDec
Calculate the Line Of Sight of the given measurement.
getObservedMeasurement() - Method in class org.orekit.estimation.measurements.EstimatedMeasurementBase
Get the associated observed measurement.
getObservedMeasurement() - Method in class org.orekit.estimation.sequential.MeasurementDecorator
Get the observed measurement.
getObservedValue() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Get the observed value.
getObservedValue() - Method in interface org.orekit.estimation.measurements.ComparableMeasurement
Get the observed value.
getObservedValue() - Method in class org.orekit.estimation.measurements.EstimatedMeasurementBase
Get the observed value.
getObserver() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Get the observer for Kalman Filter estimations.
getObserver() - Method in interface org.orekit.estimation.sequential.SemiAnalyticalProcess
Get the observer for Kalman Filter estimations.
getObserver() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel
Get the observer for Kalman Filter estimations.
getObserver() - Method in class org.orekit.propagation.events.AngularSeparationDetector
Get the observer for the spacecraft.
getObserverName() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Get name of the observer.
getObservers() - Method in class org.orekit.utils.ParameterDriver
Get the observers for this driver.
getObsUsed() - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters
Get the number of observations accepted for the OD of the object.
getObsUsed() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get number of observations accepted within the actual OD span.
getOccultationEngine() - Method in class org.orekit.propagation.events.EclipseDetector
Get the occultation engine.
getOccultationEngine() - Method in class org.orekit.propagation.events.FieldEclipseDetector
Get the occultation engine.
getOcculted() - Method in class org.orekit.utils.OccultationEngine
Getter for the occulted body.
getOccultedApparentRadius() - Method in class org.orekit.utils.OccultationEngine.FieldOccultationAngles
Get apparent radius of occulted body.
getOccultedApparentRadius() - Method in class org.orekit.utils.OccultationEngine.OccultationAngles
Get apparent radius of occulted body.
getOccultedBody() - Method in class org.orekit.forces.radiation.AbstractLightFluxModel
Getter for the occulted body's position provider.
getOccultedBodyPosition(AbsoluteDate, Frame) - Method in class org.orekit.forces.radiation.AbstractLightFluxModel
Method computing the occulted body's position at a given date and frame.
getOccultedBodyPosition(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.forces.radiation.AbstractLightFluxModel
Method computing the occulted body's position at a given date and frame.
getOccultedRadius() - Method in class org.orekit.utils.OccultationEngine
Getter for the occultedRadius.
getOcculting() - Method in class org.orekit.utils.OccultationEngine
Getter for the occulting body.
getOccultingBodies() - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel
Get all occulting bodies to consider.
getOccultingBodyRadius() - Method in class org.orekit.forces.radiation.AbstractSolarLightFluxModel
Getter for occulting body radius.
getOccultingBodyRadius() - Method in class org.orekit.propagation.events.CylindricalShadowEclipseDetector
Getter for occulting body radius.
getOccultingBodyRadius() - Method in class org.orekit.propagation.events.FieldCylindricalShadowEclipseDetector
Getter for occulting body radius.
getOceanLoadDeformationCoefficients() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Get the configured ocean load deformation coefficients.
getOceanLoadDeformationCoefficients() - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
Get the configured ocean load deformation coefficients.
getOceanPoleTide(EOPHistory) - Method in enum org.orekit.utils.IERSConventions
Get the function computing ocean pole tide (ΔC₂₁, ΔS₂₁).
getOceanTidesModel() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get ocean tides model.
getOceanTidesWaves(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Get the ocean tides waves from the first supported file.
getOceanTidesWaves(int, int) - Method in interface org.orekit.forces.gravity.potential.GravityFields
Get the ocean tides waves.
getOceanTidesWaves(int, int) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
Get the ocean tides waves.
getOcmDataElements() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the list of elements of information data blocks included in this message.
getOdEpoch() - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters
Get the epoch of the orbit determination used for this message.
getOdmMessageLink() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata
Get the Unique identifier of Orbit Data Message linked to this Attitude Data Message.
getOdmMsgLink() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get the unique identifier of Orbit Data Message(s) that are linked (relevant) to this Conjunction Data Message.
getODParametersBlock() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmData
Get the OD parameters logical block.
getOebAreaAlongIntermediate() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties
Get the cross-sectional area of Optimally Enclosing Box when viewed along the intermediate OEB direction.
getOebAreaAlongMax() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties
Get the cross-sectional area of Optimally Enclosing Box when viewed along the maximum OEB direction.
getOebAreaAlongMin() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties
Get the cross-sectional area of Optimally Enclosing Box when viewed along the minimum OEB direction.
getOebIntermediate() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties
Get the intermediate physical dimension of the OEB.
getOebMax() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties
Get the maximum physical dimension of the OEB.
getOebMin() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties
Get the minimum physical dimension of the OEB.
getOebParentFrame() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties
Get the Optimally Enclosing Box parent reference frame.
getOebParentFrameEpoch() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties
Get the Optimally Enclosing Box parent reference frame epoch.
getOebQ() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties
Get the quaternion defining Optimally Enclosing Box.
getOffset() - Method in class org.orekit.attitudes.LofOffset
Get the rotational offset.
getOffset() - Method in class org.orekit.time.ClockOffset
Get offset.
getOffset() - Method in class org.orekit.time.FieldClockOffset
Get offset.
getOffset() - Method in class org.orekit.time.OffsetModel
Offset at reference date in seconds (TAI minus UTC).
getOffset(AbsoluteDate) - Method in class org.orekit.estimation.measurements.QuadraticClockModel
Get the clock offset at date.
getOffset(AbsoluteDate) - Method in class org.orekit.time.AggregatedClockModel
Get the clock offset at date.
getOffset(AbsoluteDate) - Method in interface org.orekit.time.ClockModel
Get the clock offset at date.
getOffset(AbsoluteDate) - Method in class org.orekit.time.PerfectClockModel
Get the clock offset at date.
getOffset(AbsoluteDate) - Method in class org.orekit.time.SampledClockModel
Get the clock offset at date.
getOffset(AbsoluteDate) - Method in class org.orekit.time.UTCTAIOffset
Get the TAI - UTC offset in seconds.
getOffset(DateComponents, TimeComponents) - Method in class org.orekit.time.UTCTAIOffset
Get the TAI - UTC offset in seconds.
getOffset(FieldAbsoluteDate<T>) - Method in class org.orekit.estimation.measurements.QuadraticClockModel
Get the clock offset at date.
getOffset(FieldAbsoluteDate<T>) - Method in class org.orekit.estimation.measurements.QuadraticFieldClockModel
Get the clock offset at date.
getOffset(FieldAbsoluteDate<T>) - Method in class org.orekit.time.AggregatedClockModel
Get the clock offset at date.
getOffset(FieldAbsoluteDate<T>) - Method in interface org.orekit.time.ClockModel
Get the clock offset at date.
getOffset(FieldAbsoluteDate<T>) - Method in class org.orekit.time.PerfectClockModel
Get the clock offset at date.
getOffset(FieldAbsoluteDate<T>) - Method in class org.orekit.time.SampledClockModel
Get the clock offset at date.
getOffset(FieldAbsoluteDate<T>) - Method in class org.orekit.time.UTCTAIOffset
Get the TAI - UTC offset in seconds.
getOffsetGeodeticPoint(AbsoluteDate) - Method in class org.orekit.estimation.measurements.GroundStation
Get the geodetic point at the center of the offset frame.
getOffsetGeodeticPoint(FieldAbsoluteDate<T>) - Method in class org.orekit.estimation.measurements.GroundStation
Get the geodetic point at the center of the offset frame.
getOffsetToInertial(Frame, AbsoluteDate, boolean) - Method in class org.orekit.estimation.measurements.GroundStation
Get the transform between offset frame and inertial frame.
getOffsetToInertial(Frame, AbsoluteDate, int, Map<String, Integer>) - Method in class org.orekit.estimation.measurements.GroundStation
Get the transform between offset frame and inertial frame with derivatives.
getOffsetToInertial(Frame, FieldAbsoluteDate<Gradient>, int, Map<String, Integer>) - Method in class org.orekit.estimation.measurements.GroundStation
Get the transform between offset frame and inertial frame with derivatives.
getOffsetToInertialDownlink() - Method in class org.orekit.estimation.measurements.GroundReceiverCommonParametersWithDerivatives
Get transform between station and inertial frame.
getOffsetToInertialDownlink() - Method in class org.orekit.estimation.measurements.GroundReceiverCommonParametersWithoutDerivatives
Get transform between station and inertial frame.
getOmega() - Method in class org.orekit.data.DelaunayArguments
Get the mean longitude of the ascending node of the Moon.
getOmega() - Method in class org.orekit.data.FieldDelaunayArguments
Get the mean longitude of the ascending node of the Moon.
getOmega0() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Getter for the longitude of ascending node of orbit plane at weekly epoch.
getOmega0() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
Gets the Longitude of Ascending Node of Orbit Plane at Weekly Epoch.
getOmegaDot() - Method in class org.orekit.data.DelaunayArguments
Get the mean longitude of the ascending node of the Moon time derivative.
getOmegaDot() - Method in class org.orekit.data.FieldDelaunayArguments
Get the mean longitude of the ascending node of the Moon time derivative.
getOmegaDot() - Method in class org.orekit.gnss.rflink.gps.SubFrame3
Get dot(Ω).
getOmegaDot() - Method in class org.orekit.gnss.rflink.gps.SubFrameAlmanac
Get dot(Ω).
getOmegaDot() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Getter for the rate of right ascension.
getOmegaDot() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
Gets the Rate of Right Ascension.
getOne() - Method in class org.orekit.orbits.FieldOrbit
Getter for Field-valued one.
getOne() - Method in class org.orekit.time.AbstractFieldTimeInterpolator.InterpolationData
Get one.
getOneLetterCode() - Method in enum org.orekit.gnss.TimeSystem
Get the one letter code.
getOneWayDistance() - Method in class org.orekit.files.ilrs.CRD.Calibration
Get the one-way target distance (nominal).
getOOA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext
Get ooA = 1 / A.
getOOA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext
Get ooA = 1 / A.
getOoAB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTGravityContext
ooAB = 1 / (A * B).
getOoAB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext
Get ooAB = 1 / (A * B).
getOoAB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTGravityContext
Get ooAB = 1 / (A * B).
getOoAB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext
Get ooAB = 1 / (A * B).
getOOAB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext
Get ooAB = 1 / (A * B).
getOOAB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext
Get ooAB = 1 / (A * B).
getOoBpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext
Get ooBpo = 1 / (B + 1).
getOoBpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext
Get ooBpo = 1 / (B + 1).
getOoMU() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext
Get ooMu = 1 / mu.
getOoMU() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext
Get ooMu = 1 / mu.
getOON2A2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
Get 1 / (n² * a²).
getOON2A2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
Get 1 / (n² * a²).
getOpener() - Method in class org.orekit.data.DataSource
Get the data stream opener.
getOperator() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the operator of the space object.
getOperator() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord
Get the institution/agency/company operating the caster.
getOperator() - Method in class org.orekit.gnss.metric.ntrip.NetworkRecord
Get the institution/agency/company operating the caster.
getOperatorContactPosition() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get the contact position of the owner / operator of the object.
getOperatorEmail() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get the email of the operator of the object.
getOperatorOrganization() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get the contact organisation of the object.
getOperatorPhone() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get the contact phone of the operator of the object.
getOpsStatus() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the operational status.
getOptimum() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Get the optimum found.
getOrbAveraging() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Get type of averaging (Osculating, mean Brouwer, other.
getOrbit() - Method in class org.orekit.orbits.WalkerConstellationSlot
Get the orbit.
getOrbit() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the current orbit.
getOrbit() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the orbit.
getOrbit() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get the orbit.
getOrbit() - Method in class org.orekit.propagation.SpacecraftState
Get the current orbit.
getOrbitalElements() - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator
Get the underlying GNSS orbital elements.
getOrbitalParametersDrivers() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Get the drivers for the configurable orbital parameters.
getOrbitalParametersDrivers() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
Get the drivers for the configurable orbital parameters.
getOrbitalParametersDrivers(boolean) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Get the orbital parameters supported by this estimator.
getOrbitalParametersDrivers(boolean) - Method in class org.orekit.estimation.sequential.AbstractKalmanEstimator
Get the orbital parameters supported by this estimator.
getOrbitalPeriod() - Method in class org.orekit.orbits.CR3BPDifferentialCorrection
Get the orbital period of the required orbit.
getOrbitalPeriod() - Method in class org.orekit.orbits.LibrationOrbit
Return the orbital period of the libration orbit.
getOrbitCategory() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the orbit category.
getOrbitCenter() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get the central body for object 1 and 2.
getOrbitCorrection() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCombinedCorrectionData
Get the orbit correction data.
getOrbitCorrection() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmOrbitCorrectionData
Get the orbit correction data.
getOrbitCorrection() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01Data
Get the orbit correction data.
getOrbitCorrection() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Data
Get the orbit correction data.
getOrbitDeterminationBlock() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmData
Get orbit determination logical block.
getOrbitInterpolator() - Method in class org.orekit.propagation.AbstractStateCovarianceInterpolator
Get orbit interpolator.
getOrbitInterpolator() - Method in class org.orekit.propagation.FieldSpacecraftStateInterpolator
Get orbit interpolator.
getOrbitInterpolator() - Method in class org.orekit.propagation.SpacecraftStateInterpolator
Get orbit interpolator.
getOrbitPeriod() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext
Get the Keplerian period.
getOrbitPeriod() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext
Get the Keplerian period.
getOrbitRadius() - Method in class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElementsPropagator
Get the computed satellite's orbit.
getOrbitRadius() - Method in class org.orekit.propagation.analytical.intelsat.IntelsatElevenElementsPropagator
Get the computed satellite's orbit.
getOrbitType() - Method in class org.orekit.files.sp3.SP3Header
Returns the SP3OrbitType for this SP3 file.
getOrbitType() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester
Get the orbit type used for the matrix computation.
getOrbitType() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Get the orbit type expected for the 6 first parameters in PropagatorBuilder.buildPropagator(double[]).
getOrbitType() - Method in interface org.orekit.propagation.conversion.averaging.AveragedOrbitalState
Getter for the averaged orbit type.
getOrbitType() - Method in class org.orekit.propagation.conversion.averaging.BrouwerLyddaneOrbitalState
Getter for the averaged orbit type.
getOrbitType() - Method in class org.orekit.propagation.conversion.averaging.DSST6X0OrbitalState
Getter for the averaged orbit type.
getOrbitType() - Method in class org.orekit.propagation.conversion.averaging.EcksteinHechlerOrbitalState
Getter for the averaged orbit type.
getOrbitType() - Method in class org.orekit.propagation.conversion.averaging.SGP4OrbitalState
Getter for the averaged orbit type.
getOrbitType() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
Get the orbit type expected for the 6 first parameters in PropagatorBuilder.buildPropagator(double[]).
getOrbitType() - Method in class org.orekit.propagation.events.PositionAngleDetector
Get the orbit type defining the angle type.
getOrbitType() - Method in class org.orekit.propagation.FieldStateCovariance
Get the covariance orbit type.
getOrbitType() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get propagation parameter type.
getOrbitType() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get propagation parameter type.
getOrbitType() - Method in class org.orekit.propagation.integration.FieldStateMapper
Get propagation parameter type.
getOrbitType() - Method in class org.orekit.propagation.integration.StateMapper
Get propagation parameter type.
getOrbitType() - Method in interface org.orekit.propagation.MatricesHarvester
Get the orbit type used for the matrix computation.
getOrbitType() - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Get propagation parameter type.
getOrbitType() - Method in class org.orekit.propagation.numerical.NumericalPropagator
Get propagation parameter type.
getOrbitType() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester
Get the orbit type used for the matrix computation.
getOrbitType() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Get propagation parameter type.
getOrbitType() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Get propagation parameter type.
getOrbitType() - Method in class org.orekit.propagation.StateCovariance
Get the covariance orbit type.
getOrbitTypeKey() - Method in class org.orekit.files.sp3.SP3Header
Returns the orbit type key for this SP3 file.
getOrbRevNum() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Get the integer orbit revolution number.
getOrbRevNumBasis() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Get the basis for orbit revolution number.
getOrdinateGrid() - Method in class org.orekit.utils.InterpolationTableLoader
Returns a copy of the ordinate grid for the interpolation function.
getOrientation() - Method in class org.orekit.attitudes.Attitude
Get the complete orientation including spin.
getOrientation() - Method in class org.orekit.attitudes.FieldAttitude
Get the complete orientation including spin.
getOrigin() - Method in enum org.orekit.frames.HelmertTransformation.Predefined
Get the origin ITRF.
getOrigin() - Method in class org.orekit.frames.ITRFVersion.Converter
Get the origin ITRF.
getOriginal() - Method in class org.orekit.propagation.events.FieldNegateDetector
Get the delegate event detector.
getOriginal() - Method in class org.orekit.propagation.events.NegateDetector
Get the delegate event detector.
getOriginalEstimatedValue() - Method in class org.orekit.estimation.measurements.EstimatedMeasurementBase
Get the original estimated value prior to any modification.
getOriginator() - Method in class org.orekit.files.ccsds.section.Header
Get the message originator.
getOriginatorAddress() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata
Get the address of Programmatic Point Of Contact at originator.
getOriginatorAddress() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the address of Programmatic Point Of Contact at originator.
getOriginatorEmail() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata
Get the email address of Programmatic Point Of Contact at originator.
getOriginatorEmail() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the email address of Programmatic Point Of Contact at originator.
getOriginatorPhone() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata
Get the phone number of Programmatic Point Of Contact at originator.
getOriginatorPhone() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the phone number of Programmatic Point Of Contact at originator.
getOriginatorPOC() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata
Get the programmatic Point Of Contact at originator.
getOriginatorPOC() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the programmatic Point Of Contact at originator.
getOriginatorPosition() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata
Get the position of Programmatic Point Of Contact at originator.
getOriginatorPosition() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the position of Programmatic Point Of Contact at originator.
getOriginIndicator() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement
Get the angle origin indicator.
getOriginOfValues() - Method in class org.orekit.files.ilrs.CRD.MeteorologicalMeasurement
Get the origin of values.
getOther() - Method in class org.orekit.frames.encounter.AbstractEncounterLOF
Get the normal version of other's position and velocity coordinates.
getOther() - Method in interface org.orekit.frames.encounter.EncounterLOF
Get other's position and velocity coordinates.
getOtherAtTCA() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Get other's orbit at time of closest approach.
getOtherAtTCA() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition
Get other's orbit at time of closest approach.
getOtherCovariance() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Get other's covariance.
getOtherCovariance() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition
Get other's covariance.
getOutFrame() - Method in class org.orekit.propagation.AbstractStateCovarianceInterpolator
Get output frame.
getOutLOF() - Method in class org.orekit.propagation.AbstractStateCovarianceInterpolator
Get output local orbital frame.
getOutOrbitType() - Method in class org.orekit.propagation.AbstractStateCovarianceInterpolator
Get output orbit type.
getOutPositionAngleType() - Method in class org.orekit.propagation.AbstractStateCovarianceInterpolator
Get output position angle type.
getOutputFrame() - Method in class org.orekit.propagation.FieldSpacecraftStateInterpolator
Get output frame.
getOutputFrame() - Method in class org.orekit.propagation.SpacecraftStateInterpolator
Get output frame.
getOutputFrame() - Method in class org.orekit.utils.AbsolutePVCoordinatesHermiteInterpolator
Get output frame for the interpolated instance.
getOutputFrame() - Method in class org.orekit.utils.FieldAbsolutePVCoordinatesHermiteInterpolator
Get output frame for the interpolated instance.
getOutputInertialFrame() - Method in class org.orekit.orbits.AbstractFieldOrbitInterpolator
Get output inertial frame.
getOutputInertialFrame() - Method in class org.orekit.orbits.AbstractOrbitInterpolator
Get output inertial frame.
getOutputName() - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Get the name of the output (for error messages).
getOutputName() - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Get the name of the output (for error messages).
getOutputPulseType() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Get the output pulse type.
getOutputPulseWidth() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Get the output pulse width.
getOwner() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the owner of the space object.
getP() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the GLONASS P Word.
getP() - Method in class org.orekit.orbits.WalkerConstellation
Get the number of orbital planes.
getP() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the y component of inclination vector.
getP() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get the y component of inclination vector.
getP1() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the GLONASS P1 Word.
getP2() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the GLONASS P2 Word.
getP3() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the GLONASS P3 Word.
getP4() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the GLONASS P4 Word.
getPa() - Method in class org.orekit.data.BodiesElements
Get the general accumulated precession in longitude.
getPa() - Method in class org.orekit.data.FieldBodiesElements
Get the general accumulated precession in longitude.
getPa() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Get the orbit argument of pericenter.
getPa() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Getter for the argument of perigee.
getPa() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
 
getPa() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
Get the Argument of Perigee.
getPa() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
Gets the Argument of Perigee.
getPaDot() - Method in class org.orekit.data.BodiesElements
Get the general accumulated precession in longitude time derivative.
getPaDot() - Method in class org.orekit.data.FieldBodiesElements
Get the general accumulated precession in longitude time derivative.
getPanels() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Get the panels composing the body.
getParameterDerivatives(ParameterDriver) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Get the partial derivatives of the simulated measurement with respect to a parameter.
getParameterDerivatives(ParameterDriver, AbsoluteDate) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Get the partial derivatives of the simulated measurement with respect to a parameter.
getParameterDriver(String) - Method in interface org.orekit.utils.ParameterDriversProvider
Get parameter value from its name.
getParameters() - Method in class org.orekit.files.ccsds.ndm.odm.UserDefined
Get all user defined parameters.
getParameters() - Method in interface org.orekit.utils.ParameterDriversProvider
Get model parameters.
getParameters(Field<T>) - Method in interface org.orekit.utils.ParameterDriversProvider
Get model parameters.
getParameters(Field<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.utils.ParameterDriversProvider
Get model parameters.
getParameters(FieldSpacecraftState<Gradient>, ParameterDriversProvider) - Method in class org.orekit.propagation.integration.AbstractGradientConverter
Get the parametric model parameters, return gradient values for each span of each driver (several gradient values for each parameter).
getParameters(AbsoluteDate) - Method in interface org.orekit.utils.ParameterDriversProvider
Get model parameters.
getParametersAllValues() - Method in interface org.orekit.utils.ParameterDriversProvider
Get model parameters, return a list a all span values of all parameters.
getParametersAllValues(Field<T>) - Method in interface org.orekit.utils.ParameterDriversProvider
Get model parameters.
getParametersAtStateDate(FieldSpacecraftState<Gradient>, ParameterDriversProvider) - Method in class org.orekit.propagation.integration.AbstractGradientConverter
Get the parametric model parameters, return gradient values at state date for each driver (only 1 gradient value for each parameter).
getParametersDrivers() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.gnss.AbstractWindUp
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.AberrationModifier
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.AbstractRelativisticClockOnBoardRangeRateModifier
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.AngularIonosphericDelayModifier
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.AngularRadioRefractionModifier
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.AngularTroposphericDelayModifier
Deprecated.
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeIonosphericDelayModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeRateIonosphericDelayModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeRateTroposphericDelayModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeTroposphericDelayModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.Bias
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.InterSatellitesPhaseAmbiguityModifier
Deprecated.
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaInterSatellitesPhaseModifier
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaInterSatellitesRangeModifier
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaOneWayGNSSPhaseModifier
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaOneWayGNSSRangeModifier
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaTurnAroundRangeModifier
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OneWayGNSSPhaseAmbiguityModifier
Deprecated.
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OutlierFilter
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.PhaseAmbiguityModifier
Deprecated.
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.PhaseCentersPhaseModifier
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.PhaseCentersRangeModifier
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.PhaseIonosphericDelayModifier
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.PhaseTroposphericDelayModifier
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockInterSatellitesPhaseModifier
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockInterSatellitesRangeModifier
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockOneWayGNSSPhaseModifier
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockOneWayGNSSRangeModifier
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockPhaseModifier
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockRangeModifier
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockRangeRateModifier
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockInterSatellitesPhaseModifier
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockInterSatellitesRangeModifier
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockOneWayGNSSPhaseModifier
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockOneWayGNSSRangeModifier
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockPhaseModifier
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockRangeModifier
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.ShapiroInterSatellitePhaseModifier
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.ShapiroInterSatelliteRangeModifier
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.ShapiroOneWayGNSSPhaseModifier
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.ShapiroOneWayGNSSRangeModifier
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.ShapiroPhaseModifier
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.ShapiroRangeModifier
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.TDOAIonosphericDelayModifier
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.TDOATroposphericDelayModifier
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.TurnAroundRangeIonosphericDelayModifier
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.TurnAroundRangeTroposphericDelayModifier
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.drag.DragForce
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.drag.TimeSpanDragForce
Deprecated.
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.empirical.HarmonicAccelerationModel
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.empirical.ParametricAcceleration
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.empirical.PolynomialAccelerationModel
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.AbstractBodyAttraction
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.DeSitterRelativity
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.J2OnlyPerturbation
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.LenseThirringRelativity
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.NewtonianAttraction
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.OceanTides
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.Relativity
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.SolidTides
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.inertia.InertialForces
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.maneuvers.Maneuver
 
getParametersDrivers() - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.maneuvers.propulsion.ProfileThrustPropulsionModel
 
getParametersDrivers() - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.radiation.ECOM2
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.radiation.RadiationPressureModel
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.ionosphere.EstimatedIonosphericModel
 
getParametersDrivers() - Method in class org.orekit.models.earth.ionosphere.GlobalIonosphereMapModel
 
getParametersDrivers() - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoModel
 
getParametersDrivers() - Method in class org.orekit.models.earth.ionosphere.NeQuickModel
 
getParametersDrivers() - Method in class org.orekit.models.earth.ionosphere.SsrVtecIonosphericModel
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.AbstractVienna
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.AskneNordiusModel
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.CanonicalSaastamoinenModel
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.ConstantTroposphericModel
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.EstimatedModel
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.FixedTroposphericDelay
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.MariniMurray
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.MendesPavlisModel
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.ModifiedHopfieldModel
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.ModifiedSaastamoinenModel
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedModel
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
Deprecated.
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.TroposphericModelAdapter
Deprecated.
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.ViennaOne
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Get the parameters driver for propagation model.
getParametersDrivers() - Method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.propagation.analytical.FieldKeplerianPropagator
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElementsPropagator
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the drivers for TLE propagation SGP4 and SDP4.
getParametersDrivers() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTJ2SquaredClosedForm
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Get the drivers for parameters.
getParametersDrivers() - Method in interface org.orekit.utils.ParameterDriversProvider
Get the drivers for parameters.
getParametersDriversWithoutMu() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Get the drivers for force model parameters except the one for the central attraction coefficient.
getParametersDriversWithoutMu() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Get the drivers for force model parameters except the one for the central attraction coefficient.
getParametersDriversWithoutMu() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Get the drivers for force model parameters except the one for the central attraction coefficient.
getParametersJacobian(SpacecraftState) - Method in class org.orekit.propagation.AbstractMatricesHarvester
Get the Jacobian with respect to propagation parameters.
getParametersJacobian(SpacecraftState) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester
Get the Jacobian with respect to propagation parameters.
getParametersJacobian(SpacecraftState) - Method in interface org.orekit.propagation.MatricesHarvester
Get the Jacobian with respect to propagation parameters.
getParametersJacobian(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester
Get the Jacobian with respect to propagation parameters.
getParameterSpacing() - Method in class org.orekit.files.sinex.DcbDescription
Get the parameter spacing interval between the bias value.
getParent() - Method in class org.orekit.frames.Frame
Get the parent frame.
getParentShape() - Method in class org.orekit.frames.TopocentricFrame
Get the body shape on which the local point is defined.
getParsedEop() - Method in class org.orekit.files.sinex.SinexLoader
Get the parsed EOP data.
getParsedUnitsBehavior() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Get the behavior to adopt for handling parsed units.
getParsedUnitsBehavior() - Method in class org.orekit.files.ccsds.utils.ContextBinding
Get the behavior to adopt for handling parsed units.
getParsedUnitsBehavior() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser
Get the behavior to adopt for handling parsed units.
getParser(List<Integer>) - Method in enum org.orekit.gnss.metric.ntrip.Type
Get the message parser associated to the SSR type.
getParticipants() - Method in class org.orekit.estimation.measurements.EstimatedMeasurementBase
Get the coordinates of the measurements participants in signal travel order.
getParticipants() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the participants.
getParts() - Method in interface org.orekit.errors.LocalizedException
Get the variable parts of the error message.
getParts() - Method in exception org.orekit.errors.OrekitException
Get the variable parts of the error message.
getParts() - Method in exception org.orekit.errors.OrekitIllegalArgumentException
Get the variable parts of the error message.
getParts() - Method in exception org.orekit.errors.OrekitIllegalStateException
Get the variable parts of the error message.
getParts() - Method in exception org.orekit.errors.OrekitInternalError
Get the variable parts of the error message.
getParts() - Method in exception org.orekit.errors.OrekitIOException
Get the variable parts of the error message.
getParts() - Method in exception org.orekit.errors.OrekitParseException
Get the variable parts of the error message.
getPastInfinity() - Method in class org.orekit.time.AbstractTimeScales
 
getPastInfinity() - Method in interface org.orekit.time.TimeScales
Dummy date at infinity in the past direction.
getPastInfinity(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Dummy date at infinity in the past direction.
getPatchedSpacecraftState() - Method in class org.orekit.utils.AbstractMultipleShooting
Get the list of patched spacecraft states.
getPatchPoint(int) - Method in class org.orekit.utils.AbstractMultipleShooting
Get a patch point.
getPath() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the path.
getPath1() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the path1.
getPath2() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the path2.
getPattern() - Method in enum org.orekit.gnss.metric.parser.IgsSsrMessageType
Get the message number.
getPattern() - Method in enum org.orekit.gnss.metric.parser.RtcmMessageType
Get the message number.
getPattern(Frequency) - Method in class org.orekit.gnss.antenna.Antenna
Get a frequency pattern.
getPdop() - Method in class org.orekit.gnss.DOP
Gets the position dilution of precision.
getPeakMinusMean() - Method in class org.orekit.files.ilrs.CRD.Calibration
Get the system delay peak – mean value.
getPeakMinusMean() - Method in class org.orekit.files.ilrs.CRD.SessionStatistics
Get the session peak – mean value.
getPendingEvent() - Method in class org.orekit.propagation.events.FieldEventState
Get PendingEvent.
getPeriapsisAltitude() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Get the distance of the closest point in the objects orbit above the equatorial radius of the central body.
getPerigeeArgument() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the perigee argument.
getPerigeeArgument() - Method in class org.orekit.orbits.KeplerianOrbit
Get the perigee argument.
getPerigeeArgument() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get the argument of perigee.
getPerigeeArgument() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the argument of perigee.
getPerigeeArgumentDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the perigee argument derivative.
getPerigeeArgumentDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the perigee argument derivative.
getPermanentTide() - Method in enum org.orekit.utils.IERSConventions
Get the permanent tide to be removed from ΔC₂₀ when zero-tide potentials are used.
getPerturbationsBlock() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmData
Get perturbations logical block.
getPhase(BodiesElements) - Method in class org.orekit.models.earth.displacement.Tide
Get the phase of the tide.
getPhaseBias() - Method in class org.orekit.gnss.metric.messages.common.PhaseBias
Get the phase bias associated to the signal ID.
getPhaseBias(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data
Get the phase bias for a given signal ID.
getPhaseBiases() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data
Get the phase biases for the current satellite.
getPhaseCenterSystem() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Get satellite system for average phase center.
getPhaseCenterVariation(Vector3D) - Method in class org.orekit.gnss.antenna.FrequencyPattern
Get the value of the phase center variation in a signal direction.
getPhaseCenterVariation(Frequency, Vector3D) - Method in class org.orekit.gnss.antenna.Antenna
Get the value of the phase center variation in a signal direction.
getPhaseCenterVariationFunction() - Method in class org.orekit.gnss.antenna.FrequencyPattern
Get the phase center variation function.
getPhaseMinusCodeCombination(SatelliteSystem) - Static method in class org.orekit.estimation.measurements.gnss.MeasurementCombinationFactory
Get the phase minus code combination of measurements.
getPhaseShiftCorrections() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Get the list of phase shift correction used to generate phases consistent w/r to cycle shifts.
getPhysicalCovariances(double) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Get the covariances matrix in space flight dynamics physical units.
getPhysicalEstimatedCovarianceMatrix() - Method in class org.orekit.estimation.sequential.AbstractKalmanEstimator
Get the "physical" estimated covariance matrix (i.e.
getPhysicalEstimatedCovarianceMatrix() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the "physical" estimated covariance matrix (i.e.
getPhysicalEstimatedCovarianceMatrix() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Get the "physical" estimated covariance matrix (i.e.
getPhysicalEstimatedCovarianceMatrix() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel
Get the "physical" estimated covariance matrix (i.e.
getPhysicalEstimatedState() - Method in class org.orekit.estimation.sequential.AbstractKalmanEstimator
Get the "physical" estimated state (i.e.
getPhysicalEstimatedState() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the "physical" estimated state (i.e.
getPhysicalEstimatedState() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Get the "physical" estimated state (i.e.
getPhysicalEstimatedState() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel
Get the "physical" estimated state (i.e.
getPhysicalInnovationCovarianceMatrix() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the physical innovation covariance matrix.
getPhysicalInnovationCovarianceMatrix() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Get the physical innovation covariance matrix.
getPhysicalInnovationCovarianceMatrix() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel
Get the physical innovation covariance matrix.
getPhysicalKalmanGain() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the physical Kalman gain matrix.
getPhysicalKalmanGain() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Get the physical Kalman gain matrix.
getPhysicalKalmanGain() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel
Get the physical Kalman gain matrix.
getPhysicalMeasurementJacobian() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the physical Jacobian of the measurement with respect to the state (H matrix).
getPhysicalMeasurementJacobian() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Get the physical Jacobian of the measurement with respect to the state (H matrix).
getPhysicalMeasurementJacobian() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel
Get the physical Jacobian of the measurement with respect to the state (H matrix).
getPhysicalStateTransitionMatrix() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get physical state transition matrix between previous state and estimated (but not yet corrected) state.
getPhysicalStateTransitionMatrix() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Get physical state transition matrix between previous state and estimated (but not yet corrected) state.
getPhysicalStateTransitionMatrix() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel
Get physical state transition matrix between previous state and estimated (but not yet corrected) state.
getPhysicBlock() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmData
Get physical properties logical block.
getPhysicBlock() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmData
Get physical properties logical block.
getPlane() - Method in class org.orekit.orbits.WalkerConstellationSlot
Get the plane index.
getPlaneSection(FieldVector3D<T>, FieldVector3D<T>) - Method in class org.orekit.bodies.Ellipsoid
Compute the 2D ellipse at the intersection of the 3D ellipsoid and a plane.
getPlaneSection(Vector3D, Vector3D) - Method in class org.orekit.bodies.Ellipsoid
Compute the 2D ellipse at the intersection of the 3D ellipsoid and a plane.
getPlus(int, int) - Method in class org.orekit.utils.LoveNumbers
Get the real part of a nominal Love numbers.
getPluto() - Method in interface org.orekit.bodies.CelestialBodies
Get the Pluto singleton body.
getPluto() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Pluto singleton body.
getPluto() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
 
getPnm(int, int) - Method in class org.orekit.utils.FieldLegendrePolynomials
Return the coefficient Pnm.
getPnm(int, int) - Method in class org.orekit.utils.LegendrePolynomials
Return the coefficient Pnm.
getPoint() - Method in class org.orekit.bodies.Loxodrome
Get the geodetic point defining the loxodrome.
getPoint() - Method in class org.orekit.frames.TopocentricFrame
Get the surface point defining the origin of the frame.
getPoint(Field<T>) - Method in class org.orekit.frames.TopocentricFrame
Get the surface point defining the origin of the frame.
getPolarDriftXDriver() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
Get a driver allowing to add a polar drift along X.
getPolarDriftXDriver() - Method in class org.orekit.estimation.measurements.GroundStation
Get a driver allowing to add a polar drift along X.
getPolarDriftYDriver() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
Get a driver allowing to add a polar drift along Y.
getPolarDriftYDriver() - Method in class org.orekit.estimation.measurements.GroundStation
Get a driver allowing to add a polar drift along Y.
getPolarOffsetXDriver() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
Get a driver allowing to add a polar offset along X.
getPolarOffsetXDriver() - Method in class org.orekit.estimation.measurements.GroundStation
Get a driver allowing to add a polar offset along X.
getPolarOffsetYDriver() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
Get a driver allowing to add a polar offset along Y.
getPolarOffsetYDriver() - Method in class org.orekit.estimation.measurements.GroundStation
Get a driver allowing to add a polar offset along Y.
getPolarRadius() - Method in class org.orekit.models.earth.ReferenceEllipsoid
Get the radius of this ellipsoid at the poles.
getPole(AbsoluteDate) - Method in interface org.orekit.bodies.IAUPole
Get the body North pole direction in ICRF frame.
getPole(FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.IAUPole
Get the body North pole direction in ICRF frame.
getPoleCorrection(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory
Get the pole IERS Reference Pole correction.
getPoleCorrection(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EOPHistory
Get the pole IERS Reference Pole correction.
getPolynomial() - Method in class org.orekit.data.PoissonSeries
Get the polynomial part of the series.
getPort() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord
Get the port number.
getPort() - Method in class org.orekit.gnss.metric.ntrip.NtripClient
Get the port to use for connection.
getPosition() - Method in class org.orekit.estimation.measurements.Position
Get the position.
getPosition() - Method in class org.orekit.estimation.measurements.PV
Get the position.
getPosition() - Method in class org.orekit.files.sinex.Station
Get the station position.
getPosition() - Method in class org.orekit.orbits.FieldOrbit
Get the position in definition frame.
getPosition() - Method in class org.orekit.orbits.Orbit
Get the position in definition frame.
getPosition() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the position in orbit definition frame.
getPosition() - Method in class org.orekit.propagation.SpacecraftState
Get the position in orbit definition frame.
getPosition() - Method in class org.orekit.utils.FieldPVCoordinates
Gets the position.
getPosition() - Method in class org.orekit.utils.PVCoordinates
Gets the position.
getPosition(Frame) - Method in class org.orekit.orbits.FieldOrbit
Get the position in a specified frame.
getPosition(Frame) - Method in class org.orekit.orbits.Orbit
Get the position in a specified frame.
getPosition(Frame) - Method in class org.orekit.propagation.FieldSpacecraftState
Get the position in given output frame.
getPosition(Frame) - Method in class org.orekit.propagation.SpacecraftState
Get the position in given output frame.
getPosition(Frame) - Method in class org.orekit.utils.AbsolutePVCoordinates
Get the position in a specified frame.
getPosition(Frame) - Method in class org.orekit.utils.FieldAbsolutePVCoordinates
Get the position in a specified frame.
getPosition(AbsoluteDate, Frame) - Method in class org.orekit.bodies.AnalyticalSolarPositionProvider
Get the position of the body in the selected frame.
getPosition(AbsoluteDate, Frame) - Method in class org.orekit.files.general.EphemerisSegmentPropagator
 
getPosition(AbsoluteDate, Frame) - Method in class org.orekit.frames.TopocentricFrame
Get the position of the body in the selected frame.
getPosition(AbsoluteDate, Frame) - Method in class org.orekit.orbits.Orbit
Get the position of the body in the selected frame.
getPosition(AbsoluteDate, Frame) - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
 
getPosition(AbsoluteDate, Frame) - Method in interface org.orekit.propagation.Propagator
Get the position of the body in the selected frame.
getPosition(AbsoluteDate, Frame) - Method in class org.orekit.utils.AggregatedPVCoordinatesProvider
 
getPosition(AbsoluteDate, Frame) - Method in class org.orekit.utils.ConstantPVCoordinatesProvider
 
getPosition(AbsoluteDate, Frame) - Method in interface org.orekit.utils.PVCoordinatesProvider
Get the position of the body in the selected frame.
getPosition(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.bodies.AnalyticalSolarPositionProvider
Get the position in the selected frame.
getPosition(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.orbits.FieldOrbit
Get the position of the body in the selected frame.
getPosition(FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.propagation.FieldPropagator
Get the position of the body in the selected frame.
getPosition(FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.utils.ExtendedPositionProvider
Get the position in the selected frame.
getPosition(FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.utils.ExtendedPVCoordinatesProvider
Get the position of the body in the selected frame.
getPosition(FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.utils.FieldPVCoordinatesProvider
Get the position of the body in the selected frame.
getPositionAccuracy() - Method in class org.orekit.files.sp3.SP3Coordinate
Get the position accuracy.
getPositionAdjointContribution(AbsoluteDate, double[], double[], Frame) - Method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointGravitationalTerm
Computes the contribution to position adjoint derivatives.
getPositionAdjointContribution(AbsoluteDate, double[], double[], Frame) - Method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointNonCentralBodyTerm
Computes the contribution to position adjoint derivatives.
getPositionAdjointContribution(AbsoluteDate, double[], double[], Frame) - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointJ2Term
Computes the contribution to position adjoint derivatives.
getPositionAdjointContribution(AbsoluteDate, double[], double[], Frame) - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointKeplerianTerm
Computes the contribution to position adjoint derivatives.
getPositionAdjointFieldContribution(FieldAbsoluteDate<T>, T[], T[], Frame) - Method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointGravitationalTerm
Computes the contribution to position adjoint derivatives.
getPositionAdjointFieldContribution(FieldAbsoluteDate<T>, T[], T[], Frame) - Method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointNonCentralBodyTerm
Computes the contribution to position adjoint derivatives.
getPositionAdjointFieldContribution(FieldAbsoluteDate<T>, T[], T[], Frame) - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointJ2Term
Computes the contribution to position adjoint derivatives.
getPositionAdjointFieldContribution(FieldAbsoluteDate<T>, T[], T[], Frame) - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointKeplerianTerm
Computes the contribution to position adjoint derivatives.
getPositionAngleType() - Method in class org.orekit.estimation.sequential.UnivariateProcessNoise
Getter for the positionAngle.
getPositionAngleType() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester
Get the position angle used for the matrix computation.
getPositionAngleType() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Get the position angle type expected for the 6 first parameters in PropagatorBuilder.buildPropagator(double[]).
getPositionAngleType() - Method in interface org.orekit.propagation.conversion.averaging.AveragedOrbitalState
Getter for the averaged position angle.
getPositionAngleType() - Method in class org.orekit.propagation.conversion.averaging.BrouwerLyddaneOrbitalState
Getter for the averaged position angle.
getPositionAngleType() - Method in class org.orekit.propagation.conversion.averaging.DSST6X0OrbitalState
Getter for the averaged position angle.
getPositionAngleType() - Method in class org.orekit.propagation.conversion.averaging.EcksteinHechlerOrbitalState
Getter for the averaged position angle.
getPositionAngleType() - Method in class org.orekit.propagation.conversion.averaging.SGP4OrbitalState
Getter for the averaged position angle.
getPositionAngleType() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
Get the position angle type expected for the 6 first parameters in PropagatorBuilder.buildPropagator(double[]).
getPositionAngleType() - Method in class org.orekit.propagation.events.PositionAngleDetector
Get the type of position angle.
getPositionAngleType() - Method in class org.orekit.propagation.FieldStateCovariance
Get the covariance angle type.
getPositionAngleType() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get propagation parameter type.
getPositionAngleType() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get propagation parameter type.
getPositionAngleType() - Method in class org.orekit.propagation.integration.FieldStateMapper
Get propagation parameter type.
getPositionAngleType() - Method in class org.orekit.propagation.integration.StateMapper
Get propagation parameter type.
getPositionAngleType() - Method in interface org.orekit.propagation.MatricesHarvester
Get the position angle used for the matrix computation.
getPositionAngleType() - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Get propagation parameter type.
getPositionAngleType() - Method in class org.orekit.propagation.numerical.NumericalPropagator
Get propagation parameter type.
getPositionAngleType() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester
Get the position angle used for the matrix computation.
getPositionAngleType() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Get propagation parameter type.
getPositionAngleType() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Get propagation parameter type.
getPositionAngleType() - Method in class org.orekit.propagation.StateCovariance
Get the covariance angle type.
getPositionScale() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Get the position scale.
getPositionVector() - Method in class org.orekit.files.ccsds.ndm.cdm.StateVector
Get object Position Vector.
getPosVelBase() - Method in class org.orekit.files.sp3.SP3Header
Get the base for position/velocity accuracy.
getPotential(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel
Calculate spacecraft potential.
getPotential(SpacecraftState) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel
Calculate spacecraft potential.
getPreamble() - Method in class org.orekit.gnss.rflink.gps.SubFrame
Get telemetry preamble.
getPrecessionFunction() - Method in enum org.orekit.utils.IERSConventions
Get the function computing the precession angles.
getPrecessionFunction(TimeScales) - Method in enum org.orekit.utils.IERSConventions
Get the function computing the precession angles.
getPredictedMeasurement() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the predicted measurement.
getPredictedMeasurement() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Get the predicted measurement.
getPredictedMeasurement() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel
Get the predicted measurement.
getPredictedMeasurements(RealVector[], MeasurementDecorator) - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel
getPredictedMeasurements(RealVector[], MeasurementDecorator) - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel
getPredictedSpacecraftStates() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the predicted spacecraft states.
getPredictedSpacecraftStates() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Get the predicted spacecraft states.
getPredictedSpacecraftStates() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel
Get the predicted spacecraft states.
getPredictionProvider() - Method in class org.orekit.files.ilrs.CRDHeader
Get the prediction provider.
getPredictionType() - Method in class org.orekit.files.ilrs.CRDHeader
Get the prediction type (CPF or TLE).
getPressSensorManufacturer() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
Get the pressure sensor manufacturer.
getPressSensorModel() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
Get the pressure sensor model.
getPressSensorSerialNumber() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
Get the pressure sensor serial number.
getPressure() - Method in class org.orekit.files.ilrs.CRD.MeteorologicalMeasurement
Get the surface pressure.
getPressure() - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction
Get the local pressure at the evaluation location.
getPressure() - Method in class org.orekit.models.earth.weather.FieldPressureTemperature
Get pressure.
getPressure() - Method in class org.orekit.models.earth.weather.GlobalPressureTemperature2Model
Deprecated.
Returns the pressure at the station [hPa].
getPressure() - Method in class org.orekit.models.earth.weather.GlobalPressureTemperatureModel
Deprecated.
Get the atmospheric pressure of the station depending its position.
getPressure() - Method in class org.orekit.models.earth.weather.PressureTemperature
Get pressure.
getPressureTemperatureHumidity(AbsoluteDate) - Method in class org.orekit.estimation.measurements.GroundStation
Get the weather parameters.
getPressureTemperatureHumidity(FieldAbsoluteDate<T>) - Method in class org.orekit.estimation.measurements.GroundStation
Get the weather parameters.
getPrevId() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination
Get identification of previous orbit determination.
getPrevId() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get identification of previous orbit determination.
getPrevID() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver
Get identification number of previous maneuver.
getPreviousMessageEpoch() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the UTC epoch of the previous CDM issued for the event identified by CONJUNCTION_ID.
getPreviousMessageEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the creation date of previous message from a given originator.
getPreviousMessageId() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the ID of previous CDM issued for event identified by CONJUNCTION_ID.
getPreviousMessageID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the unique ID identifying previous message from a given originator.
getPreviousParam() - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData.LocalSolarActivity
 
getPreviousState() - Method in interface org.orekit.propagation.sampling.FieldOrekitStepInterpolator
Get the state at previous grid point date.
getPreviousState() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator
Get the state at previous grid point date.
getPrf() - Method in class org.orekit.files.ilrs.CPFHeader
Get the Pulse Repetition Frequency (PRF).
getPrimary() - Method in class org.orekit.bodies.CR3BPSystem
Get the primary CelestialBody.
getPrimary() - Method in class org.orekit.estimation.measurements.gnss.Dipole
Get the primary dipole vector.
getPrimaryObject() - Method in class org.orekit.propagation.events.AngularSeparationFromSatelliteDetector
Get the primaryObject, at the center of the proximity zone.
getPrimaryStation() - Method in class org.orekit.estimation.measurements.TurnAroundRange
Get the primary ground station from which measurement is performed.
getPrimaryWavelength() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
Get the primary wavelength.
getPrimeMeridianAngle(AbsoluteDate) - Method in interface org.orekit.bodies.IAUPole
Get the prime meridian angle.
getPrimeMeridianAngle(FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.IAUPole
Get the prime meridian angle.
getPrimeMeridianDriftDriver() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
Get a driver allowing to add a prime meridian rotation rate.
getPrimeMeridianDriftDriver() - Method in class org.orekit.estimation.measurements.GroundStation
Get a driver allowing to add a prime meridian rotation rate.
getPrimeMeridianOffsetDriver() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
Get a driver allowing to add a prime meridian rotation.
getPrimeMeridianOffsetDriver() - Method in class org.orekit.estimation.measurements.GroundStation
Get a driver allowing to add a prime meridian rotation.
getPrimeStation() - Method in class org.orekit.estimation.measurements.FDOA
Get the prime ground station, the one that gives the date of the measurement.
getPrimeStation() - Method in class org.orekit.estimation.measurements.TDOA
Get the prime ground station, the one that gives the date of the measurement.
getPrmMessageLink() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the Unique identifier of Pointing Request Message linked to this Orbit Data Message.
getPrn() - Method in class org.orekit.files.rinex.navigation.TypeSvMessage
Get satellite number.
getPRN() - Method in class org.orekit.files.sinex.DcbSatellite
Return the satellite PRN, as a String.
getPRN() - Method in class org.orekit.gnss.rflink.gps.SubFrameAlmanac
Get the PRN code phase of the SV.
getPRN() - Method in class org.orekit.gnss.SatInSystem
Get the Pseudo Random Number of the satellite.
getPRN() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Getter for the PRN number of the satellite.
getPRN() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Getter for the PRN number of the satellite.
getPRN() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
Gets the PRN number of the GNSS satellite.
getPRN() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
Gets the PRN number of the SBAS satellite.
getPrnNumber() - Method in class org.orekit.estimation.measurements.gnss.CombinedObservationDataSet
Get PRN number.
getPrnNumber() - Method in class org.orekit.gnss.antenna.SatelliteAntenna
Get PRN number.
getPRNNumbers() - Method in class org.orekit.gnss.SEMParser
Gets the PRN numbers of all the GPS almanacs read from the file.
getPRNNumbers() - Method in class org.orekit.gnss.YUMAParser
Gets the PRN numbers of all the GPS almanacs read from the file.
getProbabilityOfCollisionMethodName() - Method in class org.orekit.ssa.metrics.FieldProbabilityOfCollision
Get name of the probability computing method with which this probability was computed.
getProbabilityOfCollisionMethodName() - Method in class org.orekit.ssa.metrics.ProbabilityOfCollision
Get name of the probability computing method with which this probability was computed.
getProcessingSoftwareName() - Method in class org.orekit.files.ilrs.CRDConfiguration.CalibrationTargetConfiguration
Get the processing software name.
getProcessingSoftwares() - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration
Get the processing softwares.
getProcessingSoftwareVersion() - Method in class org.orekit.files.ilrs.CRDConfiguration.CalibrationTargetConfiguration
Get the processing software version.
getProcessingSoftwareVersions() - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration
Get the processing software versions.
getProcessNoiseMatrix(SpacecraftState, SpacecraftState) - Method in class org.orekit.estimation.sequential.ConstantProcessNoise
Get the process noise matrix between previous and current states.
getProcessNoiseMatrix(SpacecraftState, SpacecraftState) - Method in interface org.orekit.estimation.sequential.CovarianceMatrixProvider
Get the process noise matrix between previous and current states.
getProcessNoiseMatrix(SpacecraftState, SpacecraftState) - Method in class org.orekit.estimation.sequential.UnivariateProcessNoise
Get the process noise matrix between previous and current states.
getProductionEpoch() - Method in class org.orekit.files.ilrs.ILRSHeader
Get the date component of the ephemeris production.
getProductionHour() - Method in class org.orekit.files.ilrs.ILRSHeader
Get the hour of ephemeris production (UTC).
getProgDCBS() - Method in class org.orekit.files.rinex.AppliedDCBS
Get the program name used to apply DCBs.
getProgPCVS() - Method in class org.orekit.files.rinex.AppliedPCVS
Get the program name used to apply PCVs.
getProgramName() - Method in class org.orekit.files.rinex.clock.RinexClock
Getter for the program name.
getProgramName() - Method in class org.orekit.files.rinex.section.RinexBaseHeader
Getter for the program name.
getPropagationFrame() - Method in class org.orekit.control.indirect.shooting.propagation.ShootingPropagationSettings
Getter for the propagation frame.
getPropagationParametersDrivers() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Get the drivers for the configurable propagation parameters.
getPropagationParametersDrivers() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
Get the drivers for the configurable propagation parameters.
getPropagationParametersDrivers(boolean) - Method in class org.orekit.estimation.sequential.AbstractKalmanEstimator
Get the propagator parameters supported by this estimator.
getPropagationParametersEvolution() - Method in class org.orekit.estimation.sequential.UnivariateProcessNoise
Getter for the propagationParametersEvolution.
getPropagationSettings() - Method in class org.orekit.control.indirect.shooting.AbstractIndirectShooting
Getter for the propagation settings.
getPropagationType() - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder
Get the type of the orbit used for the propagation (mean or osculating).
getPropagationType() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get the propagation type.
getPropagationType() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get the propagation type.
getPropagator() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Get the orbit propagator used to generate this trajectory.
getPropagator() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
View this ephemeris segment as a propagator.
getPropagator() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris
View this ephemeris as a propagator, combining data from all segments.
getPropagator() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris
View this ephemeris as a propagator, combining data from all segments.
getPropagator() - Method in class org.orekit.files.sp3.SP3Segment
View this ephemeris segment as a propagator.
getPropagator() - Method in class org.orekit.propagation.analytical.AdapterPropagator
Get the reference propagator.
getPropagator() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
Get the propagator corresponding to the navigation message.
getPropagator() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
Get the propagator corresponding to the navigation message.
getPropagator() - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage
Get the propagator corresponding to the navigation message.
getPropagator(double) - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage
Get the propagator corresponding to the navigation message.
getPropagator(double, DataContext) - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage
Get the propagator corresponding to the navigation message.
getPropagator(double, DataContext, AttitudeProvider, Frame, double) - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage
Get the propagator corresponding to the navigation message.
getPropagator(AttitudeProvider) - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
View this ephemeris segment as a propagator.
getPropagator(AttitudeProvider) - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris
View this ephemeris as a propagator, combining data from all segments.
getPropagator(AttitudeProvider) - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris
View this ephemeris as a propagator, combining data from all segments.
getPropagator(AttitudeProvider) - Method in class org.orekit.files.sp3.SP3Segment
View this ephemeris segment as a propagator.
getPropagator(DataContext) - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
Get the propagator corresponding to the navigation message.
getPropagator(DataContext, AttitudeProvider, Frame, Frame, double) - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
Get the propagator corresponding to the navigation message.
getPropagator(ObservableSatellite) - Method in class org.orekit.estimation.measurements.generation.Generator
Get a registered propagator.
getPropagator(Frames) - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
Get the propagator corresponding to the navigation message.
getPropagator(Frames) - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage
Get the propagator corresponding to the navigation message.
getPropagator(Frames, AttitudeProvider, Frame, Frame, double) - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
Get the propagator corresponding to the navigation message.
getPropagator(Frames, AttitudeProvider, Frame, Frame, double, double) - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage
Get the propagator corresponding to the navigation message.
getPropagator(FieldSpacecraftState<Gradient>, Gradient[]) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalGradientConverter
Get the converted analytical orbit propagator.
getPropagatorIndex() - Method in class org.orekit.estimation.measurements.ObservableSatellite
Get the index of the propagator related to this satellite.
getPropagatorParametersDrivers(boolean) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Get the propagator parameters supported by this estimator.
getPropagators() - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
Deprecated.
getPropagators() - Method in class org.orekit.propagation.PropagatorsParallelizer
Get an unmodifiable list of the underlying mono-satellite propagators.
getPropagatorsMap() - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
Get the propagators map.
getPropulsionModel() - Method in class org.orekit.forces.maneuvers.Maneuver
Get the propulsion model.
getPropulsionModelParameters(double[]) - Method in class org.orekit.forces.maneuvers.Maneuver
Extract propulsion model parameters from the parameters' array called in by the ForceModel interface.
getPropulsionModelParameters(T[]) - Method in class org.orekit.forces.maneuvers.Maneuver
Extract propulsion model parameters from the parameters' array called in by the ForceModel interface.
getProvider() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Get the spherical harmonics provider.
getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.EGMFormatReader
Get a provider for read spherical harmonics coefficients.
getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.GRGSFormatReader
Get a provider for read spherical harmonics coefficients.
getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.ICGEMFormatReader
Get a provider for read spherical harmonics coefficients.
getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get a provider for read spherical harmonics coefficients.
getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.SHAFormatReader
Provider for read spherical harmonics coefficients.
getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.SHMFormatReader
Get a provider for read spherical harmonics coefficients.
getProviders() - Method in class org.orekit.data.DataProvidersManager
Get an unmodifiable view of the list of supported providers.
getProximityAngle() - Method in class org.orekit.propagation.events.AngularSeparationDetector
Get the proximity angle (rad).
getProximityAngle() - Method in class org.orekit.propagation.events.AngularSeparationFromSatelliteDetector
Get the proximity angle (rad).
getProxy() - Method in class org.orekit.gnss.metric.ntrip.NtripClient
Get proxy.
getPsdTimeSpanMap() - Method in class org.orekit.files.sinex.Station
Get the TimeSpanMap of Post-Seismic Deformation.
getPth0Provider() - Method in class org.orekit.models.earth.troposphere.ModifiedSaastamoinenModel
Get provider for atmospheric pressure, temperature and humidity at reference altitude.
getPulsations() - Method in class org.orekit.utils.SecularAndHarmonic
Get the pulsations of harmonic part.
getPulseEnergy() - Method in class org.orekit.files.ilrs.CRDConfiguration.CalibrationTargetConfiguration
Get the pulse energy.
getPulseEnergy() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
Get the pulse energy.
getPulseInOutgoingSemiTrain() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
Get the number of pulses in outgoing semi-train.
getPulseWidth() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
Get the pulse width (FWHM in ps).
getPVAFilter() - Method in class org.orekit.orbits.FieldOrbitHermiteInterpolator
Get filter for derivatives from the sample to use in position-velocity-acceleration interpolation.
getPVAFilter() - Method in class org.orekit.orbits.OrbitHermiteInterpolator
Get filter for derivatives from the sample to use in position-velocity-acceleration interpolation.
getPVCoordinates() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm
Get the position/velocity coordinates contained in the OPM.
getPVCoordinates() - Method in class org.orekit.orbits.FieldOrbit
Get the TimeStampedPVCoordinates in definition frame.
getPVCoordinates() - Method in class org.orekit.orbits.Orbit
Get the TimeStampedPVCoordinates in definition frame.
getPVCoordinates() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the TimeStampedFieldPVCoordinates in orbit definition frame.
getPVCoordinates() - Method in class org.orekit.propagation.SpacecraftState
Get the TimeStampedPVCoordinates in orbit definition frame.
getPVCoordinates() - Method in class org.orekit.utils.AbsolutePVCoordinates
Get the TimeStampedPVCoordinates.
getPVCoordinates() - Method in class org.orekit.utils.FieldAbsolutePVCoordinates
Get the TimeStampedFieldPVCoordinates.
getPVCoordinates(Frame) - Method in class org.orekit.orbits.FieldOrbit
Get the TimeStampedPVCoordinates in a specified frame.
getPVCoordinates(Frame) - Method in class org.orekit.orbits.Orbit
Get the TimeStampedPVCoordinates in a specified frame.
getPVCoordinates(Frame) - Method in class org.orekit.propagation.FieldSpacecraftState
Get the TimeStampedFieldPVCoordinates in given output frame.
getPVCoordinates(Frame) - Method in class org.orekit.propagation.SpacecraftState
Get the TimeStampedPVCoordinates in given output frame.
getPVCoordinates(Frame) - Method in class org.orekit.utils.AbsolutePVCoordinates
Get the TimeStampedPVCoordinates in a specified frame.
getPVCoordinates(Frame) - Method in class org.orekit.utils.FieldAbsolutePVCoordinates
Get the TimeStampedFieldPVCoordinates in a specified frame.
getPVCoordinates(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
Get the extrapolated position and velocity from an initial TLE.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.files.general.EphemerisSegmentPropagator
 
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.frames.TopocentricFrame
Get the PVCoordinates of the topocentric frame origin in the selected frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.orbits.Orbit
Get the PVCoordinates of the body in the selected frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
 
getPVCoordinates(AbsoluteDate, Frame) - Method in interface org.orekit.propagation.Propagator
Get the PVCoordinates of the body in the selected frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator
Get the PVCoordinates of the body in the selected frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.utils.AbsolutePVCoordinates
 
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.utils.AggregatedPVCoordinatesProvider
 
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.utils.AggregatedPVCoordinatesProvider.InvalidPVProvider
 
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.utils.ConstantPVCoordinatesProvider
 
getPVCoordinates(AbsoluteDate, Frame) - Method in interface org.orekit.utils.ExtendedPositionProvider
Get the PVCoordinates of the body in the selected frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.utils.FrameAdapter
Get the PVCoordinates of the body in the selected frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in interface org.orekit.utils.PVCoordinatesProvider
Get the PVCoordinates of the body in the selected frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.utils.ShiftingPVCoordinatesProvider
Get the PVCoordinates of the body in the selected frame.
getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.orbits.FieldOrbit
Get the FieldPVCoordinates of the body in the selected frame.
getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.propagation.FieldPropagator
Get the FieldPVCoordinates of the body in the selected frame.
getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.propagation.sampling.FieldOrekitStepInterpolator
Get the FieldPVCoordinates of the body in the selected frame.
getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.utils.ExtendedPositionProvider
Get the position-velocity-acceleration in the selected frame.
getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.utils.ExtendedPVCoordinatesProvider
Get the FieldPVCoordinates of the body in the selected frame.
getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.utils.FieldAbsolutePVCoordinates
 
getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.utils.FieldPVCoordinatesProvider
Get the FieldPVCoordinates of the body in the selected frame.
getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.utils.FieldShiftingPVCoordinatesProvider
Get the FieldPVCoordinates of the body in the selected frame.
getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.utils.FrameAdapter
Get the FieldPVCoordinates of the body in the selected frame.
getPVCoordinates(FieldAbsoluteDate<T>, T[]) - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
Get the extrapolated position and velocity from an initial TLE.
getPVCoordinatesProvider() - Method in class org.orekit.propagation.events.AlignmentDetector
Get the body to align.
getPVJacobian() - Method in interface org.orekit.frames.FieldKinematicTransform
Compute the Jacobian of the FieldKinematicTransform.transformOnlyPV(FieldPVCoordinates) (FieldPVCoordinates)} method of the transform.
getPVJacobian() - Method in interface org.orekit.frames.KinematicTransform
Compute the Jacobian of the KinematicTransform.transformOnlyPV(PVCoordinates) (PVCoordinates)} method of the transform.
getPvProvider() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Get PV coordinates provider.
getPvProvider() - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Get PV coordinates provider.
getPVTarget() - Method in class org.orekit.propagation.events.FieldOfViewDetector
Get the position/velocity provider of the target .
getPZ9011(IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames
 
getPZ9011(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames
Get the PZ-90.11 (Parametry Zemly – 1990.11) reference frame.
getPZ9011(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
Get the PZ-90.11 (Parametry Zemly – 1990.11) reference frame.
getQ() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the x component of inclination vector.
getQ() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get the x component of inclination vector.
getQuadraticClockModel() - Method in class org.orekit.estimation.measurements.ObservableSatellite
Get a quadratic clock model valid at some date.
getQualityIndicator() - Method in class org.orekit.files.ilrs.CRDHeader
Get the data quality indicator.
getQuantumEfficiency() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Get the quantum efficiency at applicable wavelength.
getQuaternion() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternion
Get the quaternion.
getQuaternionBlock() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData
Get the quaternion logical block.
getQuaternionDot() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternion
Get the quaternion derivative.
getQZSS() - Method in class org.orekit.time.LazyLoadedTimeScales
 
getQZSS() - Method in interface org.orekit.time.TimeScales
Get the Quasi-Zenith Satellite System time scale.
getQZSS() - Static method in class org.orekit.time.TimeScalesFactory
Get the Quasi-Zenith Satellite System time scale.
getQZSSCivilianNavigationMessages() - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Get all the QZSS navigation messages contained in the file.
getQZSSCivilianNavigationMessages(String) - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Get the QZSS navigation messages for the given satellite Id.
getQzssCodeOnL2() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data
Get the QZSS code on L2 Channel.
getQzssEpoch() - Method in class org.orekit.time.AbstractTimeScales
 
getQzssEpoch() - Method in interface org.orekit.time.TimeScales
Reference epoch for QZSS weeks: 1980-01-06T00:00:00 QZSS time.
getQzssFitInterval() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data
Get the QZSS fit interval.
getQZSSLegacyNavigationMessages() - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Get all the QZSS navigation messages contained in the file.
getQZSSLegacyNavigationMessages(String) - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Get the QZSS navigation messages for the given satellite Id.
getQzssNavigationMessage() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data
Get the QZSS navigation message corresponding to the current RTCM data.
getQzssNavigationMessage(TimeScales) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data
Get the QZSS navigation message corresponding to the current RTCM data.
getQzssToc() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data
Get the QZSS time of clock.
getR3() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext
Get the distance from center of mass of the central body to the 3rd body.
getR3() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext
Get the distance from center of mass of the central body to the 3rd body.
getRaan() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Get the orbit right ascension of ascending node.
getRaan() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get Right Ascension of the Ascending node.
getRaan() - Method in class org.orekit.propagation.analytical.tle.TLE
Get Right Ascension of the Ascending node.
getRadiationParametersDrivers() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Get the drivers for supported parameters.
getRadiationParametersDrivers() - Method in class org.orekit.forces.radiation.IsotropicRadiationClassicalConvention
Get the drivers for supported parameters.
getRadiationParametersDrivers() - Method in class org.orekit.forces.radiation.IsotropicRadiationCNES95Convention
Get the drivers for supported parameters.
getRadiationParametersDrivers() - Method in class org.orekit.forces.radiation.IsotropicRadiationSingleCoefficient
Get the drivers for supported parameters.
getRadiationParametersDrivers() - Method in interface org.orekit.forces.radiation.RadiationSensitive
Get the drivers for supported parameters.
getRadiationSensitive() - Method in class org.orekit.forces.radiation.RadiationPressureModel
Getter for radiation sensitive object.
getRadiationSensitiveSpacecraft() - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Getter for radiation-sensitive spacecraft.
getRange() - Method in class org.orekit.utils.FieldTrackingCoordinates
Get the range.
getRange() - Method in class org.orekit.utils.TrackingCoordinates
Get the range.
getRange(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.TopocentricFrame
Get the range of a point with regards to the topocentric frame center point.
getRange(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame
Get the range of a point with regards to the topocentric frame center point.
getRange1() - Method in class org.orekit.estimation.iod.IodGooding
Get range for observation (1).
getRange2() - Method in class org.orekit.estimation.iod.IodGooding
Get range for observation (2).
getRange3() - Method in class org.orekit.estimation.iod.IodGooding
Get range for observation (3).
getRangeData() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
Get the range data for the data block.
getRangeMode() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the rangeMode.
getRangeModulus(RangeUnitsConverter) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the range modulus in meters.
getRangeRate() - Method in class org.orekit.files.ilrs.CRD.RangeSupplement
Get the range rate.
getRangeRate(FieldPVCoordinates<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.TopocentricFrame
Get the range rate of a point with regards to the topocentric frame center point.
getRangeRate(PVCoordinates, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame
Get the range rate of a point with regards to the topocentric frame center point.
getRangeSupplementData() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
Get the range supplement data for the data block.
getRangeType() - Method in class org.orekit.files.ilrs.CRDHeader
Get the range type.
getRangeType(int) - Static method in enum org.orekit.files.ilrs.CRDHeader.RangeType
Get the range type for the given indicator.
getRangeUnits() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the rangeUnits.
getRangeUnitsConverter() - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder
Get the converter for Range Units.
getRate() - Method in class org.orekit.gnss.metric.ntrip.StreamedMessage
Get refresh rate.
getRate() - Method in class org.orekit.time.ClockOffset
Get rate.
getRate() - Method in class org.orekit.time.FieldClockOffset
Get rate.
getRate(BodiesElements) - Method in class org.orekit.models.earth.displacement.Tide
Get the angular rate of the tide.
getRateElementsType() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeState
Get the type of the elements rates.
getRateProcessNoiseStdDev() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination
Get process noise standard deviation if AttitudeDetermination.rateStates is RateElementsType.ANGVEL.
getRatesContribution(AbsoluteDate, double[], double[], Frame) - Method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointEquationTerm
Computes the contribution to the rates of the adjoint variables.
getRatesContribution(AbsoluteDate, double[], double[], Frame) - Method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointGravitationalTerm
Computes the contribution to the rates of the adjoint variables.
getRatesContribution(AbsoluteDate, double[], double[], Frame) - Method in interface org.orekit.control.indirect.adjoint.CartesianAdjointEquationTerm
Computes the contribution to the rates of the adjoint variables.
getRatesContribution(AbsoluteDate, double[], double[], Frame) - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointInertialTerm
Computes the contribution to the rates of the adjoint variables.
getRateStates() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination
Get attitude rate states.
getRateType() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata
Get attitude rate element set type.
getRatio() - Method in enum org.orekit.gnss.Frequency
Get the ratio f/f0, where f0 is the common frequency.
getRatio() - Method in interface org.orekit.gnss.GnssSignal
Get the ratio f/f0, where f0 is the common frequency.
getRatio() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext
Get the ratio of satellite period to central body rotation period.
getRatio() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext
Get the ratio of satellite period to central body rotation period.
getRawCnm(int, int) - Method in interface org.orekit.forces.gravity.potential.RawSphericalHarmonicsProvider.RawSphericalHarmonics
Get a spherical harmonic cosine coefficient.
getRawContent() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Get the raw content of the entry.
getRawCorrectionRange() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the raw correction for range.
getRawDrivers() - Method in class org.orekit.utils.ParameterDriversList.DelegatingDriver
Get the raw drivers to which this one delegates.
getRawPosition(AbsoluteDate) - Method in interface org.orekit.bodies.JPLEphemeridesLoader.RawPVProvider
Get the position at date.
getRawPosition(FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.JPLEphemeridesLoader.RawPVProvider
Get the position at date.
getRawProvider() - Method in class org.orekit.frames.InterpolatingTransformProvider
Get the underlying provider for raw (non-interpolated) transforms.
getRawProvider() - Method in class org.orekit.frames.ShiftingTransformProvider
Get the underlying provider for raw (non-interpolated) transforms.
getRawPV(AbsoluteDate) - Method in interface org.orekit.bodies.JPLEphemeridesLoader.RawPVProvider
Get the position-velocity at date.
getRawPV(FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.JPLEphemeridesLoader.RawPVProvider
Get the position-velocity at date.
getRawRangeModulus() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the raw range modulus.
getRawSnm(int, int) - Method in interface org.orekit.forces.gravity.potential.RawSphericalHarmonicsProvider.RawSphericalHarmonics
Get a spherical harmonic sine coefficient.
getRbar() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Get the critical distance.
getRcs() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties
Get the typical (50th percentile) radar cross-section.
getRcvrClkOffset() - Method in class org.orekit.estimation.measurements.gnss.CombinedObservationDataSet
Get receiver clock offset.
getRcvrClkOffset() - Method in class org.orekit.files.rinex.observation.ObservationDataSet
Get receiver clock offset.
getRdmMessageLink() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the Unique identifier of Reentry Data Message linked to this Orbit Data Message.
getReal(int, int) - Method in class org.orekit.utils.LoveNumbers
Get the real part of a nominal Love numbers.
getRealAPV(AbsolutePVCoordinates, AbsoluteDate, Frame) - Method in class org.orekit.bodies.CR3BPSystem
Get the AbsolutePVCoordinates from normalized units to standard units in an output frame.
getReceiveAmplitude() - Method in class org.orekit.files.ilrs.CRD.FrRangeMeasurement
Get the receive amplitude.
getReceiveBand() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the receiveBand.
getReceiveDelays() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for receiveDelays.
getReceiver() - Method in class org.orekit.estimation.measurements.gnss.AmbiguityDriver
Get receiver id.
getReceiverIdentifier() - Method in class org.orekit.files.rinex.clock.RinexClock.Receiver
Getter for the receiver identifier.
getReceiverNumber() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Get the number of the receiver.
getReceivers() - Method in class org.orekit.files.rinex.clock.RinexClock
Getter for the receivers.
getReceiversAntennas() - Method in class org.orekit.gnss.antenna.AntexLoader
Get parsed receivers antennas.
getReceiverStation() - Method in class org.orekit.estimation.measurements.BistaticRange
Get the receiver ground station.
getReceiverStation() - Method in class org.orekit.estimation.measurements.BistaticRangeRate
Get the receiver ground station.
getReceiverType() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Get the type of the receiver.
getReceiverVersion() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Get the version of the receiver.
getRecommendedOdSpan() - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters
Get the recommended OD time span calculated for the object.
getRecommendedOdSpan() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get time span of observation recommended for the OD of the object.
getRecordType() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord
Get the type of record.
getRecordType() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
Get the type of record.
getRecordType() - Method in class org.orekit.gnss.metric.ntrip.NetworkRecord
Get the type of record.
getRecordType() - Method in class org.orekit.gnss.metric.ntrip.Record
Get the type of record.
getReductionTheory() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get reduction theory used for precession and nutation modeling.
getReferenceAtTCA() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Get reference's orbit at time of closest approach.
getReferenceAtTCA() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition
Get reference's orbit at time of closest approach.
getReferenceAttitude() - Method in class org.orekit.attitudes.FixedRate
Get the reference attitude.
getReferenceClocks() - Method in class org.orekit.files.rinex.clock.RinexClock
Getter for the reference clocks.
getReferenceCovariance() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Get reference's covariance.
getReferenceCovariance() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition
Get reference's covariance.
getReferenceDate() - Method in class org.orekit.files.ccsds.definitions.TimeConverter
Get the reference date for relative dates (may be null if no relative dates are used).
getReferenceDate() - Method in class org.orekit.files.ccsds.utils.ContextBinding
Get initial date.
getReferenceDate() - Method in class org.orekit.files.rinex.navigation.TimeSystemCorrection
Getter for the reference date of the time system correction polynomial.
getReferenceDate() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
Get the reference date for the harmonics.
getReferenceDate() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider
Get the reference date for the harmonics.
getReferenceDate() - Method in class org.orekit.propagation.integration.FieldStateMapper
Get reference date.
getReferenceDate() - Method in class org.orekit.propagation.integration.StateMapper
Get reference date.
getReferenceDate() - Method in class org.orekit.utils.ParameterDriver
Get current reference date.
getReferenceDate() - Method in class org.orekit.utils.SecularAndHarmonic
Get the reference date.
getReferenceEpoch() - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage
Get the reference epoch.
getReferenceEpoch() - Method in class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage
Get the reference epoch.
getReferenceFrame() - Method in class org.orekit.attitudes.Attitude
Get the reference frame.
getReferenceFrame() - Method in class org.orekit.attitudes.AttitudeInterpolator
Get reference frame from which attitude is defined.
getReferenceFrame() - Method in class org.orekit.attitudes.FieldAttitude
Get the reference frame.
getReferenceFrame() - Method in class org.orekit.attitudes.FieldAttitudeInterpolator
Get reference frame from which attitude is defined.
getReferenceFrame() - Method in class org.orekit.estimation.measurements.AngularRaDec
Get the reference frame in which the right ascension - declination angles are given.
getReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistory
Get the reference frame from which attitude is defined.
getReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSegment
Get the reference frame from which attitude is defined.
getReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.odm.CartesianCovariance
Get the reference frame.
getReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.odm.OdmCommonMetadata
Get the value of REF_FRAME as an Orekit Frame.
getReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver
Get Coordinate system for velocity increment vector.
getReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Get the the value of REFERENCE_FRAME as an Orekit Frame.
getReferenceFrame() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.AttitudeEphemerisSegment
Get the reference frame from which attitude is defined.
getReferenceFrame() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment
Get the reference frame from which attitude is defined.
getReferenceInertialFrame() - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointInertialTerm
Getter for reference frame.
getReferenceName() - Method in class org.orekit.files.rinex.clock.RinexClock.ReferenceClock
Getter for the name of the receiver/satellite embedding the reference clock.
getReferenceRadius() - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Get the reference radius of the central body attraction model.
getReferenceRadius() - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Get the reference radius of the central body attraction model.
getReferenceTimeSystem() - Method in class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage
Get the time system used as a reference to define a time system.
getReferenceTrajectories() - Method in class org.orekit.estimation.sequential.KalmanModel
Getter for the reference trajectories.
getReferenceValue() - Method in class org.orekit.utils.ParameterDriver
Get reference parameter value.
getRefFrame() - Method in class org.orekit.files.ccsds.definitions.ModifiedFrame
Get the CCSDS reference frame.
getRefFrame() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get the value of REF_FRAME as an Orekit Frame.
getRefFrame() - Method in class org.orekit.files.ilrs.CPFHeader
Get the reference frame.
getRefFrameId() - Method in class org.orekit.files.ilrs.CPFHeader
Get the reference frame identifier.
getReflectance() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties
Get the typical (50th percentile) coefficient of reflectance.
getReflection() - Method in class org.orekit.forces.Panel
Get radiation pressure specular reflection coefficient.
getRefraction(double) - Method in interface org.orekit.models.AtmosphericRefractionModel
Compute the refraction angle from the true (geometrical) elevation.
getRefraction(double) - Method in class org.orekit.models.earth.EarthITU453AtmosphereRefraction
 
getRefraction(double) - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction
 
getRefractionModel() - Method in class org.orekit.propagation.events.ElevationDetector
Returns the currently configured refraction model.
getRefractionModel() - Method in class org.orekit.propagation.events.FieldElevationDetector
Returns the currently configured refraction model.
getRegionCode() - Method in class org.orekit.files.rinex.navigation.IonosphereKlobucharMessage
Get the region code.
getRegistrationAddress() - Method in class org.orekit.gnss.metric.ntrip.NetworkRecord
Get the web or mail address for registration.
getRelativeMetadata() - Method in class org.orekit.files.ccsds.ndm.cdm.Cdm
Get the file metadata.
getRelativeMetadata() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get the relative metadata following header, they are the common metadata for the CDM.
getRelativePosition() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the Object2’s position vector relative to Object1's at TCA in RTN frame, getX for R component, getY for T component, getZ for N component.
getRelativeSpeed() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the norm of relative velocity vector at TCA.
getRelativeVelocity() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the Object2’s velocity vector relative to Object1's at TCA in RTN frame, getX for R component, getY for T component, getZ for N component.
getRelaxationTime() - Method in class org.orekit.models.earth.displacement.PsdCorrection
Get relaxation time.
getRemainingDv() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Get the total ΔV remaining for spacecraft.
getRemoteClock() - Method in class org.orekit.estimation.measurements.gnss.AbstractInterSatellitesMeasurement
Get emitting satellite clock provider.
getRemoteClock() - Method in class org.orekit.estimation.measurements.gnss.AbstractOnBoardMeasurement
Get emitting satellite clock provider.
getRemoteClock() - Method in class org.orekit.estimation.measurements.gnss.AbstractOneWayGNSSMeasurement
Get emitting satellite clock provider.
getRemoteClock(int, Map<String, Integer>) - Method in class org.orekit.estimation.measurements.gnss.AbstractOnBoardMeasurement
Get emitting satellite clock provider.
getRemoteOffset() - Method in class org.orekit.estimation.measurements.gnss.OnBoardCommonParametersWithDerivatives
Get remote clock offset.
getRemoteOffset() - Method in class org.orekit.estimation.measurements.gnss.OnBoardCommonParametersWithoutDerivatives
Get remote clock offset.
getRemotePV() - Method in class org.orekit.estimation.measurements.gnss.OnBoardCommonParametersWithDerivatives
Get remote satellite position/velocity.
getRemotePV() - Method in class org.orekit.estimation.measurements.gnss.OnBoardCommonParametersWithoutDerivatives
Get remote satellite position/velocity.
getRemotePV(SpacecraftState[]) - Method in class org.orekit.estimation.measurements.gnss.AbstractInterSatellitesMeasurement
Get emitting satellite position/velocity provider.
getRemotePV(SpacecraftState[]) - Method in class org.orekit.estimation.measurements.gnss.AbstractOnBoardMeasurement
Get emitting satellite position/velocity provider.
getRemotePV(SpacecraftState[]) - Method in class org.orekit.estimation.measurements.gnss.AbstractOneWayGNSSMeasurement
Get emitting satellite position/velocity provider.
getRemotePV(SpacecraftState[], int) - Method in class org.orekit.estimation.measurements.gnss.AbstractInterSatellitesMeasurement
Get emitting satellite position/velocity provider.
getRemotePV(SpacecraftState[], int) - Method in class org.orekit.estimation.measurements.gnss.AbstractOnBoardMeasurement
Get emitting satellite position/velocity provider.
getRemotePV(SpacecraftState[], int) - Method in class org.orekit.estimation.measurements.gnss.AbstractOneWayGNSSMeasurement
Get emitting satellite position/velocity provider.
getRemoteRate() - Method in class org.orekit.estimation.measurements.gnss.OnBoardCommonParametersWithDerivatives
Get remote clock rate.
getRemoteRate() - Method in class org.orekit.estimation.measurements.gnss.OnBoardCommonParametersWithoutDerivatives
Get remote clock rate.
getrEq() - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointJ2Term
Getter for central body equatorial radius.
getrEq() - Method in class org.orekit.forces.gravity.J2OnlyPerturbation
Getter for equatorial radius.
getReserved03() - Method in class org.orekit.gnss.rflink.gps.SubFrame4A
Get the reserved field in word 3.
getReserved03() - Method in class org.orekit.gnss.rflink.gps.SubFrame4B
Get the reserved field in word 3.
getReserved04() - Method in class org.orekit.gnss.rflink.gps.SubFrame1
Get the reserved field in word 4.
getReserved04() - Method in class org.orekit.gnss.rflink.gps.SubFrame4A
Get the reserved field in word 4.
getReserved04() - Method in class org.orekit.gnss.rflink.gps.SubFrame4B
Get the reserved field in word 4.
getReserved05() - Method in class org.orekit.gnss.rflink.gps.SubFrame1
Get the reserved field in word 5.
getReserved05() - Method in class org.orekit.gnss.rflink.gps.SubFrame4A
Get the reserved field in word 5.
getReserved05() - Method in class org.orekit.gnss.rflink.gps.SubFrame4B
Get the reserved field in word 5.
getReserved06() - Method in class org.orekit.gnss.rflink.gps.SubFrame1
Get the reserved field in word 6.
getReserved06() - Method in class org.orekit.gnss.rflink.gps.SubFrame4A
Get the reserved field in word 6.
getReserved06() - Method in class org.orekit.gnss.rflink.gps.SubFrame4B
Get the reserved field in word 6.
getReserved07() - Method in class org.orekit.gnss.rflink.gps.SubFrame1
Get the reserved field in word 7.
getReserved07() - Method in class org.orekit.gnss.rflink.gps.SubFrame4A
Get the reserved field in word 7.
getReserved07() - Method in class org.orekit.gnss.rflink.gps.SubFrame4B
Get the reserved field in word 7.
getReserved08() - Method in class org.orekit.gnss.rflink.gps.SubFrame4A
Get the reserved field in word 8.
getReserved08() - Method in class org.orekit.gnss.rflink.gps.SubFrame4B
Get the reserved field in word 8.
getReserved09() - Method in class org.orekit.gnss.rflink.gps.SubFrame4B
Get the reserved field in word 9.
getReserved10() - Method in class org.orekit.gnss.rflink.gps.SubFrame4A
Get the reserved field in word 10.
getReserved10() - Method in class org.orekit.gnss.rflink.gps.SubFrame4B
Get the reserved field in word 10.
getReserved10() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D
Get reserved field in word 10.
getReserved10() - Method in class org.orekit.gnss.rflink.gps.SubFrame4E
Get the reserved field in word 10.
getReserved8() - Method in class org.orekit.gnss.rflink.gps.SubFrame4E
Get the reserved field in word 8.
getReservedA09() - Method in class org.orekit.gnss.rflink.gps.SubFrame4A
Get the reserved field A in word 9.
getReservedA10() - Method in class org.orekit.gnss.rflink.gps.SubFrame5B
Get the reserved field A in word 10.
getReservedB09() - Method in class org.orekit.gnss.rflink.gps.SubFrame4A
Get the reserved field B in word 9.
getReservedB10() - Method in class org.orekit.gnss.rflink.gps.SubFrame5B
Get the reserved field B in word 10.
getResetAtEnd() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Getter for the resetting flag regarding initial state.
getResetAtEnd() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Getter for the resetting flag regarding initial state.
getResidualsAccepted() - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters
Get the percentage of residuals accepted in the OD of the object (from 0 to 100).
getResults() - Method in class org.orekit.estimation.measurements.gnss.AbstractCycleSlipDetector
Get on all the results computed by the detector (e.g.: dates of cycle-slip).
getRetrogradeFactor() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the retrograde factor.
getRetrogradeFactor() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get the retrograde factor.
getReturnRate() - Method in class org.orekit.files.ilrs.CRD.Calibration
Get the return rate.
getReturnRate() - Method in class org.orekit.files.ilrs.CRD.NptRangeMeasurement
Get the return rate.
getRevAtEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
Get the revolution rumber.
getReversedProvider(TransformProvider) - Static method in class org.orekit.frames.TransformProviderUtils
Reverse a transform provider.
getRevolutionNumberAtEpoch() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get the revolution number.
getRevolutionNumberAtEpoch() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the revolution number.
getRightAscensionOfAscendingNode() - Method in class org.orekit.orbits.CircularOrbit
Get the right ascension of the ascending node.
getRightAscensionOfAscendingNode() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the right ascension of the ascending node.
getRightAscensionOfAscendingNode() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the right ascension of the ascending node.
getRightAscensionOfAscendingNode() - Method in class org.orekit.orbits.KeplerianOrbit
Get the right ascension of the ascending node.
getRightAscensionOfAscendingNodeDot() - Method in class org.orekit.orbits.CircularOrbit
Get the right ascension of the ascending node derivative.
getRightAscensionOfAscendingNodeDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the right ascension of the ascending node derivative.
getRightAscensionOfAscendingNodeDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the right ascension of the ascending node derivative.
getRightAscensionOfAscendingNodeDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the right ascension of the ascending node derivative.
getRms() - Method in class org.orekit.files.ilrs.CRD.Calibration
Get the rms of raw system delay.
getRms() - Method in class org.orekit.files.ilrs.CRD.SessionStatistics
Get the session RMS from the mean of raw accepted time-of-flight values minus the trend function.
getRms() - Method in class org.orekit.propagation.analytical.tle.generation.LeastSquaresTleGenerationAlgorithm
Get the Root Mean Square of the TLE estimation.
getRMS() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Get the Root Mean Square Deviation of the fitting.
getRnml(double, int, int, int, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.UpperBounds
Get the upper bound value Rεn,m,l(γ).
getRnml(T, int, int, int, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.UpperBounds
Get the upper bound value Rεn,m,l(γ).
getRoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTGravityContext
Get roa = R / a.
getRoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTGravityContext
Get roa = R / a.
getRolloverReference() - Static method in class org.orekit.time.GNSSDate
Get the reference date ensuring continuity across GNSS week rollover.
getRoot() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter
Get root element for XML files.
getRoot() - Method in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter
Get root element for XML files.
getRoot() - Method in interface org.orekit.files.ccsds.utils.generation.MessageWriter
Get root element for XML files.
getRoot() - Static method in class org.orekit.frames.Frame
Get the unique root frame.
getRotatingFrame() - Method in class org.orekit.bodies.CR3BPSystem
Get the CR3BP Rotating Frame.
getRotation() - Method in class org.orekit.attitudes.Attitude
Get the attitude rotation.
getRotation() - Method in class org.orekit.attitudes.FieldAttitude
Get the attitude rotation.
getRotation() - Method in interface org.orekit.frames.FieldStaticTransform
Get the underlying elementary rotation.
getRotation() - Method in class org.orekit.frames.FieldTransform
Get the underlying elementary rotation.
getRotation() - Method in interface org.orekit.frames.StaticTransform
Get the underlying elementary rotation.
getRotation() - Method in class org.orekit.frames.Transform
Get the underlying elementary rotation.
getRotation() - Method in class org.orekit.utils.AngularCoordinates
Get the rotation.
getRotation() - Method in class org.orekit.utils.FieldAngularCoordinates
Get the rotation.
getRotationAcceleration() - Method in class org.orekit.attitudes.Attitude
Get the satellite rotation acceleration.
getRotationAcceleration() - Method in class org.orekit.attitudes.FieldAttitude
Get the satellite rotation acceleration.
getRotationAcceleration() - Method in class org.orekit.frames.FieldTransform
Get the second time derivative of the rotation.
getRotationAcceleration() - Method in class org.orekit.frames.Transform
Get the second time derivative of the rotation.
getRotationAcceleration() - Method in class org.orekit.utils.AngularCoordinates
Get the rotation acceleration.
getRotationAcceleration() - Method in class org.orekit.utils.FieldAngularCoordinates
Get the rotation acceleration.
getRotationalAngleType() - Method in class org.orekit.files.ilrs.CPFHeader
Get the rotation angle type.
getRotationAngles() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler
Get the coordinates of the Euler angles.
getRotationRate() - Method in interface org.orekit.frames.FieldKinematicTransform
Get the first time derivative of the rotation.
getRotationRate() - Method in class org.orekit.frames.FieldTransform
Get the first time derivative of the rotation.
getRotationRate() - Method in interface org.orekit.frames.KinematicTransform
Get the first time derivative of the rotation.
getRotationRate() - Method in class org.orekit.frames.Transform
Get the first time derivative of the rotation.
getRotationRate() - Method in class org.orekit.utils.AngularCoordinates
Get the rotation rate.
getRotationRate() - Method in class org.orekit.utils.FieldAngularCoordinates
Get the rotation rate.
getRotationRates() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler
Get the rates of the Euler angles.
getRTNCovarianceBlock() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmData
Get the covariance matrix logical block.
getRTNCovarianceMatrix() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the RTN covariance matrix.
getRunByName() - Method in class org.orekit.files.rinex.section.RinexBaseHeader
Getter for the run/by name.
getS() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey
Get s.
getS10() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader.LineParameters
Get the EUV index (26-34 nm) scaled to F10.
getS10(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData
Get the EUV index (26-34 nm) scaled to F10.
getS10(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters
Get the EUV index (26-34 nm) scaled to F10.
getS10B() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader.LineParameters
Get the EUV 81-day averaged centered index.
getS10B(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData
Get the EUV 81-day averaged centered index.
getS10B(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters
Get the EUV 81-day averaged centered index.
getS2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTJ2SquaredClosedFormContext
Get the sine of the inclination to the power 2.
getS2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTJ2SquaredClosedFormContext
Get the sine of the inclination to the power 2.
getSample() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Get the states sample.
getSatConfiguration() - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac
Gets the satellite configuration.
getSatellite() - Method in class org.orekit.files.rinex.observation.GlonassSatelliteChannel
Get the satellite identifier.
getSatellite() - Method in class org.orekit.files.rinex.observation.ObservationDataSet
Get observed satellite.
getSatellite() - Method in class org.orekit.orbits.WalkerConstellationSlot
Get the satellite index in plane.
getSatelliteCode() - Method in class org.orekit.gnss.antenna.SatelliteAntenna
Get satellite code.
getSatelliteCount() - Method in class org.orekit.files.sp3.SP3
Get the number of satellites contained in this orbit file.
getSatelliteId(SatelliteSystem, int) - Static method in enum org.orekit.gnss.metric.parser.IgsSsrMessageType
Transform the satellite ID parsed from the IGS SSR message to the real ID.
getSatelliteID() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionData
Get the satellite ID.
getSatelliteID() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.RtcmEphemerisData
Get the satellite ID.
getSatelliteID() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgmData
Get the satellite ID.
getSatelliteName() - Method in class org.orekit.estimation.measurements.gnss.CycleSlipDetectorResults
Get the satellite name.
getSatelliteNumber() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get the satellite id.
getSatelliteNumber() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the satellite id.
getSatelliteReferenceDatum() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmOrbitCorrectionHeader
Get the satellite reference datum.
getSatelliteRevolution() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Get the number of satellite revolutions to use for converting osculating to mean elements.
getSatelliteRevolution() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Get the number of satellite revolutions to use for converting osculating to mean elements.
getSatellites() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Get the satellites related to this measurement.
getSatellites() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
Get the satellites related to this measurement.
getSatellites() - Method in interface org.orekit.estimation.measurements.generation.MeasurementBuilder
Get the satellites related to this measurement.
getSatellites() - Method in class org.orekit.estimation.measurements.generation.MultiplexedMeasurementBuilder
Get the satellites related to this measurement.
getSatellites() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
Get the satellites related to this measurement.
getSatellites() - Method in class org.orekit.files.ccsds.ndm.adm.acm.Acm
Get the loaded ephemeris for each satellite in the file.
getSatellites() - Method in class org.orekit.files.ccsds.ndm.adm.aem.Aem
Get the loaded ephemeris for each satellite in the file.
getSatellites() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Ocm
Get the loaded ephemeris for each satellite in the file.
getSatellites() - Method in class org.orekit.files.ccsds.ndm.odm.oem.Oem
Get the loaded ephemeris for each satellite in the file.
getSatellites() - Method in interface org.orekit.files.general.AttitudeEphemerisFile
Get the loaded ephemeris for each satellite in the file.
getSatellites() - Method in interface org.orekit.files.general.EphemerisFile
Get the loaded ephemeris for each satellite in the file.
getSatellites() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile
Get the loaded ephemeris for each satellite in the file.
getSatellites() - Method in class org.orekit.files.general.OrekitEphemerisFile
Get the loaded ephemeris for each satellite in the file.
getSatellites() - Method in class org.orekit.files.ilrs.CPF
Get the loaded ephemeris for each satellite in the file.
getSatellites() - Method in class org.orekit.files.rinex.clock.RinexClock
Getter for the satellites.
getSatellites() - Method in class org.orekit.files.sp3.SP3
 
getSatellites() - Method in class org.orekit.files.stk.STKEphemerisFile
Get the loaded ephemeris for each satellite in the file.
getSatellitesAntennas() - Method in class org.orekit.gnss.antenna.AntexLoader
Get parsed satellites antennas.
getSatelliteSystem() - Method in class org.orekit.estimation.measurements.gnss.CombinedObservationDataSet
Get Satellite System.
getSatelliteSystem() - Method in class org.orekit.files.rinex.AppliedDCBS
Get the satellite system.
getSatelliteSystem() - Method in class org.orekit.files.rinex.AppliedPCVS
Get the satellite system.
getSatelliteSystem() - Method in class org.orekit.files.rinex.clock.RinexClock
Getter for the satellite system.
getSatelliteSystem() - Method in class org.orekit.files.rinex.observation.PhaseShiftCorrection
Get the Satellite System.
getSatelliteSystem() - Method in class org.orekit.files.rinex.section.RinexBaseHeader
Getter for the satellite system.
getSatelliteSystem() - Method in class org.orekit.gnss.antenna.SatelliteAntenna
Get satellite system.
getSatelliteSystem() - Method in enum org.orekit.gnss.Frequency
Get the satellite system for which this frequency is defined.
getSatelliteSystem() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionMessage
Get the satellite system associated to the message.
getSatelliteSystem() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgmMessage
Get the satellite system associated to the message.
getSatelliteSytem() - Method in class org.orekit.files.sinex.DcbSatellite
Get the satellite sytem corresponding to the satellite.
getSatelliteType() - Method in class org.orekit.gnss.antenna.SatelliteAntenna
Get satellite type.
getSatelliteType() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage
Getter for satellite type.
getSatIds() - Method in class org.orekit.files.sp3.SP3Header
Get the satellite identifiers.
getSatsCorrected() - Method in class org.orekit.files.rinex.observation.PhaseShiftCorrection
Get the list of satellites involved.
getSaturn() - Method in interface org.orekit.bodies.CelestialBodies
Get the Saturn singleton body.
getSaturn() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Saturn singleton body.
getSaturn() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
 
getSbasId() - Method in class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage
Get the SBAS Id.
getSBASNavigationMessages() - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Get all the SBAS navigation messages contained in the file.
getSBASNavigationMessages(String) - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Get the SBAS navigation messages for the given satellite Id.
getSBASOrbitalElements() - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator
Get the underlying SBAS orbital elements.
getScale() - Method in class org.orekit.utils.ParameterDriver
Get scale.
getScale() - Method in class org.orekit.utils.units.PowerTerm
Get the scaling factor.
getScale() - Method in class org.orekit.utils.units.Unit
Get the scaling factor to SI units.
getScaleFactor() - Method in class org.orekit.estimation.measurements.modifiers.AbstractRelativisticClockModifier
Get the scale factor used to compute relativistic effect.
getScaleFactorCorrections(SatelliteSystem) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Get the list of scale factor correction.
getScalePositionDefects() - Method in class org.orekit.control.indirect.shooting.AbstractFixedBoundaryCartesianSingleShooting
Getter for scale of position defects.
getScaleVelocityDefects() - Method in class org.orekit.control.indirect.shooting.AbstractFixedBoundaryCartesianSingleShooting
Getter for scale of velocity defects.
getSclkOffsetAtEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the spacecraft clock count at OcmMetadata.getEpochT0().
getSclkSecPerSISec() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the number of spacecraft clock seconds occurring during one SI second.
getScreenEntryTime() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the time in UTC when Object2 enters the screening volume.
getScreenExitTime() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the time in UTC when Object2 exits the screening volume.
getScreeningDataSource() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadata
Get the source (or origin) of the specific orbital data for this object.
getScreenPcThreshold() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the collision probability screening threshold used to identify this conjunction.
getScreenType() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the type of screening to be used.
getScreenVolumeFrame() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the name of the Object1 centered reference frame in which the screening volume data are given.
getScreenVolumeRadius() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the screen volume radius.
getScreenVolumeShape() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the shape of the screening volume.
getScreenVolumeX() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the R or T (depending on if RTN or TVN is selected) component size of the screening volume in the corresponding frame.
getScreenVolumeY() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the T or V (depending on if RTN or TVN is selected) component size of the screening volume in the corresponding frame.
getScreenVolumeZ() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the N component size of the screening volume in the corresponding frame.
getSecInDay() - Method in class org.orekit.time.GLONASSDate
Get the number of seconds since Na start.
getSecond() - Method in class org.orekit.time.FieldTimeStampedPair
Get second time stamped value.
getSecond() - Method in class org.orekit.time.TimeComponents
Get the seconds number.
getSecond() - Method in class org.orekit.time.TimeStampedPair
Get second time stamped value.
getSecondary() - Method in class org.orekit.bodies.CR3BPSystem
Get the secondary CelestialBody.
getSecondary() - Method in class org.orekit.estimation.measurements.gnss.Dipole
Get the secondary dipole vector.
getSecondary() - Method in class org.orekit.propagation.events.InterSatDirectViewDetector
Get the provider for the secondary satellite.
getSecondaryObject() - Method in class org.orekit.propagation.events.AngularSeparationFromSatelliteDetector
Get the secondaryObject.
getSecondaryPVProvider() - Method in class org.orekit.propagation.events.ExtremumApproachDetector
Get the secondary position-velocity provider stored in this instance.
getSecondaryPVProvider() - Method in class org.orekit.propagation.events.FieldExtremumApproachDetector
Get the secondary position-velocity provider stored in this instance.
getSecondaryPVProvider() - Method in class org.orekit.propagation.events.FieldRelativeDistanceDetector
Get the secondary position-velocity provider stored in this instance.
getSecondaryPVProvider() - Method in class org.orekit.propagation.events.RelativeDistanceDetector
Get the secondary position-velocity provider stored in this instance.
getSecondaryStation() - Method in class org.orekit.estimation.measurements.TurnAroundRange
Get the secondary ground station reflecting the signal.
getSecondFrequencyPhaseHistory() - Method in class org.orekit.estimation.measurements.filtering.DualFrequencyHatchFilter
Get the history of phase values of the second frequency.
getSecondsInLocalDay() - Method in class org.orekit.time.TimeComponents
Get the second number within the local day, without applying the offset from UTC.
getSecondsInUTCDay() - Method in class org.orekit.time.TimeComponents
Get the second number within the UTC day, applying the offset from UTC.
getSecondsInWeek() - Method in class org.orekit.time.GNSSDate
Get the number of seconds since week start.
getSecondsOfWeek() - Method in class org.orekit.files.sp3.SP3Header
Returns the seconds of the GPS week as contained in the SP3 file.
getSecondStation() - Method in class org.orekit.estimation.measurements.FDOA
Get the second ground station, the one that gives the measurement.
getSecondStation() - Method in class org.orekit.estimation.measurements.TDOA
Get the second ground station, the one that gives the measurement.
getSecularDegree() - Method in class org.orekit.utils.SecularAndHarmonic
Get degree of polynomial secular part.
getSedr() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Get the amount of energy being removed from the object’s orbit by atmospheric drag.
getSedr() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get Specific Energy Dissipation Rate.
getSefiCollisionProbability() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the Space Environment Fragmentation Impact probability.
getSefiCollisionProbabilityMethod() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the Space Environment Fragmentation Impact probability method.
getSefiFragmentationModel() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the Space Environment Fragmentation Impact fragmentation model.
getSegments() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmSatelliteEphemeris
Get the segments of the attitude ephemeris.
getSegments() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSatelliteEphemeris
Get the segments of the attitude ephemeris.
getSegments() - Method in class org.orekit.files.ccsds.ndm.NdmConstituent
Get the segments.
getSegments() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmSatelliteEphemeris
Get the segments of the ephemeris.
getSegments() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSatelliteEphemeris
Get the segments of the ephemeris.
getSegments() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.SatelliteAttitudeEphemeris
Get the segments of the attitude ephemeris.
getSegments() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris
Get the segments of the ephemeris.
getSegments() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitSatelliteAttitudeEphemeris
Get the segments of the attitude ephemeris.
getSegments() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
Get the segments of the ephemeris.
getSegments() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris
Returns a list containing only this.
getSegments() - Method in class org.orekit.files.sp3.SP3Ephemeris
Get the segments of the ephemeris.
getSegments() - Method in class org.orekit.files.stk.STKEphemerisFile.STKEphemeris
 
getSelectedCoefficients() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Get the selected short periodic coefficients that must be stored as additional states.
getSelectedCoefficients() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Get the selected short periodic coefficients that must be stored as additional states.
getSelectedMu() - Method in class org.orekit.files.ccsds.ndm.odm.OdmParser
Select the gravitational coefficient to use.
getSelectedNormalizedParameters() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Get the current value of selected normalized parameters.
getSelectedNormalizedParameters() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
Get the current value of selected normalized parameters.
getSelectedOrbitalParametersDriversForBuilder(int) - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel
Get the selected orbital drivers for a propagatorBuilder.
getSelectedPropagationDriversForBuilder(int) - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel
Get the selected propagation drivers for a propagatorBuilder.
getSelector() - Method in class org.orekit.estimation.measurements.generation.AbstractScheduler
Get the dates selector.
getSensorFrequency() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationSensor
Get frequency of sensor data for sensor.
getSensorNoiseCovariance() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationSensor
Get standard deviation of sensor noise for sensor.
getSensorNumber() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationSensor
Get number of the sensor.
getSensors() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get description of sensors used.
getSensorsN() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get number of sensors used.
getSensorsUsed() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination
Get sensors used.
getSensorUsed() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationSensor
Get sensor used.
getSeparation() - Method in class org.orekit.utils.OccultationEngine.FieldOccultationAngles
Get apparent separation between occulting and occulted directions.
getSeparation() - Method in class org.orekit.utils.OccultationEngine.OccultationAngles
Get apparent separation between occulting and occulted directions.
getSequenceNumber() - Method in class org.orekit.files.ilrs.ILRSHeader
Get the ephemeris sequence number.
getSerialNumber() - Method in class org.orekit.gnss.antenna.ReceiverAntenna
Get the serial number.
getSessionStatisticsData() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
Get the session statistics data for the data block.
getSessionStatisticsRecord() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
Get the default (the first if there are many records) SessionStat record.
getSessionStatisticsRecord(String) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
Get the session statistics record related to the systemConfigurationId.
getSh() - Method in class org.orekit.models.earth.troposphere.FieldTroposphericDelay
Get slanted delay (m).
getSh() - Method in class org.orekit.models.earth.troposphere.TroposphericDelay
Get slanted delay (m).
getShadowBodies() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get celestial bodies casting shadows.
getShadowModel() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get shadow model used for solar radiation pressure.
getShiftTypeIndicator() - Method in class org.orekit.files.ilrs.CRD.Calibration
Get the calibration shift type indicator.
getShootingPropagationSettings() - Method in class org.orekit.control.indirect.shooting.ShootingBoundaryOutput
Getter for the shooting propagation settings.
getShortPeriodTerms() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Get the short periodic terms.
getShortPeriodTermsValue(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Get the short period terms value.
getSic() - Method in class org.orekit.files.ilrs.ILRSHeader
Get the SIC ID.
getSig3EigVec3CovarianceBlock() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmData
Get the Sigma / Eigenvector covariance logical block.
getSigma() - Method in class org.orekit.estimation.measurements.modifiers.DynamicOutlierFilter
Get the current value of sigma.
getSigmaU() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination
Get rate random walk if AttitudeDetermination.rateStates is RateElementsType.GYRO_BIAS.
getSigmaV() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination
Get angle random walk if AttitudeDetermination.rateStates is RateElementsType.GYRO_BIAS.
getSignal() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage
Getter for signal.
getSignalCode() - Method in enum org.orekit.gnss.ObservationType
Get the signal code.
getSignalID() - Method in class org.orekit.gnss.metric.messages.common.CodeBias
Get the GNSS signal and tracking mode identifier.
getSignalID() - Method in class org.orekit.gnss.metric.messages.common.PhaseBias
Get the GNSS signal and tracking mode identifier.
getSignalStrength() - Method in class org.orekit.files.rinex.observation.ObservationData
Get the signal strength.
getSignalStrengthUnit() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Get the unit of the carrier to noise ratio observables.
getSignalWideLaneIntegerIndicator() - Method in class org.orekit.gnss.metric.messages.common.PhaseBias
Get the signal Wide-Lane integer indicator.
getSij(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldFourierCjSjCoefficients
Get the coefficient Sij.
getSij(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FourierCjSjCoefficients
Get the coefficient Sij.
getSinexCode() - Method in class org.orekit.gnss.antenna.Antenna
Get the sinex code of the antenna.
getSingularPoints() - Method in class org.orekit.models.earth.tessellation.AlongTrackAiming
Get points at which aiming direction cannot be computed.
getSingularPoints() - Method in class org.orekit.models.earth.tessellation.ConstantAzimuthAiming
Get points at which aiming direction cannot be computed.
getSingularPoints() - Method in class org.orekit.models.earth.tessellation.DivertedSingularityAiming
Get points at which aiming direction cannot be computed.
getSingularPoints() - Method in interface org.orekit.models.earth.tessellation.TileAiming
Get points at which aiming direction cannot be computed.
getSisa() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage
Getter for the signal in space accuracy (m).
getSisaiOc1() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage
Getter for Signal In Space Accuracy Index (clock drift accuracy).
getSisaiOc2() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage
Getter for Signal In Space Accuracy Index (clock drift rate accuracy).
getSisaiOcb() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage
Getter for Signal In Space Accuracy Index (radial and clock).
getSisaiOe() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage
Getter for Signal In Space Accuracy Index (along track and across track).
getSismai() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage
Getter for Signal In Space Monitoring Accuracy Index.
getSiteCode() - Method in class org.orekit.files.sinex.DcbStation
Get the site code (station identifier).
getSiteCode() - Method in class org.orekit.files.sinex.Station
Get the site code (station identifier).
getSiteLocation() - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
Get the site location.
getSiteName() - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
Get the site name.
getSites() - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficientsBLQFactory
Get the list of sites for which we have found coefficients, in lexicographic order ignoring case.
getSize() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Get the size of the problem.
getSize() - Method in class org.orekit.utils.LoveNumbers
Get the size of the arrays.
getSj(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
Get the Sj coefficient.
getSj(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient
Get the Sj coefficient.
getSkew() - Method in class org.orekit.files.ilrs.CRD.Calibration
Get the skew of raw system delay values from the mean.
getSkewness() - Method in class org.orekit.files.ilrs.CRD.SessionStatistics
Get the session skewness from the mean of raw accepted time-of-flight values minus the trend function.
getSkimmingAltitude() - Method in class org.orekit.propagation.events.InterSatDirectViewDetector
Get the skimming altitude.
getSlope() - Method in class org.orekit.time.OffsetModel
Offset slope in seconds per UTC day (TAI minus UTC / dUTC).
getSlots() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the number of slots in use.
getSlotsEvictions() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the number of slots evictions.
getSma() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Getter for the semi-major axis.
getSma() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
Gets the Semi-Major Axis.
getSma() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the semi-major axis.
getSma() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get the semi-major axis.
getSmoothedData() - Method in class org.orekit.estimation.measurements.filtering.SmoothedObservationDataSet
Get the smoothed observation data.
getSnm() - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data
Get the sine parameters of spherical harmonics expansion of degree N and order M.
getSnr() - Method in class org.orekit.files.ilrs.CRD.RangeMeasurement
Get the signal to noise ratio.
getSoftwareId() - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration
Get the software configuration ID.
getSoftwareRecord() - Method in class org.orekit.files.ilrs.CRDConfiguration
Get the software configuration record.
getSoftwareRecord(CRDConfiguration.SystemConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration
Get software configuration record related to the systemRecord.
getSolarRadArea() - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters
Get the solar radiation pressure area.
getSolarRadCoeff() - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters
Get the solar radiation pressure coefficient.
getSolarRadiationPressure() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get Enum YesNoUnknown that indicates if Solar Radiation Pressure is taken into account or not.
getSolarSystemBarycenter() - Method in interface org.orekit.bodies.CelestialBodies
Get the solar system barycenter aggregated body.
getSolarSystemBarycenter() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the solar system barycenter aggregated body.
getSolarSystemBarycenter() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
 
getSolidPoleTide(EOPHistory) - Method in enum org.orekit.utils.IERSConventions
Get the function computing solid pole tide (ΔC₂₁, ΔS₂₁).
getSolidTidesModel() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get solid tides model.
getSolution() - Method in class org.orekit.estimation.measurements.gnss.IntegerLeastSquareSolution
Get the solution array.
getSolutionsSize() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Get the number of solutions found.
getSolveN() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get number of solved-for states.
getSolveStates() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get description of state elements solved-for.
getSource() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination
Get source of attitude estimate.
getSource() - Method in class org.orekit.files.ilrs.CPFHeader
Get the ephemeris source.
getSource() - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac
Gets the source of this GPS almanac.
getSource() - Method in class org.orekit.propagation.analytical.gnss.data.QZSSAlmanac
Gets the source of this QZSS almanac.
getSourceDCBS() - Method in class org.orekit.files.rinex.AppliedDCBS
Get the source of corrections.
getSourceIdentifier() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord
Get the source identifier.
getSourceIdentifier() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
Get the source identifier.
getSourcePCVS() - Method in class org.orekit.files.rinex.AppliedPCVS
Get the source of corrections.
getSourceString() - Method in enum org.orekit.errors.OrekitMessages
getSourceTable() - Method in class org.orekit.gnss.metric.ntrip.NtripClient
Get a sourcetable.
getSouth() - Method in class org.orekit.bodies.FieldGeodeticPoint
Get the direction to the south of point, expressed in parent shape frame.
getSouth() - Method in class org.orekit.bodies.GeodeticPoint
Get the direction to the south of point, expressed in parent shape frame.
getSouth() - Method in class org.orekit.frames.TopocentricFrame
Get the south direction of topocentric frame, expressed in parent shape frame.
getSouthAmplitude(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
Get the amplitude along South axis.
getSouthPhase(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
Get the phase along South axis.
getSpacecraft() - Method in class org.orekit.forces.drag.DragForce
Get spacecraft that are sensitive to atmospheric drag forces.
getSpacecraft() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Get spacecraft shape.
getSpacecraft() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Get spacecraft shape.
getSpacecraftBodyFrame() - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints
Get the spacecraft body frame.
getSpacecraftClockAndDriftApplied() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
Get the spacecraft clock offset and drift applied indicator.
getSpacecraftEpochTimeScale() - Method in class org.orekit.files.ilrs.CRDHeader
Get the spacecraft epoch time scale.
getSpacecraftParametersBlock() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmData
Get the spacecraft parameters logical block.
getSpacecraftParametersBlock() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData
Get the spacecraft parameters logical block.
getSpaceWeatherEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get epoch of the Space Weather data.
getSpaceWeatherSource() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get Space Weather data source.
getSpan() - Method in class org.orekit.files.ilrs.CRD.Calibration
Get the calibration span.
getSpan(AbsoluteDate) - Method in class org.orekit.utils.TimeSpanMap
Get the time span containing a specified date.
getSpanAfter() - Method in class org.orekit.utils.TimeSpanMap.Transition
Get the TimeSpanMap.Span valid after transition.
getSpanBefore() - Method in class org.orekit.utils.TimeSpanMap.Transition
Get the TimeSpanMap.Span valid before transition.
getSpansNumber() - Method in class org.orekit.utils.TimeSpanMap
Get the number of spans.
getSpatialFilter() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Get the spatial filter.
getSpecialXmlElementsBuilders() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmParser
Get the non-default token builders for special XML elements.
getSpecialXmlElementsBuilders() - Method in class org.orekit.files.ccsds.ndm.adm.AdmParser
Get the non-default token builders for special XML elements.
getSpecialXmlElementsBuilders() - Method in class org.orekit.files.ccsds.ndm.NdmParser
Get the non-default token builders for special XML elements.
getSpecialXmlElementsBuilders() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser
Get the non-default token builders for special XML elements.
getSpecialXmlElementsBuilders() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser
Get the non-default token builders for special XML elements.
getSpecialXmlElementsBuilders() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser
Get the non-default token builders for special XML elements.
getSpecialXmlElementsBuilders() - Method in interface org.orekit.files.ccsds.utils.lexical.MessageParser
Get the non-default token builders for special XML elements.
getSpecialXmlElementsBuilders() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser
Get the non-default token builders for special XML elements.
getSpecifier() - Method in interface org.orekit.errors.LocalizedException
Get the localizable specifier of the error message.
getSpecifier() - Method in exception org.orekit.errors.OrekitException
Get the localizable specifier of the error message.
getSpecifier() - Method in exception org.orekit.errors.OrekitIllegalArgumentException
Get the localizable specifier of the error message.
getSpecifier() - Method in exception org.orekit.errors.OrekitIllegalStateException
Get the localizable specifier of the error message.
getSpecifier() - Method in exception org.orekit.errors.OrekitInternalError
Get the localizable specifier of the error message.
getSpecifier() - Method in exception org.orekit.errors.OrekitIOException
Get the localizable specifier of the error message.
getSpecifier() - Method in exception org.orekit.errors.OrekitParseException
Get the localizable specifier of the error message.
getSpectralFilter() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Get the spectral filter.
getSphericalHarmonicsDegree() - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data
Get the degree of spherical harmonic expansion.
getSphericalHarmonicsOrder() - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data
Get the order of spherical harmonic expansion.
getSpin() - Method in class org.orekit.attitudes.Attitude
Get the satellite spin.
getSpin() - Method in class org.orekit.attitudes.FieldAttitude
Get the satellite spin.
getSpin() - Method in class org.orekit.models.earth.ReferenceEllipsoid
Gets the rotation of the ellipsoid about its axis.
getSpinAlpha() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
Get the right ascension of spin axis vector (rad).
getSpinAngle() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
Get the phase of the satellite about the spin axis (rad).
getSpinAngleVel() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
Get the angular velocity of satellite around spin axis (rad/s).
getSpinDelta() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
Get the declination of the spin axis vector (rad).
getSpinStabilizedBlock() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData
Get the spin-stabilized logical block.
getSqrtA() - Method in class org.orekit.gnss.rflink.gps.SubFrame2
Get √a.
getSqrtA() - Method in class org.orekit.gnss.rflink.gps.SubFrameAlmanac
Get √a.
getSqrtA() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Getter for Square Root of Semi-Major Axis (√m).
getSquaredDistance() - Method in class org.orekit.estimation.measurements.gnss.IntegerLeastSquareSolution
Get the squared distance to the corresponding float solution.
getSrpCoefficient() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Get the nominal SRP coefficient.
getSrpConstantArea() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Get the attitude-independent SRP area, not already into attitude-dependent area along OEB.
getSrpModel() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get Solar Radiation Pressure model.
getSrpUncertainty() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Get the SRP coefficient 1σ uncertainty.
getSsrEpoch1s() - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader
Get the SSR Epoch Time 1s.
getSsrIgm01Data() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01
Get the SSR IGM01 data parsed in the SSR message.
getSsrIgm02Data() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm02
Get the SSR IGM02 data parsed in the SSR message.
getSsrIgm03Data() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03
Get the SSR IGM03 data parsed in the SSR message.
getSsrIgm04Data() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm04
Get the SSR IGM04 data parsed in the SSR message.
getSsrIgm05Data() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm05
Get the SSR IGM05 data parsed in the SSR message.
getSsrIgm06Data() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06
Get the SSR IGM06 data parsed in the SSR message.
getSsrIgm07Data() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm07
Get the SSR IGM07 data parsed in the SSR message.
getSsrMultipleMessageIndicator() - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader
Get the SSR Multiple Message Indicator.
getSsrProviderId() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionHeader
Get the SSR Provider ID.
getSsrProviderId() - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader
Get the SSR Provider ID.
getSsrSolutionId() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionHeader
Get the SSR Solution ID.
getSsrSolutionId() - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader
Get the SSR Solution ID.
getSsrUpdateInterval() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionHeader
Get the SSR Update Interval.
getSsrUpdateInterval() - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader
Get the SSR Update Interval.
getSsrUra() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm07Data
Get the SSR User Range Accuracy (URA).
getStandardModel() - Static method in class org.orekit.models.earth.troposphere.ModifiedSaastamoinenModel
Create a new Saastamoinen model using a standard atmosphere model.
getStandardModel() - Static method in class org.orekit.models.earth.troposphere.SaastamoinenModel
Deprecated.
Create a new Saastamoinen model using a standard atmosphere model.
getStandardModel(double) - Static method in class org.orekit.models.earth.troposphere.MariniMurrayModel
Deprecated.
Create a new Marini-Murray model using a standard atmosphere model.
getStandardModel(double) - Static method in class org.orekit.models.earth.troposphere.MendesPavlisModel
Deprecated.
getStandardModel(double, Unit) - Static method in class org.orekit.models.earth.troposphere.MendesPavlisModel
Create a new Mendes-Pavlis model using a standard atmosphere model.
getStart() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
Get the start of the measurements time span.
getStart() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmSatelliteEphemeris
Get the start date of the ephemeris.
getStart() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistory
Get the start date of this ephemeris segment.
getStart() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Get the start date of this ephemeris segment.
getStart() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSatelliteEphemeris
Get the start date of the ephemeris.
getStart() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSegment
Get the start date of this ephemeris segment.
getStart() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmSatelliteEphemeris
Get the start date of the ephemeris.
getStart() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory
Get the start date of this ephemeris segment.
getStart() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSatelliteEphemeris
Get the start date of the ephemeris.
getStart() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSegment
Get the start date of this ephemeris segment.
getStart() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.AttitudeEphemerisSegment
Get the start date of this ephemeris segment.
getStart() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.SatelliteAttitudeEphemeris
Get the start date of the ephemeris.
getStart() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
Get the start date of this ephemeris segment.
getStart() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris
Get the start date of the ephemeris.
getStart() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment
Get the start date of this ephemeris segment.
getStart() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitSatelliteAttitudeEphemeris
Get the start date of the ephemeris.
getStart() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
Get the start date of this ephemeris segment.
getStart() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
Get the start date of the ephemeris.
getStart() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris
Get the start date of the ephemeris.
getStart() - Method in class org.orekit.files.sp3.SP3Ephemeris
Get the start date of the ephemeris.
getStart() - Method in class org.orekit.files.sp3.SP3Segment
Get the start date of this ephemeris segment.
getStart() - Method in class org.orekit.files.stk.STKEphemerisFile.STKEphemeris
 
getStart() - Method in class org.orekit.files.stk.STKEphemerisFile.STKEphemerisSegment
 
getStart() - Method in class org.orekit.time.OffsetModel
Get the date of the offset start.
getStart() - Method in class org.orekit.utils.TimeSpanMap.Span
Get the start of this time span.
getStartDate() - Method in class org.orekit.files.rinex.clock.RinexClock.ReferenceClock
Getter for the validity period start date.
getStartDate() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Get the start date.
getStartDate() - Method in class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers
Get the start date.
getStartDate() - Method in class org.orekit.frames.EOPHistory
Get the date of the first available Earth Orientation Parameters.
getStartDate() - Method in class org.orekit.propagation.AbstractPropagator
Get the start date.
getStartDate() - Method in class org.orekit.propagation.FieldAbstractPropagator
Get the start date.
getStartDetector() - Method in class org.orekit.forces.maneuvers.trigger.StartStopEventsTrigger
Getter for the firing start detector.
getStartDriver() - Method in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector
Get the driver for start date.
getStartDriver() - Method in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector
Get the driver for start date.
getStartEpoch() - Method in class org.orekit.files.ilrs.ILRSHeader
Get the starting epoch (UTC).
getStartScreenPeriod() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the start time in UTC of the screening period for the conjunction assessment.
getStartTime() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata
Get the time of the earliest data contained in the OCM.
getStartTime() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Get start of total time span covered by attitude data.
getStartTime() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the time of the earliest data contained in the OCM.
getStartTime() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata
Get start of total time span covered by ephemerides data and covariance data.
getStartTime() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the startTime.
getStartTransition() - Method in class org.orekit.utils.TimeSpanMap.Span
Get the transition at start of this time span.
getState() - Method in class org.orekit.estimation.measurements.CommonParametersWithDerivatives
Get spacecraft state.
getState() - Method in class org.orekit.estimation.measurements.CommonParametersWithoutDerivatives
Get spacecraft state.
getState() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalGradientConverter
Get the state with the number of parameters consistent with the propagation model.
getState() - Method in class org.orekit.propagation.events.EventsLogger.LoggedEvent
Get the triggering state.
getState() - Method in class org.orekit.propagation.events.FieldEventsLogger.FieldLoggedEvent
Get the triggering state.
getState() - Method in class org.orekit.propagation.events.handlers.FieldRecordAndContinue.Event
Get the spacecraft's state at the event.
getState() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue.Event
Get the spacecraft's state at the event.
getState(ParameterDriversProvider) - Method in class org.orekit.propagation.integration.AbstractGradientConverter
Get the state with the number of parameters consistent with parametric model.
getStateCovariance(SpacecraftState) - Method in class org.orekit.propagation.StateCovarianceMatrixProvider
Get the state covariance in the same frame/local orbital frame, orbit type and position angle as the initial covariance.
getStateCovariance(SpacecraftState, Frame) - Method in class org.orekit.propagation.StateCovarianceMatrixProvider
Get the state covariance expressed in a given frame.
getStateCovariance(SpacecraftState, OrbitType, PositionAngleType) - Method in class org.orekit.propagation.StateCovarianceMatrixProvider
Get the state covariance expressed in a given orbit type.
getStateDerivatives(int) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Get the partial derivatives of the simulated measurement with respect to state Cartesian coordinates.
getStateInterpolator() - Method in class org.orekit.propagation.analytical.Ephemeris
Get state interpolator.
getStates() - Method in class org.orekit.estimation.measurements.EstimatedMeasurementBase
Get the states of the spacecrafts.
getStateSize() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Get state size.
getStateTransitionMatrix(SpacecraftState) - Method in class org.orekit.propagation.AbstractMatricesHarvester
Extract state transition matrix from state.
getStateTransitionMatrix(SpacecraftState) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester
Extract state transition matrix from state.
getStateTransitionMatrix(SpacecraftState) - Method in interface org.orekit.propagation.MatricesHarvester
Extract state transition matrix from state.
getStateTransitionMatrix(SpacecraftState) - Method in class org.orekit.propagation.numerical.cr3bp.STMEquations
Method returning the State Transition Matrix.
getStateTransitionMatrix(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester
Extract state transition matrix from state.
getStateType() - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder
Get the type of the elements used to define the orbital state (mean or osculating).
getStateVectorBlock() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmData
Get the state vector logical block.
getStateVectorBlock() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData
Get the state vector logical block.
getStaticInverse() - Method in interface org.orekit.frames.FieldStaticTransform
Get the inverse transform of the instance in static form (without rates).
getStaticInverse() - Method in interface org.orekit.frames.StaticTransform
Get the inverse transform of the instance in static form (without rates).
getStaticTransform(AbsoluteDate) - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
Get a transform for only rotations and translations on the specified date.
getStaticTransform(AbsoluteDate) - Method in class org.orekit.frames.GTODProvider
Get a transform for only rotations and translations on the specified date.
getStaticTransform(AbsoluteDate) - Method in class org.orekit.frames.HelmertTransformation
Get a transform for only rotations and translations on the specified date.
getStaticTransform(AbsoluteDate) - Method in class org.orekit.frames.ITRFVersion.Converter
Get a transform for only rotations and translations on the specified date.
getStaticTransform(AbsoluteDate) - Method in class org.orekit.frames.L1TransformProvider
Get a transform for only rotations and translations on the specified date.
getStaticTransform(AbsoluteDate) - Method in class org.orekit.frames.ShiftingTransformProvider
Get a transform for only rotations and translations on the specified date.
getStaticTransform(AbsoluteDate) - Method in interface org.orekit.frames.TransformProvider
Get a transform for only rotations and translations on the specified date.
getStaticTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
Get a transform for only rotations and translations on the specified date.
getStaticTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.GTODProvider
Get a transform for only rotations and translations on the specified date.
getStaticTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.HelmertTransformation
Get a transform for only rotations and translations on the specified date.
getStaticTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.ITRFVersion.Converter
Get a transform for only rotations and translations on the specified date.
getStaticTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.L1TransformProvider
Get a transform for only rotations and translations on the specified date.
getStaticTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.ShiftingTransformProvider
Get a transform for only rotations and translations on the specified date.
getStaticTransform(FieldAbsoluteDate<T>) - Method in interface org.orekit.frames.TransformProvider
Get a transform for only rotations and translations on the specified date.
getStaticTransformTo(Frame, AbsoluteDate) - Method in class org.orekit.frames.Frame
Get the static portion of the transform from the instance to another frame.
getStaticTransformTo(Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.Frame
Get the static portion of the transform from the instance to another frame.
getStation() - Method in class org.orekit.estimation.measurements.GroundReceiverMeasurement
Get the ground station from which measurement is performed.
getStation(String) - Method in class org.orekit.files.sinex.SinexLoader
Get the station corresponding to the given site code.
getStationClockAndDriftApplied() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
Get the station clock offset and drift applied indicator.
getStationDownlink() - Method in class org.orekit.estimation.measurements.GroundReceiverCommonParametersWithDerivatives
Get station position in inertial frame at end of the downlink leg.
getStationDownlink() - Method in class org.orekit.estimation.measurements.GroundReceiverCommonParametersWithoutDerivatives
Get station position in inertial frame at end of the downlink leg.
getStationIdentifier() - Method in class org.orekit.files.rinex.clock.RinexClock
Getter for the station identifier.
getStationInformation() - Method in class org.orekit.files.rinex.section.RinexBaseHeader
Getter for the station information.
getStationName() - Method in class org.orekit.files.ilrs.CRDHeader
Get the station name from official list.
getStationName() - Method in class org.orekit.files.rinex.clock.RinexClock
Getter for the station name.
getStationNetword() - Method in class org.orekit.files.ilrs.CRDHeader
Get the station network.
getStationOscDrift() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
Get the estimated station oscillator drift in parts in 10¹⁵.
getStations() - Method in class org.orekit.files.sinex.SinexLoader
Get the parsed station data.
getStationUTCOffset() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
Get the estimated station UTC offset.
getStatus() - Method in class org.orekit.estimation.measurements.EstimatedMeasurementBase
Get the status.
getStatusFlags() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage
Get status flags.
getStep() - Method in class org.orekit.files.ilrs.CPFHeader
Get the time between table entries.
getStep() - Method in class org.orekit.frames.InterpolatingTransformProvider
Get the grid points time step.
getStep() - Method in class org.orekit.frames.ShiftingTransformProvider
Get the grid points time step.
getSTKVersion() - Method in class org.orekit.files.stk.STKEphemerisFile
Returns the STK version string.
getStm(Orbit, double) - Static method in class org.orekit.propagation.StateCovariance
Get the state transition matrix considering Keplerian contribution only.
getStmName() - Method in class org.orekit.propagation.AbstractMatricesHarvester
Get the State Transition Matrix state name.
getStop() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmSatelliteEphemeris
Get the end date of the ephemeris.
getStop() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistory
Get the end date of this ephemeris segment.
getStop() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Get the end date of this ephemeris segment.
getStop() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSatelliteEphemeris
Get the end date of the ephemeris.
getStop() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSegment
Get the end date of this ephemeris segment.
getStop() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmSatelliteEphemeris
Get the end date of the ephemeris.
getStop() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory
Get the end date of this ephemeris segment.
getStop() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSatelliteEphemeris
Get the end date of the ephemeris.
getStop() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSegment
Get the end date of this ephemeris segment.
getStop() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.AttitudeEphemerisSegment
Get the end date of this ephemeris segment.
getStop() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.SatelliteAttitudeEphemeris
Get the end date of the ephemeris.
getStop() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
Get the end date of this ephemeris segment.
getStop() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris
Get the end date of the ephemeris.
getStop() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment
Get the end date of this ephemeris segment.
getStop() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitSatelliteAttitudeEphemeris
Get the end date of the ephemeris.
getStop() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
Get the end date of this ephemeris segment.
getStop() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
Get the end date of the ephemeris.
getStop() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris
Get the end date of the ephemeris.
getStop() - Method in class org.orekit.files.sp3.SP3Ephemeris
Get the end date of the ephemeris.
getStop() - Method in class org.orekit.files.sp3.SP3Segment
Get the end date of this ephemeris segment.
getStop() - Method in class org.orekit.files.stk.STKEphemerisFile.STKEphemeris
 
getStop() - Method in class org.orekit.files.stk.STKEphemerisFile.STKEphemerisSegment
 
getStopDate() - Method in class org.orekit.propagation.events.EventState.EventOccurrence
Get the new time for a stop action.
getStopDate() - Method in class org.orekit.propagation.events.FieldEventState.EventOccurrence
Get the new time for a stop action.
getStopDetector() - Method in class org.orekit.forces.maneuvers.trigger.StartStopEventsTrigger
Getter for the firing stop detector.
getStopDriver() - Method in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector
Get the driver for stop date.
getStopDriver() - Method in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector
Get the driver for stop date.
getStopNumber() - Method in class org.orekit.files.ilrs.CRD.FrRangeMeasurement
Get the stop number.
getStopScreenPeriod() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the stop time in UTC of the screening period for the conjunction assessment.
getStopTime() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata
Get the time of the latest data contained in the OCM.
getStopTime() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Get end of total time span covered by attitude data.
getStopTime() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the time of the latest data contained in the OCM.
getStopTime() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata
Get end of total time span covered by ephemerides data and covariance data.
getStopTime() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the stopTime.
getStream(File) - Method in class org.orekit.data.FilesListCrawler
Get the stream to read from an input.
getStream(URL) - Method in class org.orekit.data.NetworkCrawler
Get the stream to read from an input.
getStream(T) - Method in class org.orekit.data.AbstractListCrawler
Get the stream to read from an input.
getStreamInfoAddress() - Method in class org.orekit.gnss.metric.ntrip.NetworkRecord
Get the web address for stream information.
getStrengthLevel() - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
Get the strength level for activity.
getStuffReference() - Method in class org.orekit.estimation.measurements.gnss.AbstractCycleSlipDetector
Get the stuff (all the things needed for, the detector).
getSubDailySequenceNumber() - Method in class org.orekit.files.ilrs.CPFHeader
Get the sub-daily ephemeris sequence number.
getSubInterpolators() - Method in class org.orekit.propagation.FieldSpacecraftStateInterpolator
Get all lowest level interpolators implemented by this instance, otherwise return a list with this instance only.
getSubInterpolators() - Method in class org.orekit.propagation.SpacecraftStateInterpolator
Get all lowest level interpolators implemented by this instance, otherwise return a list with this instance only.
getSubInterpolators() - Method in class org.orekit.time.AbstractFieldTimeInterpolator
Get all lowest level interpolators implemented by this instance, otherwise return a list with this instance only.
getSubInterpolators() - Method in class org.orekit.time.AbstractTimeInterpolator
Get all lowest level interpolators implemented by this instance, otherwise return a list with this instance only.
getSubInterpolators() - Method in interface org.orekit.time.FieldTimeInterpolator
Get all lowest level interpolators implemented by this instance, otherwise return a list with this instance only.
getSubInterpolators() - Method in interface org.orekit.time.TimeInterpolator
Get all lowest level interpolators implemented by this instance, otherwise return a list with this instance only.
getSumOfAllConstantDelays() - Method in class org.orekit.files.ilrs.CRDConfiguration.CalibrationTargetConfiguration
Get the sum of all constant delays (electronic, geometric, optical) that are not included in the time of flight measurements or time- variant or point angle-variant delays in the “42” record below (m, one way).
getSun() - Method in interface org.orekit.bodies.CelestialBodies
Get the Sun singleton body.
getSun() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Sun singleton body.
getSun() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
 
getSun() - Method in class org.orekit.forces.gravity.DeSitterRelativity
Get the sun model used to compute De Sitter effect.
getSunEarthCR3BP(AbsoluteDate, TimeScale) - Static method in class org.orekit.bodies.CR3BPFactory
Get the Sun-Earth CR3BP singleton bodies pair.
getSunJupiterCR3BP(AbsoluteDate, TimeScale) - Static method in class org.orekit.bodies.CR3BPFactory
Get the Sun-Jupiter CR3BP singleton bodies pair.
getSupportedNames() - Method in class org.orekit.data.AbstractSelfFeedingLoader
Get the supported names regular expression.
getSupportedNames() - Method in class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader
Get the regular expression for supported files names.
getSupportedNames() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Get the regular expression for supported files names.
getSupportedNames() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get the regular expression for supported files names.
getSupportedNames() - Method in class org.orekit.gnss.SEMParser
 
getSupportedNames() - Method in class org.orekit.gnss.YUMAParser
 
getSupportedNames() - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData
Get the supported names regular expression.
getSupportedNames() - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader
 
getSupportedNames() - Method in class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader
 
getSurveyedTargetDistance() - Method in class org.orekit.files.ilrs.CRDConfiguration.CalibrationTargetConfiguration
Get the surveyed target distance.
getSurveyError() - Method in class org.orekit.files.ilrs.CRDConfiguration.CalibrationTargetConfiguration
Get the survey error.
getSvAccuracy() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouLegacyNavigationMessage
Getter for the user SV accuray (meters).
getSvAccuracy() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage
Getter for the user SV accuray (meters).
getSvAccuracy() - Method in class org.orekit.propagation.analytical.gnss.data.LegacyNavigationMessage
Getter for the user SV accuray (meters).
getSvHealth() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1042Data
Get the satellite health status.
getSvHealth() - Method in class org.orekit.gnss.rflink.gps.SubFrame1
Get SV health.
getSvHealth() - Method in class org.orekit.gnss.rflink.gps.SubFrameAlmanac
Get SV health.
getSvHealth() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage
Getter for the satellite health status.
getSvHealth() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage
Getter for the SV health status.
getSvHealth() - Method in class org.orekit.propagation.analytical.gnss.data.IRNSSNavigationMessage
Getter for the satellite health status.
getSvHealth() - Method in class org.orekit.propagation.analytical.gnss.data.LegacyNavigationMessage
Getter for the satellite health status.
getSvHealth(int) - Method in class org.orekit.gnss.rflink.gps.SubFrame4E
Get the Sv health for a satellite.
getSvHealth(int) - Method in class org.orekit.gnss.rflink.gps.SubFrame5B
Get the SV Health for a satellite.
getSvId() - Method in class org.orekit.gnss.rflink.gps.SubFrame45
Get SV (page) ID.
getSVN() - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac
Gets the satellite "SVN" reference number.
getSw() - Method in class org.orekit.models.earth.troposphere.FieldTroposphericDelay
Get wet slanted delay (m).
getSw() - Method in class org.orekit.models.earth.troposphere.TroposphericDelay
Get wet slanted delay (m).
getSwitches() - Method in class org.orekit.attitudes.AttitudesSequence
Gets a deep copy of the switches stored in this instance.
getSystem() - Method in class org.orekit.files.rinex.navigation.TypeSvMessage
Get satellite system.
getSystem() - Method in class org.orekit.gnss.SatInSystem
Get the system this satellite belongs to.
getSystem(CelestialBody, CelestialBody, double) - Static method in class org.orekit.bodies.CR3BPFactory
Get the corresponding CR3BP System.
getSystemConfigurationId() - Method in class org.orekit.files.ilrs.CRD.Calibration
Get the system configuration id.
getSystemConfigurationId() - Method in class org.orekit.files.ilrs.CRD.RangeMeasurement
Get the system configuration id.
getSystemConfigurationId() - Method in class org.orekit.files.ilrs.CRD.RangeSupplement
Get the system configuration id.
getSystemConfigurationId() - Method in class org.orekit.files.ilrs.CRD.SessionStatistics
Get system configuration id.
getSystemConfigurationIds() - Method in class org.orekit.files.ilrs.CRDConfiguration
Get a set of configuration ids.
getSystemConfigurationRecords() - Method in class org.orekit.files.ilrs.CRDConfiguration
Get a list of system configurations.
getSystemDelay() - Method in class org.orekit.files.ilrs.CRD.Calibration
Get the calibration system delay.
getSystemId() - Method in class org.orekit.files.ilrs.CRDConfiguration.SystemConfiguration
Get the system configuration ID.
getSystemIdentifier() - Method in class org.orekit.files.ilrs.CRDHeader
Get the system identifier.
getSystemNumber() - Method in class org.orekit.files.ilrs.CRDHeader
Get the system number.
getSystemObservationTypes() - Method in class org.orekit.files.rinex.clock.RinexClock
Getter for the different observation type for each satellite system.
getSystemOccupancy() - Method in class org.orekit.files.ilrs.CRDHeader
Get the system occupancy.
getSystemRecord() - Method in class org.orekit.files.ilrs.CRDConfiguration
Get the system configuration record.
getSystemRecord(String) - Method in class org.orekit.files.ilrs.CRDConfiguration
Get system configuration record.
getSystemTimeOffsets() - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Get the system time offsets.
getT() - Method in class org.orekit.orbits.WalkerConstellation
Get the total number of satellites.
getTabDensity() - Method in class org.orekit.models.earth.atmosphere.HarrisPriester
Get the current density table.
getTable() - Method in class org.orekit.attitudes.TabulatedLofOffset
Get an unmodifiable view of the tabulated attitudes.
getTAI() - Method in class org.orekit.time.LazyLoadedTimeScales
 
getTAI() - Method in interface org.orekit.time.TimeScales
Get the International Atomic Time scale.
getTAI() - Static method in class org.orekit.time.TimeScalesFactory
Get the International Atomic Time scale.
getTaimutcT0() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata
Get the difference (TAI – UTC) in seconds at epoch AcmMetadata.getEpochT0().
getTaimutcT0() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the difference (TAI – UTC) in seconds at epoch OcmMetadata.getEpochT0().
getTargetAttitude() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver
Get target attitude (if purpose is attitude adjustment).
getTargetClass() - Method in class org.orekit.files.ilrs.ILRSHeader
Get the target class.
getTargetDirection(ExtendedPositionProvider, OneAxisEllipsoid, TimeStampedFieldPVCoordinates<T>, Frame) - Method in class org.orekit.attitudes.GroundPointTarget
Get a target vector.
getTargetDirection(ExtendedPositionProvider, OneAxisEllipsoid, TimeStampedFieldPVCoordinates<T>, Frame) - Method in interface org.orekit.attitudes.TargetProvider
Get a target vector.
getTargetDirection(ExtendedPositionProvider, OneAxisEllipsoid, TimeStampedPVCoordinates, Frame) - Method in class org.orekit.attitudes.GroundPointTarget
Get a target vector.
getTargetDirection(ExtendedPositionProvider, OneAxisEllipsoid, TimeStampedPVCoordinates, Frame) - Method in interface org.orekit.attitudes.TargetProvider
Get a target vector.
getTargetLocation() - Method in class org.orekit.files.ilrs.ILRSHeader
Get the target location.
getTargetMomentum() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver
Get target momentum (if purpose is momentum desaturation).
getTargetMomFrame() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver
Get reference frame for AttitudeManeuver.getTargetMomentum().
getTargetName() - Method in class org.orekit.files.ilrs.CRDConfiguration.CalibrationTargetConfiguration
Get the target name or ID.
getTargetPosition(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.BodyCenterPointing
Compute the target point position in specified frame.
getTargetPosition(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.GroundPointing
Compute the target point position in specified frame.
getTargetPosition(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.GroundPointingAttitudeModifier
Compute the target point position in specified frame.
getTargetPosition(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing
Compute the target point position in specified frame.
getTargetPosition(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.NadirPointing
Compute the target point position in specified frame.
getTargetPosition(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.TargetPointing
Compute the target point position in specified frame.
getTargetPosition(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.BodyCenterPointing
Compute the target point position in specified frame.
getTargetPosition(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.GroundPointing
Compute the target point position in specified frame.
getTargetPosition(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.GroundPointingAttitudeModifier
Compute the target point position in specified frame.
getTargetPosition(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing
Compute the target point position in specified frame.
getTargetPosition(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.NadirPointing
Compute the target point position in specified frame.
getTargetPosition(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.TargetPointing
Compute the target point position in specified frame.
getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.BodyCenterPointing
Compute the target point position/velocity in specified frame.
getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.GroundPointing
Compute the target point position/velocity in specified frame.
getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.GroundPointingAttitudeModifier
Compute the target point position/velocity in specified frame.
getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing
Compute the target point position/velocity in specified frame.
getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.NadirPointing
Compute the target point position/velocity in specified frame.
getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.TargetPointing
Compute the target point position/velocity in specified frame.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.BodyCenterPointing
Compute the target point position/velocity in specified frame.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.GroundPointing
Compute the target point position/velocity in specified frame.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.GroundPointingAttitudeModifier
Compute the target point position/velocity in specified frame.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing
Compute the target point position/velocity in specified frame.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.NadirPointing
Compute the target point position/velocity in specified frame.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.TargetPointing
Compute the target point position/velocity in specified frame.
getTargetPVViaInterpolation(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.NadirPointing
Compute target position-velocity-acceleration vector via interpolation (Field version).
getTargetPVViaInterpolation(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.NadirPointing
Compute target position-velocity-acceleration vector via interpolation.
getTargetSize() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Get the size of the target.
getTargetSpinRate() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver
Get target spin rate (if purpose is spin rate adjustment).
getTauC() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the GLONASS time scale correction to UTC time.
getTauD() - Method in class org.orekit.estimation.measurements.CommonParametersWithDerivatives
Get downlink delay.
getTauD() - Method in class org.orekit.estimation.measurements.CommonParametersWithoutDerivatives
Get downlink delay.
getTauGps() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the correction to GPS time relative to GLONASS time.
getTauMultiplier() - Method in class org.orekit.models.earth.displacement.Tide
Get the multiplier for the τ Doodson argument.
getTC() - Method in class org.orekit.data.DelaunayArguments
Get the offset in Julian centuries.
getTC() - Method in class org.orekit.data.FieldDelaunayArguments
Get the offset in Julian centuries.
getTca() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the date and time in UTC of the closest approach.
getTca() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Get the Time of Closest Approach.
getTca() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition
Get the Time of Closest Approach.
getTCB() - Method in class org.orekit.time.LazyLoadedTimeScales
 
getTCB() - Method in interface org.orekit.time.TimeScales
Get the Barycentric Coordinate Time scale.
getTCB() - Static method in class org.orekit.time.TimeScalesFactory
Get the Barycentric Coordinate Time scale.
getTCG() - Method in class org.orekit.time.LazyLoadedTimeScales
 
getTCG() - Method in interface org.orekit.time.TimeScales
Get the Geocentric Coordinate Time scale.
getTCG() - Static method in class org.orekit.time.TimeScalesFactory
Get the Geocentric Coordinate Time scale.
getTDB() - Method in class org.orekit.time.LazyLoadedTimeScales
 
getTDB() - Method in interface org.orekit.time.TimeScales
Get the Barycentric Dynamic Time scale.
getTDB() - Static method in class org.orekit.time.TimeScalesFactory
Get the Barycentric Dynamic Time scale.
getTdim() - Method in class org.orekit.bodies.CR3BPSystem
Get the CR3BP orbital period of m2 around m1.
getTdmMessageLink() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the Unique identifier of Tracking Data Message linked to this Orbit Data Message.
getTdop() - Method in class org.orekit.gnss.DOP
Gets the time dilution of precision.
getTechAddress() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the address of Technical Point Of Contact at originator.
getTechEmail() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the email address of Technical Point Of Contact at originator.
getTechOrg() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the creating agency or operator.
getTechPhone() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the phone number of Technical Point Of Contact at originator.
getTechPOC() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the Technical Point Of Contact at originator.
getTechPosition() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the position of Technical Point Of Contact at originator.
getTEME() - Method in class org.orekit.frames.AbstractFrames
 
getTEME() - Method in interface org.orekit.frames.Frames
Get the TEME reference frame.
getTEME() - Static method in class org.orekit.frames.FramesFactory
Get the TEME reference frame.
getTemperature() - Method in class org.orekit.files.ilrs.CRD.MeteorologicalMeasurement
Get the surface temperature.
getTemperature() - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction
Get the local temperature at the evaluation location.
getTemperature() - Method in class org.orekit.models.earth.weather.FieldPressureTemperature
Get temperature.
getTemperature() - Method in class org.orekit.models.earth.weather.GlobalPressureTemperature2Model
Deprecated.
Returns the temperature at the station [K].
getTemperature() - Method in class org.orekit.models.earth.weather.GlobalPressureTemperatureModel
Deprecated.
Get the atmospheric temperature of the station depending its position.
getTemperature() - Method in class org.orekit.models.earth.weather.PressureTemperature
Get temperature.
getTemplateTLE() - Method in class org.orekit.propagation.conversion.TLEPropagatorBuilder
Getter for the template TLE.
getTempSensorManufacturer() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
Get the temperature sensor manufacturer.
getTempSensorModel() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
Get the temperature sensor model.
getTempSensorSerialNumber() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
Get the temperature sensor serial number.
getTerminalCartesianState() - Method in class org.orekit.control.indirect.shooting.AbstractFixedBoundaryCartesianSingleShooting
Getter for the target terminal Cartesian state vector.
getTerminalCartesianState() - Method in class org.orekit.control.indirect.shooting.boundary.FixedTimeCartesianBoundaryStates
Getter for the terminal Cartesian condition.
getTerminalOrbit() - Method in class org.orekit.control.indirect.shooting.boundary.FixedTimeBoundaryOrbits
Getter for the terminal condition.
getTerminalState() - Method in class org.orekit.control.indirect.shooting.ShootingBoundaryOutput
Getter for the terminal state.
getText() - Method in class org.orekit.files.rinex.section.RinexComment
Get the text.
getTFirstObs() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Get the time of First observation record.
getTGD() - Method in class org.orekit.gnss.rflink.gps.SubFrame1
Get the TGD.
getTGD() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage
Getter for the Group Delay Differential (s).
getTGD() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSClockElements
Gets the estimated group delay differential TGD for L1-L2 correction.
getTGD() - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac
Gets for the Group Delay Differential (s).
getTGD() - Method in class org.orekit.propagation.analytical.gnss.data.IRNSSNavigationMessage
Getter for the estimated group delay differential TGD for L5-S correction.
getTGD() - Method in class org.orekit.propagation.analytical.gnss.data.LegacyNavigationMessage
Getter for the Group Delay Differential (s).
getTGD1() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouLegacyNavigationMessage
Getter for the estimated group delay differential TGD1 for B1I signal.
getTGD2() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouLegacyNavigationMessage
Getter for the estimated group delay differential TGD for B2I signal.
getTgdB1Cp() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage
Getter for B1/B3 Group Delay Differential (s).
getTgdB2ap() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage
Getter for B2 AP Group Delay Differential (s).
getTgdB2bI() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage
Getter for B2B_i / B3I Group Delay Differential (s).
getTheoreticalStandardDeviation() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Get the theoretical standard deviation.
getTheoreticalStandardDeviation() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
Get the theoretical standard deviation.
getTheoreticalStandardDeviation() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
Get the theoretical standard deviation.
getTheta() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext
Get Central body rotation angle θ.
getTheta() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext
Get Central body rotation angle θ.
getTheta0() - Method in class org.orekit.models.earth.EarthITU453AtmosphereRefraction
Get the station elevation angle under free-space propagation .
getThetaMin() - Method in class org.orekit.models.earth.EarthITU453AtmosphereRefraction
Get the station minimal elevation angle.
getThreeHourlyAp() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
Gets the array of the eight three-hourly Ap indices for the current entry.
getThreeHourlyAp(int) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
Gets the three-hourly Ap index at index i from the threeHourlyAp array.
getThreeHourlyKp() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
Gets the array of the eight three-hourly Kp indices for the current entry.
getThreeHourlyKp(int) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
Gets the three-hourly Kp index at index i from the threeHourlyKp array.
getThreeHourlyKP(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
Get the value of the 3 hours geomagnetic index.
getThreeHourlyKP(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
Get the value of the 3 hours geomagnetic index.
getThreeHourlyKP(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.DTM2000InputParameters
Get the value of the 3 hours geomagnetic index.
getThreshold() - Method in class org.orekit.attitudes.AttitudesSequence.Switch
Get the convergence threshold in the event time search.
getThreshold() - Method in class org.orekit.propagation.events.AbstractDetector
Get the convergence threshold in the event time search.
getThreshold() - Method in class org.orekit.propagation.events.AdapterDetector
Get the convergence threshold in the event time search.
getThreshold() - Method in class org.orekit.propagation.events.EventDetectionSettings
Getter for threshold.
getThreshold() - Method in interface org.orekit.propagation.events.EventDetector
Get the convergence threshold in the event time search.
getThreshold() - Method in class org.orekit.propagation.events.FieldAbstractDetector
Get the convergence threshold in the event time search.
getThreshold() - Method in class org.orekit.propagation.events.FieldAdapterDetector
Get the convergence threshold in the event time search.
getThreshold() - Method in class org.orekit.propagation.events.FieldEventDetectionSettings
Getter for threshold.
getThreshold() - Method in interface org.orekit.propagation.events.FieldEventDetector
Get the convergence threshold in the event time search.
getThrust() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Get thrust.
getThrustAcceleration() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Get the object’s acceleration due to in-track thrust used to propagate the state vector and covariance to TCA.
getThrustAccelerationVector(double[], double) - Method in interface org.orekit.control.indirect.adjoint.cost.CartesianCost
Computes the thrust acceleration vector in propagation frame from the adjoint variables and the mass.
getThrustAccelerationVector(double[], double) - Method in class org.orekit.control.indirect.adjoint.cost.UnboundedCartesianEnergyNeglectingMass
Computes the thrust acceleration vector in propagation frame from the adjoint variables and the mass.
getThrustDirectionProvider() - Method in class org.orekit.forces.maneuvers.ConfigurableLowThrustManeuver
Getter on Thrust direction and spacecraft attitude provided by an external object.
getThrustDirectionSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Get one σ angular off-nominal thrust direction.
getThrustEfficiency() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Get thrust efficiency η.
getThrusterAxisInSatelliteFrame() - Method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider
Thruster axis in satellite frame.
getThrustForceNorm(double[], double) - Method in class org.orekit.control.indirect.adjoint.cost.BoundedCartesianEnergy
Computes the Euclidean norm of the thrust force.
getThrustForceNorm(double[], double) - Method in class org.orekit.control.indirect.adjoint.cost.UnboundedCartesianEnergy
Computes the Euclidean norm of the thrust force.
getThrustInterpolation() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Get interpolation mode between current and next thrust line.
getThrustIsp() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Get thrust specific impulse.
getThrustMagnitude() - Method in class org.orekit.forces.maneuvers.ConfigurableLowThrustManeuver
Get the thrust magnitude.
getThrustMagnitude() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Get the thrust magnitude.
getThrustMagnitude() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the thrust magnitude (N).
getThrustMagnitude(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.ConfigurableLowThrustManeuver
Get the thrust magnitude.
getThrustMagnitude(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Get the thrust magnitude.
getThrustMagnitude(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the thrust magnitude (N) at given date.
getThrustMagnitudeSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Get one σ percent error on thrust magnitude.
getThrustVector() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Get the thrust vector (N) in S/C frame.
getThrustVector() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector() - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector() - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector(double[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector(double[]) - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector(double[]) - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.maneuvers.propulsion.ProfileThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector(SpacecraftState) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector(SpacecraftState) - Method in class org.orekit.forces.maneuvers.propulsion.ProfileThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector(SpacecraftState) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector(SpacecraftState, double[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector(SpacecraftState, double[]) - Method in class org.orekit.forces.maneuvers.propulsion.ProfileThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector(SpacecraftState, double[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Get the thrust vector (N) in S/C frame.
getThrustVector(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.propulsion.PolynomialThrustSegment
Get thrust vector at a specified date.
getThrustVector(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector(FieldAbsoluteDate<T>) - Method in class org.orekit.forces.maneuvers.propulsion.PolynomialThrustSegment
Get thrust vector at a specified date.
getThrustVector(T[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector(T[]) - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector(T[]) - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getTidalDisplacementFrequencyCorrectionDiurnal() - Method in enum org.orekit.utils.IERSConventions
Get the correction function for tidal displacement for diurnal tides.
getTidalDisplacementFrequencyCorrectionDiurnal(String, int, int, int, int, int) - Static method in enum org.orekit.utils.IERSConventions
Get the correction function for tidal displacement for diurnal tides.
getTidalDisplacementFrequencyCorrectionZonal() - Method in enum org.orekit.utils.IERSConventions
Get the correction function for tidal displacement for zonal tides.
getTidalDisplacementFrequencyCorrectionZonal(String, int, int, int, int, int) - Static method in enum org.orekit.utils.IERSConventions
Get the correction function for tidal displacement for zonal tides.
getTide(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
Get the tide.
getTideFrequencyDependenceFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions
Get the function computing frequency dependent terms (ΔC₂₀, ΔC₂₁, ΔS₂₁, ΔC₂₂, ΔS₂₂).
getTideFrequencyDependenceFunction(TimeScale, TimeScales) - Method in enum org.orekit.utils.IERSConventions
Get the function computing frequency dependent terms (ΔC₂₀, ΔC₂₁, ΔS₂₁, ΔC₂₂, ΔS₂₂).
getTideSystem() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Get the TideSystem used in the gravity field.
getTideSystem() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
Get the TideSystem used in the gravity field.
getTideSystem() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get the TideSystem used in the gravity field.
getTideSystem() - Method in interface org.orekit.forces.gravity.potential.TideSystemProvider
Get the TideSystem used in the gravity field.
getTime() - Method in class org.orekit.estimation.sequential.MeasurementDecorator
getTime() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Getter for the reference time of the GNSS orbit as a duration from week start.
getTime() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
 
getTime() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
 
getTime() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage
Get the Reference Time.
getTime() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
Get the Reference Time.
getTime() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
Gets the Reference Time of the GNSS orbit as a duration from week start.
getTime() - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage
Gets the Reference Time of the SBAS orbit in GPS seconds of the week.
getTime() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
Gets the Reference Time of the SBAS orbit in GPS seconds of the week.
getTime() - Method in class org.orekit.time.DateTimeComponents
Get the time component.
getTime() - Method in class org.orekit.utils.units.Unit
Get the time exponent.
getTimeBiasApplied() - Method in class org.orekit.files.ilrs.CRD.RangeSupplement
Get the time bias applied.
getTimeConverter() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter
Get the current time converter.
getTimeConverter() - Method in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter
Get the current time converter.
getTimeLastObsEnd() - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters
Get the start of a time interval (UTC) that contains the time of the last accepted observation.
getTimeLastObsStart() - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters
Get the start of a time interval (UTC) that contains the time of the last accepted observation.
getTimeOfFlight() - Method in class org.orekit.files.ilrs.CRD.RangeMeasurement
Get the time-of-flight.
getTimeOffset() - Method in class org.orekit.estimation.measurements.EstimatedMeasurementBase
Get the time offset from first state date to measurement date.
getTimeParameter(AbsoluteDate, AbsoluteDate, AbsoluteDate) - Method in class org.orekit.time.AbstractTimeInterpolator
Get the time parameter which lies between [0:1] by normalizing the difference between interpolating time and previous date by the Δt between tabulated values.
getTimeParameter(FieldAbsoluteDate<KK>, FieldAbsoluteDate<KK>, FieldAbsoluteDate<KK>) - Method in class org.orekit.time.AbstractFieldTimeInterpolator
Get the time parameter which lies between [0:1] by normalizing the difference between interpolating time and previous date by the Δt between tabulated values.
getTimer() - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration
Get the timer name.
getTimerSerialNumber() - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration
Get the timer serial number.
getTimeScale() - Method in class org.orekit.files.ccsds.definitions.TimeConverter
Get the base time scale.
getTimeScale() - Method in class org.orekit.files.ilrs.CPF
Get the time scale used in CPF file.
getTimeScale() - Method in class org.orekit.files.ilrs.CRDParser
Get the time scale used to read the file.
getTimeScale() - Method in class org.orekit.files.rinex.clock.RinexClock
Getter for the data time scale.
getTimeScale(TimeScales) - Method in enum org.orekit.gnss.ObservationTimeScale
Get time scale.
getTimeScale(TimeScales) - Method in enum org.orekit.gnss.TimeSystem
Get the time scale corresponding to time system.
getTimeScales() - Method in class org.orekit.data.CompositeDataContext
 
getTimeScales() - Method in interface org.orekit.data.DataContext
Get a factory for constructing TimeScales based on the auxiliary data in this context.
getTimeScales() - Method in class org.orekit.data.ExceptionalDataContext
 
getTimeScales() - Method in class org.orekit.data.LazyLoadedDataContext
 
getTimeScales() - Method in class org.orekit.frames.AbstractFrames
Get the time scales.
getTimeScales() - Method in class org.orekit.frames.EOPHistory
Get the time scales used in computing EOP corrections.
getTimeScales() - Static method in class org.orekit.time.TimeScalesFactory
Get the instance of TimeScales that is called by all of the static methods in this class.
getTimeSinceFirstObservation() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get time elapsed between first accepted observation on epoch.
getTimeSinceLastObservation() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get time elapsed between last accepted observation on epoch.
getTimeSource() - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration
Get the time source.
getTimeSpan() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the span of time in seconds that the OCM covers.
getTimeSystem() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the Time System that: for CDM, is used for relative metadata, metadata, OD parameters, state vector.
getTimeSystem() - Method in class org.orekit.files.ccsds.section.Metadata
Get the Time System that: for OPM, is used for metadata, state vector, maneuver and covariance data, for OMM, is used for metadata, orbit state and covariance data, for OEM, is used for metadata, ephemeris and covariance data.
getTimeSystem() - Method in class org.orekit.files.ccsds.utils.ContextBinding
Get the time system.
getTimeSystem() - Method in class org.orekit.files.rinex.clock.RinexClock
Getter for the file time system.
getTimeSystem() - Method in class org.orekit.files.sinex.DcbDescription
Get the time system for DCB data.
getTimeSystem() - Method in class org.orekit.files.sp3.SP3Header
Returns the TimeSystem used to time-stamp position entries.
getTimeSystemCorrectionA0() - Method in class org.orekit.files.rinex.navigation.TimeSystemCorrection
Getter for the A0 coefficient of the time system correction.
getTimeSystemCorrectionA1() - Method in class org.orekit.files.rinex.navigation.TimeSystemCorrection
Getter for the A1 coefficient of the time system correction.
getTimeSystemCorrections() - Method in class org.orekit.files.rinex.navigation.RinexNavigationHeader
Getter for the time system corrections contained in the file header.
getTimeSystemCorrectionType() - Method in class org.orekit.files.rinex.navigation.TimeSystemCorrection
Getter for the time system correction type.
getTimetagRef() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the timetagRef.
getTimingRecord() - Method in class org.orekit.files.ilrs.CRDConfiguration
Get the timing system configuration record.
getTimingRecord(CRDConfiguration.SystemConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration
Get timing system configuration record related to the systemRecord.
getTIRF(IERSConventions) - Method in class org.orekit.frames.AbstractFrames
 
getTIRF(IERSConventions) - Method in interface org.orekit.frames.Frames
Get the TIRF reference frame, ignoring tidal effects.
getTIRF(IERSConventions) - Static method in class org.orekit.frames.FramesFactory
Get the TIRF reference frame, ignoring tidal effects.
getTIRF(IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames
 
getTIRF(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames
Get the TIRF reference frame.
getTIRF(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
Get the TIRF reference frame.
getTk() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the time referenced to the beginning of the frame within the current day.
getTLastObs() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Get the time of last observation record.
getTLE() - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
Get the underlying TLE.
getTLE() - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
Get the underlying TLE.
getTLEBlock() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmData
Get the TLE logical block.
getTm() - Method in class org.orekit.models.earth.weather.FieldPressureTemperatureHumidity
Get mean temperature weighted with water vapor pressure.
getTm() - Method in class org.orekit.models.earth.weather.PressureTemperatureHumidity
Get mean temperature weighted with water vapor pressure.
getTN() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage
Get the correction to the satellite time relative to GLONASS system time.
getTN() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
Get the correction to the satellite time relative to GLONASS system time.
getTo() - Method in class org.orekit.utils.units.UnitsConverter
Get the destination unit.
getTOA() - Method in class org.orekit.gnss.rflink.gps.SubFrame5B
Get Time of Almanac.
getToaA() - Method in class org.orekit.gnss.rflink.gps.SubFrameAlmanac
Get Time Of Almanac.
getToc() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSClockElements
Gets the clock correction reference time toc.
getToc() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
Gets the clock correction reference time toc.
getTOC() - Method in class org.orekit.gnss.rflink.gps.SubFrame1
Get the TOC.
getTOD(boolean) - Method in class org.orekit.frames.AbstractFrames
 
getTOD(boolean) - Method in interface org.orekit.frames.Frames
Get the TOD reference frame.
getTOD(boolean) - Static method in class org.orekit.frames.FramesFactory
Get the TOD reference frame.
getTOD(IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames
 
getTOD(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames
Get the TOD reference frame.
getTOD(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
Get the TOD reference frame.
getToe() - Method in class org.orekit.gnss.rflink.gps.SubFrame2
Get Time Of Ephemeris.
getToLatitude() - Method in class org.orekit.propagation.events.FieldLatitudeRangeCrossingDetector
Get the fixed latitude range to be crossed (radians), upper boundary.
getToLatitude() - Method in class org.orekit.propagation.events.LatitudeRangeCrossingDetector
Get the fixed latitude range to be crossed (radians), upper boundary.
getTolerances(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.AbstractVariableStepFieldIntegratorBuilder
Computes tolerances.
getTolerances(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.AbstractVariableStepIntegratorBuilder
Computes tolerances.
getToLongitude() - Method in class org.orekit.propagation.events.FieldLongitudeRangeCrossingDetector
Get the fixed longitude range to be crossed (radians), upper boundary.
getToLongitude() - Method in class org.orekit.propagation.events.LongitudeRangeCrossingDetector
Get the fixed longitude range to be crossed (radians), upper boundary.
getTon2a() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext
Get ton2a = 2 / (n² * a).
getTon2a() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext
Get ton2a = 2 / (n² * a).
getTool() - Method in class org.orekit.files.ccsds.definitions.OdMethodFacade
Get the tool used for OD.
getTopocentricFrame() - Method in class org.orekit.propagation.events.ElevationDetector
Returns the currently configured topocentric frame definitions.
getTopocentricFrame() - Method in class org.orekit.propagation.events.ElevationExtremumDetector
Returns the topocentric frame centered on ground point.
getTopocentricFrame() - Method in class org.orekit.propagation.events.FieldElevationDetector
Returns the currently configured topocentric frame definitions.
getTopocentricFrame() - Method in class org.orekit.propagation.events.FieldElevationExtremumDetector
Returns the topocentric frame centered on ground point.
getTopocentricPosition(FieldTrackingCoordinates<T>) - Static method in class org.orekit.frames.TopocentricFrame
Get the topocentric position from FieldTrackingCoordinates.
getTopocentricPosition(TrackingCoordinates) - Static method in class org.orekit.frames.TopocentricFrame
Get the topocentric position from TrackingCoordinates.
getTorque() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver
Get the torque vector (N.m).
getTot() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D
Get TOT field.
getTotalEclipse() - Method in class org.orekit.propagation.events.EclipseDetector
Get the total eclipse detection flag.
getTotalEclipse() - Method in class org.orekit.propagation.events.FieldEclipseDetector
Get the total eclipse detection flag.
getTotalIntensity() - Method in class org.orekit.models.earth.GeoMagneticElements
Returns the total intensity of the magnetic field (= norm of the field vector).
getTotalNumberOfDataLines() - Method in class org.orekit.files.rinex.clock.RinexClock
Get the total number of complete data lines in the file.
getTow() - Method in class org.orekit.gnss.rflink.gps.SubFrame
Get Time Of Week of next 12 second message.
getTrackId() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the tracking data identifier.
getTrackingCoordinates(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.TopocentricFrame
Get the tracking coordinates of a point with regards to the local point.
getTrackingCoordinates(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame
Get the tracking coordinates of a point with regards to the local point.
getTrackingSoftwares() - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration
Get the tracking softwares.
getTrackingSoftwareVersions() - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration
Get the tracking software versions.
getTracksAvailable() - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters
Get the number of sensor tracks available for the OD of the object.
getTracksAvailable() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get number of sensors tracks available for the OD within the actual OD span.
getTracksUsed() - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters
Get the number of sensor tracks used for the OD of the object.
getTracksUsed() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get number of sensors tracks accepted for the OD within the actual OD span.
getTrajBasis() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Get basis of this trajectory state time history data.
getTrajBasisID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Get identification number of the orbit determination or simulation upon which this trajectory is based.
getTrajectoryBlocks() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmData
Get trajectory state histories logical blocks.
getTrajectoryStates() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory
Get the trajectory states.
getTrajFrameEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Get epoch of the trajectory reference frame.
getTrajID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Get trajectory identification number.
getTrajNextID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Get identification number of next trajectory.
getTrajPrevID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Get identification number of previous trajectory.
getTrajReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Get reference frame of the trajectory.
getTrajType() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Get trajectory element set type.
getTrajUnits() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Get trajectory element set units.
getTransform(FrameFacade, FrameFacade, Frame, AbsoluteDate, PVCoordinatesProvider) - Static method in class org.orekit.files.ccsds.definitions.FrameFacade
Get the transform between CCSDS frames.
getTransform(AbsoluteDate) - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
Get the Transform corresponding to specified date.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.EclipticProvider
 
getTransform(AbsoluteDate) - Method in class org.orekit.frames.FixedTransformProvider
Get the Transform corresponding to specified date.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.GTODProvider
Get the Transform corresponding to specified date.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.HelmertTransformation
Get the Transform corresponding to specified date.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.InterpolatingTransformProvider
Get the Transform corresponding to specified date.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.ITRFVersion.Converter
Get the Transform corresponding to specified date.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.L1TransformProvider
Get the Transform corresponding to specified date.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.ShiftingTransformProvider
Get the Transform corresponding to specified date.
getTransform(AbsoluteDate) - Method in interface org.orekit.frames.TransformProvider
Get the Transform corresponding to specified date.
getTransform(FieldAbsoluteDate<Gradient>, int, Map<String, Integer>) - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
Get the transform with derivatives.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
Get the FieldTransform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EclipticProvider
 
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.FixedTransformProvider
Get the FieldTransform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.GTODProvider
Get the FieldTransform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.HelmertTransformation
Get the FieldTransform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.InterpolatingTransformProvider
Get the FieldTransform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.ITRFVersion.Converter
Get the FieldTransform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.L1TransformProvider
Get the FieldTransform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.ShiftingTransformProvider
Get the FieldTransform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in interface org.orekit.frames.TransformProvider
Get the FieldTransform corresponding to specified date.
getTransformation() - Method in enum org.orekit.frames.HelmertTransformation.Predefined
Get the underlying HelmertTransformation.
getTransformation(TimeScale) - Method in enum org.orekit.frames.HelmertTransformation.Predefined
Get the underlying HelmertTransformation.
getTransformProvider() - Method in class org.orekit.frames.Frame
Get the provider for transform from parent frame to instance.
getTransformTo(Frame, AbsoluteDate) - Method in class org.orekit.frames.Frame
Get the transform from the instance to another frame.
getTransformTo(Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.Frame
Get the transform from the instance to another frame.
getTransitionDates() - Method in class org.orekit.utils.ParameterDriver
Get the dates of the transitions for the drag sensitive models TimeSpanMap.
getTransitions() - Method in class org.orekit.utils.FieldTimeSpanMap
Get an unmodifiable view of the sorted transitions.
getTransitPV() - Method in class org.orekit.estimation.measurements.CommonParametersWithDerivatives
Get transit position/velocity.
getTransitPV() - Method in class org.orekit.estimation.measurements.CommonParametersWithoutDerivatives
Get transit position/velocity.
getTransitState() - Method in class org.orekit.estimation.measurements.CommonParametersWithDerivatives
Get transit state.
getTransitState() - Method in class org.orekit.estimation.measurements.CommonParametersWithoutDerivatives
Get transit state.
getTranslation() - Method in interface org.orekit.frames.FieldStaticTransform
Get the underlying elementary translation.
getTranslation() - Method in class org.orekit.frames.FieldTransform
Get the underlying elementary translation.
getTranslation() - Method in interface org.orekit.frames.StaticTransform
Get the underlying elementary translation.
getTranslation() - Method in class org.orekit.frames.Transform
Get the underlying elementary translation.
getTransmissionOfSpectralFilter() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Get the percentage of transmission of spectral filter.
getTransmissionTime() - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage
Get the message transmission time.
getTransmissionTime() - Method in class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage
Get the message transmission time.
getTransmissionTime() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Getter for transmission time.
getTransmitAmplitude() - Method in class org.orekit.files.ilrs.CRD.FrRangeMeasurement
Get the transmit amplitude.
getTransmitBand() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the transmitBand.
getTransmitDelays() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the transmitDelays.
getTransmitTime() - Method in class org.orekit.files.rinex.navigation.IonosphereBaseMessage
Get the transmit time.
getTranspClkRef() - Method in class org.orekit.files.ilrs.CPFHeader
Get the transponder Clock Reference Time.
getTranspClkRefTime() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
Get the transponder clock reference time.
getTransponderId() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
Get the transponder configuration ID.
getTransponderRecord() - Method in class org.orekit.files.ilrs.CRDConfiguration
Get the transponder configuration record.
getTransponderRecord(CRDConfiguration.SystemConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration
Get transponder configuration record related to the systemRecord.
getTranspOscDrift() - Method in class org.orekit.files.ilrs.CPFHeader
Get the transponder Oscillator Drift in parts in 10^15.
getTranspOscDrift() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
Get the estimated transponder oscillator drift in parts in 10¹⁵.
getTranspTransmitDelay() - Method in class org.orekit.files.ilrs.CPFHeader
Get the transponder transmit delay.
getTranspUtcOffset() - Method in class org.orekit.files.ilrs.CPFHeader
Get the transponder UTC offset.
getTranspUTCOffset() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
Get the estimated transponder UTC offset.
getTrigger() - Method in class org.orekit.forces.maneuvers.FieldImpulseManeuver
Get the triggering event.
getTrigger() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
Get the triggering event.
getTriggeredIncreasing() - Method in enum org.orekit.propagation.events.FilterType
Get the increasing status of triggered events.
getTropoModel() - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeRateTroposphericDelayModifier
Get the tropospheric delay model.
getTropoModel() - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeTroposphericDelayModifier
Get the tropospheric delay model.
getTroposphericModel(AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedModel
Get the EstimatedModel model valid at a date.
getTroposphericModel(AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
Deprecated.
Get the EstimatedTroposphericModel model valid at a date.
getTroposphericRefractionCorrection() - Method in class org.orekit.files.ilrs.CRD.RangeSupplement
Get the tropospheric refraction correction.
getTrueAnomaly() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the true anomaly.
getTrueAnomaly() - Method in class org.orekit.orbits.KeplerianOrbit
Get the true anomaly.
getTrueAnomalyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the true anomaly derivative.
getTrueAnomalyDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the true anomaly derivative.
getTT() - Method in class org.orekit.time.LazyLoadedTimeScales
 
getTT() - Method in interface org.orekit.time.TimeScales
Get the Terrestrial Time scale.
getTT() - Static method in class org.orekit.time.TimeScalesFactory
Get the Terrestrial Time scale.
getTurnaroundDenominator() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the turnaroundDenominator.
getTurnaroundNumerator() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the turnaroundNumerator.
getTwoDigitsRinexPRN() - Method in class org.orekit.gnss.SatInSystem
Get a 2-digits Pseudo Random Number for RINEX files.
getTwoLettersCode() - Method in enum org.orekit.gnss.TimeSystem
Get the two letters code.
getTypAreaForCollisionProbability() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Get the typical (50th percentile) cross-sectional area for collision probability estimation purposes.
getType() - Method in class org.orekit.files.ccsds.definitions.OdMethodFacade
Get the method type.
getType() - Method in class org.orekit.files.ccsds.definitions.PocMethodFacade
Get the method type.
getType() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovariance
Get the type of the elements.
getType() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovariance
Get the type of the elements.
getType() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryState
Get the type of the elements.
getType() - Method in class org.orekit.files.ccsds.ndm.tdm.Observation
Get the type of observation.
getType() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Get the type of the token.
getType() - Method in class org.orekit.files.sp3.SP3Header
Returns the SP3FileType associated with this SP3 file.
getType() - Method in class org.orekit.gnss.antenna.Antenna
Get the type of the antenna.
getType() - Method in class org.orekit.orbits.CartesianOrbit
Get the orbit type.
getType() - Method in class org.orekit.orbits.CircularOrbit
Get the orbit type.
getType() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the orbit type.
getType() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the orbit type.
getType() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the orbit type.
getType() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the orbit type.
getType() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the orbit type.
getType() - Method in class org.orekit.orbits.FieldOrbit
Get the orbit type.
getType() - Method in class org.orekit.orbits.KeplerianOrbit
Get the orbit type.
getType() - Method in class org.orekit.orbits.Orbit
Get the orbit type.
getType() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Alfano2005
Get type of the method.
getType() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Alfriend1999
Get type of the method.
getType() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Alfriend1999Max
Get type of the method.
getType() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Chan1997
Get type of the method.
getType() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Laas2015
Get type of the method.
getType() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Patera2005
Get type of the method.
getType() - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod
Get type of the method.
getTypeCode() - Method in class org.orekit.gnss.metric.messages.ParsedMessage
Get the code for the message type.
getTypeIndicator() - Method in class org.orekit.files.ilrs.CRD.Calibration
Get the calibration type indicator.
getTypeObs() - Method in class org.orekit.files.rinex.observation.PhaseShiftCorrection
Get the Carrier Phase Observation Code.
getTypeObs() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Get an unmodifiable view of the map of observation types.
getTypeOfData() - Method in class org.orekit.files.ilrs.CRD.Calibration
Get the type of data.
getTypesObsScaled() - Method in class org.orekit.files.rinex.observation.ScaleFactorCorrection
Get the list of Observation Types scaled.
getU() - Method in class org.orekit.bodies.Ellipse
Get the unit vector along the major axis.
getU() - Method in class org.orekit.bodies.FieldEllipse
Get the unit vector along the major axis.
getU1(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldUijVijCoefficients
Get the coefficient U₁j for Fourier index i.
getU1(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.UijVijCoefficients
Get the coefficient U₁j for Fourier index i.
getU2(int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldUijVijCoefficients
Get the coefficient U₂j for Fourier index = 1 (i == 0).
getU2(int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.UijVijCoefficients
Get the coefficient U₂j for Fourier index = 1 (i == 0).
getUnderlyingAttitudeProvider() - Method in interface org.orekit.attitudes.AttitudeProviderModifier
Get the underlying attitude provider.
getUnderlyingAttitudeProvider() - Method in class org.orekit.attitudes.GroundPointingAttitudeModifier
Getter for underlying ground pointing law.
getUnderlyingAttitudeProvider() - Method in class org.orekit.attitudes.SpinStabilized
Get the underlying attitude provider.
getUndulation(double, double, AbsoluteDate) - Method in class org.orekit.models.earth.Geoid
Gets the Undulation of the Geoid, N at the given position.
getUnit() - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
Get the field unit.
getUnits() - Method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceType
Get the elements units.
getUnits() - Method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeElementsType
Get the elements units.
getUnits() - Method in enum org.orekit.files.ccsds.ndm.adm.acm.RateElementsType
Get the elements units.
getUnits() - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitElementsType
Get the elements units.
getUnits() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Get the units.
getUnits(String) - Method in class org.orekit.utils.units.UnitsCache
Get units from a string specification.
getUnnormalizationFactors(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Get a un-normalization factors array.
getUnnormalizedC20(AbsoluteDate) - Method in interface org.orekit.forces.gravity.potential.UnnormalizedSphericalHarmonicsProvider
Get the un-normalized coefficient of degree 2 and order 0 at a specific instance in time.
getUnnormalizedCnm(int, int) - Method in interface org.orekit.forces.gravity.potential.UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics
Get a spherical harmonic cosine coefficient.
getUnnormalizedProvider(double, double, TideSystem, double[][], double[][]) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Create a time-independent UnnormalizedSphericalHarmonicsProvider from canonical coefficients.
getUnnormalizedProvider(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Get the gravity field coefficients provider from the first supported file.
getUnnormalizedProvider(int, int) - Method in interface org.orekit.forces.gravity.potential.GravityFields
Get a gravity field unnormalized coefficients provider.
getUnnormalizedProvider(int, int) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
Get a gravity field unnormalized coefficients provider.
getUnnormalizedProvider(NormalizedSphericalHarmonicsProvider) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
getUnnormalizedSnm(int, int) - Method in interface org.orekit.forces.gravity.potential.UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics
Get a spherical harmonic sine coefficient.
getUnoccultedFluxVector(FieldVector3D<T>) - Method in class org.orekit.forces.radiation.AbstractLightFluxModel
Get the light flux vector, not considering any shadowing effect.
getUnoccultedFluxVector(FieldVector3D<T>) - Method in class org.orekit.forces.radiation.AbstractSolarLightFluxModel
Get the light flux vector, not considering any shadowing effect.
getUnoccultedFluxVector(Vector3D) - Method in class org.orekit.forces.radiation.AbstractLightFluxModel
Get the light flux vector, not considering any shadowing effect.
getUnoccultedFluxVector(Vector3D) - Method in class org.orekit.forces.radiation.AbstractSolarLightFluxModel
Get the light flux vector, not considering any shadowing effect.
getUpdateInterval() - Method in class org.orekit.gnss.metric.messages.common.SsrUpdateInterval
Get the update interval.
getUpperCaseAbbreviation() - Method in enum org.orekit.time.Month
Get the upper case three letters abbreviation.
getUpperCaseName() - Method in enum org.orekit.time.Month
Get the upper case full name.
getUppercaseOmega0() - Method in class org.orekit.gnss.rflink.gps.SubFrame3
Get Ω₀.
getUppercaseOmega0() - Method in class org.orekit.gnss.rflink.gps.SubFrameAlmanac
Get Ω₀.
getUpperLimit() - Method in class org.orekit.ssa.metrics.FieldProbabilityOfCollision
Get upper limit of the probability of collision value.
getUpperLimit() - Method in class org.orekit.ssa.metrics.ProbabilityOfCollision
Get upper limit of the probability of collision value.
getURA() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage
Getter for the user range accuray (meters).
getURA() - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac
Gets the average URA number.
getURA() - Method in class org.orekit.propagation.analytical.gnss.data.IRNSSNavigationMessage
Getter for the user range accuray (meters).
getURA() - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage
Getter for the user range accuray (meters).
getUraiEd() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage
Getter for Elevation-Dependent User Range Accuracy.
getUraIndex() - Method in class org.orekit.gnss.rflink.gps.SubFrame1
Get URA index.
getUraiNed0() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage
Getter for term 0 of Non-Elevation-Dependent User Range Accuracy.
getUraiNed1() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage
Getter for term 1 of Non-Elevation-Dependent User Range Accuracy.
getUraiNed2() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage
Getter for term 2 of Non-Elevation-Dependent User Range Accuracy.
getUranus() - Method in interface org.orekit.bodies.CelestialBodies
Get the Uranus singleton body.
getUranus() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Uranus singleton body.
getUranus() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
 
getUseableStartTime() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Get start of useable time span covered by attitude data.
getUseableStartTime() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Get start of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.
getUseableStartTime() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata
Get start of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.
getUseableStopTime() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Get end of useable time span covered by ephemerides data.
getUseableStopTime() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Get end of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.
getUseableStopTime() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata
Get end of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.
getUsedObservationData() - Method in class org.orekit.estimation.measurements.gnss.CombinedObservationData
Get the list of observation data used to perform the combination of measurements.
getUserDefinedBlock() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmData
Get user defined parameters logical block.
getUserDefinedBlock() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmData
Get the user defined logical block.
getUserDefinedBlock() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmData
Get user defined parameters logical block.
getUserDefinedBlock() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmData
Get the user defined parameters logical block.
getUserDefinedBlock() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData
Get the user defined parameters logical block.
getUserDefinedParameters() - Method in class org.orekit.files.ccsds.ndm.cdm.Cdm
Get user defined parameters.
getUT1(EOPHistory) - Method in class org.orekit.time.AbstractTimeScales
Get the Universal Time 1 scale.
getUT1(EOPHistory) - Method in class org.orekit.time.LazyLoadedTimeScales
Get the Universal Time 1 scale.
getUT1(EOPHistory) - Static method in class org.orekit.time.TimeScalesFactory
Get the Universal Time 1 scale.
getUT1(IERSConventions, boolean) - Method in class org.orekit.time.AbstractTimeScales
 
getUT1(IERSConventions, boolean) - Method in class org.orekit.time.LazyLoadedTimeScales
 
getUT1(IERSConventions, boolean) - Method in interface org.orekit.time.TimeScales
Get the Universal Time 1 scale.
getUT1(IERSConventions, boolean) - Static method in class org.orekit.time.TimeScalesFactory
Get the Universal Time 1 scale.
getUt1MinusUtc() - Method in class org.orekit.files.sinex.SinexEopEntry
Get the UT1-UTC offset.
getUT1MinusUTC() - Method in class org.orekit.frames.EOPEntry
Get the UT1-UTC value.
getUT1MinusUTC(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory
Get the UT1-UTC value.
getUT1MinusUTC(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EOPHistory
Get the UT1-UTC value.
getUt1mutcT0() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the difference (UT1 – UTC) in seconds at epoch OcmMetadata.getEpochT0().
getUtc() - Method in class org.orekit.frames.AbstractEopLoader
Get the UTC time scale.
getUtc() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the UTC time scale used to create this TLE.
getUTC() - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData
Get the UTC timescale.
getUTC() - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityDataLoader
Get the UTC timescale.
getUTC() - Method in class org.orekit.time.LazyLoadedTimeScales
 
getUTC() - Method in interface org.orekit.time.TimeScales
Get the Universal Time Coordinate scale.
getUTC() - Static method in class org.orekit.time.TimeScalesFactory
Get the Universal Time Coordinate scale.
getUtcId() - Method in class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage
Get the UTC Id.
getUTCScale() - Method in class org.orekit.time.UT1Scale
Get the associated UTC scale.
getUTCTAIOffsets() - Method in class org.orekit.time.UTCScale
Returns the UTC-TAI offsets underlying this UTC scale.
getV() - Method in class org.orekit.bodies.Ellipse
Get the unit vector along the minor axis.
getV() - Method in class org.orekit.bodies.FieldEllipse
Get the unit vector along the minor axis.
getV1(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldUijVijCoefficients
Get the coefficient V₁j for Fourier index i.
getV1(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.UijVijCoefficients
Get the coefficient V₁j for Fourier index i.
getV2(int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldUijVijCoefficients
Get the coefficient V₂j for Fourier index = 1 (i == 0).
getV2(int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.UijVijCoefficients
Get the coefficient V₂j for Fourier index = 1 (i == 0).
getValidFrom() - Method in class org.orekit.files.sinex.Station
Get start of validity.
getValidFrom() - Method in class org.orekit.gnss.antenna.SatelliteAntenna
Get start of validity.
getValidityEnd() - Method in class org.orekit.estimation.measurements.QuadraticClockModel
Get validity end.
getValidityEnd() - Method in class org.orekit.time.AggregatedClockModel
Get validity end.
getValidityEnd() - Method in interface org.orekit.time.ClockModel
Get validity end.
getValidityEnd() - Method in class org.orekit.time.PerfectClockModel
Get validity end.
getValidityEnd() - Method in class org.orekit.time.SampledClockModel
Get validity end.
getValidityStart() - Method in class org.orekit.estimation.measurements.QuadraticClockModel
Get validity start.
getValidityStart() - Method in class org.orekit.time.AggregatedClockModel
Get validity start.
getValidityStart() - Method in interface org.orekit.time.ClockModel
Get validity start.
getValidityStart() - Method in class org.orekit.time.PerfectClockModel
Get validity start.
getValidityStart() - Method in class org.orekit.time.SampledClockModel
Get validity start.
getValidityStart() - Method in class org.orekit.time.UTCTAIOffset
Get the start time of validity for this offset.
getValidUntil() - Method in class org.orekit.files.sinex.Station
Get end of validity.
getValidUntil() - Method in class org.orekit.gnss.antenna.SatelliteAntenna
Get end of validity.
getValue() - Method in class org.orekit.estimation.measurements.gnss.CombinedObservationData
Get the combined observed value.
getValue() - Method in class org.orekit.estimation.sequential.MeasurementDecorator
getValue() - Method in enum org.orekit.files.ccsds.ndm.cdm.Maneuvrable
Get the String representation of the enum.
getValue() - Method in class org.orekit.files.rinex.observation.ObservationData
Get the observed value.
getValue() - Method in class org.orekit.ssa.metrics.FieldProbabilityOfCollision
Get value of the probability of collision.
getValue() - Method in class org.orekit.ssa.metrics.ProbabilityOfCollision
Get value of the probability of collision.
getValue() - Method in class org.orekit.time.TimeStampedDouble
Get value.
getValue() - Method in class org.orekit.time.TimeStampedField
Get value.
getValue() - Method in class org.orekit.utils.DoubleArrayDictionary.Entry
Get the value.
getValue() - Method in class org.orekit.utils.FieldArrayDictionary.Entry
Get the value.
getValue() - Method in class org.orekit.utils.ParameterDriver
Get current parameter value.
getValue(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenTesseralLinear
Compute the value of the Hansen coefficient Kj-n-1, s.
getValue(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenThirdBodyLinear
Compute the value of the Hansen coefficient K₀n, s.
getValue(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenZonalLinear
Get the K₀-n-1,s coefficient value.
getValue(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGammaMnsFunction
Get Γ function value.
getValue(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GammaMnsFunction
Get Γ function value.
getValue(int, int, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.NewcombOperators
Get the Newcomb operator evaluated at n, s, ρ, σ.
getValue(int, int, int, FieldGradient<T>) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.JacobiPolynomials
Returns the value and derivatives of the Jacobi polynomial Plv,w evaluated at γ.
getValue(int, int, int, Gradient) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.JacobiPolynomials
Returns the value and derivatives of the Jacobi polynomial Plv,w evaluated at γ.
getValue(int, Map<String, Integer>) - Method in class org.orekit.utils.ParameterDriver
Get the value as a gradient at special date.
getValue(int, Map<String, Integer>, AbsoluteDate) - Method in class org.orekit.utils.ParameterDriver
Get the value as a gradient at special date.
getValue(int, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenTesseralLinear
Compute the value of the Hansen coefficient Kj-n-1, s.
getValue(int, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenThirdBodyLinear
Compute the value of the Hansen coefficient K₀n, s.
getValue(int, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenZonalLinear
Get the K₀-n-1,s coefficient value.
getValue(AbsoluteDate) - Method in class org.orekit.utils.ParameterDriver
Get current parameter value at specific date, depending on isContinuousEstimation value, the value returned will be obtained by step estimation or continuous estimation.
getValueAndDerivative(int, int, int, double) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.JacobiPolynomials
Returns the value and derivatives of the Jacobi polynomial Plv,w evaluated at γ.
getValueContinuousEstimation(AbsoluteDate) - Method in class org.orekit.utils.ParameterDriver
Get current parameter value at specific date with continuous estimation.
getValues() - Method in class org.orekit.utils.ParameterDriver
Get all values of the valueSpanMap in the chronological order.
getValueSpanMap() - Method in class org.orekit.utils.ParameterDriver
Get value time span map for parameterDriver.
getValuesSamples() - Method in class org.orekit.utils.InterpolationTableLoader
Returns a copy of the values samples for the interpolation function.
getValueStepEstimation(AbsoluteDate) - Method in class org.orekit.utils.ParameterDriver
Get current parameter value at specific date with step estimation.
getVdim() - Method in class org.orekit.bodies.CR3BPSystem
Get the CR3BP orbital velocity of m2.
getVdop() - Method in class org.orekit.gnss.DOP
Gets the vertical dilution of precision.
getVectorF() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get equinoctial frame vector f.
getVectorF() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get equinoctial frame vector f.
getVectorG() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get equinoctial frame vector g.
getVectorG() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get equinoctial frame vector g.
getVectorW() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get equinoctial frame vector w.
getVectorW() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get equinoctial frame vector w.
getVeis1950() - Method in class org.orekit.frames.AbstractFrames
 
getVeis1950() - Method in interface org.orekit.frames.Frames
Get the VEIS 1950 reference frame.
getVeis1950() - Static method in class org.orekit.frames.FramesFactory
Get the VEIS 1950 reference frame.
getVelocity() - Method in class org.orekit.estimation.measurements.PV
Get the velocity.
getVelocity() - Method in class org.orekit.files.sinex.Station
Get the station velocity.
getVelocity() - Method in interface org.orekit.frames.FieldKinematicTransform
Get the first time derivative of the translation.
getVelocity() - Method in class org.orekit.frames.FieldTransform
Get the first time derivative of the translation.
getVelocity() - Method in interface org.orekit.frames.KinematicTransform
Get the first time derivative of the translation.
getVelocity() - Method in class org.orekit.frames.Transform
Get the first time derivative of the translation.
getVelocity() - Method in class org.orekit.utils.FieldPVCoordinates
Gets the velocity.
getVelocity() - Method in class org.orekit.utils.PVCoordinates
Gets the velocity.
getVelocity(AbsoluteDate, Vector3D, Frame) - Method in interface org.orekit.models.earth.atmosphere.Atmosphere
Get the inertial velocity of atmosphere molecules.
getVelocity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in interface org.orekit.models.earth.atmosphere.Atmosphere
Get the inertial velocity of atmosphere molecules.
getVelocityAccuracy() - Method in class org.orekit.files.sp3.SP3Coordinate
Get the velocity accuracy.
getVelocityVector() - Method in class org.orekit.files.ccsds.ndm.cdm.StateVector
Get object Velocity Vector.
getVenus() - Method in interface org.orekit.bodies.CelestialBodies
Get the Venus singleton body.
getVenus() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Venus singleton body.
getVenus() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
 
getVersion() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter
Get current format version.
getVersion() - Method in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter
Get current format version.
getVersion() - Method in interface org.orekit.files.ccsds.utils.generation.MessageWriter
Get current format version.
getVersion() - Method in class org.orekit.files.ilrs.ILRSHeader
Get the format version.
getVersion() - Method in class org.orekit.files.sp3.SP3Header
Get the file version.
getVersion() - Method in class org.orekit.frames.ITRFVersionLoader.ITRFVersionConfiguration
Get ITRF version.
getVertices() - Method in class org.orekit.models.earth.tessellation.Tile
Get the four vertices.
getVmAbsolute() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties
Get the typical (50th percentile) visual magnitude.
getVmApparent() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties
Get the typical (50th percentile) apparent visual magnitude.
getVmApparentMax() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties
Get the maximum apparent visual magnitude.
getVmApparentMin() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties
Get the minimum apparent visual magnitude.
getVmns(int, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory
Get the Vn,sm coefficient from Vn,s.
getVtecQualityIndicator() - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Header
Get the VTEC quality indicator.
getWarmup() - Method in class org.orekit.estimation.measurements.modifiers.OutlierFilter
Get the value of warmup iterations.
getWaterVaporPressure() - Method in class org.orekit.models.earth.weather.FieldPressureTemperatureHumidity
Get humidity as water vapor pressure.
getWaterVaporPressure() - Method in class org.orekit.models.earth.weather.GlobalPressureTemperature2Model
Deprecated.
Returns the water vapor pressure at the station [hPa].
getWaterVaporPressure() - Method in class org.orekit.models.earth.weather.PressureTemperatureHumidity
Get humidity as water vapor pressure.
getWavelength() - Method in class org.orekit.estimation.measurements.gnss.AmbiguityDriver
Get signal wavelength.
getWavelength() - Method in class org.orekit.estimation.measurements.gnss.InterSatellitesPhase
Get the wavelength.
getWavelength() - Method in class org.orekit.estimation.measurements.gnss.OneWayGNSSPhase
Get the wavelength.
getWavelength() - Method in class org.orekit.estimation.measurements.gnss.Phase
Get the wavelength.
getWavelength() - Method in class org.orekit.files.ilrs.CRDConfiguration.SystemConfiguration
Get the transmit wavelength.
getWavelength() - Method in interface org.orekit.gnss.RadioWave
Get the wavelength in meters.
getWavelength(CRD.RangeMeasurement) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
Get the wavelength related to the given RangeMeasurement.
getWaves() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Get the loaded waves.
getWeatherParamerers(FieldGeodeticPoint<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.weather.AbstractGlobalPressureTemperature
Provide weather parameters.
getWeatherParamerers(FieldGeodeticPoint<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.weather.ConstantPressureTemperatureHumidityProvider
Provide weather parameters.
getWeatherParamerers(FieldGeodeticPoint<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.models.earth.weather.PressureTemperatureHumidityProvider
Provide weather parameters.
getWeatherParamerers(GeodeticPoint, AbsoluteDate) - Method in class org.orekit.models.earth.weather.AbstractGlobalPressureTemperature
Provide weather parameters.
getWeatherParamerers(GeodeticPoint, AbsoluteDate) - Method in class org.orekit.models.earth.weather.ConstantPressureTemperatureHumidityProvider
Provide weather parameters.
getWeatherParamerers(GeodeticPoint, AbsoluteDate) - Method in interface org.orekit.models.earth.weather.PressureTemperatureHumidityProvider
Provide weather parameters.
getWeatherParameters(GeodeticPoint, AbsoluteDate) - Method in class org.orekit.models.earth.weather.GlobalPressureTemperature
Provide weather parameters.
getWeek() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Getter for the reference week of the GNSS orbit.
getWeek() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
Gets the Reference Week of the GNSS orbit.
getWeek() - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage
Gets the Reference Week of the SBAS orbit.
getWeek() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
Gets the Reference Week of the SBAS orbit.
getWeekNumber() - Method in class org.orekit.gnss.rflink.gps.SubFrame1
Get Week Number.
getWeekNumber() - Method in class org.orekit.gnss.rflink.gps.SubFrame5B
Get the almanac week number.
getWeekNumber() - Method in class org.orekit.time.GNSSDate
Get the week number since the GNSS reference epoch.
getWeekNumberLsf() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D
Get Week Number LSF field.
getWeekNumberT() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D
Get Week Number T field.
getWeightedRms() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get weighted RMS residual ratio.
getWeightedRMS() - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters
Get the weighted Root Mean Square (RMS) of the residuals from a batch least squares OD.
getWest() - Method in class org.orekit.bodies.FieldGeodeticPoint
Get the direction to the west of point, expressed in parent shape frame.
getWest() - Method in class org.orekit.bodies.GeodeticPoint
Get the direction to the west of point, expressed in parent shape frame.
getWest() - Method in class org.orekit.frames.TopocentricFrame
Get the west direction of topocentric frame, expressed in parent shape frame.
getWestAmplitude(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
Get the amplitude along west axis.
getWestPhase(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
Get the phase along West axis.
getWetMass() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalProperties
Get the total mass at T₀.
getWetMass() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Get the total mass at T₀.
getWgs84(Frame) - Static method in class org.orekit.models.earth.ReferenceEllipsoid
Get the WGS84 ellipsoid, attached to the given body frame.
getWideLaneCombination(SatelliteSystem) - Static method in class org.orekit.estimation.measurements.gnss.MeasurementCombinationFactory
Get the Wide-Lane combination of measurements.
getWindowLength() - Method in class org.orekit.files.ilrs.CRD.NptRangeMeasurement
Get the normal point window length.
getWindUp(SatelliteSystem, int, Dipole, String) - Method in class org.orekit.estimation.measurements.gnss.WindUpFactory
Get a modifier for a satellite/receiver pair.
getWindUp(SatelliteSystem, int, Dipole, SatelliteSystem, int, Dipole) - Method in class org.orekit.estimation.measurements.gnss.InterSatellitesWindUpFactory
Get a modifier for an emitter/receiver pair.
getWMM(double) - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory
Get the WMM model for the given year.
getWMM(double) - Method in interface org.orekit.models.earth.GeoMagneticFields
Get the WMM model for the given year.
getWMM(double) - Method in class org.orekit.models.earth.LazyLoadedGeoMagneticFields
 
getX() - Method in class org.orekit.files.rinex.clock.RinexClock.Receiver
Getter for the X coordinate in meters in considered Earth centered frame.
getX() - Method in class org.orekit.frames.EOPEntry
Get the X component of the pole motion.
getX() - Method in class org.orekit.geometry.fov.SmoothFieldOfView
Get the X axis defining FoV boundary.
getX() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Getter for the satellite X position.
getX() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
 
getX() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
Get the ECEF-X component of satellite coordinates in PZ-90 datum.
getX() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
Get the ECEF-X component of satellite coordinates.
getX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext
Get Χ = 1 / sqrt(1 - e²) = 1 / B.
getX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
Deprecated.
since 12.2 Use getChi() instead
getX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext
Get Χ = 1 / sqrt(1 - e²) = 1 / B.
getX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
Deprecated.
since 12.2 Use getChi() instead
getX2ON2A2XP1() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
Get (χ²) / (n² * a² * (χ + 1 ) ).
getX2ON2A2XP1() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
Get (χ²) / (n² * a² * (χ + 1 ) ).
getX3ON2A() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
Get χ³ / (n² * a).
getX3ON2A() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
Get χ³ / (n² * a).
getXDot() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Getter for the satellite X velocity.
getXDot() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
 
getXDot() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
Get the ECEF-X component of satellite velocity vector in PZ-90 datum.
getXDot() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
Get the ECEF-X component of satellite velocity vector.
getXDotDot() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Getter for the satellite X acceleration.
getXDotDot() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
 
getXDotDot() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
Get the GLONASS ECEF-X component of satellite acceleration vector in PZ-90 datum.
getXDotDot() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
Get the ECEF-X component of satellite acceleration vector.
getXM10() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader.LineParameters
Get the MG2 index scaled to F10.
getXM10(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData
Get the MG2 index scaled to F10.
getXM10(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters
Get the MG2 index scaled to F10.
getXM10B() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader.LineParameters
Get the MG2 81-day average centered index.
getXM10B(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData
Get the MG2 81-day average centered index.
getXM10B(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters
Get the MG2 81-day average centered index.
getXON2A2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
Get χ / (n² * a²).
getXON2A2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
Get χ / (n² * a²).
getXp() - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage
Get the X component of the pole.
getXp() - Method in class org.orekit.frames.EOPFittedModel
Get the fitted secular and harmonics model for pole x component.
getXp() - Method in class org.orekit.frames.FieldPoleCorrection
Get the xp parameter.
getXp() - Method in class org.orekit.frames.PoleCorrection
Get the xp parameter.
getXpDot() - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage
Get the X component of the pole first derivative.
getXpDotDot() - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage
Get the X component of the pole second derivative.
getXPo() - Method in class org.orekit.files.sinex.SinexEopEntry
Get the X polar motion.
getXRate() - Method in class org.orekit.frames.EOPEntry
Get the X component of the pole motion rate.
getXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext
Get Χ².
getXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
Deprecated.
since 12.2 Use getChi2() instead
getXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext
Get Χ².
getXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
Deprecated.
since 12.2 Use getChi2() instead
getXXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
Deprecated.
since 12.2 Use getChi3() instead
getXXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
Deprecated.
since 12.2 Use getChi3() instead
getXYSpXY2Function() - Method in enum org.orekit.utils.IERSConventions
Get the function computing the Celestial Intermediate Pole and Celestial Intermediate Origin components.
getXYSpXY2Function(TimeScales) - Method in enum org.orekit.utils.IERSConventions
Get the function computing the Celestial Intermediate Pole and Celestial Intermediate Origin components.
getXYZCovarianceBlock() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmData
Get the Covariance Matrix in the XYZ Coordinate Frame (defined by value of CdmMetadataKey.ALT_COV_REF_FRAME).
getXYZCovarianceMatrix() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the XYZ covariance matrix.
getY() - Method in class org.orekit.files.rinex.clock.RinexClock.Receiver
Getter for the Y coordinate in meters in considered Earth centered frame.
getY() - Method in class org.orekit.frames.EOPEntry
Get the Y component of the pole motion.
getY() - Method in class org.orekit.geometry.fov.SmoothFieldOfView
Get the Y axis defining FoV boundary.
getY() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Getter for the satellite Y position.
getY() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
 
getY() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
Get the ECEF-Y component of satellite coordinates in PZ-90 datum.
getY() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
Get the ECEF-Y component of satellite coordinates.
getY10() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader.LineParameters
Get the Solar X-Ray & Lya index scaled to F10.
getY10(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData
Get the Solar X-Ray & Lya index scaled to F10.
getY10(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters
Get the Solar X-Ray & Lya index scaled to F10.
getY10B() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader.LineParameters
Get the Solar X-Ray & Lya 81-day ave.
getY10B(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData
Get the Solar X-Ray & Lya 81-day ave.
getY10B(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters
Get the Solar X-Ray & Lya 81-day ave.
getYawAngle() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data
Get the yaw angle used for computation of phase wind-up correction.
getYawAngle(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawCompensation
Compute the yaw compensation angle at date.
getYawAngle(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawCompensation
Compute the yaw compensation angle at date.
getYawRate() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data
Get the yaw rate.
getYDot() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Getter for the satellite Y velocity.
getYDot() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
 
getYDot() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
Get the ECEF-Y component of satellite velocity vector in PZ-90 datum.
getYDot() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
Get the ECEF-Y component of satellite velocity vector.
getYDotDot() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Getter for the satellite Y acceleration.
getYDotDot() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
 
getYDotDot() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
Get the GLONASS ECEF-Y component of satellite acceleration vector in PZ-90 datum.
getYDotDot() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
Get the ECEF-Y component of satellite acceleration vector.
getYear() - Method in enum org.orekit.frames.ITRFVersion
Get the reference year of the frame version.
getYear() - Method in class org.orekit.time.DateComponents
Get the year number.
getYearOfCentury() - Method in class org.orekit.files.ilrs.CRDHeader
Get the year of century from CPF or TLE.
getYp() - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage
Get the Y component of the pole.
getYp() - Method in class org.orekit.frames.EOPFittedModel
Get the fitted secular and harmonics model for pole y component.
getYp() - Method in class org.orekit.frames.FieldPoleCorrection
Get the yp parameter.
getYp() - Method in class org.orekit.frames.PoleCorrection
Get the yp parameter.
getYpDot() - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage
Get the Y component of the pole first derivative.
getYpDotDot() - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage
Get the Y component of the pole second derivative.
getYPo() - Method in class org.orekit.files.sinex.SinexEopEntry
Get the Y polar motion.
getYRate() - Method in class org.orekit.frames.EOPEntry
Get the Y component of the pole motion rate.
getZ() - Method in class org.orekit.files.rinex.clock.RinexClock.Receiver
Getter for the Z coordinate in meters in considered Earth centered frame.
getZ() - Method in class org.orekit.geometry.fov.SmoothFieldOfView
Get the Z axis defining FoV boundary.
getZ() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Getter for the satellite Z position.
getZ() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
 
getZ() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
Get the ECEF-Z component of satellite coordinates in PZ-90 datum.
getZ() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
Get the ECEF-Z component of satellite coordinates.
getZDot() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Getter for the satellite Z velocity.
getZDot() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
 
getZDot() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
Get the ECEF-Z component of satellite velocity vector in PZ-90 datum.
getZDot() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
Get the ECEF-Z component of satellite velocity vector.
getZDotDot() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Getter for the satellite Z acceleration.
getZDotDot() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
 
getZDotDot() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
Get the GLONASS ECEF-Z component of satellite acceleration vector in PZ-90 datum.
getZDotDot() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
Get the ECEF-Z component of satellite acceleration vector.
getZenith() - Method in class org.orekit.bodies.FieldGeodeticPoint
Get the direction above the point, expressed in parent shape frame.
getZenith() - Method in class org.orekit.bodies.GeodeticPoint
Get the direction above the point, expressed in parent shape frame.
getZenith() - Method in class org.orekit.frames.TopocentricFrame
Get the zenith direction of topocentric frame, expressed in parent shape frame.
getZenithAmplitude(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
Get the amplitude along zenith axis.
getZenithDelay() - Method in class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader
Returns the zenith delay array.
getZenithOffsetDriver() - Method in class org.orekit.estimation.measurements.GroundStation
Get a driver allowing to change station position along Zenith axis.
getZenithPhase(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
Get the phase along zenith axis.
getZero() - Method in class org.orekit.orbits.FieldOrbit
Getter for Field-valued zero.
getZero() - Method in class org.orekit.time.AbstractFieldTimeInterpolator.InterpolationData
Get zero.
getZero(Field<T>) - Static method in class org.orekit.utils.FieldPVCoordinates
Get fixed position/velocity at origin (both p, v and a are zero vectors).
getZh() - Method in class org.orekit.models.earth.troposphere.FieldTroposphericDelay
Get hydrostatic zenith delay (m).
getZh() - Method in class org.orekit.models.earth.troposphere.TroposphericDelay
Get hydrostatic zenith delay (m).
getZInverseTransformationReference() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Get a reference to the Z inverse transformation matrix.
getZipJarCrawler(File) - Method in class org.orekit.data.FilesListCrawler
Get a zip/jar crawler for an input.
getZipJarCrawler(URL) - Method in class org.orekit.data.NetworkCrawler
Get a zip/jar crawler for an input.
getZipJarCrawler(T) - Method in class org.orekit.data.AbstractListCrawler
Get a zip/jar crawler for an input.
getZone() - Method in class org.orekit.geometry.fov.PolygonalFieldOfView
Get the interior zone.
getZone() - Method in class org.orekit.propagation.events.FootprintOverlapDetector
Get the geographic zone triggering the events.
getZone() - Method in class org.orekit.propagation.events.GeographicZoneDetector
Get the geographic zone.
getZw() - Method in class org.orekit.models.earth.troposphere.FieldTroposphericDelay
Get wet zenith delay (m).
getZw() - Method in class org.orekit.models.earth.troposphere.TroposphericDelay
Get wet zenith delay (m).
GHIJjsPolynomials - Class in org.orekit.propagation.semianalytical.dsst.utilities
Compute the Gjs, Hjs, Ijs and Jjs polynomials in the equinoctial elements h, k and the direction cosines α and β and their partial derivatives with respect to k, h, α and β.
GHIJjsPolynomials(double, double, double, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Create a set of Gjs, Hjs, Ijs and Jjs polynomials.
GHmsjPolynomials - Class in org.orekit.propagation.semianalytical.dsst.utilities
Compute the Gmsj and the Hmsj polynomials in the equinoctial elements h, k and the direction cosines α and β and their partial derivatives with respect to k, h, α and β.
GHmsjPolynomials(double, double, double, double, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Create a set of Gmsj and Hmsj polynomials.
GHO - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCategory
GEO-superGEO, Crossing Orbit 31570 < hp < 40002 km, 40002 km < ha.
GillFieldIntegratorBuilder<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.conversion
Builder for GillFieldIntegrator.
GillFieldIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.GillFieldIntegratorBuilder
Constructor.
GillFieldIntegratorBuilder(T) - Constructor for class org.orekit.propagation.conversion.GillFieldIntegratorBuilder
Constructor using a "fielded" step.
GillIntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for GillIntegrator.
GillIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.GillIntegratorBuilder
Build a new instance.
GLO - org.orekit.gnss.metric.ntrip.NavigationSystem
Glonass.
GLO - org.orekit.gnss.ObservationTimeScale
GLONASS time scale.
GLOBAL_DRAG_FACTOR - Static variable in interface org.orekit.forces.drag.DragSensitive
Parameter name for global multiplicative factor.
GLOBAL_RADIATION_FACTOR - Static variable in interface org.orekit.forces.radiation.RadiationSensitive
Parameter name for global multiplicative factor.
GlobalIonosphereMapModel - Class in org.orekit.models.earth.ionosphere
Global Ionosphere Map (GIM) model.
GlobalIonosphereMapModel(String) - Constructor for class org.orekit.models.earth.ionosphere.GlobalIonosphereMapModel
Constructor with supported names given by user.
GlobalIonosphereMapModel(String, DataProvidersManager, TimeScale) - Constructor for class org.orekit.models.earth.ionosphere.GlobalIonosphereMapModel
Constructor that uses user defined supported names and data context.
GlobalIonosphereMapModel(TimeScale, DataSource...) - Constructor for class org.orekit.models.earth.ionosphere.GlobalIonosphereMapModel
Constructor that uses user defined data sources.
GlobalMappingFunctionModel - Class in org.orekit.models.earth.troposphere
The Global Mapping Function model for radio techniques.
GlobalMappingFunctionModel() - Constructor for class org.orekit.models.earth.troposphere.GlobalMappingFunctionModel
Build a new instance.
GlobalMappingFunctionModel(TimeScale) - Constructor for class org.orekit.models.earth.troposphere.GlobalMappingFunctionModel
Build a new instance.
GlobalPressureTemperature - Class in org.orekit.models.earth.weather
The Global Pressure and Temperature model.
GlobalPressureTemperature(Geoid) - Constructor for class org.orekit.models.earth.weather.GlobalPressureTemperature
Build a new instance.
GlobalPressureTemperature(Geoid, TimeScale) - Constructor for class org.orekit.models.earth.weather.GlobalPressureTemperature
Build a new instance.
GlobalPressureTemperature2 - Class in org.orekit.models.earth.weather
The Global Pressure and Temperature 2 (GPT2) model.
GlobalPressureTemperature2(String, DataProvidersManager, TimeScale) - Constructor for class org.orekit.models.earth.weather.GlobalPressureTemperature2
Deprecated.
as of 12.1 used only by GlobalPressureTemperature2Model
GlobalPressureTemperature2(DataSource, TimeScale) - Constructor for class org.orekit.models.earth.weather.GlobalPressureTemperature2
Constructor with source of GPT2 auxiliary data given by user.
GlobalPressureTemperature2Model - Class in org.orekit.models.earth.weather
Deprecated.
GlobalPressureTemperature2Model(double, double, Geoid) - Constructor for class org.orekit.models.earth.weather.GlobalPressureTemperature2Model
Deprecated.
Constructor with default supported names.
GlobalPressureTemperature2Model(String, double, double, Geoid) - Constructor for class org.orekit.models.earth.weather.GlobalPressureTemperature2Model
Deprecated.
Constructor with supported names given by user.
GlobalPressureTemperature2Model(String, double, double, Geoid, DataProvidersManager, TimeScale) - Constructor for class org.orekit.models.earth.weather.GlobalPressureTemperature2Model
Deprecated.
Constructor with supported names and source of GPT2 auxiliary data given by user.
GlobalPressureTemperature2w - Class in org.orekit.models.earth.weather
The Global Pressure and Temperature 2w (GPT2w) model.
GlobalPressureTemperature2w(DataSource, TimeScale) - Constructor for class org.orekit.models.earth.weather.GlobalPressureTemperature2w
Constructor with supported names and source of GPT2w auxiliary data given by user.
GlobalPressureTemperature3 - Class in org.orekit.models.earth.weather
The Global Pressure and Temperature 3 (GPT3) model.
GlobalPressureTemperature3(DataSource, TimeScale) - Constructor for class org.orekit.models.earth.weather.GlobalPressureTemperature3
Constructor with source of GPT3 auxiliary data given by user.
GlobalPressureTemperatureModel - Class in org.orekit.models.earth.weather
Deprecated.
as of 12.1, replaced by GlobalPressureTemperature
GlobalPressureTemperatureModel(double, double, Frame) - Constructor for class org.orekit.models.earth.weather.GlobalPressureTemperatureModel
Deprecated.
Build a new instance.
GlobalPressureTemperatureModel(double, double, Frame, DataContext) - Constructor for class org.orekit.models.earth.weather.GlobalPressureTemperatureModel
Deprecated.
Build a new instance.
Glonass - Class in org.orekit.gnss.attitude
Attitude providers for Glonass navigation satellites.
Glonass(double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.Glonass
Simple constructor.
GLONASS - org.orekit.files.sp3.SP3FileType
GLONASS only file.
GLONASS - org.orekit.gnss.antenna.SatelliteType
GLONASS : GLONASS no.
GLONASS - org.orekit.gnss.SatelliteSystem
GLONASS system.
GLONASS - org.orekit.gnss.TimeSystem
GLONASS.
GLONASS_COD_PHS_BIS - org.orekit.files.rinex.section.RinexLabels
GLONASS phase bias corrections.
GLONASS_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Reference epoch for GLONASS four-year interval number: 1996-01-01T00:00:00 GLONASS time.
GLONASS_EPOCH - Static variable in class org.orekit.time.DateComponents
Reference epoch for GLONASS four-year interval number: 1996-01-01.
GLONASS_K1 - org.orekit.gnss.antenna.SatelliteType
GLONASS-K1 : IGS SVN R801-R802 (GLO no.
GLONASS_K2 - org.orekit.gnss.antenna.SatelliteType
GLONASS-K2.
GLONASS_M - org.orekit.gnss.antenna.SatelliteType
GLONASS-M : GLONASS no.
GLONASS_MU - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
Value of the Earth's universal gravitational parameter for GLONASS user in m³/s².
GLONASS_PI - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
Value of Pi for conversion from semicircles to radian.
GLONASS_SLOT_FRQ_NB - org.orekit.files.rinex.section.RinexLabels
GLONASS slot and frequency number.
GLONASSAlmanac - Class in org.orekit.propagation.analytical.gnss.data
This class holds a GLONASS almanac as read from .agl files.
GLONASSAlmanac(int, int, int, int, int, double, double, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
Constructor.
GLONASSAlmanac(int, int, int, int, int, double, double, double, double, double, double, double, double, double, double, TimeScale) - Constructor for class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
Constructor.
GLONASSAnalyticalPropagator - Class in org.orekit.propagation.analytical.gnss
This class aims at propagating a GLONASS orbit from GLONASSOrbitalElements.
GLONASSAnalyticalPropagatorBuilder - Class in org.orekit.propagation.analytical.gnss
This nested class aims at building a GLONASSAnalyticalPropagator.
GLONASSAnalyticalPropagatorBuilder(GLONASSOrbitalElements) - Constructor for class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagatorBuilder
Initializes the builder.
GLONASSAnalyticalPropagatorBuilder(GLONASSOrbitalElements, DataContext) - Constructor for class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagatorBuilder
Initializes the builder.
GLONASSDate - Class in org.orekit.time
Container for date in GLONASS form.
GLONASSDate(int, int, double) - Constructor for class org.orekit.time.GLONASSDate
Build an instance corresponding to a GLONASS date.
GLONASSDate(int, int, double, TimeScale) - Constructor for class org.orekit.time.GLONASSDate
Build an instance corresponding to a GLONASS date.
GLONASSDate(AbsoluteDate) - Constructor for class org.orekit.time.GLONASSDate
Build an instance from an absolute date.
GLONASSDate(AbsoluteDate, TimeScale) - Constructor for class org.orekit.time.GLONASSDate
Build an instance from an absolute date.
GLONASSEphemeris - Class in org.orekit.propagation.analytical.gnss.data
Class for GLONASS ephemeris used by the GLONASSNumericalPropagator.
GLONASSEphemeris(int, int, double, double, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
Build a new instance.
GLONASSEphemeris(int, int, double, double, double, double, double, double, double, double, double, double, AbsoluteDate) - Constructor for class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
Build a new instance.
GLONASSNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data
Container for data contained in a Glonass navigation message.
GLONASSNavigationMessage() - Constructor for class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage
Constructor.
GLONASSNumericalPropagator - Class in org.orekit.propagation.numerical
This class propagates GLONASS orbits using numerical integration.
GLONASSNumericalPropagator(ClassicalRungeKuttaIntegrator, GLONASSOrbitalElements, Frame, AttitudeProvider, double, DataContext, boolean) - Constructor for class org.orekit.propagation.numerical.GLONASSNumericalPropagator
Private constructor.
GLONASSNumericalPropagatorBuilder - Class in org.orekit.propagation.numerical
This nested class aims at building a GLONASSNumericalPropagator.
GLONASSNumericalPropagatorBuilder(ClassicalRungeKuttaIntegrator, GLONASSOrbitalElements, boolean) - Constructor for class org.orekit.propagation.numerical.GLONASSNumericalPropagatorBuilder
Initializes the builder.
GLONASSNumericalPropagatorBuilder(ClassicalRungeKuttaIntegrator, GLONASSOrbitalElements, boolean, DataContext) - Constructor for class org.orekit.propagation.numerical.GLONASSNumericalPropagatorBuilder
Initializes the builder.
GLONASSOrbitalElements - Interface in org.orekit.propagation.analytical.gnss.data
This interface provides the minimal set of orbital elements needed by the GLONASSAnalyticalPropagator and the GLONASSNumericalPropagator.
GlonassSatelliteChannel - Class in org.orekit.files.rinex.observation
Container for association between GLONASS satellites and frequency channels (f = f₀ + k Δf with k ranging-7 to +6).
GlonassSatelliteChannel(SatInSystem, int) - Constructor for class org.orekit.files.rinex.observation.GlonassSatelliteChannel
Simple constructor.
GLONASSScale - Class in org.orekit.time
GLONASS time scale.
GlonassUserRangeAccuracy - Class in org.orekit.gnss.metric.messages.common
Enumerate for GLONASS User Range Accuracy.
GlonassUserRangeAccuracy(int) - Constructor for class org.orekit.gnss.metric.messages.common.GlonassUserRangeAccuracy
Simple constructor.
GM - org.orekit.files.ccsds.ndm.odm.KeplerianElementsKey
Gravitational coefficient.
GM - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey
Central body oblate spheroid oblateness.
GMST - org.orekit.files.ccsds.definitions.TimeSystem
Greenwich Mean Sidereal Time.
GMSTScale - Class in org.orekit.time
Greenwich Mean Sidereal Time.
GMT - org.orekit.gnss.TimeSystem
GMT (should only be used in RUN BY / DATE entries).
GNSS_PARITY_ERROR - org.orekit.errors.OrekitMessages
GNSS_PARITY_ERROR.
GNSS_PI - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
Value of Pi for conversion from semicircles to radians in GNSS.
GNSS_WEEK_IN_SECONDS - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
Duration of the GNSS week in seconds.
GNSSAttitudeProvider - Interface in org.orekit.gnss.attitude
Attitude providers for navigation satellites.
GNSSClockElements - Interface in org.orekit.propagation.analytical.gnss.data
This interface provides the minimal set of orbital elements needed by the ClockCorrectionsProvider.
GNSSConstants - Interface in org.orekit.propagation.analytical.gnss.data
Set of useful physical constants used in Global Navigation Satellite Systems (GNSS).
GnssData - Class in org.orekit.gnss.metric.ntrip
GNSS data retrieved from Ntrip caster.
GnssData(byte[], int) - Constructor for class org.orekit.gnss.metric.ntrip.GnssData
Build a GNSS data bloc.
GNSSDate - Class in org.orekit.time
Container for date in GNSS form.
GNSSDate(int, double, SatelliteSystem) - Constructor for class org.orekit.time.GNSSDate
Build an instance corresponding to a GNSS date.
GNSSDate(int, double, SatelliteSystem, DateComponents, TimeScales) - Constructor for class org.orekit.time.GNSSDate
Build an instance corresponding to a GNSS date.
GNSSDate(int, double, SatelliteSystem, TimeScales) - Constructor for class org.orekit.time.GNSSDate
Build an instance corresponding to a GNSS date.
GNSSDate(AbsoluteDate, SatelliteSystem) - Constructor for class org.orekit.time.GNSSDate
Build an instance from an absolute date.
GNSSDate(AbsoluteDate, SatelliteSystem, TimeScales) - Constructor for class org.orekit.time.GNSSDate
Build an instance from an absolute date.
GNSSOrbitalElements - Interface in org.orekit.propagation.analytical.gnss.data
This interface provides the minimal set of orbital elements needed by the GNSSPropagator.
GNSSPropagator - Class in org.orekit.propagation.analytical.gnss
Common handling of AbstractAnalyticalPropagator methods for GNSS propagators.
GNSSPropagatorBuilder - Class in org.orekit.propagation.analytical.gnss
This nested class aims at building a GNSSPropagator.
GNSSPropagatorBuilder(GNSSOrbitalElements) - Constructor for class org.orekit.propagation.analytical.gnss.GNSSPropagatorBuilder
Initializes the builder.
GNSSPropagatorBuilder(GNSSOrbitalElements, Frames) - Constructor for class org.orekit.propagation.analytical.gnss.GNSSPropagatorBuilder
Initializes the builder.
GnssSignal - Interface in org.orekit.gnss
Intermediate level interface for radio waves related to GNSS common frequency.
GPS - org.orekit.files.ccsds.definitions.TimeSystem
Global Positioning System.
GPS - org.orekit.files.rinex.navigation.IonosphericCorrectionType
GPS α/β.
GPS - org.orekit.files.sp3.SP3FileType
GPS only file.
GPS - org.orekit.gnss.metric.ntrip.NavigationSystem
GPS.
GPS - org.orekit.gnss.ObservationTimeScale
GPS time scale.
GPS - org.orekit.gnss.SatelliteSystem
GPS system.
GPS - org.orekit.gnss.TimeSystem
Global Positioning System.
GPS_AV - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
Value of the earth's rotation rate in rad/s for GPS user.
GPS_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Reference epoch for GPS weeks: 1980-01-06T00:00:00 GPS time.
GPS_EPOCH - Static variable in class org.orekit.time.DateComponents
Reference epoch for GPS weeks: 1980-01-06.
GPS_MU - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
WGS 84 value of the Earth's universal gravitational parameter for GPS user in m³/s².
GPS_WEEK_NB - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
Number of weeks in the GPS cycle.
GPSAlmanac - Class in org.orekit.propagation.analytical.gnss.data
This class holds a GPS almanac as read from SEM or YUMA files.
GPSAlmanac() - Constructor for class org.orekit.propagation.analytical.gnss.data.GPSAlmanac
Constructor.
GPSBlockIIA - Class in org.orekit.gnss.attitude
Attitude providers for GPS block IIA navigation satellites.
GPSBlockIIA(double, double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.GPSBlockIIA
Simple constructor.
GPSBlockIIF - Class in org.orekit.gnss.attitude
Attitude providers for GPS block IIF navigation satellites.
GPSBlockIIF(double, double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.GPSBlockIIF
Simple constructor.
GPSBlockIIR - Class in org.orekit.gnss.attitude
Attitude providers for GPS block IIR navigation satellites.
GPSBlockIIR(double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.GPSBlockIIR
Simple constructor.
GPSCivilianNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data
Container for data contained in a GPS navigation message.
GPSCivilianNavigationMessage(boolean) - Constructor for class org.orekit.propagation.analytical.gnss.data.GPSCivilianNavigationMessage
Constructor.
GPSLegacyNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data
Container for data contained in a GPS navigation message.
GPSLegacyNavigationMessage() - Constructor for class org.orekit.propagation.analytical.gnss.data.GPSLegacyNavigationMessage
Constructor.
GPSScale - Class in org.orekit.time
GPS time scale.
gradient(AbsoluteDate, Vector3D, double) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Compute the gradient of the non-central part of the gravity field.
gradient(FieldAbsoluteDate<T>, FieldVector3D<T>, T) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Compute the gradient of the non-central part of the gravity field.
GraggBulirschStoerIntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for GraggBulirschStoerIntegrator.
GraggBulirschStoerIntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.GraggBulirschStoerIntegratorBuilder
Build a new instance.
GraggBulirschStoerIntegratorBuilder(double, double, double, double) - Constructor for class org.orekit.propagation.conversion.GraggBulirschStoerIntegratorBuilder
Build a new instance.
GRAM - Static variable in class org.orekit.utils.units.Unit
Gram unit.
GRAPHIC - org.orekit.estimation.measurements.gnss.CombinationType
GRoup And Phase Ionospheric Calibration (GRAPHIC) combination.
GRAPHICCombination - Class in org.orekit.estimation.measurements.gnss
GRoup And Phase Ionospheric Calibration (GRAPHIC) combination.
GRAV_ASSIST_NAME - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey
Origin of maneuver gravitational assist body.
GRAVITY_FIELD_NORMALIZATION_UNDERFLOW - org.orekit.errors.OrekitMessages
GRAVITY_FIELD_NORMALIZATION_UNDERFLOW.
GRAVITY_MODEL - org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey
Gravity model.
GRAVITY_MODEL - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey
Gravity model.
GravityFieldFactory - Class in org.orekit.forces.gravity.potential
Factory used to read gravity field files in several supported formats.
GravityFields - Interface in org.orekit.forces.gravity.potential
Defines methods for obtaining gravity fields.
GRC - org.orekit.files.ccsds.definitions.CelestialBodyFrame
Greenwich Rotating Coordinates.
greatCircleBuilder(OneAxisEllipsoid) - Static method in class org.orekit.utils.WaypointPVBuilder
Construct a waypoint builder interpolating points using a great-circle.
GRGS_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory
Default regular expression for GRGS files.
GRGSFormatReader - Class in org.orekit.forces.gravity.potential
Reader for the GRGS gravity field format.
GRGSFormatReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.GRGSFormatReader
Simple constructor.
GRGSFormatReader(String, boolean, TimeScale) - Constructor for class org.orekit.forces.gravity.potential.GRGSFormatReader
Simple constructor.
GRIM5C1_EARTH_ANGULAR_VELOCITY - Static variable in interface org.orekit.utils.Constants
Earth angular velocity from GRIM5C1 model: 7.292115e-5 rad/s.
GRIM5C1_EARTH_C20 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized second zonal coefficient from GRIM5C1 model: -1.082626110612609e-3.
GRIM5C1_EARTH_C30 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized third zonal coefficient from GRIM5C1 model: 2.536150841690056e-6.
GRIM5C1_EARTH_C40 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized fourth zonal coefficient from GRIM5C1 model: 1.61936352497151e-6.
GRIM5C1_EARTH_C50 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized fifth zonal coefficient from GRIM5C1 model: 2.231013736607540e-7.
GRIM5C1_EARTH_C60 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized sixth zonal coefficient from GRIM5C1 model: -5.402895357302363e-7.
GRIM5C1_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Earth equatorial radius from GRIM5C1 model: 6378136.46 m.
GRIM5C1_EARTH_FLATTENING - Static variable in interface org.orekit.utils.Constants
Earth flattening from GRIM5C1 model: 1.0 / 298.25765.
GRIM5C1_EARTH_MU - Static variable in interface org.orekit.utils.Constants
Earth gravitational constant from GRIM5C1 model: 3.986004415e14 m³/s².
GroundAtNightDetector - Class in org.orekit.propagation.events
Detector for ground location being at night.
GroundAtNightDetector(TopocentricFrame, PVCoordinatesProvider, double, AtmosphericRefractionModel) - Constructor for class org.orekit.propagation.events.GroundAtNightDetector
Simple constructor.
GroundAtNightDetector(TopocentricFrame, PVCoordinatesProvider, double, AtmosphericRefractionModel, AdaptableInterval, double, int, EventHandler) - Constructor for class org.orekit.propagation.events.GroundAtNightDetector
Private constructor.
GroundFieldOfViewDetector - Class in org.orekit.propagation.events
Finder for satellite entry/exit events with respect to a sensor Field Of View attached to an arbitrary frame.
GroundFieldOfViewDetector(Frame, FieldOfView) - Constructor for class org.orekit.propagation.events.GroundFieldOfViewDetector
Build a new instance.
GroundFieldOfViewDetector(AdaptableInterval, double, int, EventHandler, Frame, FieldOfView) - Constructor for class org.orekit.propagation.events.GroundFieldOfViewDetector
Protected constructor with full parameters.
GroundPointing - Class in org.orekit.attitudes
Base class for ground pointing attitude providers.
GroundPointing(Frame, Frame) - Constructor for class org.orekit.attitudes.GroundPointing
Default constructor.
GroundPointingAttitudeModifier - Class in org.orekit.attitudes
Abstract class for attitude provider modifiers using an underlying ground pointing law.
GroundPointingAttitudeModifier(Frame, Frame, GroundPointing) - Constructor for class org.orekit.attitudes.GroundPointingAttitudeModifier
Constructor.
GroundPointTarget - Class in org.orekit.attitudes
Ground point target for AlignedAndConstrained.
GroundPointTarget(Vector3D) - Constructor for class org.orekit.attitudes.GroundPointTarget
Simple constructor.
GroundReceiverCommonParametersWithDerivatives - Class in org.orekit.estimation.measurements
Common intermediate parameters used to estimate measurements where receiver is a ground station.
GroundReceiverCommonParametersWithDerivatives(SpacecraftState, Map<String, Integer>, FieldTransform<Gradient>, TimeStampedFieldPVCoordinates<Gradient>, Gradient, SpacecraftState, TimeStampedFieldPVCoordinates<Gradient>) - Constructor for class org.orekit.estimation.measurements.GroundReceiverCommonParametersWithDerivatives
Simple constructor.
GroundReceiverCommonParametersWithoutDerivatives - Class in org.orekit.estimation.measurements
Common intermediate parameters used to estimate measurements where receiver is a ground station.
GroundReceiverCommonParametersWithoutDerivatives(SpacecraftState, Transform, TimeStampedPVCoordinates, double, SpacecraftState, TimeStampedPVCoordinates) - Constructor for class org.orekit.estimation.measurements.GroundReceiverCommonParametersWithoutDerivatives
Simple constructor.
GroundReceiverMeasurement<T extends GroundReceiverMeasurement<T>> - Class in org.orekit.estimation.measurements
Base class modeling a measurement where receiver is a ground station.
GroundReceiverMeasurement(GroundStation, boolean, AbsoluteDate, double[], double[], double[], ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.GroundReceiverMeasurement
Simple constructor.
GroundReceiverMeasurement(GroundStation, boolean, AbsoluteDate, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.GroundReceiverMeasurement
Simple constructor.
GroundStation - Class in org.orekit.estimation.measurements
Class modeling a ground station that can perform some measurements.
GroundStation(TopocentricFrame) - Constructor for class org.orekit.estimation.measurements.GroundStation
Build a ground station ignoring station displacements.
GroundStation(TopocentricFrame, EOPHistory, StationDisplacement...) - Constructor for class org.orekit.estimation.measurements.GroundStation
GroundStation(TopocentricFrame, PressureTemperatureHumidityProvider) - Constructor for class org.orekit.estimation.measurements.GroundStation
Build a ground station ignoring station displacements.
GroundStation(TopocentricFrame, PressureTemperatureHumidityProvider, EOPHistory, StationDisplacement...) - Constructor for class org.orekit.estimation.measurements.GroundStation
Simple constructor.
GRS80_EARTH_ANGULAR_VELOCITY - Static variable in interface org.orekit.utils.Constants
Earth angular velocity from GRS80 model: 7.292115e-5 rad/s.
GRS80_EARTH_C20 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized second zonal coefficient from GRS80 model: -1.08263e-3.
GRS80_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Earth equatorial radius from GRS80 model: 6378137.0 m.
GRS80_EARTH_FLATTENING - Static variable in interface org.orekit.utils.Constants
Earth flattening from GRS80 model: 1.0 / 298.257222101.
GRS80_EARTH_MU - Static variable in interface org.orekit.utils.Constants
Earth gravitational constant from GRS80 model: 3.986005e14 m³/s².
GSO - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCategory
GeoStationary Orbit, with 3° < i < 25°, 35586 < hp < 35986 km, 35586 < ha < 35986 km.
GTO - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCategory
Geosynchronous Transfer Orbit, i < 90°, hp < 2000 km, 31570 < ha < 40002 km.
GTOD - org.orekit.files.ccsds.definitions.CelestialBodyFrame
Greenwich True Of Date.
GTOD_CONVENTIONS_1996_ACCURATE_EOP - org.orekit.frames.Predefined
GTOD, IERS 1996 conventions, with accurate EOP interpolation.
GTOD_CONVENTIONS_1996_SIMPLE_EOP - org.orekit.frames.Predefined
GTOD, IERS 1996 conventions, with simple EOP interpolation.
GTOD_CONVENTIONS_2003_ACCURATE_EOP - org.orekit.frames.Predefined
GTOD, IERS 2003 conventions, with accurate EOP interpolation.
GTOD_CONVENTIONS_2003_SIMPLE_EOP - org.orekit.frames.Predefined
GTOD, IERS 2003 conventions, with simple EOP interpolation.
GTOD_CONVENTIONS_2010_ACCURATE_EOP - org.orekit.frames.Predefined
GTOD, IERS 2010 conventions, with accurate EOP interpolation.
GTOD_CONVENTIONS_2010_SIMPLE_EOP - org.orekit.frames.Predefined
GTOD, IERS 2010 conventions, with simple EOP interpolation.
GTOD_WITHOUT_EOP_CORRECTIONS - org.orekit.frames.Predefined
GTOD, IERS 1996 conventions without EOP corrections.
GTODProvider - Class in org.orekit.frames
Greenwich True Of Date Frame, also known as True of Date Rotating frame (TDR) or Greenwich Rotating Coordinate frame (GCR).
GTODProvider(IERSConventions, EOPHistory, TimeScales) - Constructor for class org.orekit.frames.GTODProvider
Simple constructor.
guessCenter(Frame) - Static method in enum org.orekit.files.ccsds.definitions.CenterName
Guess the name of the center of the reference frame.
guessFrame(String) - Static method in class org.orekit.files.sp3.SP3Parser
Deprecated.
as of 12.1, replaced by IGSUtils.guessFrame(String)
guessFrame(String) - Static method in class org.orekit.gnss.IGSUtils
Default string to Frame conversion for SP3Parser or RinexClockParser.
guessFrame(Frame) - Static method in enum org.orekit.files.ccsds.definitions.CelestialBodyFrame
Guesses names from ODM Table 5-3 and Annex A.
guessFrame(Frames, String) - Static method in class org.orekit.gnss.IGSUtils
Default string to Frame conversion for SP3Parser or RinexClockParser.
GYRO - org.orekit.files.ccsds.definitions.SpacecraftBodyFrame.BaseEquipment
Gyro reference frame (this name was used in ADM V1.0 (CCSDS 504.0-B-1).
GYRO_BIAS - org.orekit.files.ccsds.ndm.adm.acm.RateElementsType
Correction to gyro rates.
GYRO_FRAME - org.orekit.files.ccsds.definitions.SpacecraftBodyFrame.BaseEquipment
Gyro reference frame (this name is used in SANA registry https://sanaregistry.org/r/spacecraft_body_reference_frames/).
GzipFilter - Class in org.orekit.data
Filter for gzip compressed data.
GzipFilter() - Constructor for class org.orekit.data.GzipFilter
Empty constructor.

H

H_X - Static variable in enum org.orekit.orbits.OrbitType
Name for inclination vector first component.
H_Y - Static variable in enum org.orekit.orbits.OrbitType
Name for inclination vector second component .
H00 - Static variable in class org.orekit.time.TimeComponents
Constant for commonly used hour 00:00:00.
H1 - org.orekit.files.ilrs.StreamingCpfWriter.HeaderLineWriter
Header first line.
H12 - Static variable in class org.orekit.time.TimeComponents
Constant for commonly used hour 12:00:00.
H2 - org.orekit.files.ilrs.StreamingCpfWriter.HeaderLineWriter
Header second line.
HALO - org.orekit.orbits.LibrationOrbitType
Halo orbit type.
HaloOrbit - Class in org.orekit.orbits
Class calculating different parameters of a Halo Orbit.
HaloOrbit(CR3BPSystem, PVCoordinates, double) - Constructor for class org.orekit.orbits.HaloOrbit
Simple Constructor.
HaloOrbit(RichardsonExpansion, double, LibrationOrbitFamily) - Constructor for class org.orekit.orbits.HaloOrbit
Simple Constructor.
HaloXZPlaneCrossingDetector - Class in org.orekit.propagation.events
Detector for XZ Plane crossing.
HaloXZPlaneCrossingDetector(double, double) - Constructor for class org.orekit.propagation.events.HaloXZPlaneCrossingDetector
Simple Constructor.
HaloXZPlaneCrossingDetector(AdaptableInterval, double, int, EventHandler) - Constructor for class org.orekit.propagation.events.HaloXZPlaneCrossingDetector
Protected constructor with full parameters.
handleGeneratedMeasurement(ObservedMeasurement<?>) - Method in class org.orekit.estimation.measurements.generation.GatheringSubscriber
Handle a generated measurement.
handleGeneratedMeasurement(ObservedMeasurement<?>) - Method in interface org.orekit.estimation.measurements.generation.GeneratedMeasurementSubscriber
Handle a generated measurement.
handleNaN(String) - Static method in class org.orekit.files.ilrs.CRD
Replace all " NaN" with " na".
handleStep(List<OrekitStepInterpolator>) - Method in interface org.orekit.propagation.sampling.MultiSatStepHandler
Handle the current step.
handleStep(List<OrekitStepInterpolator>) - Method in class org.orekit.propagation.sampling.MultisatStepNormalizer
Handle the current step.
handleStep(List<SpacecraftState>) - Method in interface org.orekit.propagation.sampling.MultiSatFixedStepHandler
Handle the current step.
handleStep(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.sampling.FieldOrekitFixedStepHandler
Handle the current step.
handleStep(FieldOrekitStepInterpolator<T>) - Method in interface org.orekit.propagation.sampling.FieldOrekitStepHandler
Handle the current step.
handleStep(FieldOrekitStepInterpolator<T>) - Method in class org.orekit.propagation.sampling.FieldOrekitStepNormalizer
Handle the current step.
handleStep(FieldOrekitStepInterpolator<T>) - Method in class org.orekit.propagation.sampling.FieldStepHandlerMultiplexer
Handle the current step.
handleStep(OrekitStepInterpolator) - Method in class org.orekit.estimation.sequential.SemiAnalyticalMeasurementHandler
Handle the current step.
handleStep(OrekitStepInterpolator) - Method in interface org.orekit.propagation.sampling.OrekitStepHandler
Handle the current step.
handleStep(OrekitStepInterpolator) - Method in class org.orekit.propagation.sampling.OrekitStepNormalizer
Handle the last accepted step.
handleStep(OrekitStepInterpolator) - Method in class org.orekit.propagation.sampling.StepHandlerMultiplexer
Handle the current step.
handleStep(SpacecraftState) - Method in class org.orekit.files.ccsds.ndm.adm.aem.StreamingAemWriter.SegmentWriter
Handle the current step.
handleStep(SpacecraftState) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.StreamingOcmWriter.BlockWriter
Handle the current step.
handleStep(SpacecraftState) - Method in class org.orekit.files.ccsds.ndm.odm.oem.StreamingOemWriter.SegmentWriter
Handle the current step.
handleStep(SpacecraftState) - Method in class org.orekit.files.ilrs.StreamingCpfWriter.Segment
Handle the current step.
handleStep(SpacecraftState) - Method in interface org.orekit.propagation.sampling.OrekitFixedStepHandler
Handle the current step.
HansenTesseralLinear - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen
Hansen coefficients K(t,n,s) for t!=0 and n < 0.
HansenTesseralLinear(int, int, int, int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenTesseralLinear
Constructor.
HansenThirdBodyLinear - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen
Hansen coefficients K(t,n,s) for t=0 and n > 0.
HansenThirdBodyLinear(int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenThirdBodyLinear
Constructor.
HansenUtilities - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen
Utilities class.
HansenZonalLinear - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen
Hansen coefficients K(t,n,s) for t=0 and n < 0.
HansenZonalLinear(int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenZonalLinear
Constructor.
HAO - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCategory
High Altitude Earth Orbit, 40002 km < hp, 40002 km < ha.
HarmonicAccelerationModel - Class in org.orekit.forces.empirical
Harmonic acceleration model.
HarmonicAccelerationModel(String, AbsoluteDate, double, int) - Constructor for class org.orekit.forces.empirical.HarmonicAccelerationModel
Simple constructor.
HarrisPriester - Class in org.orekit.models.earth.atmosphere
This atmosphere model is the realization of the Modified Harris-Priester model.
HarrisPriester(PVCoordinatesProvider, OneAxisEllipsoid) - Constructor for class org.orekit.models.earth.atmosphere.HarrisPriester
Simple constructor for Modified Harris-Priester atmosphere model.
HarrisPriester(PVCoordinatesProvider, OneAxisEllipsoid, double) - Constructor for class org.orekit.models.earth.atmosphere.HarrisPriester
Constructor for Modified Harris-Priester atmosphere model.
HarrisPriester(PVCoordinatesProvider, OneAxisEllipsoid, double[][]) - Constructor for class org.orekit.models.earth.atmosphere.HarrisPriester
Constructor for Modified Harris-Priester atmosphere model.
HarrisPriester(PVCoordinatesProvider, OneAxisEllipsoid, double[][], double) - Constructor for class org.orekit.models.earth.atmosphere.HarrisPriester
Constructor for Modified Harris-Priester atmosphere model.
hasAcceleration() - Method in class org.orekit.files.ccsds.ndm.odm.StateVector
Check if state contains acceleration data.
hasAdditionalState(String) - Method in class org.orekit.propagation.FieldSpacecraftState
Check if an additional state is available.
hasAdditionalState(String) - Method in class org.orekit.propagation.SpacecraftState
Check if an additional state is available.
hasAdditionalStateDerivative(String) - Method in class org.orekit.propagation.FieldSpacecraftState
Check if an additional state derivative is available.
hasAdditionalStateDerivative(String) - Method in class org.orekit.propagation.SpacecraftState
Check if an additional state derivative is available.
hasAngles() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler
Check if the logical block includes angles.
hasClockEvent() - Method in class org.orekit.files.sp3.SP3Coordinate
Get clock event flag.
hasClockPrediction() - Method in class org.orekit.files.sp3.SP3Coordinate
Get clock prediction flag.
hasDataFor(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory
Check if the cache has data for the given date using EOPHistory.getStartDate() and EOPHistory.getEndDate().
hasDerivatives() - Method in class org.orekit.orbits.CartesianOrbit
Check if orbit includes derivatives.
hasDerivatives() - Method in class org.orekit.orbits.FieldCartesianOrbit
Check if orbit includes derivatives.
hasDerivatives() - Method in class org.orekit.orbits.FieldCircularOrbit
Check if orbit includes derivatives.
hasDerivatives() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Check if orbit includes derivatives.
hasDerivatives() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Check if orbit includes derivatives.
hasDerivatives() - Method in class org.orekit.orbits.FieldOrbit
Check if orbit includes derivatives.
hasDerivatives() - Method in class org.orekit.orbits.Orbit
Check if orbit includes derivatives.
hasDopplerCountRollover() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Check if there is a Doppler count rollover.
hashCode() - Method in class org.orekit.bodies.FieldGeodeticPoint
 
hashCode() - Method in class org.orekit.bodies.GeodeticPoint
 
hashCode() - Method in class org.orekit.estimation.measurements.ObservableSatellite
hashCode() - Method in class org.orekit.files.ilrs.CRDConfiguration.BaseConfiguration
 
hashCode() - Method in class org.orekit.gnss.SatInSystem
 
hashCode() - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityDataLoader.LineParameters
Get a hashcode for this date.
hashCode() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
Get a hashcode for this date.
hashCode() - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimationLoader.LineParameters
Get a hashcode for this date.
hashCode() - Method in class org.orekit.models.earth.displacement.Tide
 
hashCode() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get a hashcode for this tle.
hashCode() - Method in class org.orekit.propagation.analytical.tle.TLE
Get a hashcode for this tle.
hashCode() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey
hashCode() - Method in class org.orekit.time.AbsoluteDate
Get a hashcode for this date.
hashCode() - Method in class org.orekit.time.DateComponents
hashCode() - Method in class org.orekit.time.DateTimeComponents
hashCode() - Method in class org.orekit.time.FieldAbsoluteDate
Get a hashcode for this date.
hashCode() - Method in class org.orekit.time.TimeComponents
hashCode() - Method in class org.orekit.utils.units.Unit
Get a hashcode for this unit.
hasManeuvers() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData
Get boolean testing whether the APM contains at least one maneuver.
hasManeuvers() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm
check whether the OPM contains at least one maneuver.
hasManeuvers() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData
Get boolean testing whether the APM contains at least one maneuver.
hasMomentum() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
Check if the logical block includes momentum.
hasNonKeplerianAcceleration(FieldPVCoordinates<T>, T) - Static method in class org.orekit.orbits.FieldOrbit
Check if Cartesian coordinates include non-Keplerian acceleration.
hasNonKeplerianAcceleration(PVCoordinates, double) - Static method in class org.orekit.orbits.Orbit
Check if Cartesian coordinates include non-Keplerian acceleration.
hasNutation() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
Check if the logical block includes nutation.
hasOrbitManeuverEvent() - Method in class org.orekit.files.sp3.SP3Coordinate
Get orbit maneuver event flag.
hasOrbitPrediction() - Method in class org.orekit.files.sp3.SP3Coordinate
Get orbit prediction flag.
hasParityErrors() - Method in class org.orekit.gnss.rflink.gps.SubFrame
Check if the sub-frame has parity errors.
hasRates() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternion
Check if the logical block includes rates.
hasRates() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler
Check if the logical block includes rates.
hasRates() - Method in class org.orekit.orbits.CircularOrbit
Tells whether the instance holds rates (first-order time derivatives) for dependent variables.
hasRates() - Method in class org.orekit.orbits.EquinoctialOrbit
Tells whether the instance holds rates (first-order time derivatives) for dependent variables.
hasRates() - Method in class org.orekit.orbits.FieldCircularOrbit
Tells whether the instance holds rates (first-order time derivatives) for dependent variables.
hasRates() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Tells whether the instance holds rates (first-order time derivatives) for dependent variables.
hasRates() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Tells whether the instance holds rates (first-order time derivatives) for dependent variables.
hasRates() - Method in class org.orekit.orbits.KeplerianOrbit
Tells whether the instance holds rates (first-order time derivatives) for dependent variables.
hasRates() - Method in interface org.orekit.orbits.PositionAngleBased
Tells whether the instance holds rates (first-order time derivatives) for dependent variables.
hasZeroField() - Method in class org.orekit.time.FieldAbsoluteDate
Check if the Field is semantically equal to zero.
HatanakaCompressFilter - Class in org.orekit.files.rinex
Decompression filter for Hatanaka compressed RINEX files.
HatanakaCompressFilter() - Constructor for class org.orekit.files.rinex.HatanakaCompressFilter
Empty constructor.
HBR - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
Object hard body radius.
header - org.orekit.files.ccsds.section.XmlStructureKey
Header structure.
Header - Class in org.orekit.files.ccsds.section
Header of a CCSDS Navigation Data Message.
Header(double, double) - Constructor for class org.orekit.files.ccsds.section.Header
Constructor.
HEADER_ALREADY_WRITTEN - org.orekit.errors.OrekitMessages
HEADER_ALREADY_WRITTEN.
HEADER_NOT_WRITTEN - org.orekit.errors.OrekitMessages
HEADER_NOT_WRITTEN.
HeaderKey - Enum in org.orekit.files.ccsds.section
Keywords allowed in Header.
HeaderProcessingState - Class in org.orekit.files.ccsds.section
HeaderProcessingState(AbstractConstituentParser<?, ?, ?>) - Constructor for class org.orekit.files.ccsds.section.HeaderProcessingState
Simple constructor.
HECTO_PASCAL - Static variable in class org.orekit.files.ccsds.definitions.Units
HectoPascal unit.
HECTO_PASCAL - Static variable in class org.orekit.models.earth.troposphere.TroposphericModelUtils
HectoPascal unit.
HeightDependentPressureTemperatureHumidityConverter - Class in org.orekit.models.earth.weather
Converter for weather parameters that change with height.
HeightDependentPressureTemperatureHumidityConverter(WaterVaporPressureProvider) - Constructor for class org.orekit.models.earth.weather.HeightDependentPressureTemperatureHumidityConverter
Simple constructor.
HelmertTransformation - Class in org.orekit.frames
Transformation class for geodetic systems.
HelmertTransformation(AbsoluteDate, double, double, double, double, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.frames.HelmertTransformation
Build a transform from its primitive operations.
HelmertTransformation.Predefined - Enum in org.orekit.frames
Enumerate for predefined Helmert transformations.
HEO - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCategory
Highly Eccentric Earth Orbit, hp < 31570 km, 40002 km < ha.
HERMITE - org.orekit.files.ccsds.ndm.odm.oem.InterpolationMethod
Hermite interpolation.
HERTZ - Static variable in class org.orekit.utils.units.Unit
Hertz unit.
HexadecimalSequenceEncodedMessage - Class in org.orekit.gnss.metric.parser
Encoded message as an hexadecimal characters sequence.
HexadecimalSequenceEncodedMessage(CharSequence) - Constructor for class org.orekit.gnss.metric.parser.HexadecimalSequenceEncodedMessage
Simple constructor.
HighamHall54FieldIntegratorBuilder<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.conversion
Builder for HighamHall54Integrator.
HighamHall54FieldIntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.HighamHall54FieldIntegratorBuilder
Build a new instance.
HighamHall54FieldIntegratorBuilder(double, double, double, double) - Constructor for class org.orekit.propagation.conversion.HighamHall54FieldIntegratorBuilder
Build a new instance.
HighamHall54IntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for HighamHall54Integrator.
HighamHall54IntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.HighamHall54IntegratorBuilder
Build a new instance.
HighamHall54IntegratorBuilder(double, double, double, double) - Constructor for class org.orekit.propagation.conversion.HighamHall54IntegratorBuilder
Build a new instance.
HLM - org.orekit.files.sp3.SP3OrbitType
fitted after applying a Helmert transformation.
HolmesFeatherstoneAttractionModel - Class in org.orekit.forces.gravity
This class represents the gravitational field of a celestial body.
HolmesFeatherstoneAttractionModel(Frame, NormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Creates a new instance.
HOUR - Static variable in class org.orekit.utils.units.Unit
Hour unit.
HYPERBOLIC_ORBIT_NOT_HANDLED_AS - org.orekit.errors.OrekitMessages
HYPERBOLIC_ORBIT_NOT_HANDLED_AS.
hyperbolicEccentricToMean(double, double) - Static method in class org.orekit.orbits.KeplerianAnomalyUtility
Computes the hyperbolic mean anomaly from the hyperbolic eccentric anomaly.
hyperbolicEccentricToMean(T, T) - Static method in class org.orekit.orbits.FieldKeplerianAnomalyUtility
Computes the hyperbolic mean anomaly from the hyperbolic eccentric anomaly.
hyperbolicEccentricToTrue(double, double) - Static method in class org.orekit.orbits.KeplerianAnomalyUtility
Computes the hyperbolic true anomaly from the hyperbolic eccentric anomaly.
hyperbolicEccentricToTrue(T, T) - Static method in class org.orekit.orbits.FieldKeplerianAnomalyUtility
Computes the hyperbolic true anomaly from the hyperbolic eccentric anomaly.
hyperbolicMeanToEccentric(double, double) - Static method in class org.orekit.orbits.KeplerianAnomalyUtility
Computes the hyperbolic eccentric anomaly from the hyperbolic mean anomaly.
hyperbolicMeanToEccentric(T, T) - Static method in class org.orekit.orbits.FieldKeplerianAnomalyUtility
Computes the hyperbolic eccentric anomaly from the hyperbolic mean anomaly.
hyperbolicMeanToTrue(double, double) - Static method in class org.orekit.orbits.KeplerianAnomalyUtility
Computes the hyperbolic true anomaly from the hyperbolic mean anomaly.
hyperbolicMeanToTrue(T, T) - Static method in class org.orekit.orbits.FieldKeplerianAnomalyUtility
Computes the hyperbolic true anomaly from the hyperbolic mean anomaly.
hyperbolicTrueToEccentric(double, double) - Static method in class org.orekit.orbits.KeplerianAnomalyUtility
Computes the hyperbolic eccentric anomaly from the hyperbolic true anomaly.
hyperbolicTrueToEccentric(T, T) - Static method in class org.orekit.orbits.FieldKeplerianAnomalyUtility
Computes the hyperbolic eccentric anomaly from the hyperbolic true anomaly.
hyperbolicTrueToMean(double, double) - Static method in class org.orekit.orbits.KeplerianAnomalyUtility
Computes the hyperbolic mean anomaly from the hyperbolic true anomaly.
hyperbolicTrueToMean(T, T) - Static method in class org.orekit.orbits.FieldKeplerianAnomalyUtility
Computes the hyperbolic mean anomaly from the hyperbolic true anomaly.
HZ_PER_S - Static variable in class org.orekit.files.ccsds.definitions.Units
Hertz per second unit.

I

i - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
final inclination.
i - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
final inclination.
I - org.orekit.gnss.SignalCode
GPS I / GLONASS I / Galileo I F/NAV, I I/NAV and I / SBAS I/ Beidou I codes.
I05 - org.orekit.gnss.Frequency
IRNSS L5.
I09 - org.orekit.gnss.Frequency
IRNSS S (2492.028 MHz).
I11 - org.orekit.files.ccsds.ndm.adm.apm.InertiaKey
Moment of inertia about X-axis (ADM V1 only).
I12 - org.orekit.files.ccsds.ndm.adm.apm.InertiaKey
Inertia cross product of the X and Y axes (ADM V1 only).
I13 - org.orekit.files.ccsds.ndm.adm.apm.InertiaKey
Inertia cross product of the X and Z axes (ADM V1 only).
I22 - org.orekit.files.ccsds.ndm.adm.apm.InertiaKey
Moment of inertia about Y-axis (ADM V1 only).
I23 - org.orekit.files.ccsds.ndm.adm.apm.InertiaKey
Inertia cross product of the Y and Z axes (ADM V1 only).
I33 - org.orekit.files.ccsds.ndm.adm.apm.InertiaKey
Moment of inertia about Z-axis (ADM V1 only).
IAU_2012_ASTRONOMICAL_UNIT - Static variable in interface org.orekit.utils.Constants
Astronomical unit as a conventional unit of length since IAU 2012 resolution B2: 149597870700.0 m.
IAU_2015_NOMINAL_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Earth equatorial radius as defined by IAU 2015 resolution B3: 6.3781e6 (m).
IAU_2015_NOMINAL_EARTH_GM - Static variable in interface org.orekit.utils.Constants
Earth attraction coefficient as defined by IAU 2015 resolution B3: 3.986004e14 (m³/s²).
IAU_2015_NOMINAL_EARTH_POLAR_RADIUS - Static variable in interface org.orekit.utils.Constants
Earth polar radius as defined by IAU 2015 resolution B3: 6.3568e6 (m).
IAU_2015_NOMINAL_JUPITER_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Jupiter equatorial radius as defined by IAU 2015 resolution B3: 7.1492e7 (m).
IAU_2015_NOMINAL_JUPITER_GM - Static variable in interface org.orekit.utils.Constants
Jupiter attraction coefficient as defined by IAU 2015 resolution B3: 1.2668653e17 (m³/s²).
IAU_2015_NOMINAL_JUPITER_POLAR_RADIUS - Static variable in interface org.orekit.utils.Constants
Jupiter polar radius as defined by IAU 2015 resolution B3: 6.6854e7 (m).
IAU_2015_NOMINAL_SOLAR_RADIUS - Static variable in interface org.orekit.utils.Constants
Solar radius as defined by IAU 2015 resolution B3: 695700000.0 m.
IAU_2015_NOMINAL_SUN_GM - Static variable in interface org.orekit.utils.Constants
Sun attraction coefficient as defined by IAU 2015 resolution B3: 1.3271244e20 (m³/s²).
IAUPole - Interface in org.orekit.bodies
Interface for IAU pole and prime meridian orientations.
ICGEM_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory
Default regular expression for ICGEM files.
ICGEMFormatReader - Class in org.orekit.forces.gravity.potential
Reader for the ICGEM gravity field format.
ICGEMFormatReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.ICGEMFormatReader
Simple constructor.
ICGEMFormatReader(String, boolean, TimeScale) - Constructor for class org.orekit.forces.gravity.potential.ICGEMFormatReader
Simple constructor.
ICRF - org.orekit.files.ccsds.definitions.CelestialBodyFrame
International Celestial Reference Frame.
ICRF - org.orekit.files.stk.STKEphemerisFile.STKCoordinateSystem
International Celestial Reference Frame.
ICRF - org.orekit.frames.Predefined
ICRF frame.
IDENTITY - Static variable in class org.orekit.frames.Transform
Identity transform.
IDENTITY - Static variable in class org.orekit.utils.AngularCoordinates
Fixed orientation parallel with reference frame (identity rotation, zero rotation rate and acceleration).
IDENTITY - Static variable in class org.orekit.utils.units.UnitsConverter
Identity converter.
IDENTITY_PROVIDER - Static variable in class org.orekit.frames.TransformProviderUtils
Identity provider.
IdentityConverter - Class in org.orekit.files.ccsds.ndm.tdm
Identity converter for Range Units.
IdentityConverter() - Constructor for class org.orekit.files.ccsds.ndm.tdm.IdentityConverter
Empty constructor.
IDF001 - org.orekit.gnss.metric.parser.IgsSsrDataField
IGS SSR Version.
IDF002 - org.orekit.gnss.metric.parser.IgsSsrDataField
IGS Message number.
IDF003 - org.orekit.gnss.metric.parser.IgsSsrDataField
SSR Epoch time 1s.
IDF004 - org.orekit.gnss.metric.parser.IgsSsrDataField
SSR Update interval.
IDF005 - org.orekit.gnss.metric.parser.IgsSsrDataField
Multiple Message Indicator.
IDF006 - org.orekit.gnss.metric.parser.IgsSsrDataField
Global/Regional CRS Indicator.
IDF007 - org.orekit.gnss.metric.parser.IgsSsrDataField
IOD SSR.
IDF008 - org.orekit.gnss.metric.parser.IgsSsrDataField
SSR Provider ID.
IDF009 - org.orekit.gnss.metric.parser.IgsSsrDataField
SSR Solution ID.
IDF010 - org.orekit.gnss.metric.parser.IgsSsrDataField
Number of satellites.
IDF011 - org.orekit.gnss.metric.parser.IgsSsrDataField
GNSS satellite ID.
IDF012 - org.orekit.gnss.metric.parser.IgsSsrDataField
GNSS IOD.
IDF013 - org.orekit.gnss.metric.parser.IgsSsrDataField
Delta Orbit Radial (m).
IDF014 - org.orekit.gnss.metric.parser.IgsSsrDataField
Delta Along-Track (m).
IDF015 - org.orekit.gnss.metric.parser.IgsSsrDataField
Delta Cross-Track (m).
IDF016 - org.orekit.gnss.metric.parser.IgsSsrDataField
Dot Delta Radial (m/s).
IDF017 - org.orekit.gnss.metric.parser.IgsSsrDataField
Dot Delta Along-Track (m/s).
IDF018 - org.orekit.gnss.metric.parser.IgsSsrDataField
Dot Delta Cross-Track (m/s).
IDF019 - org.orekit.gnss.metric.parser.IgsSsrDataField
Delta Clock C0.
IDF020 - org.orekit.gnss.metric.parser.IgsSsrDataField
Delta Clock C1.
IDF021 - org.orekit.gnss.metric.parser.IgsSsrDataField
Delta Clock C2.
IDF022 - org.orekit.gnss.metric.parser.IgsSsrDataField
High Rate Clock Correction.
IDF023 - org.orekit.gnss.metric.parser.IgsSsrDataField
No.
IDF024 - org.orekit.gnss.metric.parser.IgsSsrDataField
GNSS Signal and Tracking Mode Identifier.
IDF025 - org.orekit.gnss.metric.parser.IgsSsrDataField
Code Bias for specified GNSS signal.
IDF026 - org.orekit.gnss.metric.parser.IgsSsrDataField
Yaw angle used for computation of phase wind-up correction.
IDF027 - org.orekit.gnss.metric.parser.IgsSsrDataField
Yaw rate.
IDF028 - org.orekit.gnss.metric.parser.IgsSsrDataField
Phase Bias for specified GNSS signal (m).
IDF029 - org.orekit.gnss.metric.parser.IgsSsrDataField
Signal Integer Indicator.
IDF030 - org.orekit.gnss.metric.parser.IgsSsrDataField
Signal Wide-Lane Integer Indicator.
IDF031 - org.orekit.gnss.metric.parser.IgsSsrDataField
Signal Discontinuity Counter.
IDF032 - org.orekit.gnss.metric.parser.IgsSsrDataField
Dispersive Bias Consistency Indicator.
IDF033 - org.orekit.gnss.metric.parser.IgsSsrDataField
Melbourne-Wübbena Consistency Indicator.
IDF034 - org.orekit.gnss.metric.parser.IgsSsrDataField
SSR URA.
IDF035 - org.orekit.gnss.metric.parser.IgsSsrDataField
Number of Ionospheric Layers.
IDF036 - org.orekit.gnss.metric.parser.IgsSsrDataField
Height of the Ionospheric layer (m).
IDF037 - org.orekit.gnss.metric.parser.IgsSsrDataField
Spherical Harmonic Degree.
IDF038 - org.orekit.gnss.metric.parser.IgsSsrDataField
Spherical Harmonic Order.
IDF039 - org.orekit.gnss.metric.parser.IgsSsrDataField
Spherical Harmonic Coefficient C (TECU).
IDF040 - org.orekit.gnss.metric.parser.IgsSsrDataField
Spherical Harmonic Coefficient S (TECU).
IDF041 - org.orekit.gnss.metric.parser.IgsSsrDataField
VTEC Quality Indicator (TECU).
IERS_1996 - org.orekit.forces.gravity.potential.OceanLoadDeformationCoefficients
Coefficients from IERS 1996 conventions.
IERS_1996 - org.orekit.utils.IERSConventions
Constant for IERS 1996 conventions.
IERS_2003 - org.orekit.forces.gravity.potential.OceanLoadDeformationCoefficients
Coefficients from IERS 2003 conventions.
IERS_2003 - org.orekit.utils.IERSConventions
Constant for IERS 2003 conventions.
IERS_2010 - org.orekit.forces.gravity.potential.OceanLoadDeformationCoefficients
Coefficients from IERS 2010 conventions.
IERS_2010 - org.orekit.utils.IERSConventions
Constant for IERS 2010 conventions.
IERS2003_EARTH_ANGULAR_VELOCITY - Static variable in interface org.orekit.utils.Constants
Earth angular velocity from IERS2003 model: 7.292115e-5 rad/s.
IERS2003_EARTH_C20 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized second zonal coefficient from IERS2003 model: -1.0826359e-3.
IERS2003_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Earth equatorial radius from IERS2003 model: 6378136.6 m.
IERS2003_EARTH_FLATTENING - Static variable in interface org.orekit.utils.Constants
Earth flattening from IERS2003 model: 1.0 / 298.25642.
IERS2003_EARTH_MU - Static variable in interface org.orekit.utils.Constants
Earth gravitational constant from IERS2003 model: 3.986004418e14 m³/s².
IERS2010_EARTH_ANGULAR_VELOCITY - Static variable in interface org.orekit.utils.Constants
Earth angular velocity from IERS2010 model: 7.292115e-5 rad/s.
IERS2010_EARTH_C20 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized second zonal coefficient from IERS2010 model: -1.0826359e-3.
IERS2010_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Earth equatorial radius from IERS2010 model: 6378136.6 m.
IERS2010_EARTH_FLATTENING - Static variable in interface org.orekit.utils.Constants
Earth flattening from IERS2010 model: 1.0 / 298.25642.
IERS2010_EARTH_MU - Static variable in interface org.orekit.utils.Constants
Earth gravitational constant from IERS2010 model: 3.986004418e14 m³/s².
IERS96_EARTH_ANGULAR_VELOCITY - Static variable in interface org.orekit.utils.Constants
Earth angular velocity from IERS96 model: 7.292115e-5 rad/s.
IERS96_EARTH_C20 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized second zonal coefficient from IERS96 model: -1.0826359e-3.
IERS96_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Earth equatorial radius from IERS96 model: 6378136.49 m.
IERS96_EARTH_FLATTENING - Static variable in interface org.orekit.utils.Constants
Earth flattening from IERS96 model: 1.0 / 298.25642.
IERS96_EARTH_MU - Static variable in interface org.orekit.utils.Constants
Earth gravitational constant from IERS96 model: 3.986004418e14 m³/s².
IERSConventions - Enum in org.orekit.utils
Supported IERS conventions.
IERSConventions.NutationCorrectionConverter - Interface in org.orekit.utils
Interface for functions converting nutation corrections between δΔψ/δΔε to δX/δY.
IGM_01 - org.orekit.gnss.metric.parser.IgsSsrMessageType
SSR Orbit Correction.
IGM_02 - org.orekit.gnss.metric.parser.IgsSsrMessageType
SSR Clock Correction.
IGM_03 - org.orekit.gnss.metric.parser.IgsSsrMessageType
SSR Combined Orbit and Clock Correction.
IGM_04 - org.orekit.gnss.metric.parser.IgsSsrMessageType
SSR High Rate Clock Correction.
IGM_05 - org.orekit.gnss.metric.parser.IgsSsrMessageType
SSR Code Bias.
IGM_06 - org.orekit.gnss.metric.parser.IgsSsrMessageType
SSR Phase Bias.
IGM_07 - org.orekit.gnss.metric.parser.IgsSsrMessageType
SSR URA.
IGNORE_PARSED - org.orekit.files.ccsds.ndm.ParsedUnitsBehavior
Ignore parsed units, just relying on CCSDS standard.
IGO - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCategory
Inclined Geosynchronous Orbit, 37948 < a < 46380 km, e < 0.25, 25° < i < 180°.
IGRF - org.orekit.models.earth.GeoMagneticFieldFactory.FieldModel
International Geomagnetic Reference Field.
IGS_SSR - org.orekit.gnss.metric.ntrip.Type
IGS SSR.
IGSO - org.orekit.propagation.analytical.gnss.data.BeidouSatelliteType
Inclined geosynchronous.
IgsSsrDataField - Enum in org.orekit.gnss.metric.parser
Enum containing all intermediate level data fields that can be parsed to build an IGS SSR message.
IgsSsrMessagesParser - Class in org.orekit.gnss.metric.parser
Parser for SSR encoded messages.
IgsSsrMessagesParser(List<Integer>) - Constructor for class org.orekit.gnss.metric.parser.IgsSsrMessagesParser
Constructor.
IgsSsrMessageType - Enum in org.orekit.gnss.metric.parser
Enum containing the supported IGS SSR messages types.
IGSUtils - Class in org.orekit.gnss
Utility for IGS files.
ILRSHeader - Class in org.orekit.files.ilrs
Container for common data contains in International Laser Ranging Service (ILRS) files header.
ILRSHeader() - Constructor for class org.orekit.files.ilrs.ILRSHeader
Empty constructor.
IM_201 - org.orekit.gnss.metric.parser.IgsSsrMessageType
SSR Ionosphere VTEC Spherical Harmonics Message.
ImmutableFieldTimeStampedCache<T extends FieldTimeStamped<KK>,​KK extends CalculusFieldElement<KK>> - Class in org.orekit.utils
A cache of TimeStamped data that provides concurrency through immutability.
ImmutableFieldTimeStampedCache(int, Collection<? extends T>) - Constructor for class org.orekit.utils.ImmutableFieldTimeStampedCache
Create a new cache with the given neighbors size and data.
ImmutableTimeStampedCache<T extends TimeStamped> - Class in org.orekit.utils
A cache of TimeStamped data that provides concurrency through immutability.
ImmutableTimeStampedCache(int, Collection<? extends T>) - Constructor for class org.orekit.utils.ImmutableTimeStampedCache
Create a new cache with the given neighbors size and data.
ImpulseManeuver - Class in org.orekit.forces.maneuvers
Impulse maneuver model.
ImpulseManeuver(AdaptableInterval, double, int, EventHandler, EventDetector, AttitudeProvider, Vector3D, double, Control3DVectorCostType) - Constructor for class org.orekit.forces.maneuvers.ImpulseManeuver
Protected constructor with full parameters.
ImpulseManeuver(EventDetector, Vector3D, double) - Constructor for class org.orekit.forces.maneuvers.ImpulseManeuver
Build a new instance.
ImpulseManeuver(EventDetector, AttitudeProvider, Vector3D, double) - Constructor for class org.orekit.forces.maneuvers.ImpulseManeuver
Build a new instance.
ImpulseManeuver(EventDetector, AttitudeProvider, Vector3D, double, Control3DVectorCostType) - Constructor for class org.orekit.forces.maneuvers.ImpulseManeuver
Build a new instance.
IMU_FRAME - org.orekit.files.ccsds.definitions.SpacecraftBodyFrame.BaseEquipment
Inertial Measurement Unit.
INC - Static variable in enum org.orekit.orbits.OrbitType
Name for inclination.
INCLINATION - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
The angle between the objects orbit plane and the orbit centers equatorial plane.
INCLINATION - org.orekit.files.ccsds.ndm.odm.KeplerianElementsKey
Orbit inclination.
INCOMPATIBLE_FRAMES - org.orekit.errors.OrekitMessages
INCOMPATIBLE_FRAMES.
INCOMPATIBLE_FREQUENCIES_FOR_COMBINATION_OF_MEASUREMENTS - org.orekit.errors.OrekitMessages
INCOMPATIBLE_FREQUENCIES_FOR_COMBINATION_OF_MEASUREMENTS.
INCOMPATIBLE_UNITS - org.orekit.errors.OrekitMessages
INCOMPATIBLE_UNITS.
INCOMPLETE_HEADER - org.orekit.errors.OrekitMessages
INCOMPLETE_HEADER.
INCONSISTENT_ASTRONOMICAL_UNIT_IN_FILES - org.orekit.errors.OrekitMessages
INCONSISTENT_ASTRONOMICAL_UNIT_IN_FILES.
INCONSISTENT_DATES_IN_IERS_FILE - org.orekit.errors.OrekitMessages
INCONSISTENT_DATES_IN_IERS_FILE.
INCONSISTENT_EARTH_MOON_RATIO_IN_FILES - org.orekit.errors.OrekitMessages
INCONSISTENT_EARTH_MOON_RATIO_IN_FILES.
INCONSISTENT_NUMBER_OF_ELEMENTS - org.orekit.errors.OrekitMessages
INCONSISTENT_NUMBER_OF_ELEMENTS.
INCONSISTENT_NUMBER_OF_SATS - org.orekit.errors.OrekitMessages
INCONSISTENT_NUMBER_OF_SATS.
INCONSISTENT_NUMBER_OF_TEC_MAPS_IN_FILE - org.orekit.errors.OrekitMessages
INCONSISTENT_NUMBER_OF_TEC_MAPS_IN_FILE.
INCONSISTENT_SAMPLING_DATE - org.orekit.errors.OrekitMessages
INCONSISTENT_SAMPLING_DATE.
INCONSISTENT_SATELLITE_SYSTEM - org.orekit.errors.OrekitMessages
INCONSISTENT_SATELLITE_SYSTEM.
INCONSISTENT_SELECTION - org.orekit.errors.OrekitMessages
INCONSISTENT_SELECTION.
increment(double[]) - Method in class org.orekit.utils.DoubleArrayDictionary.Entry
Increment the value.
increment(double[]) - Method in class org.orekit.utils.FieldArrayDictionary.Entry
Increment the value.
increment(T[]) - Method in class org.orekit.utils.FieldArrayDictionary.Entry
Increment the value.
incrementTrajID(String) - Static method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Increments a trajectory ID.
inData() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmParser
Acknowledge data parsing has started.
inData() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser
Acknowledge data parsing has started.
inData() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser
Acknowledge data parsing has started.
inData() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmParser
Acknowledge data parsing has started.
inData() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser
Acknowledge data parsing has started.
inData() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser
Acknowledge data parsing has started.
inData() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser
Acknowledge data parsing has started.
inData() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser
Acknowledge data parsing has started.
inData() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser
Acknowledge data parsing has started.
inData() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser
Acknowledge data parsing has started.
indexAccuracy(Unit, double, double) - Static method in class org.orekit.files.sp3.SP3Utils
Convert an accuracy from SI units.
Inertia - Class in org.orekit.attitudes
Container for inertia of a 3D object.
Inertia - Class in org.orekit.files.ccsds.ndm.adm.apm
Inertia.
Inertia() - Constructor for class org.orekit.files.ccsds.ndm.adm.apm.Inertia
Simple constructor.
Inertia(InertiaAxis, InertiaAxis, InertiaAxis) - Constructor for class org.orekit.attitudes.Inertia
Simple constructor from principal axes.
INERTIA_REF_FRAME - org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalPropertiesKey
Inertia reference frame.
INERTIA_REF_FRAME - org.orekit.files.ccsds.ndm.adm.apm.InertiaKey
Frame in which inertia is defined.
InertiaAxis - Class in org.orekit.attitudes
Container for inertial axis.
InertiaAxis(double, Vector3D) - Constructor for class org.orekit.attitudes.InertiaAxis
Simple constructor to pair a moment of inertia with its associated axis.
InertiaKey - Enum in org.orekit.files.ccsds.ndm.adm.apm
Keys for inertia entries.
INERTIAL - org.orekit.files.stk.STKEphemerisFile.STKCoordinateSystem
Central-body-dependent inertial frame, equivalent to ICRF for Earth.
INERTIAL_FORCE_MODEL_MISSING - org.orekit.errors.OrekitMessages
INERTIAL_FORCE_MODEL_MISSING.
InertialForces - Class in org.orekit.forces.inertia
Inertial force model.
InertialForces(Frame) - Constructor for class org.orekit.forces.inertia.InertialForces
Simple constructor.
INF_NORM - org.orekit.forces.maneuvers.Control3DVectorCostType
Infinite norm also known as Max.
INFINITE_NRLMSISE00_DENSITY - org.orekit.errors.OrekitMessages
INFINITE_NRMSISE00_DENSITY.
inHeader() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmParser
Acknowledge header parsing has started.
inHeader() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser
Acknowledge header parsing has started.
inHeader() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser
Acknowledge header parsing has started.
inHeader() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmParser
Acknowledge header parsing has started.
inHeader() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser
Acknowledge header parsing has started.
inHeader() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser
Acknowledge header parsing has started.
inHeader() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser
Acknowledge header parsing has started.
inHeader() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser
Acknowledge header parsing has started.
inHeader() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser
Acknowledge header parsing has started.
inHeader() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser
Acknowledge header parsing has started.
init(JavacTask, String...) - Method in class org.orekit.compiler.plugin.DefaultDataContextPlugin
 
init(List<SpacecraftState>, AbsoluteDate) - Method in interface org.orekit.propagation.sampling.MultiSatStepHandler
Initialize step handler at the start of a propagation.
init(List<SpacecraftState>, AbsoluteDate) - Method in class org.orekit.propagation.sampling.MultisatStepNormalizer
Initialize step handler at the start of a propagation.
init(List<SpacecraftState>, AbsoluteDate, double) - Method in interface org.orekit.propagation.sampling.MultiSatFixedStepHandler
Initialize step handler at the start of a propagation.
init(FieldSpacecraftState<D>, FieldAbsoluteDate<D>) - Method in class org.orekit.forces.maneuvers.trigger.IntervalEventTrigger
Initialization method called at propagation start.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.control.indirect.adjoint.FieldCartesianAdjointDerivativesProvider
Initialize the generator at the start of propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.forces.ForceModel
Initialize the force model at the start of propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.forces.maneuvers.FieldImpulseManeuver
Initialize event handler at the start of a propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.forces.maneuvers.Maneuver
Initialize the force model at the start of propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel
Initialization method.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers
Initialization method called at propagation start.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.forces.maneuvers.trigger.FieldManeuverTriggersResetter
Initialization method called at propagation start.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggers
Initialization method called at propagation start.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.forces.radiation.ConicallyShadowedLightFluxModel
Perform initialization steps before starting propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.forces.radiation.LightFluxModel
Perform initialization steps before starting propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.forces.radiation.RadiationPressureModel
Initialize the force model at the start of propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.events.FieldAbstractDetector
Initialize event handler at the start of a propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.events.FieldAdapterDetector
Initialize event handler at the start of a propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.events.FieldBooleanDetector
 
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.events.FieldEventDetector
Initialize event handler at the start of a propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.events.FieldEventEnablingPredicateFilter
Initialize event handler at the start of a propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.events.FieldEventSlopeFilter
Initialize event handler at the start of a propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.events.FieldEventState
Initialize event handler at the start of a propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.events.FieldLongitudeCrossingDetector
Initialize event handler at the start of a propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.events.FieldNegateDetector
 
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.FieldAdditionalStateProvider
Initialize the additional state provider at the start of propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.integration.FieldAbstractIntegratedPropagator.MainStateEquations
Initialize the equations at the start of propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.integration.FieldAdditionalDerivativesProvider
Initialize the generator at the start of propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.sampling.FieldOrekitStepHandler
Initialize step handler at the start of a propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.sampling.FieldOrekitStepNormalizer
Initialize step handler at the start of a propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.sampling.FieldStepHandlerMultiplexer
Initialize step handler at the start of a propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Initialize the force model at the start of propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Initialize the force model at the start of propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>, FieldEventDetector<T>) - Method in interface org.orekit.propagation.events.handlers.FieldEventHandler
Initialize event handler at the start of a propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>, FieldEventDetector<T>) - Method in class org.orekit.propagation.events.handlers.FieldRecallLastOccurrence
Initialize event handler at the start of a propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>, T) - Method in interface org.orekit.propagation.sampling.FieldOrekitFixedStepHandler
Initialize step handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.attitudes.AttitudesSequence.Switch
Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointDerivativesProvider
Initialize the generator at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.estimation.sequential.SemiAnalyticalMeasurementHandler
Initialize step handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.forces.empirical.AccelerationModel
Initialize the acceleration model at the start of the propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.empirical.HarmonicAccelerationModel
Initialize the acceleration model at the start of the propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.empirical.ParametricAcceleration
Initialize the force model at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.empirical.PolynomialAccelerationModel
Initialize the acceleration model at the start of the propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
Initialize the force model at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.forces.ForceModel
Initialize the force model at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.maneuvers.jacobians.MassDepletionDelay
Initialize the generator at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.maneuvers.jacobians.TriggerDate
Initialize the additional state provider at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.maneuvers.Maneuver
Initialize the force model at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel
Initialization method.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers
Initialization method called at propagation start.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.maneuvers.trigger.IntervalEventTrigger
Initialization method called at propagation start.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggers
Initialization method called at propagation start.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggersResetter
Initialization method called at propagation start.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.maneuvers.trigger.StartStopEventsTrigger
Initialization method called at propagation start.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.radiation.ConicallyShadowedLightFluxModel
Perform initialization steps before starting propagation.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.forces.radiation.LightFluxModel
Perform initialization steps before starting propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.radiation.RadiationPressureModel
Initialize the force model at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.AdditionalStateProvider
Initialize the additional state provider at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.AbstractDetector
Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.AdapterDetector
Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.BooleanDetector
 
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.events.EventDetector
Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.EventEnablingPredicateFilter
Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.EventShifter
Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.EventSlopeFilter
Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.EventState
Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.LongitudeCrossingDetector
Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.MagneticFieldDetector
Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.NegateDetector
 
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.PositionAngleDetector
Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.integration.AbstractIntegratedPropagator.MainStateEquations
Initialize the equations at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.integration.AdditionalDerivativesProvider
Initialize the generator at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.sampling.OrekitStepHandler
Initialize step handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.sampling.OrekitStepNormalizer
Initialize step handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.sampling.StepHandlerMultiplexer
Initialize step handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Initialize the force model at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Initialize the force model at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.StateCovarianceMatrixProvider
Initialize the additional state provider at the start of propagation.
init(SpacecraftState, AbsoluteDate, double) - Method in class org.orekit.files.ccsds.ndm.adm.aem.StreamingAemWriter.SegmentWriter
Initialize step handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate, double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.StreamingOcmWriter.BlockWriter
Initialize step handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate, double) - Method in class org.orekit.files.ccsds.ndm.odm.oem.StreamingOemWriter.SegmentWriter
Initialize step handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate, double) - Method in interface org.orekit.propagation.sampling.OrekitFixedStepHandler
Initialize step handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate, EventDetector) - Method in interface org.orekit.propagation.events.handlers.EventHandler
Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate, EventDetector) - Method in class org.orekit.propagation.events.handlers.EventMultipleHandler
Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate, EventDetector) - Method in class org.orekit.propagation.events.handlers.RecallLastOccurrence
Initialize event handler at the start of a propagation.
init(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
Initialize builder at the start of a measurements generation.
init(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.estimation.measurements.generation.AbstractScheduler
Initialize scheduler at the start of a measurements generation.
init(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.estimation.measurements.generation.GatheringSubscriber
Initialize subscriber at the start of a measurements generation.
init(AbsoluteDate, AbsoluteDate) - Method in interface org.orekit.estimation.measurements.generation.GeneratedMeasurementSubscriber
Initialize subscriber at the start of a measurements generation.
init(AbsoluteDate, AbsoluteDate) - Method in interface org.orekit.estimation.measurements.generation.MeasurementBuilder
Initialize builder at the start of a measurements generation.
init(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.estimation.measurements.generation.MultiplexedMeasurementBuilder
Initialize builder at the start of a measurements generation.
init(AbsoluteDate, AbsoluteDate) - Method in interface org.orekit.estimation.measurements.generation.Scheduler
Initialize scheduler at the start of a measurements generation.
INITIAL_MATRIX_AND_PARAMETERS_NUMBER_MISMATCH - org.orekit.errors.OrekitMessages
INITIAL_MATRIX_AND_PARAMETERS_NUMBER_MISMATCH.
INITIAL_STATE_NOT_SPECIFIED_FOR_ORBIT_PROPAGATION - org.orekit.errors.OrekitMessages
INITIAL_STATE_NOT_SPECIFIED_FOR_ORBIT_PROPAGATION.
INITIAL_WET_MASS - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Total mass at beginning of life.
initialIsOsculating() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Check if the initial state is provided in osculating elements.
initialIsOsculating() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Check if the initial state is provided in osculating elements.
initializeAdditionalStates(AbsoluteDate) - Method in class org.orekit.propagation.AbstractPropagator
Initialize the additional state providers at the start of propagation.
initializeAdditionalStates(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator
Initialize the additional state providers at the start of propagation.
initializeAttitudeProviderForDerivatives() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Method called when initializing the attitude provider used when evaluating derivatives.
initializeAttitudeProviderForDerivatives() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Method called when initializing the attitude provider used when evaluating derivatives.
initializeAttitudeProviderForDerivatives() - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Method called when initializing the attitude provider used when evaluating derivatives.
initializeAttitudeProviderForDerivatives() - Method in class org.orekit.propagation.numerical.NumericalPropagator
Method called when initializing the attitude provider used when evaluating derivatives.
initializeFieldShortPeriodTerms(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester
Initialize the short periodic terms for the "field" elements.
initializeFieldShortPeriodTerms(SpacecraftState, PropagationType) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester
Initialize the short periodic terms for the "field" elements.
initializePropagation() - Method in class org.orekit.propagation.AbstractPropagator
Initialize propagation.
initializePropagation() - Method in class org.orekit.propagation.FieldAbstractPropagator
Initialize propagation.
initializeResetters(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers
Initialize resetters.
initializeResetters(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers
Initialize resetters.
initializeShortPeriodicTerms(SpacecraftState) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Initialize the short periodic terms for the Kalman Filter.
initializeShortPeriodicTerms(SpacecraftState) - Method in interface org.orekit.estimation.sequential.SemiAnalyticalProcess
Initialize the short periodic terms for the Kalman Filter.
initializeShortPeriodicTerms(SpacecraftState) - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel
Initialize the short periodic terms for the Kalman Filter.
initializeShortPeriodTerms(AuxiliaryElements, PropagationType, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Performs initialization prior to propagation for the current force model.
initializeShortPeriodTerms(AuxiliaryElements, PropagationType, double[]) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Performs initialization prior to propagation for the current force model.
initializeShortPeriodTerms(AuxiliaryElements, PropagationType, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTJ2SquaredClosedForm
Performs initialization prior to propagation for the current force model.
initializeShortPeriodTerms(AuxiliaryElements, PropagationType, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction
Performs initialization prior to propagation for the current force model.
initializeShortPeriodTerms(AuxiliaryElements, PropagationType, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Performs initialization prior to propagation for the current force model.
initializeShortPeriodTerms(AuxiliaryElements, PropagationType, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Computes the highest power of the eccentricity and the highest power of a/R3 to appear in the truncated analytical power series expansion.
initializeShortPeriodTerms(AuxiliaryElements, PropagationType, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Performs initialization prior to propagation for the current force model.
initializeShortPeriodTerms(AuxiliaryElements, PropagationType, double[]) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.J2SquaredModel
Performs initialization of J2-squared short period terms prior to propagation.
initializeShortPeriodTerms(FieldAuxiliaryElements<T>, PropagationType, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Performs initialization prior to propagation for the current force model.
initializeShortPeriodTerms(FieldAuxiliaryElements<T>, PropagationType, T[]) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Performs initialization prior to propagation for the current force model.
initializeShortPeriodTerms(FieldAuxiliaryElements<T>, PropagationType, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTJ2SquaredClosedForm
Performs initialization prior to propagation for the current force model.
initializeShortPeriodTerms(FieldAuxiliaryElements<T>, PropagationType, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction
Performs initialization prior to propagation for the current force model.
initializeShortPeriodTerms(FieldAuxiliaryElements<T>, PropagationType, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Performs initialization prior to propagation for the current force model.
initializeShortPeriodTerms(FieldAuxiliaryElements<T>, PropagationType, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Performs initialization prior to propagation for the current force model.
initializeShortPeriodTerms(FieldAuxiliaryElements<T>, PropagationType, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Performs initialization prior to propagation for the current force model.
initializeShortPeriodTerms(FieldAuxiliaryElements<T>, PropagationType, T[]) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.J2SquaredModel
Performs initialization of J2-squared short period terms prior to propagation.
initMapper() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Initialize the mapper.
initMapper(Field<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Initialize the mapper.
initPosition() - Method in class org.orekit.orbits.CartesianOrbit
Compute the position coordinates from the canonical parameters.
initPosition() - Method in class org.orekit.orbits.CircularOrbit
Compute the position coordinates from the canonical parameters.
initPosition() - Method in class org.orekit.orbits.EquinoctialOrbit
Compute the position coordinates from the canonical parameters.
initPosition() - Method in class org.orekit.orbits.FieldCartesianOrbit
Compute the position coordinates from the canonical parameters.
initPosition() - Method in class org.orekit.orbits.FieldCircularOrbit
Compute the position coordinates from the canonical parameters.
initPosition() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Compute the position coordinates from the canonical parameters.
initPosition() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Compute the position coordinates from the canonical parameters.
initPosition() - Method in class org.orekit.orbits.FieldOrbit
Compute the position coordinates from the canonical parameters.
initPosition() - Method in class org.orekit.orbits.KeplerianOrbit
Compute the position coordinates from the canonical parameters.
initPosition() - Method in class org.orekit.orbits.Orbit
Compute the position coordinates from the canonical parameters.
initPVCoordinates() - Method in class org.orekit.orbits.CartesianOrbit
Compute the position/velocity coordinates from the canonical parameters.
initPVCoordinates() - Method in class org.orekit.orbits.CircularOrbit
Compute the position/velocity coordinates from the canonical parameters.
initPVCoordinates() - Method in class org.orekit.orbits.EquinoctialOrbit
Compute the position/velocity coordinates from the canonical parameters.
initPVCoordinates() - Method in class org.orekit.orbits.FieldCartesianOrbit
Compute the position/velocity coordinates from the canonical parameters.
initPVCoordinates() - Method in class org.orekit.orbits.FieldCircularOrbit
Compute the position/velocity coordinates from the canonical parameters.
initPVCoordinates() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Compute the position/velocity coordinates from the canonical parameters.
initPVCoordinates() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Compute the position/velocity coordinates from the canonical parameters.
initPVCoordinates() - Method in class org.orekit.orbits.FieldOrbit
Compute the position/velocity coordinates from the canonical parameters.
initPVCoordinates() - Method in class org.orekit.orbits.KeplerianOrbit
Compute the position/velocity coordinates from the canonical parameters.
initPVCoordinates() - Method in class org.orekit.orbits.Orbit
Compute the position/velocity coordinates from the canonical parameters.
initStates(FieldSpacecraftState<Gradient>) - Method in class org.orekit.propagation.integration.AbstractGradientConverter
Initialize first state with 0 parameters.
inMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmParser
Acknowledge metada parsing has started.
inMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser
Acknowledge metada parsing has started.
inMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser
Acknowledge metada parsing has started.
inMetadata() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmParser
Acknowledge metada parsing has started.
inMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser
Acknowledge metada parsing has started.
inMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser
Acknowledge metada parsing has started.
inMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser
Acknowledge metada parsing has started.
inMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser
Acknowledge metada parsing has started.
inMetadata() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser
Acknowledge metada parsing has started.
inMetadata() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser
Acknowledge metada parsing has started.
inputAndOutputAreIdentical(OrbitType, PositionAngleType, OrbitType, PositionAngleType) - Static method in class org.orekit.propagation.StateCovariance
Checks if input/output orbit and angle types are identical.
inputAndOutputOrbitTypesAreCartesian(OrbitType, OrbitType) - Static method in class org.orekit.propagation.StateCovariance
Checks if input and output orbit types are both OrbitType.CARTESIAN.
InputStreamEncodedMessage - Class in org.orekit.gnss.metric.parser
Encoded message from an input stream.
InputStreamEncodedMessage(InputStream) - Constructor for class org.orekit.gnss.metric.parser.InputStreamEncodedMessage
Simple constructor.
INSIDE_CONE_TOUCHING_POLYGON_AT_EDGES_MIDDLE - org.orekit.geometry.fov.PolygonalFieldOfView.DefiningConeType
Constant for cones inside polygons and touching it at polygon edges middle points.
insideLeap(AbsoluteDate) - Method in class org.orekit.time.GLONASSScale
Check if date is within a leap second introduction in this time scale.
insideLeap(AbsoluteDate) - Method in interface org.orekit.time.TimeScale
Check if date is within a leap second introduction in this time scale.
insideLeap(AbsoluteDate) - Method in class org.orekit.time.UTCScale
Check if date is within a leap second introduction in this time scale.
insideLeap(FieldAbsoluteDate<T>) - Method in class org.orekit.time.GLONASSScale
Check if date is within a leap second introduction in this time scale.
insideLeap(FieldAbsoluteDate<T>) - Method in interface org.orekit.time.TimeScale
Check if date is within a leap second introduction in this time scale.
insideLeap(FieldAbsoluteDate<T>) - Method in class org.orekit.time.UTCScale
Check if date is within a leap second introduction in this time scale.
INSTRUMENT - org.orekit.files.ccsds.definitions.SpacecraftBodyFrame.BaseEquipment
Instrument.
INT_10 - org.orekit.gnss.metric.parser.DataType
10 bits signed integer.
INT_11 - org.orekit.gnss.metric.parser.DataType
11 bits signed integer.
INT_14 - org.orekit.gnss.metric.parser.DataType
14 bits signed integer.
INT_15 - org.orekit.gnss.metric.parser.DataType
15 bits signed integer.
INT_16 - org.orekit.gnss.metric.parser.DataType
16 bits signed integer.
INT_17 - org.orekit.gnss.metric.parser.DataType
17 bits signed integer.
INT_18 - org.orekit.gnss.metric.parser.DataType
18 bits signed integer.
INT_19 - org.orekit.gnss.metric.parser.DataType
19 bits signed integer.
INT_20 - org.orekit.gnss.metric.parser.DataType
20 bits signed integer.
INT_21 - org.orekit.gnss.metric.parser.DataType
21 bits signed integer.
INT_22 - org.orekit.gnss.metric.parser.DataType
22 bits signed integer.
INT_23 - org.orekit.gnss.metric.parser.DataType
23 bits signed integer.
INT_24 - org.orekit.gnss.metric.parser.DataType
24 bits signed integer.
INT_25 - org.orekit.gnss.metric.parser.DataType
25 bits signed integer.
INT_26 - org.orekit.gnss.metric.parser.DataType
26 bits signed integer.
INT_27 - org.orekit.gnss.metric.parser.DataType
27 bits signed integer.
INT_30 - org.orekit.gnss.metric.parser.DataType
30 bits signed integer.
INT_31 - org.orekit.gnss.metric.parser.DataType
31 bits signed integer.
INT_32 - org.orekit.gnss.metric.parser.DataType
32 bits signed integer.
INT_34 - org.orekit.gnss.metric.parser.DataType
34 bits signed integer.
INT_35 - org.orekit.gnss.metric.parser.DataType
35 bits signed integer.
INT_38 - org.orekit.gnss.metric.parser.DataType
38 bits signed integer.
INT_6 - org.orekit.gnss.metric.parser.DataType
6 bits signed integer.
INT_8 - org.orekit.gnss.metric.parser.DataType
8 bits signed integer.
INT_9 - org.orekit.gnss.metric.parser.DataType
9 bits signed integer.
INT_S_11 - org.orekit.gnss.metric.parser.DataType
11 bits sign-magnitude integer.
INT_S_22 - org.orekit.gnss.metric.parser.DataType
22 bits sign-magnitude integer.
INT_S_24 - org.orekit.gnss.metric.parser.DataType
24 bits sign-magnitude integer.
INT_S_27 - org.orekit.gnss.metric.parser.DataType
27 bits sign-magnitude integer.
INT_S_32 - org.orekit.gnss.metric.parser.DataType
32 bits sign-magnitude integer.
INT_S_5 - org.orekit.gnss.metric.parser.DataType
5 bits sign-magnitude integer.
intArrayToString(int[]) - Method in class org.orekit.files.ccsds.section.AbstractWriter
Convert an array of integer to a comma-separated list.
IntegerBootstrapping - Class in org.orekit.estimation.measurements.gnss
Bootstrapping engine for ILS problem solving.
IntegerBootstrapping(double) - Constructor for class org.orekit.estimation.measurements.gnss.IntegerBootstrapping
Constructor for the bootstrapping ambiguity estimator.
integerGaussTransformation(int, int) - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Perform one integer Gauss transformation.
IntegerLeastSquareComparator - Class in org.orekit.estimation.measurements.gnss
Comparator for IntegerLeastSquareSolution instance.
IntegerLeastSquareComparator() - Constructor for class org.orekit.estimation.measurements.gnss.IntegerLeastSquareComparator
Simple constructor.
IntegerLeastSquareSolution - Class in org.orekit.estimation.measurements.gnss
Class holding a solution to an Integer Least Square problem.
IntegerLeastSquareSolution(long[], double) - Constructor for class org.orekit.estimation.measurements.gnss.IntegerLeastSquareSolution
Simple constructor.
IntegerLeastSquareSolver - Interface in org.orekit.estimation.measurements.gnss
Interface for algorithms solving integer least square problems.
integrate(CalculusFieldUnivariateVectorFunction<T>, T, T, Field<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.GaussQuadrature
Integrates a given function on the given interval.
integrate(UnivariateVectorFunction, double, double) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.GaussQuadrature
Integrates a given function on the given interval.
IntegratedEphemeris - Class in org.orekit.propagation.integration
This class stores sequentially generated orbital parameters for later retrieval.
IntegratedEphemeris(AbsoluteDate, AbsoluteDate, AbsoluteDate, StateMapper, PropagationType, DenseOutputModel, DoubleArrayDictionary, List<AdditionalStateProvider>, String[], int[]) - Constructor for class org.orekit.propagation.integration.IntegratedEphemeris
Creates a new instance of IntegratedEphemeris.
INTEGRATION_INTERVAL - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Integration interval entry.
INTEGRATION_REF - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Integration reference entry.
IntegrationReference - Enum in org.orekit.files.ccsds.ndm.tdm
Relationship between time tag and integration interval.
IntelsatElevenElements - Class in org.orekit.propagation.analytical.intelsat
This class is a container for a single set of Intelsat's 11 Elements data.
IntelsatElevenElements(AbsoluteDate, double, double, double, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.intelsat.IntelsatElevenElements
Constructor.
IntelsatElevenElementsPropagator - Class in org.orekit.propagation.analytical.intelsat
This class provides elements to propagate Intelsat's 11 elements.
IntelsatElevenElementsPropagator(IntelsatElevenElements) - Constructor for class org.orekit.propagation.analytical.intelsat.IntelsatElevenElementsPropagator
Default constructor.
IntelsatElevenElementsPropagator(IntelsatElevenElements, Frame, Frame) - Constructor for class org.orekit.propagation.analytical.intelsat.IntelsatElevenElementsPropagator
Constructor.
IntelsatElevenElementsPropagator(IntelsatElevenElements, Frame, Frame, AttitudeProvider, double) - Constructor for class org.orekit.propagation.analytical.intelsat.IntelsatElevenElementsPropagator
Constructor.
INTERMEDIATE_SUFFIX - Static variable in class org.orekit.estimation.measurements.GroundStation
Suffix for ground station intermediate frame name.
INTERNAL_ERROR - org.orekit.errors.OrekitMessages
INTERNAL_ERROR.
INTERNATIONAL_DESIGNATOR - org.orekit.files.ccsds.ndm.adm.acm.AcmMetadataKey
International designator for the object as assigned by the UN Committee on Space Research (COSPAR) and the US National Space Science Data Center (NSSDC).
INTERNATIONAL_DESIGNATOR - org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey
Full international designator name for the object.
INTERNATIONAL_DESIGNATOR - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
International designator for the object as assigned by the UN Committee on Space Research (COSPAR) and the US National Space Science Data Center (NSSDC).
INTERP_METHOD_EOP - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Interpolation method for Earth Orientation Parameters.
interpolate(AbsoluteDate, Collection<Orbit>) - Method in class org.orekit.orbits.AbstractOrbitInterpolator
Get an interpolated instance.
interpolate(AbsoluteDate, Collection<SpacecraftState>) - Method in class org.orekit.propagation.SpacecraftStateInterpolator
Get an interpolated instance.
interpolate(AbsoluteDate, Collection<T>) - Method in class org.orekit.time.AbstractTimeInterpolator
Get an interpolated instance.
interpolate(AbsoluteDate, Collection<T>) - Method in interface org.orekit.time.FieldTimeInterpolator
Get an interpolated instance.
interpolate(AbsoluteDate, Collection<T>) - Method in interface org.orekit.time.TimeInterpolator
Get an interpolated instance.
interpolate(AbsoluteDate, Stream<Transform>) - Method in class org.orekit.frames.Transform
Interpolate a transform from a sample set of existing transforms.
interpolate(AbsoluteDate, Stream<T>) - Method in class org.orekit.time.AbstractTimeInterpolator
Get an interpolated instance.
interpolate(AbsoluteDate, Stream<T>) - Method in interface org.orekit.time.FieldTimeInterpolator
Get an interpolated instance.
interpolate(AbsoluteDate, Stream<T>) - Method in interface org.orekit.time.TimeInterpolator
Get an interpolated instance.
interpolate(AbsoluteDate, CartesianDerivativesFilter, AngularDerivativesFilter, Collection<Transform>) - Static method in class org.orekit.frames.Transform
Interpolate a transform from a sample set of existing transforms.
interpolate(AbstractFieldTimeInterpolator.InterpolationData) - Method in class org.orekit.attitudes.FieldAttitudeInterpolator
Interpolate instance from given interpolation data.
interpolate(AbstractFieldTimeInterpolator.InterpolationData) - Method in class org.orekit.orbits.FieldOrbitBlender
Interpolate instance from given interpolation data.
interpolate(AbstractFieldTimeInterpolator.InterpolationData) - Method in class org.orekit.orbits.FieldOrbitHermiteInterpolator
Interpolate instance from given interpolation data.
interpolate(AbstractFieldTimeInterpolator.InterpolationData) - Method in class org.orekit.propagation.FieldSpacecraftStateInterpolator
Interpolate instance from given interpolation data.
interpolate(AbstractFieldTimeInterpolator.InterpolationData) - Method in class org.orekit.time.FieldClockOffsetHermiteInterpolator
Interpolate instance from given interpolation data.
interpolate(AbstractFieldTimeInterpolator.InterpolationData) - Method in class org.orekit.time.TimeStampedFieldHermiteInterpolator
Interpolate instance from given interpolation data.
interpolate(AbstractFieldTimeInterpolator.InterpolationData) - Method in class org.orekit.utils.FieldAbsolutePVCoordinatesHermiteInterpolator
Interpolate instance from given interpolation data.
interpolate(AbstractFieldTimeInterpolator.InterpolationData) - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinatesHermiteInterpolator
Interpolate instance from given interpolation data.
interpolate(AbstractFieldTimeInterpolator.InterpolationData) - Method in class org.orekit.utils.TimeStampedFieldPVCoordinatesHermiteInterpolator
Interpolate instance from given interpolation data.
interpolate(AbstractFieldTimeInterpolator.InterpolationData) - Method in class org.orekit.time.AbstractFieldTimeInterpolator
Interpolate instance from given interpolation data.
interpolate(AbstractTimeInterpolator.InterpolationData) - Method in class org.orekit.attitudes.AttitudeInterpolator
Interpolate instance from given interpolation data.
interpolate(AbstractTimeInterpolator.InterpolationData) - Method in class org.orekit.files.sp3.SP3CoordinateHermiteInterpolator
Interpolate instance from given interpolation data.
interpolate(AbstractTimeInterpolator.InterpolationData) - Method in class org.orekit.orbits.OrbitBlender
Interpolate instance from given interpolation data.
interpolate(AbstractTimeInterpolator.InterpolationData) - Method in class org.orekit.orbits.OrbitHermiteInterpolator
Interpolate instance from given interpolation data.
interpolate(AbstractTimeInterpolator.InterpolationData) - Method in class org.orekit.propagation.SpacecraftStateInterpolator
Interpolate instance from given interpolation data.
interpolate(AbstractTimeInterpolator.InterpolationData) - Method in class org.orekit.time.ClockOffsetHermiteInterpolator
Interpolate instance from given interpolation data.
interpolate(AbstractTimeInterpolator.InterpolationData) - Method in class org.orekit.time.TimeStampedDoubleHermiteInterpolator
Interpolate instance from given interpolation data.
interpolate(AbstractTimeInterpolator.InterpolationData) - Method in class org.orekit.time.TimeStampedDoubleAndDerivativeHermiteInterpolator
Interpolate instance from given interpolation data.
interpolate(AbstractTimeInterpolator.InterpolationData) - Method in class org.orekit.propagation.AbstractStateCovarianceInterpolator
Interpolate orbit and associated covariance.
interpolate(AbstractTimeInterpolator.InterpolationData) - Method in class org.orekit.utils.AbsolutePVCoordinatesHermiteInterpolator
Interpolate instance from given interpolation data.
interpolate(AbstractTimeInterpolator.InterpolationData) - Method in class org.orekit.utils.TimeStampedAngularCoordinatesHermiteInterpolator
Interpolate instance from given interpolation data.
interpolate(AbstractTimeInterpolator.InterpolationData) - Method in class org.orekit.utils.TimeStampedPVCoordinatesHermiteInterpolator
Interpolate instance from given interpolation data.
interpolate(AbstractTimeInterpolator.InterpolationData) - Method in class org.orekit.time.AbstractTimeInterpolator
Interpolate instance from given interpolation data.
interpolate(FieldAbsoluteDate<KK>, Collection<FieldOrbit<KK>>) - Method in class org.orekit.orbits.AbstractFieldOrbitInterpolator
Get an interpolated instance.
interpolate(FieldAbsoluteDate<KK>, Collection<FieldSpacecraftState<KK>>) - Method in class org.orekit.propagation.FieldSpacecraftStateInterpolator
Get an interpolated instance.
interpolate(FieldAbsoluteDate<KK>, Collection<T>) - Method in class org.orekit.time.AbstractFieldTimeInterpolator
Get an interpolated instance.
interpolate(FieldAbsoluteDate<KK>, Collection<T>) - Method in interface org.orekit.time.FieldTimeInterpolator
Get an interpolated instance.
interpolate(FieldAbsoluteDate<KK>, Stream<T>) - Method in class org.orekit.time.AbstractFieldTimeInterpolator
Get an interpolated instance.
interpolate(FieldAbsoluteDate<KK>, Stream<T>) - Method in interface org.orekit.time.FieldTimeInterpolator
Get an interpolated instance.
interpolate(FieldAbsoluteDate<T>, Collection<FieldTransform<T>>) - Static method in class org.orekit.frames.FieldTransform
Interpolate a transform from a sample set of existing transforms.
interpolate(FieldAbsoluteDate<T>, CartesianDerivativesFilter, AngularDerivativesFilter, Collection<FieldTransform<T>>) - Static method in class org.orekit.frames.FieldTransform
Interpolate a transform from a sample set of existing transforms.
interpolate(FieldAbsoluteDate<T>, CartesianDerivativesFilter, AngularDerivativesFilter, Stream<FieldTransform<T>>) - Static method in class org.orekit.frames.FieldTransform
Interpolate a transform from a sample set of existing transforms.
interpolateOrbit(AbsoluteDate, List<TimeStampedPair<Orbit, StateCovariance>>) - Method in class org.orekit.propagation.AbstractStateCovarianceInterpolator
Interpolate orbit at given interpolation date.
InterpolatingTransformProvider - Class in org.orekit.frames
Transform provider using thread-safe interpolation on transforms sample.
InterpolatingTransformProvider(TransformProvider, CartesianDerivativesFilter, AngularDerivativesFilter, int, double, int, double, double) - Constructor for class org.orekit.frames.InterpolatingTransformProvider
Simple constructor.
INTERPOLATION - org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadataKey
Interpolation method to be used.
INTERPOLATION - org.orekit.files.ccsds.ndm.odm.oem.OemMetadataKey
Interpolation method in ephemeris.
INTERPOLATION - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Interpolation method for transmit phase count.
INTERPOLATION_DEGREE - org.orekit.files.ccsds.ndm.adm.aem.AemMetadataKey
Interpolation degree in ephemeris.
INTERPOLATION_DEGREE - org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadataKey
Interpolation degree.
INTERPOLATION_DEGREE - org.orekit.files.ccsds.ndm.odm.oem.OemMetadataKey
Interpolation degree in ephemeris.
INTERPOLATION_DEGREE - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Interpolation degree for transmit phase count.
INTERPOLATION_METHOD - org.orekit.files.ccsds.ndm.adm.aem.AemMetadataKey
Interpolation method in ephemeris.
InterpolationData(AbsoluteDate, Collection<T>) - Constructor for class org.orekit.time.AbstractTimeInterpolator.InterpolationData
Constructor.
InterpolationData(FieldAbsoluteDate<KK>, Collection<T>) - Constructor for class org.orekit.time.AbstractFieldTimeInterpolator.InterpolationData
Constructor.
InterpolationGrid - Interface in org.orekit.propagation.semianalytical.dsst.utilities
Interface for interpolation grids.
InterpolationMethod - Enum in org.orekit.files.ccsds.ndm.odm.oem
OEM interpolation method.
InterpolationTableLoader - Class in org.orekit.utils
Used to read an interpolation table from a data file.
InterpolationTableLoader() - Constructor for class org.orekit.utils.InterpolationTableLoader
Empty constructor.
InterSatDirectViewDetector - Class in org.orekit.propagation.events
Detector for inter-satellites direct view (i.e.
InterSatDirectViewDetector(OneAxisEllipsoid, double, PVCoordinatesProvider, AdaptableInterval, double, int, EventHandler) - Constructor for class org.orekit.propagation.events.InterSatDirectViewDetector
Private constructor.
InterSatDirectViewDetector(OneAxisEllipsoid, PVCoordinatesProvider) - Constructor for class org.orekit.propagation.events.InterSatDirectViewDetector
simple constructor.
InterSatellitesOneWayRangeRate - Class in org.orekit.estimation.measurements.gnss
One way range-rate measurement between two satellites.
InterSatellitesOneWayRangeRate(ObservableSatellite, ObservableSatellite, AbsoluteDate, double, double, double) - Constructor for class org.orekit.estimation.measurements.gnss.InterSatellitesOneWayRangeRate
Constructor.
InterSatellitesOneWayRangeRateBuilder - Class in org.orekit.estimation.measurements.generation
Builder for InterSatellitesOneWayRangeRate measurements.
InterSatellitesOneWayRangeRateBuilder(CorrelatedRandomVectorGenerator, ObservableSatellite, ObservableSatellite, double, double) - Constructor for class org.orekit.estimation.measurements.generation.InterSatellitesOneWayRangeRateBuilder
Simple constructor.
InterSatellitesPhase - Class in org.orekit.estimation.measurements.gnss
Phase measurement between two satellites.
InterSatellitesPhase(ObservableSatellite, ObservableSatellite, AbsoluteDate, double, double, double, double) - Constructor for class org.orekit.estimation.measurements.gnss.InterSatellitesPhase
InterSatellitesPhase(ObservableSatellite, ObservableSatellite, AbsoluteDate, double, double, double, double, AmbiguityCache) - Constructor for class org.orekit.estimation.measurements.gnss.InterSatellitesPhase
Constructor.
InterSatellitesPhaseAmbiguityModifier - Class in org.orekit.estimation.measurements.modifiers
Deprecated.
as of 12.1 ambiguity is managed directly by raw measurements InterSatellitesPhase
InterSatellitesPhaseAmbiguityModifier(int, double) - Constructor for class org.orekit.estimation.measurements.modifiers.InterSatellitesPhaseAmbiguityModifier
Deprecated.
Constructor.
InterSatellitesPhaseBuilder - Class in org.orekit.estimation.measurements.generation
Builder for InterSatellitesPhase measurements.
InterSatellitesPhaseBuilder(CorrelatedRandomVectorGenerator, ObservableSatellite, ObservableSatellite, double, double, double) - Constructor for class org.orekit.estimation.measurements.generation.InterSatellitesPhaseBuilder
InterSatellitesPhaseBuilder(CorrelatedRandomVectorGenerator, ObservableSatellite, ObservableSatellite, double, double, double, AmbiguityCache) - Constructor for class org.orekit.estimation.measurements.generation.InterSatellitesPhaseBuilder
Simple constructor.
InterSatellitesRange - Class in org.orekit.estimation.measurements
One-way or two-way range measurements between two satellites.
InterSatellitesRange(ObservableSatellite, ObservableSatellite, boolean, AbsoluteDate, double, double, double) - Constructor for class org.orekit.estimation.measurements.InterSatellitesRange
Simple constructor.
InterSatellitesRangeBuilder - Class in org.orekit.estimation.measurements.generation
Builder for InterSatellitesRange measurements.
InterSatellitesRangeBuilder(CorrelatedRandomVectorGenerator, ObservableSatellite, ObservableSatellite, boolean, double, double) - Constructor for class org.orekit.estimation.measurements.generation.InterSatellitesRangeBuilder
Simple constructor.
InterSatellitesWindUp - Class in org.orekit.estimation.measurements.gnss
Modifier for wind-up effect in GNSS inter-satellites phase measurements.
InterSatellitesWindUpFactory - Class in org.orekit.estimation.measurements.gnss
Factory for wind-up modifiers.
InterSatellitesWindUpFactory() - Constructor for class org.orekit.estimation.measurements.gnss.InterSatellitesWindUpFactory
Simple constructor.
INTERVAL - org.orekit.files.rinex.section.RinexLabels
Observation interval.
IntervalEventTrigger<T extends AbstractDetector<T>> - Class in org.orekit.forces.maneuvers.trigger
Maneuver triggers based on a single event detector that defines firing intervals.
IntervalEventTrigger(T) - Constructor for class org.orekit.forces.maneuvers.trigger.IntervalEventTrigger
Simple constructor.
INTRACK_THRUST - org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey
Indication of whether in-track thrust modeling used for the object.
intValue(EncodedMessage) - Method in interface org.orekit.gnss.metric.parser.DataField
Get the value of the field as an integer.
INVALID_GNSS_DATA - org.orekit.errors.OrekitMessages
INVALID_GNSS_DATA.
INVALID_MEASUREMENT_TYPES_FOR_COMBINATION_OF_MEASUREMENTS - org.orekit.errors.OrekitMessages
INVALID_MEASUREMENT_TYPES_FOR_COMBINATION_OF_MEASUREMENTS.
INVALID_PARAMETER_RANGE - org.orekit.errors.OrekitMessages
INVALID_PARAMETER_RANGE.
INVALID_RANGE_INDICATOR_IN_CRD_FILE - org.orekit.errors.OrekitMessages
INVALID_RANGE_INDICATOR_IN_CRD_FILE.
INVALID_SATELLITE_ID - org.orekit.errors.OrekitMessages
INVALID_SATELLITE_ID.
INVALID_SATELLITE_SYSTEM - org.orekit.errors.OrekitMessages
INVALID_SATELLITE_SYSTEM.
INVALID_TYPE_FOR_FUNCTION - org.orekit.errors.OrekitMessages
INVALID_TYPE_FOR_FUNCTION.
invalidAfter() - Method in class org.orekit.utils.WaypointPVBuilder
Indicate the resulting PVCoordinatesProvider should be invalid after the last waypoint.
invalidAfter(AbsoluteDate) - Method in class org.orekit.utils.AggregatedPVCoordinatesProvider.Builder
Indicate the date after which the resulting PVCoordinatesProvider is invalid.
invalidBefore() - Method in class org.orekit.utils.WaypointPVBuilder
Indicate the resulting PVCoordinatesProvider should be invalid before the first waypoint.
invalidBefore(AbsoluteDate) - Method in class org.orekit.utils.AggregatedPVCoordinatesProvider.Builder
Indicate the date before which the resulting PVCoordinatesProvider is invalid.
InvalidPVProvider() - Constructor for class org.orekit.utils.AggregatedPVCoordinatesProvider.InvalidPVProvider
Empty constructor.
inverseDecomposition() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Inverse the decomposition.
inverseDecomposition() - Method in class org.orekit.estimation.measurements.gnss.LambdaMethod
Inverse the decomposition.
inverseDecomposition() - Method in class org.orekit.estimation.measurements.gnss.ModifiedLambdaMethod
Inverse the decomposition.
IodGauss - Class in org.orekit.estimation.iod
Gauss angles-only Initial Orbit Determination (IOD) algorithm.
IodGauss(double) - Constructor for class org.orekit.estimation.iod.IodGauss
Constructor.
IodGibbs - Class in org.orekit.estimation.iod
Gibbs position-based Initial Orbit Determination (IOD) algorithm.
IodGibbs(double) - Constructor for class org.orekit.estimation.iod.IodGibbs
Creator.
IodGooding - Class in org.orekit.estimation.iod
Gooding angles only Initial Orbit Determination (IOD) algorithm, assuming Keplerian motion.
IodGooding(double) - Constructor for class org.orekit.estimation.iod.IodGooding
Constructor.
IodLambert - Class in org.orekit.estimation.iod
Lambert position-based Initial Orbit Determination (IOD) algorithm, assuming Keplerian motion.
IodLambert(double) - Constructor for class org.orekit.estimation.iod.IodLambert
Creator.
IodLaplace - Class in org.orekit.estimation.iod
Laplace angles-only Initial Orbit Determination (IOD) algorithm, assuming Keplerian motion.
IodLaplace(double) - Constructor for class org.orekit.estimation.iod.IodLaplace
Constructor.
IONO_FREE - org.orekit.estimation.measurements.gnss.CombinationType
Ionosphere-free combination.
IonosphereBaseMessage - Class in org.orekit.files.rinex.navigation
Base container for data contained in a ionosphere message.
IonosphereBaseMessage(SatelliteSystem, int, String) - Constructor for class org.orekit.files.rinex.navigation.IonosphereBaseMessage
Simple constructor.
IonosphereBDGIMMessage - Class in org.orekit.files.rinex.navigation
Container for data contained in a ionosphere BDGIM message.
IonosphereBDGIMMessage(SatelliteSystem, int, String) - Constructor for class org.orekit.files.rinex.navigation.IonosphereBDGIMMessage
Simple constructor.
IonosphereFreeCombination - Class in org.orekit.estimation.measurements.gnss
Ionosphere-free combination.
IonosphereKlobucharMessage - Class in org.orekit.files.rinex.navigation
Container for data contained in a ionosphere Klobuchar message.
IonosphereKlobucharMessage(SatelliteSystem, int, String) - Constructor for class org.orekit.files.rinex.navigation.IonosphereKlobucharMessage
Simple constructor.
IonosphereNequickGMessage - Class in org.orekit.files.rinex.navigation
Container for data contained in a ionosphere Nequick G message.
IonosphereNequickGMessage(SatelliteSystem, int, String) - Constructor for class org.orekit.files.rinex.navigation.IonosphereNequickGMessage
Simple constructor.
IonosphericCorrectionType - Enum in org.orekit.files.rinex.navigation
Ionospheric correction type.
IonosphericMappingFunction - Interface in org.orekit.models.earth.ionosphere
Interface for mapping functions used in the ionospheric delay computation.
IonosphericModel - Interface in org.orekit.models.earth.ionosphere
Defines a ionospheric model, used to calculate the path delay imposed to electro-magnetic signals between an orbital satellite and a ground station.
IRN - org.orekit.files.rinex.navigation.IonosphericCorrectionType
IRNSS α/β.
IRN - org.orekit.files.rinex.navigation.UtcId
UTCIRN / UTC(NPLI).
IRN - org.orekit.gnss.ObservationTimeScale
IRNSS time scale.
IRNSS - org.orekit.files.sp3.SP3FileType
IRNSS only file.
IRNSS - org.orekit.gnss.SatelliteSystem
Indian Regional Navigation Satellite System system (NavIC).
IRNSS - org.orekit.gnss.TimeSystem
IRNSS.
IRNSS_1GEO - org.orekit.gnss.antenna.SatelliteType
IRNSS-1 GEO.
IRNSS_1IGSO - org.orekit.gnss.antenna.SatelliteType
IRNSS-1 IGSO.
IRNSS_AV - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
Value of the earth's rotation rate in rad/s for IRNSS user.
IRNSS_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Reference epoch for IRNSS weeks: 1999-08-22T00:00:00 IRNSS time.
IRNSS_EPOCH - Static variable in class org.orekit.time.DateComponents
Reference epoch for IRNSS weeks: 1999-08-22.
IRNSS_MU - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
WGS 84 value of the Earth's universal gravitational parameter for IRNSS user in m³/s².
IRNSS_WEEK_NB - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
Number of weeks in the IRNSS cycle.
IRNSSAlmanac - Class in org.orekit.propagation.analytical.gnss.data
Class for IRNSS almanac.
IRNSSAlmanac() - Constructor for class org.orekit.propagation.analytical.gnss.data.IRNSSAlmanac
Constructor.
IRNSSNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data
Container for data contained in an IRNSS navigation message.
IRNSSNavigationMessage() - Constructor for class org.orekit.propagation.analytical.gnss.data.IRNSSNavigationMessage
Constructor.
IRNSSScale - Class in org.orekit.time
IRNSS time scale (also called IRNWT for IRNSS NetWork Time).
IRREGULAR_OR_INCOMPLETE_GRID - org.orekit.errors.OrekitMessages
IRREGULAR_OR_INCOMPLETE_GRID.
IRS - org.orekit.gnss.metric.ntrip.NavigationSystem
IRNSS.
isA2b() - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints
Check if rotation direction is from frame A to frame B.
isAdditionalStateManaged(String) - Method in class org.orekit.propagation.AbstractPropagator
Check if an additional state is managed.
isAdditionalStateManaged(String) - Method in class org.orekit.propagation.analytical.Ephemeris
Check if an additional state is managed.
isAdditionalStateManaged(String) - Method in class org.orekit.propagation.FieldAbstractPropagator
Check if an additional state is managed.
isAdditionalStateManaged(String) - Method in interface org.orekit.propagation.FieldPropagator
Check if an additional state is managed.
isAdditionalStateManaged(String) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Check if an additional state is managed.
isAdditionalStateManaged(String) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Check if an additional state is managed.
isAdditionalStateManaged(String) - Method in interface org.orekit.propagation.Propagator
Check if an additional state is managed.
isAfter(FieldTimeStamped<T>) - Method in class org.orekit.time.FieldAbsoluteDate
Check if the instance represents a time that is strictly after another.
isAfter(TimeStamped) - Method in class org.orekit.time.AbsoluteDate
Check if the instance represents a time that is strictly after another.
isAfterOrEqualTo(FieldTimeStamped<T>) - Method in class org.orekit.time.FieldAbsoluteDate
Check if the instance represents a time that is after or equal to another.
isAfterOrEqualTo(TimeStamped) - Method in class org.orekit.time.AbsoluteDate
Check if the instance represents a time that is after or equal to another.
isAltCovFlagSet() - Method in class org.orekit.files.ccsds.ndm.cdm.SigmaEigenvectorsCovariance
Get the flag indicating whether the alternate covariance type set in the CDM Object metadata section is Sigma/Eigenvectors Covariance.
isAMaximumProbabilityOfCollisionMethod() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter2DPOCMethod
Get flag that defines if the method is a maximum probability of collision computing method.
isAMaximumProbabilityOfCollisionMethod() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Alfriend1999
Get flag that defines if the method is a maximum probability of collision computing method.
isAMaximumProbabilityOfCollisionMethod() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Alfriend1999Max
Get flag that defines if the method is a maximum probability of collision computing method.
isAMaximumProbabilityOfCollisionMethod() - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod
Get flag that defines if the method is a maximum probability of collision computing method.
isBefore(FieldTimeStamped<T>) - Method in class org.orekit.time.FieldAbsoluteDate
Check if the instance represents a time that is strictly before another.
isBefore(TimeStamped) - Method in class org.orekit.time.AbsoluteDate
Check if the instance represents a time that is strictly before another.
isBeforeOrEqualTo(FieldTimeStamped<T>) - Method in class org.orekit.time.FieldAbsoluteDate
Check if the instance represents a time that is before or equal to another.
isBeforeOrEqualTo(TimeStamped) - Method in class org.orekit.time.AbsoluteDate
Check if the instance represents a time that is before or equal to another.
isBetween(FieldTimeStamped<T>, FieldTimeStamped<T>) - Method in class org.orekit.time.FieldAbsoluteDate
Check if the instance represents a time that is strictly between two others representing the boundaries of a time span.
isBetween(TimeStamped, TimeStamped) - Method in class org.orekit.time.AbsoluteDate
Check if the instance represents a time that is strictly between two others representing the boundaries of a time span.
isBetweenOrEqualTo(FieldTimeStamped<T>, FieldTimeStamped<T>) - Method in class org.orekit.time.FieldAbsoluteDate
Check if the instance represents a time that is between two others representing the boundaries of a time span, or equal to one of them.
isBetweenOrEqualTo(TimeStamped, TimeStamped) - Method in class org.orekit.time.AbsoluteDate
Check if the instance represents a time that is between two others representing the boundaries of a time span, or equal to one of them.
isCenterOfMassCorrectionApplied() - Method in class org.orekit.files.ilrs.CPFHeader
Get the flag telling if the center of mass correction is applied.
isCenterOfMassCorrectionApplied() - Method in class org.orekit.files.ilrs.CRDHeader
Get the center of mass correction applied indicator.
isChildOf(Frame) - Method in class org.orekit.frames.Frame
Determine if a Frame is a child of another one.
isCloseTo(FieldTimeStamped<T>, double) - Method in class org.orekit.time.FieldAbsoluteDate
Check if the instance time is close to another.
isCloseTo(TimeStamped, double) - Method in class org.orekit.time.AbsoluteDate
Check if the instance time is close to another.
isCnv2() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage
Check it message is a CNV2 message.
isCompatibleWith(AttitudeEndpoints) - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints
Check if a endpoint is compatible with another one.
isCompatibleWithTIVs() - Method in class org.orekit.files.ilrs.CPFHeader
Get the flag for compatibility with TIVs.
isConsistencyMaintained() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Header
Get the flag indicating if phase biases maintain consistency between non-dispersive and all original dispersive phase signals.
isContinuousEstimation() - Method in class org.orekit.utils.ParameterDriver
Check if parameter estimation is continuous, that is to say when a value wants to be known at date t, the value returned will be an interpolation between start value on span corresponding for date t and end value (which corresponds to the start of the next span), continuous estimation.
isConverged() - Method in class org.orekit.control.indirect.shooting.ShootingBoundaryOutput
Getter for convergence flag.
isConverged(PVCoordinates, PVCoordinates) - Method in interface org.orekit.control.indirect.shooting.boundary.CartesianBoundaryConditionChecker
Asserts convergence.
isConverged(PVCoordinates, PVCoordinates) - Method in class org.orekit.control.indirect.shooting.boundary.NormBasedCartesianConditionChecker
Asserts convergence.
isCovXYZset() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Get the flag indicating whether the alternate covariance type set in the CDM Object metadata section is XYZ.
isCurrentStateInterpolated() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator
Determines if the current state is computed directly by the integrator, or if it is calculated using interpolation.
isDoubleSided() - Method in class org.orekit.forces.Panel
Check if the panel is double-sided (typically solar arrays).
isDSStateDerivative(FieldSpacecraftState<T>) - Method in class org.orekit.forces.drag.AbstractDragForceModel
Check if a field state corresponds to derivatives with respect to state.
isElliptical() - Method in class org.orekit.orbits.FieldOrbit
Returns true if and only if the orbit is elliptical i.e.
isElliptical() - Method in class org.orekit.orbits.Orbit
Returns true if and only if the orbit is elliptical i.e.
isEnabled() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Check if a measurement is enabled.
isEnabled() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
Check if a measurement is enabled.
isEqualTo(FieldTimeStamped<T>) - Method in class org.orekit.time.FieldAbsoluteDate
Check if the instance represents the same time as another.
isEqualTo(TimeStamped) - Method in class org.orekit.time.AbsoluteDate
Check if the instance represents the same time as another.
isExternal2SpacecraftBody() - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints
Check if attitude is from external frame to spacecraft body frame.
isFiring(FieldSpacecraftState<T>) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Check if maneuvering is on.
isFiring(SpacecraftState) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Check if maneuvering is on.
isFiring(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Check if maneuvering is on.
isFiring(AbsoluteDate, double[]) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers
Find out if the maneuver is firing or not.
isFiring(AbsoluteDate, double[]) - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggers
Find out if the maneuver is firing or not.
isFiring(FieldAbsoluteDate<S>, S[]) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers
Find out if the maneuver is firing or not.
isFiring(FieldAbsoluteDate<T>, T[]) - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggers
Find out if the maneuver is firing or not.
isFiringOnInitialState(SpacecraftState, boolean) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers
Method to check if the thruster is firing on initialization.
isFiringOnInitialState(SpacecraftState, boolean) - Method in class org.orekit.forces.maneuvers.trigger.IntervalEventTrigger
Method to check if the thruster is firing on initialization.
isFiringOnInitialState(SpacecraftState, boolean) - Method in class org.orekit.forces.maneuvers.trigger.StartStopEventsTrigger
Method to check if the thruster is firing on initialization.
isFirst() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Get the flag for the placement of the quaternion QC in the attitude data.
isFormatOK(String, String) - Static method in class org.orekit.propagation.analytical.tle.FieldTLE
Check the lines format validity.
isFormatOK(String, String) - Static method in class org.orekit.propagation.analytical.tle.TLE
Check the lines format validity.
isForward() - Method in class org.orekit.propagation.events.AbstractDetector
Check if the current propagation is forward or backward.
isForward() - Method in class org.orekit.propagation.events.FieldAbstractDetector
Check if the current propagation is forward or backward.
isForward() - Method in interface org.orekit.propagation.sampling.FieldOrekitStepInterpolator
Check is integration direction is forward in date.
isForward() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator
Check is integration direction is forward in date.
isForwardPropagation() - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel
Return the forward propagation flag.
isGradientStateDerivative(FieldSpacecraftState<T>) - Method in class org.orekit.forces.drag.AbstractDragForceModel
Check if a field state corresponds to derivatives with respect to state.
isHealthAvailable() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the flag indicating if GLONASS almanac health is available.
isIncreasing() - Method in class org.orekit.propagation.events.EventsLogger.LoggedEvent
Get the Increasing/decreasing status of the event.
isIncreasing() - Method in class org.orekit.propagation.events.FieldEventsLogger.FieldLoggedEvent
Get the Increasing/decreasing status of the event.
isIncreasing() - Method in class org.orekit.propagation.events.handlers.FieldRecordAndContinue.Event
Is the g() function increasing?
isIncreasing() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue.Event
Is the g() function increasing?
isInside(FieldVector3D<T>) - Method in class org.orekit.bodies.Ellipsoid
Check if a point is inside the ellipsoid.
isInside(Vector3D) - Method in class org.orekit.bodies.Ellipsoid
Check if a point is inside the ellipsoid.
isMaxProbability() - Method in class org.orekit.ssa.metrics.FieldProbabilityOfCollision
Get flag that defines if this probability of collision can be considered a maximum probability of collision.
isMaxProbability() - Method in class org.orekit.ssa.metrics.ProbabilityOfCollision
Get flag that defines if this probability of collision can be considered a maximum probability of collision.
isMeanOrbit() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Check if only the mean elements should be used in a semi-analytical propagation.
isMelbourneWubbenaConsistencyMaintained() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Header
Get the flag indicating if consistency between code and phase biases is maintained for the MW combinations.
isNetworked() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
Check if the stream is generated from a network of stations.
isNMEARequired() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
Check if NMEA message must be sent to caster.
isOn() - Method in enum org.orekit.files.ccsds.definitions.OnOff
Check if status is "on".
isOnlyPosition() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Check if fitting uses only sample positions.
isOrbitDefined() - Method in class org.orekit.propagation.FieldSpacecraftState
Check if the state contains an orbit part.
isOrbitDefined() - Method in class org.orekit.propagation.SpacecraftState
Check if the state contains an orbit part.
IsotropicDrag - Class in org.orekit.forces.drag
This class models isotropic drag effects.
IsotropicDrag(double, double) - Constructor for class org.orekit.forces.drag.IsotropicDrag
Constructor with drag coefficient min/max set to ±∞.
IsotropicDrag(double, double, double, double) - Constructor for class org.orekit.forces.drag.IsotropicDrag
Constructor with drag coefficient min/max set by user.
IsotropicRadiationClassicalConvention - Class in org.orekit.forces.radiation
This class represents the features of a simplified spacecraft.
IsotropicRadiationClassicalConvention(double, double, double) - Constructor for class org.orekit.forces.radiation.IsotropicRadiationClassicalConvention
Simple constructor.
IsotropicRadiationCNES95Convention - Class in org.orekit.forces.radiation
This class represents the features of a simplified spacecraft.
IsotropicRadiationCNES95Convention(double, double, double) - Constructor for class org.orekit.forces.radiation.IsotropicRadiationCNES95Convention
Simple constructor.
IsotropicRadiationSingleCoefficient - Class in org.orekit.forces.radiation
This class represents the features of a simplified spacecraft.
IsotropicRadiationSingleCoefficient(double, double) - Constructor for class org.orekit.forces.radiation.IsotropicRadiationSingleCoefficient
Constructor with reflection coefficient min/max set to ±∞.
IsotropicRadiationSingleCoefficient(double, double, double, double) - Constructor for class org.orekit.forces.radiation.IsotropicRadiationSingleCoefficient
Constructor with reflection coefficient min/max set by user.
isPositionAngleBased() - Method in enum org.orekit.orbits.OrbitType
Tells if the orbit type is based on position angles or not.
isPreviousStateInterpolated() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator
Determines if the previous state is computed directly by the integrator, or if it is calculated using interpolation.
isPseudoInertial() - Method in class org.orekit.frames.Frame
Check if the frame is pseudo-inertial.
isQuasiInertial() - Method in enum org.orekit.files.ccsds.definitions.OrbitRelativeFrame
Check if frame should be treated as inertial.
isQuasiInertial() - Method in interface org.orekit.frames.encounter.EncounterLOF
Get flag that indicates if current local orbital frame shall be treated as pseudo-inertial.
isQuasiInertial() - Method in interface org.orekit.frames.LOF
Get flag that indicates if current local orbital frame shall be treated as pseudo-inertial.
isReceiveAmplitudeCorrectionApplied() - Method in class org.orekit.files.ilrs.CRDHeader
Get the receive amplitude correction applied indicator.
isRefractionCorrected() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement
Get the flag indicating if the refraction is corrected.
isSelected() - Method in class org.orekit.utils.ParameterDriver
Check if parameter is selected.
isSignalInteger() - Method in class org.orekit.gnss.metric.messages.common.PhaseBias
Get the flag indicating is signal has integer property.
isSimpleEop() - Method in class org.orekit.frames.EOPHistory
Determine if this history uses simplified EOP corrections.
isSimpleEOP() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Check if tidal effects are ignored when interpolating EOP.
isSimpleEOP() - Method in class org.orekit.files.ccsds.utils.ContextBinding
Get EOP interpolation method.
isSimpleEOP() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser
Get EOP interpolation method.
isSpacecraftBodyRate() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Check if rates are specified in spacecraft body frame.
isSpacecraftBodyRate() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler
Check if rates are specified in spacecraft body frame.
isSpacecraftTimeSimplified() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
Get the spacecraft time simplified flag.
isStart() - Method in class org.orekit.utils.DateDriver
Check if driver corresponds to a start date.
isStationSystemDelayApplied() - Method in class org.orekit.files.ilrs.CRDHeader
Get the station system delay applied indicator.
isSupported(String) - Method in interface org.orekit.utils.ParameterDriversProvider
Check if a parameter is supported.
isSupported(DataProvider) - Method in class org.orekit.data.DataProvidersManager
Check if some provider is supported.
isTime() - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
Check if a field is a time field.
isTransponderDelayApplied() - Method in class org.orekit.files.ilrs.CRDHeader
Get the spacecraft system delay applied (transponders) indicator.
isTroposphericRefractionApplied() - Method in class org.orekit.files.ilrs.CRDHeader
Get the tropospheric refraction correction applied indicator.
isTwoWay() - Method in class org.orekit.estimation.measurements.GroundReceiverMeasurement
Check if the instance represents a two-way measurement.
isTwoWay() - Method in class org.orekit.estimation.measurements.InterSatellitesRange
Check if the instance represents a two-way measurement.
isValid(int) - Method in class org.orekit.frames.ITRFVersionLoader.ITRFVersionConfiguration
Check if configuration entry is valid for a date.
isVariable(DerivativeStructure, int) - Method in class org.orekit.forces.drag.AbstractDragForceModel
Check if a derivative represents a specified variable.
isVariable(Gradient, int) - Method in class org.orekit.forces.drag.AbstractDragForceModel
Check if a derivative represents a specified variable.
ITRF - org.orekit.files.ccsds.definitions.CelestialBodyFrame
Latest International Terrestrial Reference Frame.
ITRF_1988 - org.orekit.frames.ITRFVersion
Constant for ITRF 88.
ITRF_1989 - org.orekit.frames.ITRFVersion
Constant for ITRF 89.
ITRF_1990 - org.orekit.frames.ITRFVersion
Constant for ITRF 1990.
ITRF_1991 - org.orekit.frames.ITRFVersion
Constant for ITRF 1991.
ITRF_1992 - org.orekit.frames.ITRFVersion
Constant for ITRF 1992.
ITRF_1993 - org.orekit.frames.ITRFVersion
Constant for ITRF 1993.
ITRF_1994 - org.orekit.frames.ITRFVersion
Constant for ITRF 1994.
ITRF_1996 - org.orekit.frames.ITRFVersion
Constant for ITRF 1996.
ITRF_1997 - org.orekit.frames.ITRFVersion
Constant for ITRF 1997.
ITRF_2000 - org.orekit.frames.ITRFVersion
Constant for ITRF 2000.
ITRF_2005 - org.orekit.frames.ITRFVersion
Constant for ITRF 2005.
ITRF_2008 - org.orekit.frames.ITRFVersion
Constant for ITRF 2008.
ITRF_2008_TO_ITRF_1988 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2008 To ITRF 88.
ITRF_2008_TO_ITRF_1989 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2008 To ITRF 89.
ITRF_2008_TO_ITRF_1990 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2008 To ITRF 90.
ITRF_2008_TO_ITRF_1991 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2008 To ITRF 91.
ITRF_2008_TO_ITRF_1992 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2008 To ITRF 92.
ITRF_2008_TO_ITRF_1993 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2008 To ITRF 93.
ITRF_2008_TO_ITRF_1994 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2008 To ITRF 94.
ITRF_2008_TO_ITRF_1996 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2008 To ITRF 96.
ITRF_2008_TO_ITRF_1997 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2008 To ITRF 97.
ITRF_2008_TO_ITRF_2000 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2008 To ITRF 2000.
ITRF_2008_TO_ITRF_2005 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2008 To ITRF 2005.
ITRF_2014 - org.orekit.frames.ITRFVersion
Constant for ITRF 2014.
ITRF_2014_TO_ITRF_1988 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2014 To ITRF 88.
ITRF_2014_TO_ITRF_1989 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2014 To ITRF 89.
ITRF_2014_TO_ITRF_1990 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2014 To ITRF 90.
ITRF_2014_TO_ITRF_1991 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2014 To ITRF 91.
ITRF_2014_TO_ITRF_1992 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2014 To ITRF 92.
ITRF_2014_TO_ITRF_1993 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2014 To ITRF 93.
ITRF_2014_TO_ITRF_1994 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2014 To ITRF 94.
ITRF_2014_TO_ITRF_1996 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2014 To ITRF 96.
ITRF_2014_TO_ITRF_1997 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2014 To ITRF 97.
ITRF_2014_TO_ITRF_2000 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2014 To ITRF 2000.
ITRF_2014_TO_ITRF_2005 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2014 To ITRF 2005.
ITRF_2014_TO_ITRF_2008 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2014 To ITRF 2008.
ITRF_2020 - org.orekit.frames.ITRFVersion
Constant for ITRF 2020.
ITRF_2020_TO_ITRF_1988 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2020 To ITRF 88.
ITRF_2020_TO_ITRF_1989 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2020 To ITRF 89.
ITRF_2020_TO_ITRF_1990 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2020 To ITRF 90.
ITRF_2020_TO_ITRF_1991 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2020 To ITRF 91.
ITRF_2020_TO_ITRF_1992 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2020 To ITRF 92.
ITRF_2020_TO_ITRF_1993 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2020 To ITRF 93.
ITRF_2020_TO_ITRF_1994 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2020 To ITRF 94.
ITRF_2020_TO_ITRF_1996 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2020 To ITRF 96.
ITRF_2020_TO_ITRF_1997 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2020 To ITRF 97.
ITRF_2020_TO_ITRF_2000 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2020 To ITRF 2000.
ITRF_2020_TO_ITRF_2005 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2020 To ITRF 2005.
ITRF_2020_TO_ITRF_2008 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2020 To ITRF 2008.
ITRF_2020_TO_ITRF_2014 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2020 To ITRF 2014.
ITRF_CIO_CONV_1996_ACCURATE_EOP - org.orekit.frames.Predefined
CIO-based ITRF, IERS 1996 conventions with accurate EOP interpolation.
ITRF_CIO_CONV_1996_SIMPLE_EOP - org.orekit.frames.Predefined
CIO-based ITRF, IERS 1996 conventions with simple EOP interpolation.
ITRF_CIO_CONV_2003_ACCURATE_EOP - org.orekit.frames.Predefined
CIO-based ITRF, IERS 2003 conventions with accurate EOP interpolation.
ITRF_CIO_CONV_2003_SIMPLE_EOP - org.orekit.frames.Predefined
CIO-based ITRF, IERS 2003 conventions with simple EOP interpolation.
ITRF_CIO_CONV_2010_ACCURATE_EOP - org.orekit.frames.Predefined
CIO-based ITRF, IERS 2010 conventions with accurate EOP interpolation.
ITRF_CIO_CONV_2010_SIMPLE_EOP - org.orekit.frames.Predefined
CIO-based ITRF, IERS 2010 conventions with simple EOP interpolation.
ITRF_EQUINOX_CONV_1996_ACCURATE_EOP - org.orekit.frames.Predefined
Equinox-based ITRF, IERS 1996 conventions with accurate EOP interpolation.
ITRF_EQUINOX_CONV_1996_SIMPLE_EOP - org.orekit.frames.Predefined
Equinox-based ITRF, IERS 1996 conventions with simple EOP interpolation.
ITRF_EQUINOX_CONV_2003_ACCURATE_EOP - org.orekit.frames.Predefined
Equinox-based ITRF, IERS 2003 conventions with accurate EOP interpolation.
ITRF_EQUINOX_CONV_2003_SIMPLE_EOP - org.orekit.frames.Predefined
Equinox-based ITRF, IERS 2003 conventions with simple EOP interpolation.
ITRF_EQUINOX_CONV_2010_ACCURATE_EOP - org.orekit.frames.Predefined
Equinox-based ITRF, IERS 2010 conventions with accurate EOP interpolation.
ITRF_EQUINOX_CONV_2010_SIMPLE_EOP - org.orekit.frames.Predefined
Equinox-based ITRF, IERS 2010 conventions with simple EOP interpolation.
ITRF_VERSIONS_PREFIX_ONLY - org.orekit.errors.OrekitMessages
ITRF_VERSIONS_PREFIX_ONLY.
ITRF1988 - org.orekit.files.ccsds.definitions.CelestialBodyFrame
International Terrestrial Reference Frame 1988.
ITRF1989 - org.orekit.files.ccsds.definitions.CelestialBodyFrame
International Terrestrial Reference Frame 1989.
ITRF1990 - org.orekit.files.ccsds.definitions.CelestialBodyFrame
International Terrestrial Reference Frame 1990.
ITRF1991 - org.orekit.files.ccsds.definitions.CelestialBodyFrame
International Terrestrial Reference Frame 1991.
ITRF1992 - org.orekit.files.ccsds.definitions.CelestialBodyFrame
International Terrestrial Reference Frame 1992.
ITRF1993 - org.orekit.files.ccsds.definitions.CelestialBodyFrame
International Terrestrial Reference Frame 1993.
ITRF1994 - org.orekit.files.ccsds.definitions.CelestialBodyFrame
International Terrestrial Reference Frame 1994.
ITRF1996 - org.orekit.files.ccsds.definitions.CelestialBodyFrame
International Terrestrial Reference Frame 1996.
ITRF1997 - org.orekit.files.ccsds.definitions.CelestialBodyFrame
International Terrestrial Reference Frame 1997.
ITRF2000 - org.orekit.files.ccsds.definitions.CelestialBodyFrame
International Terrestrial Reference Frame 2000.
ITRF2005 - org.orekit.files.ccsds.definitions.CelestialBodyFrame
International Terrestrial Reference Frame 2005.
ITRF2008 - org.orekit.files.ccsds.definitions.CelestialBodyFrame
International Terrestrial Reference Frame 2008.
ITRF2014 - org.orekit.files.ccsds.definitions.CelestialBodyFrame
International Terrestrial Reference Frame 2014.
ITRF2020 - org.orekit.files.ccsds.definitions.CelestialBodyFrame
International Terrestrial Reference Frame 2020.
ITRFVersion - Enum in org.orekit.frames
Enumerate for ITRF versions.
ITRFVersion.Converter - Class in org.orekit.frames
Specialized transform provider between ITRF frames.
ITRFVersionConfiguration(String, ITRFVersion, int, int) - Constructor for class org.orekit.frames.ITRFVersionLoader.ITRFVersionConfiguration
Simple constructor.
ITRFVersionLoader - Class in org.orekit.frames
Loader for ITRF version configuration file.
ITRFVersionLoader() - Constructor for class org.orekit.frames.ITRFVersionLoader
Build a loader for ITRF version configuration file using the default name.
ITRFVersionLoader(String) - Constructor for class org.orekit.frames.ITRFVersionLoader
Build a loader for ITRF version configuration file.
ITRFVersionLoader(String, DataProvidersManager) - Constructor for class org.orekit.frames.ITRFVersionLoader
Build a loader for ITRF version configuration file.
ITRFVersionLoader.ITRFVersionConfiguration - Class in org.orekit.frames
ITRF version configuration entry.
ItrfVersionProvider - Interface in org.orekit.frames
Interface for retrieving the ITRF version for a given set of EOP data.
IXX - org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalPropertiesKey
Moment of inertia about X-axis.
IXX - org.orekit.files.ccsds.ndm.adm.apm.InertiaKey
Moment of inertia about X-axis.
IXX - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Moment of inertia about X-axis.
IXY - org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalPropertiesKey
Inertia cross product of the X and Y axes.
IXY - org.orekit.files.ccsds.ndm.adm.apm.InertiaKey
Inertia cross product of the X and Y axes.
IXY - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Inertia cross product of the X and Y axes.
IXZ - org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalPropertiesKey
Inertia cross product of the X and Z axes.
IXZ - org.orekit.files.ccsds.ndm.adm.apm.InertiaKey
Inertia cross product of the X and Z axes.
IXZ - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Inertia cross product of the X and Z axes.
IYY - org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalPropertiesKey
Moment of inertia about Y-axis.
IYY - org.orekit.files.ccsds.ndm.adm.apm.InertiaKey
Moment of inertia about Y-axis.
IYY - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Moment of inertia about Y-axis.
IYZ - org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalPropertiesKey
Inertia cross product of the Y and Z axes.
IYZ - org.orekit.files.ccsds.ndm.adm.apm.InertiaKey
Inertia cross product of the Y and Z axes.
IYZ - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Inertia cross product of the Y and Z axes.
IZZ - org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalPropertiesKey
Moment of inertia about Z-axis.
IZZ - org.orekit.files.ccsds.ndm.adm.apm.InertiaKey
Moment of inertia about Z-axis.
IZZ - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Moment of inertia about Z-axis.

J

J01 - org.orekit.gnss.Frequency
QZSS L1 (1575.42 MHz).
J02 - org.orekit.gnss.Frequency
QZSS L2 (1227.6 MHz).
J05 - org.orekit.gnss.Frequency
QZSS L5 (1176.45 MHz).
J06 - org.orekit.gnss.Frequency
QZSS LEX (1278.75 MHz).
J2000 - org.orekit.files.ccsds.definitions.CelestialBodyFrame
Earth Mean Equator and Equinox of J2000.
J2000 - org.orekit.files.stk.STKEphemerisFile.STKCoordinateSystem
Mean equator and mean equinox of the J2000 epoch.
J2000_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
J2000.0 Reference epoch: 2000-01-01T12:00:00 Terrestrial Time (not UTC).
J2000_EPOCH - Static variable in class org.orekit.time.DateComponents
J2000.0 Reference epoch: 2000-01-01.
J2DifferentialEffect - Class in org.orekit.propagation.analytical
Analytical model for J2 effect.
J2DifferentialEffect(Orbit, Orbit, boolean, double, double, double) - Constructor for class org.orekit.propagation.analytical.J2DifferentialEffect
Simple constructor.
J2DifferentialEffect(Orbit, Orbit, boolean, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.J2DifferentialEffect
Simple constructor.
J2DifferentialEffect(SpacecraftState, AdapterPropagator.DifferentialEffect, boolean, double, double, double) - Constructor for class org.orekit.propagation.analytical.J2DifferentialEffect
Simple constructor.
J2DifferentialEffect(SpacecraftState, AdapterPropagator.DifferentialEffect, boolean, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.J2DifferentialEffect
Simple constructor.
J2OnlyPerturbation - Class in org.orekit.forces.gravity
J2-only force model.
J2OnlyPerturbation(double, double, double, Frame) - Constructor for class org.orekit.forces.gravity.J2OnlyPerturbation
Constructor with constant J2.
J2OnlyPerturbation(double, double, TimeScalarFunction, Frame) - Constructor for class org.orekit.forces.gravity.J2OnlyPerturbation
Constructor with TimeScalarFunction.
J2OnlyPerturbation(UnnormalizedSphericalHarmonicsProvider, Frame) - Constructor for class org.orekit.forces.gravity.J2OnlyPerturbation
Constructor with spherical harmonics provider.
J2SquaredModel - Interface in org.orekit.propagation.semianalytical.dsst.forces
Semi-analytical J2-squared model.
JacobianPropagatorConverter - Class in org.orekit.propagation.conversion
Propagator converter using the real Jacobian.
JacobianPropagatorConverter(NumericalPropagatorBuilder, double, int) - Constructor for class org.orekit.propagation.conversion.JacobianPropagatorConverter
Simple constructor.
JacobiPolynomials - Class in org.orekit.propagation.semianalytical.dsst.utilities
Provider of the Jacobi polynomials Plv,w.
JANUARY - org.orekit.time.Month
January.
JAPAN - org.orekit.files.rinex.navigation.RegionCode
Japan area (for QZSS only).
JAVA_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Java Reference epoch: 1970-01-01T00:00:00 Universal Time Coordinate.
JAVA_EPOCH - Static variable in class org.orekit.time.DateComponents
Java Reference epoch: 1970-01-01.
JB2008 - Class in org.orekit.models.earth.atmosphere
This is the realization of the Jacchia-Bowman 2008 atmospheric model.
JB2008(JB2008InputParameters, PVCoordinatesProvider, BodyShape) - Constructor for class org.orekit.models.earth.atmosphere.JB2008
Constructor with space environment information for internal computation.
JB2008(JB2008InputParameters, PVCoordinatesProvider, BodyShape, TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.JB2008
Constructor with space environment information for internal computation.
JB2008InputParameters - Interface in org.orekit.models.earth.atmosphere
Interface for solar activity and magnetic activity data.
JB2008SpaceEnvironmentData - Class in org.orekit.models.earth.atmosphere.data
This class provides a container for the solar indices data required by the JB2008 atmospheric model.
JB2008SpaceEnvironmentData(String, String) - Constructor for class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData
Simple constructor.
JB2008SpaceEnvironmentData(String, String, DataProvidersManager, TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData
Constructor that allows specifying the source of the SOLFSMY space weather file.
JB2008SpaceEnvironmentData(DataSource, DataSource) - Constructor for class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData
Simple constructor.
JB2008SpaceEnvironmentData(DataSource, DataSource, TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData
Constructor that allows specifying the source of the SOLFSMY space weather file.
JD_TO_MJD - Static variable in class org.orekit.time.DateComponents
Offset between julian day epoch and modified julian day epoch.
JOULE - Static variable in class org.orekit.utils.units.Unit
Joule unit.
JPL_SSD_ASTRONOMICAL_UNIT - Static variable in interface org.orekit.utils.Constants
Astronomical Unit: 149597870691 m.
JPL_SSD_EARTH_GM - Static variable in interface org.orekit.utils.Constants
Earth attraction coefficient (m³/s²).
JPL_SSD_EARTH_MOON_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Earth/Moon mass ratio: 81.30059.
JPL_SSD_EARTH_PLUS_MOON_GM - Static variable in interface org.orekit.utils.Constants
Sun/(Earth + Moon) attraction coefficient (m³/s²).
JPL_SSD_GAUSSIAN_GRAVITATIONAL_CONSTANT - Static variable in interface org.orekit.utils.Constants
Gaussian gravitational constant: 0.01720209895 √(AU³/d²).
JPL_SSD_JUPITER_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants
Sun/(Jupiter system) ttraction coefficient (m³/s²).
JPL_SSD_MARS_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants
Sun/(Mars system) attraction coefficient (m³/s²).
JPL_SSD_MERCURY_GM - Static variable in interface org.orekit.utils.Constants
Sun/Mercury attraction coefficient (m³/s²).
JPL_SSD_MOON_GM - Static variable in interface org.orekit.utils.Constants
Moon attraction coefficient (m³/s²).
JPL_SSD_NEPTUNE_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants
Sun/(Neptune system) attraction coefficient (m³/s²).
JPL_SSD_PLUTO_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants
Sun/(Pluto system) ttraction coefficient (m³/s²).
JPL_SSD_SATURN_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants
Sun/(Saturn system) attraction coefficient (m³/s²).
JPL_SSD_SUN_EARTH_PLUS_MOON_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Sun/(Earth + Moon) mass ratio: 328900.56.
JPL_SSD_SUN_GM - Static variable in interface org.orekit.utils.Constants
Sun attraction coefficient (m³/s²).
JPL_SSD_SUN_JUPITER_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Sun/(Jupiter system) mass ratio: 1047.3486.
JPL_SSD_SUN_MARS_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Sun/(Mars system) mass ratio: 3098708.0.
JPL_SSD_SUN_MERCURY_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Sun/Mercury mass ratio: 6023600.
JPL_SSD_SUN_NEPTUNE_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Sun/(Neptune system) mass ratio: 19412.24.
JPL_SSD_SUN_PLUTO_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Sun/(Pluto system) mass ratio: 1.35e8.
JPL_SSD_SUN_SATURN_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Sun/(Saturn system) mass ratio: 3497.898.
JPL_SSD_SUN_URANUS_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Sun/(Uranus system) mass ratio: 22902.98.
JPL_SSD_SUN_VENUS_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Sun/Venus mass ratio: 408523.71.
JPL_SSD_URANUS_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants
Sun/(Uranus system) attraction coefficient (m³/s²).
JPL_SSD_VENUS_GM - Static variable in interface org.orekit.utils.Constants
Sun/Venus attraction coefficient (m³/s²).
JPLEphemeridesLoader - Class in org.orekit.bodies
Loader for JPL ephemerides binary files (DE 4xx) and similar formats (INPOP 06/08/10).
JPLEphemeridesLoader(String, JPLEphemeridesLoader.EphemerisType) - Constructor for class org.orekit.bodies.JPLEphemeridesLoader
Create a loader for JPL ephemerides binary files.
JPLEphemeridesLoader(String, JPLEphemeridesLoader.EphemerisType, DataProvidersManager, TimeScales, Frame) - Constructor for class org.orekit.bodies.JPLEphemeridesLoader
Create a loader for JPL ephemerides binary files.
JPLEphemeridesLoader.EphemerisType - Enum in org.orekit.bodies
List of supported ephemerides types.
JPLEphemeridesLoader.RawPVProvider - Interface in org.orekit.bodies
Interface for raw position-velocity retrieval.
JULIAN_CENTURY - Static variable in interface org.orekit.utils.Constants
Duration of a Julian century: 36525 Constants.JULIAN_DAY.
JULIAN_DAY - Static variable in interface org.orekit.utils.Constants
Duration of a mean solar day: 86400.0 s.
JULIAN_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Reference epoch for julian dates: -4712-01-01T12:00:00 Terrestrial Time.
JULIAN_EPOCH - Static variable in class org.orekit.time.DateComponents
Reference epoch for julian dates: -4712-01-01.
JULIAN_EPOCH - Static variable in class org.orekit.time.DateTimeComponents
The Julian Epoch.
JULIAN_YEAR - Static variable in interface org.orekit.utils.Constants
Duration of a Julian year: 365.25 Constants.JULIAN_DAY.
JULY - org.orekit.time.Month
July.
JUNE - org.orekit.time.Month
June.
JUPITER - org.orekit.bodies.JPLEphemeridesLoader.EphemerisType
Constant for Jupiter.
JUPITER - org.orekit.files.ccsds.definitions.CenterName
Jupiter body.
JUPITER - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Jupiter.

K

K - Static variable in class org.orekit.propagation.analytical.intelsat.IntelsatElevenElements
PI over 360.
K1 - Static variable in class org.orekit.models.earth.displacement.Tide
K₁ tide.
K2 - Static variable in class org.orekit.models.earth.displacement.Tide
K₂ tide.
KalmanEstimation - Interface in org.orekit.estimation.sequential
Interface for accessing Kalman filter estimations.
KalmanEstimator - Class in org.orekit.estimation.sequential
Implementation of a Kalman filter to perform orbit determination.
KalmanEstimatorBuilder - Class in org.orekit.estimation.sequential
Builder for a Kalman filter estimator.
KalmanEstimatorBuilder() - Constructor for class org.orekit.estimation.sequential.KalmanEstimatorBuilder
Default constructor.
KalmanEstimatorUtil - Class in org.orekit.estimation.sequential
Utility class for Kalman Filter.
KalmanModel - Class in org.orekit.estimation.sequential
Class defining the process model dynamics to use with a KalmanEstimator.
KalmanModel(List<PropagatorBuilder>, List<CovarianceMatrixProvider>, ParameterDriversList, CovarianceMatrixProvider) - Constructor for class org.orekit.estimation.sequential.KalmanModel
Kalman process model constructor.
KalmanObserver - Interface in org.orekit.estimation.sequential
Observer for Kalman filter estimations.
KASS - org.orekit.files.rinex.navigation.SbasId
Korea Augmentation Satellite System.
KEPLERIAN - org.orekit.files.ccsds.ndm.odm.ocm.OrbitElementsType
Keplerian 6-element classical set (a, e, i, Ω, ω, ν).
KEPLERIAN - org.orekit.orbits.OrbitType
Type for orbital representation in KeplerianOrbit and FieldKeplerianOrbit parameters.
KeplerianAnomalyUtility - Class in org.orekit.orbits
Utility methods for converting between different Keplerian anomalies.
KeplerianElements - Class in org.orekit.files.ccsds.ndm.odm
Container for Keplerian elements.
KeplerianElements() - Constructor for class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Simple constructor.
KeplerianElementsKey - Enum in org.orekit.files.ccsds.ndm.odm
Keys for Keplerian elements entries.
KEPLERIANMEAN - org.orekit.files.ccsds.ndm.odm.ocm.OrbitElementsType
Keplerian 6-element classical set (a, e, i, Ω, ω, M).
KeplerianMotionCartesianUtility - Class in org.orekit.orbits
Utility class to predict position and velocity under Keplerian motion, using lightweight routines based on Cartesian coordinates.
KeplerianOrbit - Class in org.orekit.orbits
This class handles traditional Keplerian orbital parameters.
KeplerianOrbit(double, double, double, double, double, double, double, double, double, double, double, double, PositionAngleType, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.KeplerianOrbit
Creates a new instance with cached position angle same as value inputted.
KeplerianOrbit(double, double, double, double, double, double, double, double, double, double, double, double, PositionAngleType, PositionAngleType, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.KeplerianOrbit
Creates a new instance.
KeplerianOrbit(double, double, double, double, double, double, PositionAngleType, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.KeplerianOrbit
Creates a new instance without derivatives and with cached position angle same as value inputted.
KeplerianOrbit(double, double, double, double, double, double, PositionAngleType, PositionAngleType, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.KeplerianOrbit
Creates a new instance.
KeplerianOrbit(Orbit) - Constructor for class org.orekit.orbits.KeplerianOrbit
Constructor from any kind of orbital parameters.
KeplerianOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.KeplerianOrbit
Constructor from Cartesian parameters.
KeplerianOrbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.KeplerianOrbit
Constructor from Cartesian parameters.
KeplerianPropagator - Class in org.orekit.propagation.analytical
Simple Keplerian orbit propagator.
KeplerianPropagator(Orbit) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator
Build a propagator from orbit only.
KeplerianPropagator(Orbit, double) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator
Build a propagator from orbit and central attraction coefficient μ.
KeplerianPropagator(Orbit, AttitudeProvider) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator
Build a propagator from orbit and attitude provider.
KeplerianPropagator(Orbit, AttitudeProvider, double) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator
Build a propagator from orbit, attitude provider and central attraction coefficient μ.
KeplerianPropagator(Orbit, AttitudeProvider, double, double) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator
Build propagator from orbit, attitude provider, central attraction coefficient μ and mass.
KeplerianPropagatorBuilder - Class in org.orekit.propagation.conversion
Builder for Keplerian propagator.
KeplerianPropagatorBuilder(Orbit, PositionAngleType, double) - Constructor for class org.orekit.propagation.conversion.KeplerianPropagatorBuilder
Build a new instance.
KeplerianPropagatorBuilder(Orbit, PositionAngleType, double, AttitudeProvider) - Constructor for class org.orekit.propagation.conversion.KeplerianPropagatorBuilder
Build a new instance.
KG_M2 - Static variable in class org.orekit.files.ccsds.definitions.Units
kg.m² unit.
KILOGRAM - Static variable in class org.orekit.utils.units.Unit
Kilogram unit.
KILOMETRE - Static variable in class org.orekit.utils.units.Unit
Kilometre unit.
KILOMETRES_2_TO_METRES_2 - Static variable in class org.orekit.utils.units.UnitsConverter
Square kilometres to square metres converter.
KILOMETRES_TO_METRES - Static variable in class org.orekit.utils.units.UnitsConverter
Kilometres to metres converter.
KinematicTransform - Interface in org.orekit.frames
A transform that only includes translation and rotation as well as their respective rates.
KLOBUCHAR_ALPHA_BETA_NOT_AVAILABLE_FOR_DATE - org.orekit.errors.OrekitMessages
KLOBUCHAR_ALPHA_BETA_NOT_AVAILABLE_FOR_DATE.
KLOBUCHAR_ALPHA_BETA_NOT_LOADED - org.orekit.errors.OrekitMessages
KLOBUCHAR_ALPHA_BETA_NOT_LOADED.
KlobucharIonoCoefficientsLoader - Class in org.orekit.models.earth.ionosphere
Loads Klobuchar-Style ionospheric coefficients a given input stream.
KlobucharIonoCoefficientsLoader() - Constructor for class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader
Constructor with default supported names.
KlobucharIonoCoefficientsLoader(String) - Constructor for class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader
Constructor with supported names given by user.
KlobucharIonoCoefficientsLoader(String, DataProvidersManager) - Constructor for class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader
Constructor that uses user defined supported names and data context.
KlobucharIonoModel - Class in org.orekit.models.earth.ionosphere
Klobuchar ionospheric delay model.
KlobucharIonoModel(double[], double[]) - Constructor for class org.orekit.models.earth.ionosphere.KlobucharIonoModel
Create a new Klobuchar ionospheric delay model, when a single frequency system is used.
KlobucharIonoModel(double[], double[], TimeScale) - Constructor for class org.orekit.models.earth.ionosphere.KlobucharIonoModel
Create a new Klobuchar ionospheric delay model, when a single frequency system is used.
km - org.orekit.files.ccsds.ndm.tdm.RangeUnits
Range in kilometers.
KM_PER_S - Static variable in class org.orekit.files.ccsds.definitions.Units
Kilometers per second units.
KM_PER_S - Static variable in class org.orekit.gnss.metric.parser.Units
Kilometers par second units.
KM_PER_S2 - Static variable in class org.orekit.files.ccsds.definitions.Units
Kilometers per square second units.
KM_PER_S2 - Static variable in class org.orekit.gnss.metric.parser.Units
Kilometers par square second units.
KM2 - Static variable in class org.orekit.files.ccsds.definitions.Units
Square kilometers units.
KM2_PER_S - Static variable in class org.orekit.files.ccsds.definitions.Units
Square kilometers per second units.
KM2_PER_S2 - Static variable in class org.orekit.files.ccsds.definitions.Units
Square kilometers per square second units.
KM3_P_S2_TO_M3_P_S2 - Static variable in class org.orekit.utils.units.UnitsConverter
km³/s² to m³/s² converter.
KM3_PER_S2 - Static variable in class org.orekit.files.ccsds.definitions.Units
km³/s² unit.
KnockeRediffusedForceModel - Class in org.orekit.forces.radiation
The Knocke Earth Albedo and IR emission force model.
KnockeRediffusedForceModel(ExtendedPVCoordinatesProvider, RadiationSensitive, double, double) - Constructor for class org.orekit.forces.radiation.KnockeRediffusedForceModel
Default Constructor.
KnockeRediffusedForceModel(ExtendedPVCoordinatesProvider, RadiationSensitive, double, double, TimeScale) - Constructor for class org.orekit.forces.radiation.KnockeRediffusedForceModel
General constructor.
KVN - org.orekit.files.ccsds.utils.FileFormat
Key-Value Notation format.
KVN_PADDING_WIDTH - Static variable in class org.orekit.files.ccsds.ndm.adm.acm.AcmWriter
Padding width for aligning the '=' sign.
KVN_PADDING_WIDTH - Static variable in class org.orekit.files.ccsds.ndm.adm.aem.AemWriter
Padding width for aligning the '=' sign.
KVN_PADDING_WIDTH - Static variable in class org.orekit.files.ccsds.ndm.adm.apm.ApmWriter
Padding width for aligning the '=' sign.
KVN_PADDING_WIDTH - Static variable in class org.orekit.files.ccsds.ndm.cdm.CdmWriter
Padding width for aligning the '=' sign.
KVN_PADDING_WIDTH - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.OcmWriter
Padding width for aligning the '=' sign.
KVN_PADDING_WIDTH - Static variable in class org.orekit.files.ccsds.ndm.odm.oem.OemWriter
Padding width for aligning the '=' sign.
KVN_PADDING_WIDTH - Static variable in class org.orekit.files.ccsds.ndm.odm.omm.OmmWriter
Padding width for aligning the '=' sign.
KVN_PADDING_WIDTH - Static variable in class org.orekit.files.ccsds.ndm.odm.opm.OpmWriter
Padding width for aligning the '=' sign.
KVN_PADDING_WIDTH - Static variable in class org.orekit.files.ccsds.ndm.tdm.TdmWriter
Padding width for aligning the '=' sign.
KvnGenerator - Class in org.orekit.files.ccsds.utils.generation
Generator for Key-Value Notation CCSDS messages.
KvnGenerator(Appendable, int, String, double, int) - Constructor for class org.orekit.files.ccsds.utils.generation.KvnGenerator
Simple constructor.
KvnLexicalAnalyzer - Class in org.orekit.files.ccsds.utils.lexical
Lexical analyzer for Key-Value Notation CCSDS messages.
KvnLexicalAnalyzer(DataSource) - Constructor for class org.orekit.files.ccsds.utils.lexical.KvnLexicalAnalyzer
Simple constructor.
KvnStructureKey - Enum in org.orekit.files.ccsds.section
Keys for FileFormat.KVN format structure.
KvnStructureProcessingState - Class in org.orekit.files.ccsds.section
ProcessingState for structure of FileFormat.KVN CCSDS Messages.
KvnStructureProcessingState(AbstractConstituentParser<?, ?, ?>) - Constructor for class org.orekit.files.ccsds.section.KvnStructureProcessingState
Simple constructor.

L

L - org.orekit.gnss.SignalCode
GPS L1C (P) and L2C (L) / QZSS L1C (P), L2C (L) and L code.
L0 - org.orekit.gnss.ObservationType
Carrier-phase for Rinex3.
L1 - org.orekit.gnss.metric.ntrip.CarrierPhase
Yes, L1.
L1 - org.orekit.gnss.ObservationType
Carrier-phase GPS L1 / GLONASS G1 / Galileo E2-L1-E1 / SBAS L1 for Rinex2.
L1 - org.orekit.utils.LagrangianPoints
Lagrangian Point L1.
L1_L2 - org.orekit.gnss.metric.ntrip.CarrierPhase
Yes, L1&L2.
L1A - org.orekit.gnss.ObservationType
Carrier-phase Galileo E1 A / Beidou B1 B1A for Rinex3.
L1B - org.orekit.gnss.ObservationType
Carrier-phase Galileo E1 I/NAV OS/CS/SoL / QZSS geo signal for Rinex3.
L1C - org.orekit.gnss.ObservationType
Carrier-phase GPS L1 C/A / GLONASS G1 C/A / Galileo E1 C / SBAS L1 C/A / QZSS L1 C/A for Rinex3.
L1D - org.orekit.gnss.ObservationType
Carrier-phase Beidou B1 Data for Rinex3.
L1E - org.orekit.gnss.ObservationType
Carrier-phase QZSS L1 C/B for Rinex4.
L1Frame - Class in org.orekit.frames
Class to create a L1 centered frame with L1TransformProvider.
L1Frame(CelestialBody, CelestialBody) - Constructor for class org.orekit.frames.L1Frame
Simple constructor.
L1I - org.orekit.gnss.ObservationType
Carrier-phase Beidou B1 I for Rinex3.
L1L - org.orekit.gnss.ObservationType
Carrier-phase GPS L1 L1C(P) / QZSS L1 L1C(P) for Rinex3, Beidou B1A for Rinex3.03.
L1M - org.orekit.gnss.ObservationType
Carrier-phase GPS L2 M for Rinex3.
L1N - org.orekit.gnss.ObservationType
Carrier-phase GPS L1 codeless for Rinex3.
L1P - org.orekit.gnss.ObservationType
Carrier-phase GPS L2 P(AS off) / GLONASS G2 P / Beidou B1 Pilot for Rinex3.
L1S - org.orekit.gnss.ObservationType
Carrier-phase GPS L1 L1C(D) / QZSS L1 L1C(D) for Rinex3, Beidou B1A for Rinex3.03.
L1TransformProvider - Class in org.orekit.frames
L1 Transform provider for a frame on the L1 Lagrange point of two celestial bodies.
L1TransformProvider(CelestialBody, CelestialBody) - Constructor for class org.orekit.frames.L1TransformProvider
Simple constructor.
L1W - org.orekit.gnss.ObservationType
Carrier-phase GPS L1 Z-tracking and similar (AS on) for Rinex3.
L1X - org.orekit.gnss.ObservationType
Carrier-phase GPS L1 L1C (D+P) / Galileo E1 B+C / QZSS L1 L1C(D+P) / Beidou B1 Data+Pilot for Rinex3.
L1Y - org.orekit.gnss.ObservationType
Carrier-phase GPS L1 Y for Rinex3.
L1Z - org.orekit.gnss.ObservationType
Carrier-phase Galileo E1 C1Z A+B+C / QZSS L1 L1-SAIF for Rinex3, Beidou B1A for Rinex3.03.
L2 - org.orekit.gnss.ObservationType
Carrier-phase GPS L2 / GLONASS G2 / Beidou B02 for Rinex2.
L2 - org.orekit.utils.LagrangianPoints
Lagrangian Point L2.
L2C - org.orekit.gnss.ObservationType
Carrier-phase GPS L2 C/A / GLONASS G2 C/A for Rinex3.
L2D - org.orekit.gnss.ObservationType
Carrier-phase GPS L1(C/A)+(P2-P1) (semi-codeless) for Rinex3.
L2Frame - Class in org.orekit.frames
Class to create a L2 centered frame with L2TransformProvider.
L2Frame(CelestialBody, CelestialBody) - Constructor for class org.orekit.frames.L2Frame
Simple constructor.
L2I - org.orekit.gnss.ObservationType
Carrier-phase Beidou B1 I for Rinex3.03.
L2L - org.orekit.gnss.ObservationType
Carrier-phase GPS L2 L2C(L) / QZSS L2 L2C(2) for Rinex3.
L2M - org.orekit.gnss.ObservationType
Carrier-phase GPS L2 M for Rinex3.
L2N - org.orekit.gnss.ObservationType
Carrier-phase GPS L2 codeless.
L2P - org.orekit.gnss.ObservationType
Carrier-phase GPS L2 P(AS off) / GLONASS G2 P for Rinex3.
L2Q - org.orekit.gnss.ObservationType
Carrier-phase Beidou B1 Q for Rinex3.03.
L2S - org.orekit.gnss.ObservationType
Carrier-phase GPS L2 L2C(M) / QZSS L2 L2C(M) for Rinex3.
L2W - org.orekit.gnss.ObservationType
Carrier-phase GPS L2 Z-tracking and similar (AS on) for Rinex3.
L2X - org.orekit.gnss.ObservationType
Carrier-phase GPS L2 L2C (M+L) / QZSS L2 L2C(M+L) for Rinex3, Beidou B1 I+Q for Rinex3.03.
L2Y - org.orekit.gnss.ObservationType
Carrier-phase GPS L2 Y for Rinex3.
L3 - org.orekit.utils.LagrangianPoints
Lagrangian Point L3.
L3I - org.orekit.gnss.ObservationType
Carrier-phase GLONASS G3 I for Rinex3.
L3Q - org.orekit.gnss.ObservationType
Carrier-phase GLONASS G3 Q for Rinex3.
L3X - org.orekit.gnss.ObservationType
Carrier-phase GLONASS G3 I+Q for Rinex3.
L4 - org.orekit.utils.LagrangianPoints
Lagrangian Point L4.
L4A - org.orekit.gnss.ObservationType
Carrier-phase GLONASS G1a L1OCd for Rinex3.
L4B - org.orekit.gnss.ObservationType
Carrier-phase GLONASS G1a L1OCp for Rinex3.
L4X - org.orekit.gnss.ObservationType
Carrier-phase GLONASS G1a L1OCd+L1OCd for Rinex3.
L5 - org.orekit.gnss.ObservationType
Carrier-phase GPS L5 / Galileo E5a / SBAS L5 for Rinex2.
L5 - org.orekit.utils.LagrangianPoints
Lagrangian Point L5.
L5A - org.orekit.gnss.ObservationType
Carrier-phase IRNSS L5 A for Rinex3.
L5B - org.orekit.gnss.ObservationType
Carrier-phase IRNSS L5 B for Rinex3.
L5C - org.orekit.gnss.ObservationType
Carrier-phase IRNSS L5 C for Rinex3.
L5D - org.orekit.gnss.ObservationType
Carrier-phase QZSS L5 / Beidou B2a Data D for Rinex3.
L5I - org.orekit.gnss.ObservationType
Carrier-phase GPS L5 I/ Galileo E5a F/NAV OS / SBAS L5 I / QZSS L5 I for Rinex3.
L5P - org.orekit.gnss.ObservationType
Carrier-phase QZSS L5 P / Beidou B2a Pilot for Rinex3.
L5Q - org.orekit.gnss.ObservationType
Carrier-phase GPS L5 Q/ Galileo E5a Q / SBAS L5 Q / QZSS L5 Q for Rinex3.
L5X - org.orekit.gnss.ObservationType
Carrier-phase GPS L5 I+Q/ Galileo E5a I+Q / SBAS L5 I+Q / QZSS L5 I+Q / IRNSS L5 B+C / Beidou B2a Data+Pilot for Rinex3.
L5Z - org.orekit.gnss.ObservationType
Carrier-phase QZSS L5 D+P for Rinex3.
L6 - org.orekit.gnss.ObservationType
Carrier-phase Galileo E6 / Beidou B03 for Rinex2.
L6A - org.orekit.gnss.ObservationType
Carrier-phase Galileo E6 A PRS / GLONASS G2a L2CSI / Beidou B3A for Rinex3.
L6B - org.orekit.gnss.ObservationType
Carrier-phase Galileo E6 B C/NAV CS / GLONASS G2a L2OCp for Rinex3.
L6C - org.orekit.gnss.ObservationType
Carrier-phase Galileo E6 C no data for Rinex3.
L6D - org.orekit.gnss.ObservationType
Carrier-phase Beidou B3A for Rinex3.
L6E - org.orekit.gnss.ObservationType
Carrier-phase QZSS L6E for Rinex3.
L6I - org.orekit.gnss.ObservationType
Carrier-phase Beidou B3 I for Rinex3.
L6L - org.orekit.gnss.ObservationType
Carrier-phase QZSS LEX(6) L for Rinex3.
L6P - org.orekit.gnss.ObservationType
Carrier-phase Beidou B3A for Rinex3.
L6Q - org.orekit.gnss.ObservationType
Carrier-phase Beidou B3 Q for Rinex3.
L6S - org.orekit.gnss.ObservationType
Carrier-phase QZSS LEX(6) S for Rinex3.
L6X - org.orekit.gnss.ObservationType
Carrier-phase Galileo E6 B+C / QZSS LEX(6) S+L / Beidou B3 I+Q / GLONASS G2a L2CSI+L2OCp for Rinex3.
L6Z - org.orekit.gnss.ObservationType
Carrier-phase Galileo E6 A+B+C / QZSS L6(D+E) / Beidou B3A for Rinex3.
L7 - org.orekit.gnss.ObservationType
Carrier-phase Galileo E5b / Beidou B02 for Rinex2.
L7D - org.orekit.gnss.ObservationType
Carrier-phase Beidou B2b Data for Rinex3.
L7I - org.orekit.gnss.ObservationType
Carrier-phase Galileo E5b I I/NAV OS/CS/SoL / Beidou B2 I for Rinex3.
L7P - org.orekit.gnss.ObservationType
Carrier-phase Beidou B2b Pilot for Rinex3.
L7Q - org.orekit.gnss.ObservationType
Carrier-phase Galileo Q no data / Beidou B2 Q for Rinex3.
L7X - org.orekit.gnss.ObservationType
Carrier-phase Galileo E5b I+Q / Beidou B2 I+Q for Rinex3.
L7Z - org.orekit.gnss.ObservationType
Carrier-phase Beidou B2b Data+Pilot for Rinex3.
L8 - org.orekit.gnss.ObservationType
Carrier-phase Galileo E5a+b for Rinex2.
L8D - org.orekit.gnss.ObservationType
Carrier-phase Beidou B2(B2a+B2b) Data for Rinex3.
L8I - org.orekit.gnss.ObservationType
Carrier-phase Galileo E5(E5a+E5b) I for Rinex3.
L8P - org.orekit.gnss.ObservationType
Carrier-phase Beidou B2(B2a+B2b) Pilot for Rinex3.
L8Q - org.orekit.gnss.ObservationType
Carrier-phase Galileo E5(E5a+E5b) Q for Rinex3.
L8X - org.orekit.gnss.ObservationType
Carrier-phase Galileo E5(E5a+E5b) I+Q / Beidou B2(B2a+B2b) Data+Pilot for Rinex3.
L9A - org.orekit.gnss.ObservationType
Carrier-phase IRNSS S A for Rinex3.
L9B - org.orekit.gnss.ObservationType
Carrier-phase IRNSS S B for Rinex3.
L9C - org.orekit.gnss.ObservationType
Carrier-phase IRNSS S C for Rinex3.
L9X - org.orekit.gnss.ObservationType
Carrier-phase IRNSS S B+C for Rinex3.
LA - org.orekit.gnss.ObservationType
Carrier-phase GPS L1 C/A / GLONASS G1 C/A for Rinex2.
LAAS_2015 - org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethodType
Probability of collision computing method described in :"SERRA, Romain, ARZELIER, Denis, JOLDES, Mioara, et al.
Laas2015 - Class in org.orekit.ssa.collision.shorttermencounter.probability.twod
Compute the probability of collision using the method described in : "SERRA, Romain, ARZELIER, Denis, JOLDES, Mioara, et al.
Laas2015() - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.Laas2015
Default constructor.
Laas2015(double, int) - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.Laas2015
Simple constructor.
LABEL_INDEX - Static variable in class org.orekit.files.rinex.utils.parsing.RinexUtils
Index of label in header lines.
LAGRANGE - org.orekit.files.ccsds.ndm.odm.oem.InterpolationMethod
Lagrange interpolation.
LagrangianPoints - Enum in org.orekit.utils
Enumerate for selecting which Lagrangian Point to consider in different classes.
LambdaMethod - Class in org.orekit.estimation.measurements.gnss
Decorrelation/reduction engine for LAMBDA method.
LambdaMethod() - Constructor for class org.orekit.estimation.measurements.gnss.LambdaMethod
Empty constructor.
LaserConfiguration() - Constructor for class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
Empty constructor.
LatitudeCrossingDetector - Class in org.orekit.propagation.events
Detector for geographic latitude crossing.
LatitudeCrossingDetector(double, double, OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.LatitudeCrossingDetector
Build a detector.
LatitudeCrossingDetector(OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.LatitudeCrossingDetector
Build a new detector.
LatitudeCrossingDetector(AdaptableInterval, double, int, EventHandler, OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.LatitudeCrossingDetector
Protected constructor with full parameters.
LatitudeExtremumDetector - Class in org.orekit.propagation.events
Detector for geographic latitude extremum.
LatitudeExtremumDetector(double, double, OneAxisEllipsoid) - Constructor for class org.orekit.propagation.events.LatitudeExtremumDetector
Build a detector.
LatitudeExtremumDetector(OneAxisEllipsoid) - Constructor for class org.orekit.propagation.events.LatitudeExtremumDetector
Build a new detector.
LatitudeExtremumDetector(AdaptableInterval, double, int, EventHandler, OneAxisEllipsoid) - Constructor for class org.orekit.propagation.events.LatitudeExtremumDetector
Protected constructor with full parameters.
LatitudeRangeCrossingDetector - Class in org.orekit.propagation.events
Detector for geographic latitude crossing.
LatitudeRangeCrossingDetector(double, double, OneAxisEllipsoid, double, double) - Constructor for class org.orekit.propagation.events.LatitudeRangeCrossingDetector
Build a detector.
LatitudeRangeCrossingDetector(OneAxisEllipsoid, double, double) - Constructor for class org.orekit.propagation.events.LatitudeRangeCrossingDetector
Build a new detector.
LatitudeRangeCrossingDetector(AdaptableInterval, double, int, EventHandler, OneAxisEllipsoid, double, double) - Constructor for class org.orekit.propagation.events.LatitudeRangeCrossingDetector
Private constructor with full parameters.
LazyLoadedCelestialBodies - Class in org.orekit.bodies
This class lazily loads auxiliary data when it is needed by a requested body.
LazyLoadedCelestialBodies(DataProvidersManager, TimeScales, Frame) - Constructor for class org.orekit.bodies.LazyLoadedCelestialBodies
Create a celestial body factory with the given auxiliary data sources.
LazyLoadedDataContext - Class in org.orekit.data
A data context that aims to match the behavior of Orekit 10.0 regarding auxiliary data.
LazyLoadedDataContext() - Constructor for class org.orekit.data.LazyLoadedDataContext
Create a new data context that only loads auxiliary data when it is first accessed and allows configuration of the auxiliary data sources until then.
LazyLoadedEop - Class in org.orekit.frames
Loads Earth Orientation Parameters (EOP) from a configured set of EopHistoryLoaders on demand.
LazyLoadedEop(DataProvidersManager) - Constructor for class org.orekit.frames.LazyLoadedEop
Create a new instance for loading EOP data from multiple EopHistoryLoaders.
LazyLoadedFrames - Class in org.orekit.frames
This class lazily loads auxiliary data when it is needed by a requested frame.
LazyLoadedFrames(LazyLoadedEop, TimeScales, CelestialBodies) - Constructor for class org.orekit.frames.LazyLoadedFrames
Create a collection of frames from the given auxiliary data.
LazyLoadedGeoMagneticFields - Class in org.orekit.models.earth
Loads magnetic fields on request and can be configured after creation.
LazyLoadedGeoMagneticFields(DataProvidersManager) - Constructor for class org.orekit.models.earth.LazyLoadedGeoMagneticFields
Create a factory for magnetic fields that uses the given data manager to load magnetic field files.
LazyLoadedGravityFields - Class in org.orekit.forces.gravity.potential
Loads gravity fields when first requested and can be configured until then.
LazyLoadedGravityFields(DataProvidersManager, TimeScale) - Constructor for class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
Create a factory for gravity fields that uses the given data manager to load the gravity field files.
LazyLoadedTimeScales - Class in org.orekit.time
An implementation of TimeScales that loads auxiliary data, leap seconds and UT1-UTC, when it is first accessed.
LazyLoadedTimeScales(LazyLoadedEop) - Constructor for class org.orekit.time.LazyLoadedTimeScales
Create a new set of time scales with the given sources of auxiliary data.
LB - org.orekit.gnss.ObservationType
Carrier-phase GPS L1C for Rinex2.
LC - org.orekit.gnss.ObservationType
Carrier-phase GPS L2C for Rinex2.
LD - org.orekit.gnss.ObservationType
Carrier-phase GLONASS G2 for Rinex2.
LDBARV - org.orekit.files.ccsds.ndm.odm.ocm.OrbitElementsType
Modified spherical 6-element set (λ, δ, β, A, r, v).
LEAP_SECONDS - org.orekit.files.rinex.section.RinexLabels
Leap seconds.
LeastSquaresTleGenerationAlgorithm - Class in org.orekit.propagation.analytical.tle.generation
Least squares method to generate a usable TLE from a spacecraft state.
LeastSquaresTleGenerationAlgorithm() - Constructor for class org.orekit.propagation.analytical.tle.generation.LeastSquaresTleGenerationAlgorithm
Default constructor.
LeastSquaresTleGenerationAlgorithm(int) - Constructor for class org.orekit.propagation.analytical.tle.generation.LeastSquaresTleGenerationAlgorithm
Default constructor.
LeastSquaresTleGenerationAlgorithm(int, TimeScale, Frame) - Constructor for class org.orekit.propagation.analytical.tle.generation.LeastSquaresTleGenerationAlgorithm
Constructor.
LegacyNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data
Container for data contained in a GPS/QZNSS legacy navigation message.
LegacyNavigationMessage(double, double, int) - Constructor for class org.orekit.propagation.analytical.gnss.data.LegacyNavigationMessage
Constructor.
LegendrePolynomials - Class in org.orekit.utils
Computes the Pnm(t) coefficients.
LegendrePolynomials(int, int, double) - Constructor for class org.orekit.utils.LegendrePolynomials
Create Legendre polynomials for the given degree and order.
LenseThirringRelativity - Class in org.orekit.forces.gravity
Lense-Thirring post-Newtonian correction force due to general relativity.
LenseThirringRelativity(double, Frame) - Constructor for class org.orekit.forces.gravity.LenseThirringRelativity
Constructor.
LEO - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCategory
Low Earth Orbit, hp < 2000 km, ha < 2000 km.
LEO - org.orekit.files.sp3.SP3FileType
LEO only file.
LexicalAnalyzer - Interface in org.orekit.files.ccsds.utils.lexical
Interface for CCSDS messages lexical analysis.
LexicalAnalyzerSelector - Class in org.orekit.files.ccsds.utils.lexical
Utility class for selecting either XmlLexicalAnalyzer or KvnLexicalAnalyzer depending on data first bytes.
LibrationOrbit - Class in org.orekit.orbits
Base class for libration orbits.
LibrationOrbit(CR3BPSystem, PVCoordinates, double) - Constructor for class org.orekit.orbits.LibrationOrbit
Constructor.
LibrationOrbitFamily - Enum in org.orekit.orbits
Enumerate for Libration Orbit family.
LibrationOrbitType - Enum in org.orekit.orbits
Enumerate for Libration Orbit type.
LICENSE - org.orekit.files.rinex.section.RinexLabels
Llicense.
LIFT_RATIO - Static variable in interface org.orekit.forces.drag.DragSensitive
Parameter name for lift ration enabling Jacobian processing.
LightFluxModel - Interface in org.orekit.forces.radiation
Interface describing flux models from a light source, including shadowing effects from occulting bodies.
lIndex(int, int) - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Get the index of an entry in the lower triangular matrix.
LINEAR - org.orekit.files.ccsds.ndm.odm.oem.InterpolationMethod
Linear interpolation.
LineOrientedFilteringReader - Class in org.orekit.data
Base class for implementing line-oriented data filtering readers.
LineOrientedFilteringReader(String, Reader) - Constructor for class org.orekit.data.LineOrientedFilteringReader
Simple constructor.
LineParameters(AbsoluteDate) - Constructor for class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityDataLoader.LineParameters
Constructor.
LineParameters(AbsoluteDate, double) - Constructor for class org.orekit.models.earth.atmosphere.data.DtcDataLoader.LineParameters
Constructor.
LineParameters(AbsoluteDate, double[], double, double[], double, double, int, double, double, double, double, double) - Constructor for class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
Constructor.
LineParameters(AbsoluteDate, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader.LineParameters
Constructor.
LMO - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCategory
LEO-MEO Crossing Orbit, hp < 2000 km, 2000 < ha < 31570 km.
LNAV - Static variable in class org.orekit.propagation.analytical.gnss.data.LegacyNavigationMessage
Identifier for message type.
LnsCoefficients - Class in org.orekit.propagation.semianalytical.dsst.utilities
Compute the Lns(γ).
LnsCoefficients(int, int, double[][], SortedMap<CoefficientsFactory.NSKey, Double>, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.LnsCoefficients
Create a set of Lns(γ) coefficients.
loadCelestialBody(String) - Method in interface org.orekit.bodies.CelestialBodyLoader
Load celestial body.
loadCelestialBody(String) - Method in class org.orekit.bodies.JPLEphemeridesLoader
Load celestial body.
loadData() - Method in class org.orekit.gnss.SEMParser
Loads almanacs.
loadData() - Method in class org.orekit.gnss.YUMAParser
Loads almanacs.
loadData(InputStream, String) - Method in interface org.orekit.data.DataLoader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.EGMFormatReader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.FESCHatEpsilonReader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.FESCnmSnmReader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.GRGSFormatReader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.ICGEMFormatReader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.SHAFormatReader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.SHMFormatReader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.gnss.SEMParser
 
loadData(InputStream, String) - Method in class org.orekit.gnss.YUMAParser
 
loadData(InputStream, String) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.models.earth.atmosphere.data.DtcDataLoader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimationLoader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.models.earth.GeoMagneticModelLoader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader
Load Klobuchar-Style ionospheric coefficients read from some file.
loadData(InputStream, String) - Method in class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader
 
loadData(InputStream, String) - Method in class org.orekit.utils.InterpolationTableLoader
Loads an bi-variate interpolation table from the given InputStream.
loadKlobucharIonosphericCoefficients() - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader
Load the data using supported names .
loadKlobucharIonosphericCoefficients(DateComponents) - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader
Load the data for a given day.
loadLoveNumbers(String) - Method in enum org.orekit.utils.IERSConventions
Load the Love numbers.
loadOffsets() - Method in class org.orekit.time.AGILeapSecondFilesLoader
Load UTC-TAI offsets entries.
loadOffsets() - Method in class org.orekit.time.TAIUTCDatFilesLoader
Load UTC-TAI offsets entries.
loadOffsets() - Method in class org.orekit.time.UTCTAIBulletinAFilesLoader
Load UTC-TAI offsets entries.
loadOffsets() - Method in class org.orekit.time.UTCTAIHistoryFilesLoader
Load UTC-TAI offsets entries.
loadOffsets() - Method in interface org.orekit.time.UTCTAIOffsetsLoader
Load UTC-TAI offsets entries.
loadViennaCoefficients() - Method in class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader
Load the data using supported names .
loadViennaCoefficients(DateTimeComponents) - Method in class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader
Load the data for a given day.
LocalizedException - Interface in org.orekit.errors
This interface specified methods implemented by localized exception classes.
LocalMagneticFieldFrame - Class in org.orekit.frames
This class handles a magnetic field variation attitude provider.
LocalMagneticFieldFrame(Frame, GeoMagneticField, Frame) - Constructor for class org.orekit.frames.LocalMagneticFieldFrame
Constructor with default definition of the local orbital frame: x: Magnetic field y: Completes orthonormal frame z: Cross product of the magnetic field with the orbital momentum .
LocalMagneticFieldFrame(Frame, GeoMagneticField, LocalMagneticFieldFrame.LOFBuilderVector, Frame) - Constructor for class org.orekit.frames.LocalMagneticFieldFrame
Constructor with custom definition of the local orbital frame: x: Magnetic field y: Completes orthonormal frame z: Cross product of the magnetic field with chosen vector For near-polar orbits, it is suggested to use the orbital momentum to define the local orbital frame.
LocalMagneticFieldFrame.LOFBuilderVector - Enum in org.orekit.frames
Enum defining how the +j axis of the local orbital frame will be defined.
LocalOrbitalFrame - Class in org.orekit.frames
Class for frames moving with an orbiting satellite.
LocalOrbitalFrame(Frame, LOF, PVCoordinatesProvider, String) - Constructor for class org.orekit.frames.LocalOrbitalFrame
Build a new instance.
LocalSolarActivity(AbsoluteDate) - Constructor for class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData.LocalSolarActivity
Constructor.
LOF - Interface in org.orekit.frames
Interface for local orbital frame.
LofOffset - Class in org.orekit.attitudes
Attitude law defined by fixed Roll, Pitch and Yaw angles (in any order) with respect to a local orbital frame.
LofOffset(Frame, LOF) - Constructor for class org.orekit.attitudes.LofOffset
Create a LOF-aligned attitude.
LofOffset(Frame, LOF, RotationOrder, double, double, double) - Constructor for class org.orekit.attitudes.LofOffset
Creates new instance.
LofOffsetPointing - Class in org.orekit.attitudes
This class provides a default attitude provider.
LofOffsetPointing(Frame, BodyShape, AttitudeProvider, Vector3D) - Constructor for class org.orekit.attitudes.LofOffsetPointing
Creates new instance.
LOFType - Enum in org.orekit.frames
Enumerate for different types of Local Orbital Frames.
LOG - org.orekit.models.earth.displacement.PsdCorrection.TimeEvolution
Logarithmic evolution.
LongitudeCrossingDetector - Class in org.orekit.propagation.events
Detector for geographic longitude crossing.
LongitudeCrossingDetector(double, double, OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.LongitudeCrossingDetector
Build a detector.
LongitudeCrossingDetector(OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.LongitudeCrossingDetector
Build a new detector.
LongitudeCrossingDetector(AdaptableInterval, double, int, EventHandler, OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.LongitudeCrossingDetector
Protected constructor with full parameters.
LongitudeExtremumDetector - Class in org.orekit.propagation.events
Detector for geographic longitude extremum.
LongitudeExtremumDetector(double, double, OneAxisEllipsoid) - Constructor for class org.orekit.propagation.events.LongitudeExtremumDetector
Build a detector.
LongitudeExtremumDetector(OneAxisEllipsoid) - Constructor for class org.orekit.propagation.events.LongitudeExtremumDetector
Build a new detector.
LongitudeExtremumDetector(AdaptableInterval, double, int, EventHandler, OneAxisEllipsoid) - Constructor for class org.orekit.propagation.events.LongitudeExtremumDetector
Protected constructor with full parameters.
LongitudeRangeCrossingDetector - Class in org.orekit.propagation.events
Detector for geographic longitude crossing.
LongitudeRangeCrossingDetector(double, double, OneAxisEllipsoid, double, double) - Constructor for class org.orekit.propagation.events.LongitudeRangeCrossingDetector
Build a detector.
LongitudeRangeCrossingDetector(OneAxisEllipsoid, double, double) - Constructor for class org.orekit.propagation.events.LongitudeRangeCrossingDetector
Build a new detector.
LongitudeRangeCrossingDetector(AdaptableInterval, double, int, EventHandler, OneAxisEllipsoid, double, double) - Constructor for class org.orekit.propagation.events.LongitudeRangeCrossingDetector
Private constructor with full parameters.
LoveNumbers - Class in org.orekit.utils
Container for Love numbers.
LoveNumbers(double[][], double[][], double[][]) - Constructor for class org.orekit.utils.LoveNumbers
Simple constructor.
LOW_ELEVATION_THRESHOLD - Static variable in class org.orekit.models.earth.troposphere.AskneNordiusModel
Lowest acceptable elevation angle [rad].
lowestAltitudeIntermediate(FieldVector3D<T>, FieldVector3D<T>) - Method in class org.orekit.bodies.OneAxisEllipsoid
Find intermediate point of lowest altitude along a line between two endpoints.
lowestAltitudeIntermediate(Vector3D, Vector3D) - Method in class org.orekit.bodies.OneAxisEllipsoid
Find intermediate point of lowest altitude along a line between two endpoints.
Loxodrome - Class in org.orekit.bodies
Perform calculations on a loxodrome (commonly, a rhumb line) on an ellipsoid.
Loxodrome(GeodeticPoint, double, OneAxisEllipsoid) - Constructor for class org.orekit.bodies.Loxodrome
Constructor building a loxodrome from an initial point and an azimuth-off-local-north heading.
Loxodrome(GeodeticPoint, double, OneAxisEllipsoid, double) - Constructor for class org.orekit.bodies.Loxodrome
Constructor building a loxodrome from an initial point and an azimuth-off-local-north heading.
LoxodromeArc - Class in org.orekit.bodies
Loxodrome defined by a start and ending point.
LoxodromeArc(GeodeticPoint, GeodeticPoint, OneAxisEllipsoid) - Constructor for class org.orekit.bodies.LoxodromeArc
Class constructor where the arc's altitude is the average of the initial and final points.
LoxodromeArc(GeodeticPoint, GeodeticPoint, OneAxisEllipsoid, double) - Constructor for class org.orekit.bodies.LoxodromeArc
Class constructor.
loxodromeBuilder(OneAxisEllipsoid) - Static method in class org.orekit.utils.WaypointPVBuilder
Construct a waypoint builder interpolating points using a loxodrome (or Rhumbline).
ltdlDecomposition() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Perform Lᵀ.D.L = Q decomposition of the covariance matrix.
ltdlDecomposition() - Method in class org.orekit.estimation.measurements.gnss.LambdaMethod
Perform Lᵀ.D.L = Q decomposition of the covariance matrix.
ltdlDecomposition() - Method in class org.orekit.estimation.measurements.gnss.ModifiedLambdaMethod
Compute the LᵀDL factorization with symmetric pivoting decomposition of Q (symmetric definite positive matrix) with a minimum symmetric pivoting: Q = ZᵀLᵀDLZ.
LTM - org.orekit.files.ccsds.ndm.odm.ocm.Ordering
Lower Triangular Matrix.
LTMWCC - org.orekit.files.ccsds.ndm.odm.ocm.Ordering
Lower Triangular Matrix conflated with cross-correlation terms.
luniSolarTermsComputation() - Method in class org.orekit.propagation.analytical.tle.DeepSDP4
Computes luni - solar terms from initial coordinates and epoch.
luniSolarTermsComputation() - Method in class org.orekit.propagation.analytical.tle.FieldDeepSDP4
Computes luni - solar terms from initial coordinates and epoch.
LutherFieldIntegratorBuilder<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.conversion
Builder for LutherFieldIntegrator.
LutherFieldIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.LutherFieldIntegratorBuilder
Constructor.
LutherFieldIntegratorBuilder(T) - Constructor for class org.orekit.propagation.conversion.LutherFieldIntegratorBuilder
Constructor using a "fielded" step.
LutherIntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for LutherIntegrator.
LutherIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.LutherIntegratorBuilder
Build a new instance.
LVLH - org.orekit.files.ccsds.definitions.OrbitRelativeFrame
Local vertical, Local Horizontal (Z towards nadir, Y opposite to momentum).
LVLH - org.orekit.frames.LOFType
Constant for Local Vertical, Local Horizontal frame (X axis aligned with position, Z axis aligned with orbital momentum).
LVLH_CCSDS - org.orekit.frames.LOFType
Constant for Local Vertical, Local Horizontal frame as defined by CCSDS (Z axis aligned with opposite of position, Y axis aligned with opposite of orbital momentum).
LVLH_CCSDS_INERTIAL - org.orekit.frames.LOFType
Constant for Local Vertical, Local Horizontal frame as defined by CCSDS considered inertial (Z axis aligned with opposite of position, Y axis aligned with opposite of orbital momentum).
LVLH_INERTIAL - org.orekit.files.ccsds.definitions.OrbitRelativeFrame
Local vertical, Local Horizontal (Z towards nadir, Y opposite to momentum).
LVLH_INERTIAL - org.orekit.frames.LOFType
Constant for Local Vertical, Local Horizontal frame considered inertial (X axis aligned with position, Z axis aligned with orbital momentum).
LVLH_ROTATING - org.orekit.files.ccsds.definitions.OrbitRelativeFrame
Local vertical, Local Horizontal (Z towards nadir, Y opposite to momentum).
LYAPUNOV - org.orekit.orbits.LibrationOrbitType
Lyapunov orbit type.
LyapunovOrbit - Class in org.orekit.orbits
Class calculating different parameters of a Lyapunov Orbit.
LyapunovOrbit(CR3BPSystem, PVCoordinates, double) - Constructor for class org.orekit.orbits.LyapunovOrbit
Simple Constructor.
LyapunovOrbit(RichardsonExpansion, double) - Constructor for class org.orekit.orbits.LyapunovOrbit
Simple Constructor.

M

M - org.orekit.gnss.SignalCode
GPS M code.
M_PER_S - Static variable in class org.orekit.files.ccsds.definitions.Units
Meters per second units.
M_PER_S2 - Static variable in class org.orekit.files.ccsds.definitions.Units
Meters per square second units.
M2 - Static variable in class org.orekit.files.ccsds.definitions.Units
m² unit.
M2 - Static variable in class org.orekit.models.earth.displacement.Tide
M₂ tide.
M2 - Static variable in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Default value for M2 coefficient.
M2_NAME - Static variable in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Parameter name for M2 coefficient.
M2_PER_KG - Static variable in class org.orekit.files.ccsds.definitions.Units
m² per kilograms units.
M2_PER_S - Static variable in class org.orekit.files.ccsds.definitions.Units
Square meters per second units.
M2_PER_S2 - Static variable in class org.orekit.files.ccsds.definitions.Units
Square meters per square second units.
M2_PER_S3 - Static variable in class org.orekit.files.ccsds.definitions.Units
Square meters per cube second units.
M2_PER_S4 - Static variable in class org.orekit.files.ccsds.definitions.Units
Square meters per s⁴ units.
M3_PER_KG - Static variable in class org.orekit.files.ccsds.definitions.Units
m³ per kilograms units.
M3_PER_KGS - Static variable in class org.orekit.files.ccsds.definitions.Units
Cubic meters per kilograms second units.
M3_PER_KGS2 - Static variable in class org.orekit.files.ccsds.definitions.Units
Cubic meters per kilograms (square second) units.
M4 - Static variable in class org.orekit.files.ccsds.definitions.Units
m⁴ unit.
M4_PER_KG - Static variable in class org.orekit.files.ccsds.definitions.Units
m⁴ per kilograms units.
M4_PER_KG2 - Static variable in class org.orekit.files.ccsds.definitions.Units
m⁴ per square kilograms units.
MAG - org.orekit.files.ccsds.ndm.tdm.ObservationType
Data: visual magnitude.
MagneticFieldDetector - Class in org.orekit.propagation.events
Detector for Earth magnetic field strength.
MagneticFieldDetector(double, double, double, GeoMagneticFieldFactory.FieldModel, OneAxisEllipsoid, boolean) - Constructor for class org.orekit.propagation.events.MagneticFieldDetector
Build a detector.
MagneticFieldDetector(double, double, double, GeoMagneticFieldFactory.FieldModel, OneAxisEllipsoid, boolean, DataContext) - Constructor for class org.orekit.propagation.events.MagneticFieldDetector
Build a detector.
MagneticFieldDetector(double, GeoMagneticFieldFactory.FieldModel, OneAxisEllipsoid) - Constructor for class org.orekit.propagation.events.MagneticFieldDetector
Build a new detector.
MagneticFieldDetector(double, GeoMagneticFieldFactory.FieldModel, OneAxisEllipsoid, boolean) - Constructor for class org.orekit.propagation.events.MagneticFieldDetector
Build a new detector.
MagneticFieldDetector(AdaptableInterval, double, int, EventHandler, double, GeoMagneticFieldFactory.FieldModel, OneAxisEllipsoid, boolean, DataContext) - Constructor for class org.orekit.propagation.events.MagneticFieldDetector
Protected constructor with full parameters.
MAHALANOBIS_DISTANCE - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
The length of the relative position vector, normalized to one-sigma dispersions of the combined error covariance in the direction of the relative position vector.
man - org.orekit.files.ccsds.ndm.adm.acm.AcmDataSubStructureKey
Maneuvers section.
man - org.orekit.files.ccsds.ndm.odm.ocm.OcmDataSubStructureKey
Maneuvers section.
MAN - org.orekit.files.ccsds.ndm.adm.acm.AcmDataSubStructureKey
Maneuvers section.
MAN - org.orekit.files.ccsds.ndm.adm.acm.AcmElements
Maneuver.
MAN - org.orekit.files.ccsds.ndm.odm.ocm.OcmDataSubStructureKey
Maneuvers section.
MAN - org.orekit.files.ccsds.ndm.odm.ocm.OcmElements
Maneuver.
MAN_BASIS - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey
Basis of this maneuver history data.
MAN_BASIS_ID - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey
Identification number of the orbit determination or simulation upon which this maneuver is based.
MAN_BEGIN_TIME - org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuverKey
Start time of actual maneuver, relative to t₀.
MAN_COMPOSITION - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey
Maneuver elements of information.
MAN_DELTA_MASS - org.orekit.files.ccsds.ndm.adm.apm.ManeuverKey
Mass change entry.
MAN_DELTA_MASS - org.orekit.files.ccsds.ndm.odm.opm.ManeuverKey
Mass change during maneuver (value is < 0).
MAN_DEVICE_ID - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey
Identifier of the device used for this maneuver.
MAN_DURA - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
Maneuver duration.
MAN_DURATION - org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuverKey
Duration.
MAN_DURATION - org.orekit.files.ccsds.ndm.adm.apm.ManeuverKey
Duration entry.
MAN_DURATION - org.orekit.files.ccsds.ndm.odm.opm.ManeuverKey
Maneuver duration (0 for impulsive maneuvers).
MAN_DV_1 - org.orekit.files.ccsds.ndm.odm.opm.ManeuverKey
First component of the velocity increment.
MAN_DV_2 - org.orekit.files.ccsds.ndm.odm.opm.ManeuverKey
Second component of the velocity increment.
MAN_DV_3 - org.orekit.files.ccsds.ndm.odm.opm.ManeuverKey
Third component of the velocity increment.
MAN_END_TIME - org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuverKey
End time of actual maneuver, relative to t₀.
MAN_EPOCH_IGNITION - org.orekit.files.ccsds.ndm.odm.opm.ManeuverKey
Epoch of ignition.
MAN_EPOCH_START - org.orekit.files.ccsds.ndm.adm.apm.ManeuverKey
Epoch start entry.
MAN_FRAME_EPOCH - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey
MAN_ID - org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuverKey
Maneuver identification number.
MAN_ID - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey
Maneuver identification number.
MAN_LINE - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.Ocm
Maneuver line element for XML messages.
MAN_NEXT_EPOCH - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey
Start time of next maneuver.
MAN_NEXT_ID - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey
Identification number of next maneuver.
MAN_PRED_SOURCE - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey
Prediction source on which this maneuver is based.
MAN_PREV_EPOCH - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey
Completion time of previous maneuver.
MAN_PREV_ID - org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuverKey
Identification number of previous maneuver.
MAN_PREV_ID - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey
Identification number of previous maneuver.
MAN_PURPOSE - org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuverKey
Purpose of the maneuver.
MAN_PURPOSE - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey
Purposes of the maneuver.
MAN_REF_FRAME - org.orekit.files.ccsds.ndm.adm.apm.ManeuverKey
Reference frame entry.
MAN_REF_FRAME - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey
Reference frame of the maneuver.
MAN_REF_FRAME - org.orekit.files.ccsds.ndm.odm.opm.ManeuverKey
Coordinate system for velocity increment vector.
MAN_TOR_1 - org.orekit.files.ccsds.ndm.adm.apm.ManeuverKey
First torque vector component entry (ADM V1 only).
MAN_TOR_2 - org.orekit.files.ccsds.ndm.adm.apm.ManeuverKey
Second torque vector component entry (ADM V1 only).
MAN_TOR_3 - org.orekit.files.ccsds.ndm.adm.apm.ManeuverKey
Third torque vector component entry (ADM V1 only).
MAN_TOR_X - org.orekit.files.ccsds.ndm.adm.apm.ManeuverKey
First torque vector component entry.
MAN_TOR_Y - org.orekit.files.ccsds.ndm.adm.apm.ManeuverKey
Second torque vector component entry.
MAN_TOR_Z - org.orekit.files.ccsds.ndm.adm.apm.ManeuverKey
Third torque vector component entry.
MAN_UNITS - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey
SI units for each elements of the maneuver.
manageData(ObservationDataSet) - Method in class org.orekit.estimation.measurements.gnss.AbstractCycleSlipDetector
The method is in charge of collecting the measurements, manage them, and call the detection method.
manageData(ObservationDataSet) - Method in class org.orekit.estimation.measurements.gnss.GeometryFreeCycleSlipDetector
The method is in charge of collecting the measurements, manage them, and call the detection method.
manageData(ObservationDataSet) - Method in class org.orekit.estimation.measurements.gnss.PhaseMinusCodeCycleSlipDetector
The method is in charge of collecting the measurements, manage them, and call the detection method.
ManBasis - Enum in org.orekit.files.ccsds.ndm.odm.ocm
Basis of maneuver used in CCSDS Orbit Comprehensive Messages.
Maneuver - Class in org.orekit.files.ccsds.ndm.adm.apm
Maneuver in an APM file.
Maneuver - Class in org.orekit.files.ccsds.ndm.odm.opm
Maneuver in an OPM file.
Maneuver - Class in org.orekit.forces.maneuvers
A generic model for maneuvers with finite-valued acceleration magnitude, as opposed to instantaneous changes in the velocity vector which are defined via detectors (in ImpulseManeuver and FieldImpulseManeuver).
Maneuver() - Constructor for class org.orekit.files.ccsds.ndm.adm.apm.Maneuver
Simple constructor.
Maneuver() - Constructor for class org.orekit.files.ccsds.ndm.odm.opm.Maneuver
Simple constructor.
Maneuver(AttitudeProvider, ManeuverTriggers, PropulsionModel) - Constructor for class org.orekit.forces.maneuvers.Maneuver
Generic maneuver constructor.
MANEUVERABLE - org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey
Manoeuver capacity.
ManeuverFieldType - Enum in org.orekit.files.ccsds.ndm.odm.ocm
Maneuver field type used in CCSDS Orbit Comprehensive Messages.
ManeuverKey - Enum in org.orekit.files.ccsds.ndm.adm.apm
Keys for APM maneuver entries.
ManeuverKey - Enum in org.orekit.files.ccsds.ndm.odm.opm
Keys for OPM maneuver entries.
maneuverTriggered(FieldSpacecraftState<T>, boolean) - Method in interface org.orekit.forces.maneuvers.trigger.FieldManeuverTriggersResetter
Observe a maneuver trigger.
maneuverTriggered(SpacecraftState, boolean) - Method in class org.orekit.forces.maneuvers.jacobians.TriggerDate
Observe a maneuver trigger.
maneuverTriggered(SpacecraftState, boolean) - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggersResetter
Observe a maneuver trigger.
ManeuverTriggers - Interface in org.orekit.forces.maneuvers.trigger
Generic interface for the maneuver triggers used in a Maneuver.
ManeuverTriggersResetter - Interface in org.orekit.forces.maneuvers.trigger
Resetter for maneuver triggers.
Maneuvrable - Enum in org.orekit.files.ccsds.ndm.cdm
Maneuvrable possibilities used in CCSDS Conjunction Data Messages.
MANUFACTURER - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Satellite manufacturer name.
map(Frame) - Static method in enum org.orekit.files.ccsds.definitions.CelestialBodyFrame
Map an Orekit frame to a CCSDS frame.
map(Frame) - Static method in enum org.orekit.files.ccsds.definitions.CenterName
Map an Orekit frame to a CCSDS center.
map(Frame) - Static method in class org.orekit.files.ccsds.definitions.FrameFacade
Map an Orekit frame to a CCSDS frame facade.
mapArrayToOrbit(double[], double[], PositionAngleType, AbsoluteDate, double, Frame) - Method in enum org.orekit.orbits.OrbitType
Convert state array to orbital parameters.
mapArrayToOrbit(T[], T[], PositionAngleType, FieldAbsoluteDate<T>, T, Frame) - Method in enum org.orekit.orbits.OrbitType
Convert state array to orbital parameters.
mapArrayToState(double, double[], double[], PropagationType) - Method in class org.orekit.propagation.integration.StateMapper
Map the raw double components to a spacecraft state.
mapArrayToState(AbsoluteDate, double[], double[], PropagationType) - Method in class org.orekit.propagation.integration.StateMapper
Map the raw double components to a spacecraft state.
mapArrayToState(FieldAbsoluteDate<T>, T[], T[], PropagationType) - Method in class org.orekit.propagation.integration.FieldStateMapper
Map the raw double components to a spacecraft state.
mapArrayToState(T, T[], T[], PropagationType) - Method in class org.orekit.propagation.integration.FieldStateMapper
Map the raw double components to a spacecraft state.
mapDateToDouble(AbsoluteDate) - Method in class org.orekit.propagation.integration.StateMapper
Map a date to a raw double time offset.
mapDateToDouble(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldStateMapper
Map a date to a raw double time offset.
mapDoubleToDate(double) - Method in class org.orekit.propagation.integration.StateMapper
Map the raw double time offset to a date.
mapDoubleToDate(double, AbsoluteDate) - Method in class org.orekit.propagation.integration.StateMapper
Map the raw double time offset to a date.
mapDoubleToDate(T) - Method in class org.orekit.propagation.integration.FieldStateMapper
Map the raw double time offset to a date.
mapDoubleToDate(T, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldStateMapper
Map the raw double time offset to a date.
mapOrbitToArray(FieldOrbit<T>, PositionAngleType, T[], T[]) - Method in enum org.orekit.orbits.OrbitType
Convert orbit to state array.
mapOrbitToArray(Orbit, PositionAngleType, double[], double[]) - Method in enum org.orekit.orbits.OrbitType
Convert orbit to state array.
mappingFactor(double) - Method in interface org.orekit.models.earth.ionosphere.IonosphericMappingFunction
This method allows the computation of the ionospheric mapping factor.
mappingFactor(double) - Method in class org.orekit.models.earth.ionosphere.SingleLayerModelMappingFunction
This method allows the computation of the ionospheric mapping factor.
mappingFactor(T) - Method in interface org.orekit.models.earth.ionosphere.IonosphericMappingFunction
This method allows the computation of the ionospheric mapping factor.
mappingFactor(T) - Method in class org.orekit.models.earth.ionosphere.SingleLayerModelMappingFunction
This method allows the computation of the ionospheric mapping factor.
mappingFactors(double, GeodeticPoint, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.GlobalMappingFunctionModel
Deprecated.
mappingFactors(double, GeodeticPoint, AbsoluteDate) - Method in interface org.orekit.models.earth.troposphere.MappingFunction
Deprecated.
This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(double, GeodeticPoint, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.MendesPavlisModel
Deprecated.
mappingFactors(double, GeodeticPoint, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.NiellMappingFunctionModel
Deprecated.
mappingFactors(double, GeodeticPoint, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.ViennaOneModel
Deprecated.
mappingFactors(double, GeodeticPoint, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.ViennaThreeModel
Deprecated.
mappingFactors(FieldTrackingCoordinates<T>, FieldGeodeticPoint<T>, FieldPressureTemperatureHumidity<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.AbstractChaoMappingFunction
This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(FieldTrackingCoordinates<T>, FieldGeodeticPoint<T>, FieldPressureTemperatureHumidity<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.DummyMappingFunction
This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(FieldTrackingCoordinates<T>, FieldGeodeticPoint<T>, FieldPressureTemperatureHumidity<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.GlobalMappingFunctionModel
This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(FieldTrackingCoordinates<T>, FieldGeodeticPoint<T>, FieldPressureTemperatureHumidity<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.MendesPavlisModel
With the Mendes Pavlis tropospheric model, the mapping function is not split into hydrostatic and wet component.
mappingFactors(FieldTrackingCoordinates<T>, FieldGeodeticPoint<T>, FieldPressureTemperatureHumidity<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.NiellMappingFunctionModel
This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(FieldTrackingCoordinates<T>, FieldGeodeticPoint<T>, FieldPressureTemperatureHumidity<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.models.earth.troposphere.TroposphereMappingFunction
This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(FieldTrackingCoordinates<T>, FieldGeodeticPoint<T>, FieldPressureTemperatureHumidity<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.TroposphereMappingFunctionAdapter
Deprecated.
This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(FieldTrackingCoordinates<T>, FieldGeodeticPoint<T>, FieldPressureTemperatureHumidity<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.ViennaOne
This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(FieldTrackingCoordinates<T>, FieldGeodeticPoint<T>, FieldPressureTemperatureHumidity<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.ViennaThree
This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(TrackingCoordinates, GeodeticPoint, PressureTemperatureHumidity, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.AbstractChaoMappingFunction
This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(TrackingCoordinates, GeodeticPoint, PressureTemperatureHumidity, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.DummyMappingFunction
This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(TrackingCoordinates, GeodeticPoint, PressureTemperatureHumidity, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.GlobalMappingFunctionModel
This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(TrackingCoordinates, GeodeticPoint, PressureTemperatureHumidity, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.MendesPavlisModel
With the Mendes Pavlis tropospheric model, the mapping function is not split into hydrostatic and wet component.
mappingFactors(TrackingCoordinates, GeodeticPoint, PressureTemperatureHumidity, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.NiellMappingFunctionModel
This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(TrackingCoordinates, GeodeticPoint, PressureTemperatureHumidity, AbsoluteDate) - Method in interface org.orekit.models.earth.troposphere.TroposphereMappingFunction
This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(TrackingCoordinates, GeodeticPoint, PressureTemperatureHumidity, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.TroposphereMappingFunctionAdapter
Deprecated.
This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(TrackingCoordinates, GeodeticPoint, PressureTemperatureHumidity, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.ViennaOne
This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(TrackingCoordinates, GeodeticPoint, PressureTemperatureHumidity, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.ViennaThree
This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(T, FieldGeodeticPoint<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.GlobalMappingFunctionModel
Deprecated.
mappingFactors(T, FieldGeodeticPoint<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.models.earth.troposphere.MappingFunction
Deprecated.
This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(T, FieldGeodeticPoint<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.MendesPavlisModel
Deprecated.
mappingFactors(T, FieldGeodeticPoint<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.NiellMappingFunctionModel
Deprecated.
mappingFactors(T, FieldGeodeticPoint<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.ViennaOneModel
Deprecated.
mappingFactors(T, FieldGeodeticPoint<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.ViennaThreeModel
Deprecated.
mappingFunction(double, double, double, double) - Static method in class org.orekit.models.earth.troposphere.TroposphericModelUtils
Compute the mapping function related to the coefficient values and the elevation.
mappingFunction(T, T, T, T) - Static method in class org.orekit.models.earth.troposphere.TroposphericModelUtils
Compute the mapping function related to the coefficient values and the elevation.
MappingFunction - Interface in org.orekit.models.earth.troposphere
Deprecated.
as of 12.1, replaced by TroposphereMappingFunction
mapStateToArray(FieldSpacecraftState<T>, T[], T[]) - Method in class org.orekit.propagation.integration.FieldStateMapper
Map a spacecraft state to raw double components.
mapStateToArray(SpacecraftState, double[], double[]) - Method in class org.orekit.propagation.integration.StateMapper
Map a spacecraft state to raw double components.
MARCH - org.orekit.time.Month
March.
MariniMurray - Class in org.orekit.models.earth.troposphere
The Marini-Murray tropospheric delay model for laser ranging.
MariniMurray(double, Unit) - Constructor for class org.orekit.models.earth.troposphere.MariniMurray
Create a new Marini-Murray model for the troposphere.
MariniMurrayModel - Class in org.orekit.models.earth.troposphere
Deprecated.
as of 12.1, replaced by MariniMurray
MariniMurrayModel(double, double, double, double) - Constructor for class org.orekit.models.earth.troposphere.MariniMurrayModel
Deprecated.
Create a new Marini-Murray model for the troposphere using the given environmental conditions.
MARKER_NAME - org.orekit.files.rinex.section.RinexLabels
Marker name.
MARKER_NUMBER - org.orekit.files.rinex.section.RinexLabels
Marker number.
MARKER_TYPE - org.orekit.files.rinex.section.RinexLabels
Marker type.
MARS - org.orekit.bodies.JPLEphemeridesLoader.EphemerisType
Constant for Mars.
MARS - org.orekit.files.ccsds.definitions.CenterName
Mars body.
MARS - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Mars.
MarshallSolarActivityFutureEstimation - Class in org.orekit.models.earth.atmosphere.data
This class provides solar activity data needed by atmospheric models: F107 solar flux, Ap and Kp indexes.
MarshallSolarActivityFutureEstimation(String, MarshallSolarActivityFutureEstimation.StrengthLevel) - Constructor for class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
Simple constructor.
MarshallSolarActivityFutureEstimation(String, MarshallSolarActivityFutureEstimation.StrengthLevel, DataProvidersManager, TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
Constructor that allows specifying the source of the MSAFE auxiliary data files.
MarshallSolarActivityFutureEstimation(String, MarshallSolarActivityFutureEstimation.StrengthLevel, DataProvidersManager, TimeScale, int, double, double, double) - Constructor for class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
Constructor that allows specifying the source of the MSAFE auxiliary data files and customizable thread safe cache configuration.
MarshallSolarActivityFutureEstimation(DataSource, MarshallSolarActivityFutureEstimation.StrengthLevel) - Constructor for class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
Simple constructor which use the default data context.
MarshallSolarActivityFutureEstimation(DataSource, MarshallSolarActivityFutureEstimation.StrengthLevel, TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
Simple constructor.
MarshallSolarActivityFutureEstimation(DataSource, MarshallSolarActivityFutureEstimation.StrengthLevel, TimeScale, int, double, double, double) - Constructor for class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
Constructor with customizable thread safe cache configuration.
MarshallSolarActivityFutureEstimation.StrengthLevel - Enum in org.orekit.models.earth.atmosphere.data
Strength level of activity.
MarshallSolarActivityFutureEstimationLoader - Class in org.orekit.models.earth.atmosphere.data
This class reads solar activity data needed by atmospheric models: F107 solar flux, Ap and Kp indexes.
MarshallSolarActivityFutureEstimationLoader(MarshallSolarActivityFutureEstimation.StrengthLevel) - Constructor for class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimationLoader
Simple constructor.
MarshallSolarActivityFutureEstimationLoader(MarshallSolarActivityFutureEstimation.StrengthLevel, TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimationLoader
Constructor that allows specifying the source of the MSAFE auxiliary data files.
MarshallSolarActivityFutureEstimationLoader.LineParameters - Class in org.orekit.models.earth.atmosphere.data
Container class for Solar activity indexes.
mass(double) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagatorBuilder
Sets the mass.
mass(double) - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagatorBuilder
Sets the mass.
mass(double) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagatorBuilder
Sets the mass.
mass(double) - Method in class org.orekit.propagation.numerical.GLONASSNumericalPropagatorBuilder
Sets the mass.
MASS - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
The mass of the object.
MASS - org.orekit.files.ccsds.ndm.odm.SpacecraftParametersKey
Spacecraft mass.
MASS_RATIO_SUFFIX - Static variable in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel
Suffix for parameter name for Mass Ratio enabling Jacobian processing.
MassDepletionDelay - Class in org.orekit.forces.maneuvers.jacobians
Generator for effect of delaying mass depletion when delaying a maneuver.
MassDepletionDelay(String, boolean, Maneuver) - Constructor for class org.orekit.forces.maneuvers.jacobians.MassDepletionDelay
Simple constructor.
matches(String) - Method in enum org.orekit.files.rinex.section.RinexLabels
Check if label matches.
matchesLabel(String, String) - Static method in class org.orekit.files.rinex.utils.parsing.RinexUtils
Check if a header line matches an expected label.
MatricesHarvester - Interface in org.orekit.propagation
Interface for extracting State Transition Matrices and Jacobians matrices from spacecraft state.
MAX_EPOCH - Static variable in class org.orekit.time.DateComponents
Maximum supported date.
MAX_ITERATIONS_DEFAULT - Static variable in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Default value for maxIterations.
MAX_ITERATIONS_DEFAULT - Static variable in class org.orekit.propagation.analytical.tle.generation.FixedPointTleGenerationAlgorithm
Default value for maxIterations.
MAX_POWER - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Max power for summation.
MAX_THRUST - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Maximum composite thrust the spacecraft can accomplish.
MaxGapInterpolationGrid - Class in org.orekit.propagation.semianalytical.dsst.utilities
Interpolation grid where points obey a maximum time gap.
MaxGapInterpolationGrid(double) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.MaxGapInterpolationGrid
Constructor.
MAXIMUM_OBS_GAP - org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey
Maximum time between observations in the OD of the object.
maxStep - Variable in class org.orekit.propagation.conversion.AbstractVariableStepFieldIntegratorBuilder
Maximum step size (s).
maxStep - Variable in class org.orekit.propagation.conversion.AbstractVariableStepIntegratorBuilder
Maximum step size (s).
maxValueChanged(double, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver
Notify that a parameter maximum value has been changed.
MAY - org.orekit.time.Month
May.
MCI - org.orekit.files.ccsds.definitions.CelestialBodyFrame
Mars Centered Inertial.
MCKINLEY_2006 - org.orekit.files.ccsds.definitions.PocMethodType
McKinley 2006 method.
MEAN - org.orekit.orbits.PositionAngleType
Mean angle.
MEAN - org.orekit.propagation.PropagationType
Mean propagation.
MEAN_ANOM - Static variable in enum org.orekit.orbits.OrbitType
Name for mean anomaly.
MEAN_ANOMALY - org.orekit.files.ccsds.ndm.odm.KeplerianElementsKey
Orbit mean anomaly.
MEAN_ELEMENT_THEORY - org.orekit.files.ccsds.ndm.odm.omm.OmmMetadataKey
Description of the Mean Element Theory.
MEAN_LAT_ARG - Static variable in enum org.orekit.orbits.OrbitType
Name for mean argument of latitude.
MEAN_LON_ARG - Static variable in enum org.orekit.orbits.OrbitType
Name for mean argument of longitude.
MEAN_MOTION - org.orekit.files.ccsds.ndm.odm.KeplerianElementsKey
Mean motion.
MEAN_MOTION_DDOT - org.orekit.files.ccsds.ndm.odm.omm.OmmTleKey
Second time derivative of mean motion.
MEAN_MOTION_DOT - org.orekit.files.ccsds.ndm.odm.omm.OmmTleKey
First time derivative of mean motion.
MEAN_OF_DATE - org.orekit.files.stk.STKEphemerisFile.STKCoordinateSystem
Mean equator and mean equinox of date.
meanDerivative(AbsoluteDate, int, int) - Method in class org.orekit.utils.SecularAndHarmonic
Get mean derivative, truncated to first components.
meanSecondDerivative(AbsoluteDate, int, int) - Method in class org.orekit.utils.SecularAndHarmonic
Get mean second derivative, truncated to first components.
meanToEccentric(double, double, double) - Static method in class org.orekit.orbits.CircularLatitudeArgumentUtility
Computes the eccentric latitude argument from the mean latitude argument.
meanToEccentric(double, double, double) - Static method in class org.orekit.orbits.CircularOrbit
Deprecated.
meanToEccentric(double, double, double) - Static method in class org.orekit.orbits.EquinoctialLongitudeArgumentUtility
Computes the eccentric longitude argument from the mean longitude argument.
meanToEccentric(double, double, double) - Static method in class org.orekit.orbits.EquinoctialOrbit
Deprecated.
meanToEccentric(T, T, T) - Static method in class org.orekit.orbits.FieldCircularLatitudeArgumentUtility
Computes the eccentric latitude argument from the mean latitude argument.
meanToEccentric(T, T, T) - Static method in class org.orekit.orbits.FieldCircularOrbit
Deprecated.
meanToEccentric(T, T, T) - Static method in class org.orekit.orbits.FieldEquinoctialLongitudeArgumentUtility
Computes the eccentric longitude argument from the mean longitude argument.
meanToEccentric(T, T, T) - Static method in class org.orekit.orbits.FieldEquinoctialOrbit
Deprecated.
meanToTrue(double, double, double) - Static method in class org.orekit.orbits.CircularLatitudeArgumentUtility
Computes the true latitude argument from the eccentric latitude argument.
meanToTrue(double, double, double) - Static method in class org.orekit.orbits.EquinoctialLongitudeArgumentUtility
Computes the true longitude argument from the eccentric longitude argument.
meanToTrue(T, T, T) - Static method in class org.orekit.orbits.FieldCircularLatitudeArgumentUtility
Computes the true latitude argument from the eccentric latitude argument.
meanToTrue(T, T, T) - Static method in class org.orekit.orbits.FieldEquinoctialLongitudeArgumentUtility
Computes the true longitude argument from the eccentric longitude argument.
meanValue(AbsoluteDate, int, int) - Method in class org.orekit.utils.SecularAndHarmonic
Get mean value, truncated to first components.
MEASUREMENT_TYPE - Static variable in class org.orekit.estimation.measurements.AngularAzEl
Type of the measurement.
MEASUREMENT_TYPE - Static variable in class org.orekit.estimation.measurements.AngularRaDec
Type of the measurement.
MEASUREMENT_TYPE - Static variable in class org.orekit.estimation.measurements.BistaticRange
Type of the measurement.
MEASUREMENT_TYPE - Static variable in class org.orekit.estimation.measurements.BistaticRangeRate
Type of the measurement.
MEASUREMENT_TYPE - Static variable in class org.orekit.estimation.measurements.FDOA
Type of the measurement.
MEASUREMENT_TYPE - Static variable in class org.orekit.estimation.measurements.gnss.InterSatellitesOneWayRangeRate
Type of the measurement.
MEASUREMENT_TYPE - Static variable in class org.orekit.estimation.measurements.gnss.InterSatellitesPhase
Type of the measurement.
MEASUREMENT_TYPE - Static variable in class org.orekit.estimation.measurements.gnss.OneWayGNSSPhase
Type of the measurement.
MEASUREMENT_TYPE - Static variable in class org.orekit.estimation.measurements.gnss.OneWayGNSSRange
Type of the measurement.
MEASUREMENT_TYPE - Static variable in class org.orekit.estimation.measurements.gnss.OneWayGNSSRangeRate
Type of the measurement.
MEASUREMENT_TYPE - Static variable in class org.orekit.estimation.measurements.gnss.Phase
Type of the measurement.
MEASUREMENT_TYPE - Static variable in class org.orekit.estimation.measurements.InterSatellitesRange
Type of the measurement.
MEASUREMENT_TYPE - Static variable in class org.orekit.estimation.measurements.MultiplexedMeasurement
Type of the measurement.
MEASUREMENT_TYPE - Static variable in class org.orekit.estimation.measurements.Position
Type of the measurement.
MEASUREMENT_TYPE - Static variable in class org.orekit.estimation.measurements.PV
Type of the measurement.
MEASUREMENT_TYPE - Static variable in class org.orekit.estimation.measurements.Range
Type of the measurement.
MEASUREMENT_TYPE - Static variable in class org.orekit.estimation.measurements.RangeRate
Type of the measurement.
MEASUREMENT_TYPE - Static variable in class org.orekit.estimation.measurements.TDOA
Type of the measurement.
MEASUREMENT_TYPE - Static variable in class org.orekit.estimation.measurements.TurnAroundRange
Type of the measurement.
MeasurementBuilder<T extends ObservedMeasurement<T>> - Interface in org.orekit.estimation.measurements.generation
Interface for generating individual measurements.
MeasurementCombination - Interface in org.orekit.estimation.measurements.gnss
Interface for combination of measurements.
MeasurementCombinationFactory - Class in org.orekit.estimation.measurements.gnss
Factory for predefined combination of measurements.
MeasurementDecorator - Class in org.orekit.estimation.sequential
Decorator adding Measurement API to an ObservedMeasurement.
MeasurementDecorator(ObservedMeasurement<?>, RealMatrix, AbsoluteDate) - Constructor for class org.orekit.estimation.sequential.MeasurementDecorator
Simple constructor.
MeasurementFilter<T extends ObservedMeasurement<T>> - Interface in org.orekit.estimation.measurements.filtering
Interface for measurement pre-processing filter.
measurementIsFeasible(double) - Method in enum org.orekit.estimation.measurements.generation.SignSemantic
Check if measurement is feasible.
measurementIsFeasible(AbsoluteDate) - Method in class org.orekit.estimation.measurements.generation.AbstractScheduler
Check if a measurement is feasible at some date.
measurementIsFeasible(AbsoluteDate) - Method in class org.orekit.estimation.measurements.generation.ContinuousScheduler
Check if a measurement is feasible at some date.
measurementIsFeasible(AbsoluteDate) - Method in class org.orekit.estimation.measurements.generation.EventBasedScheduler
Check if a measurement is feasible at some date.
MeasurementType - Enum in org.orekit.gnss
Enumerate for measurement type.
MEDIAN_SUFFIX - Static variable in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector
Default suffix for median driver.
MEDIAN_SUFFIX - Static variable in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector
Default suffix for median driver.
MedianDate - Class in org.orekit.forces.maneuvers.jacobians
Generator for one column of a Jacobian matrix for special case of maneuver median date.
MedianDate(String, String, String) - Constructor for class org.orekit.forces.maneuvers.jacobians.MedianDate
Simple constructor.
MELBOURNE_WUBBENA - org.orekit.estimation.measurements.gnss.CombinationType
Melbourne-Wübbena combination.
MelbourneWubbenaCombination - Class in org.orekit.estimation.measurements.gnss
Melbourne-Wübbena combination.
MendesPavlisModel - Class in org.orekit.models.earth.troposphere
The Mendes - Pavlis tropospheric delay model for optical techniques.
MendesPavlisModel(double, double, double, double) - Constructor for class org.orekit.models.earth.troposphere.MendesPavlisModel
MendesPavlisModel(PressureTemperatureHumidityProvider, double, Unit) - Constructor for class org.orekit.models.earth.troposphere.MendesPavlisModel
Create a new Mendes-Pavlis model for the troposphere.
MEO - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCategory
Medium Earth Orbit, 2000 < hp < 31570 km, 2000 < ha < 31570 km.
MEO - org.orekit.propagation.analytical.gnss.data.BeidouSatelliteType
Middle Earth Orbit.
MERCURY - org.orekit.bodies.JPLEphemeridesLoader.EphemerisType
Constant for Mercury.
MERCURY - org.orekit.files.ccsds.definitions.CenterName
Mercury body.
MERCURY - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Mercury.
MESSAGE_FOR - org.orekit.files.ccsds.ndm.cdm.CdmHeaderKey
Creating spacecraft name for which the CDM is provided.
MESSAGE_ID - org.orekit.files.ccsds.section.HeaderKey
ID that uniquely identifies a message from a given originator.
messageAvailable(String, ParsedMessage) - Method in interface org.orekit.gnss.metric.ntrip.MessageObserver
Notify that an encoded message is available.
messageNumberToSatelliteSystem(int) - Static method in enum org.orekit.gnss.metric.parser.IgsSsrMessageType
Find the satellite system corresponding to the sub-type message number.
MessageObserver - Interface in org.orekit.gnss.metric.ntrip
Interface for objects that needs to be notified when new encoded messages are available.
MessageParser<T> - Interface in org.orekit.files.ccsds.utils.lexical
Parser for CCSDS messages.
MessagesParser - Class in org.orekit.gnss.metric.parser
Parser for IGS encoded messages.
MessagesParser(List<Integer>) - Constructor for class org.orekit.gnss.metric.parser.MessagesParser
Constructor.
MessageType - Interface in org.orekit.gnss.metric.parser
Interface for encoded message types.
MessageVersionXmlTokenBuilder - Class in org.orekit.files.ccsds.utils.lexical
Builder for the root element with CCSDS message version.
MessageVersionXmlTokenBuilder() - Constructor for class org.orekit.files.ccsds.utils.lexical.MessageVersionXmlTokenBuilder
Empty constructor.
MessageWriter<H extends Header,​S extends Segment<?,​?>,​F extends NdmConstituent<H,​S>> - Interface in org.orekit.files.ccsds.utils.generation
Interface for writing Navigation Data Message (NDM) files.
MET - org.orekit.files.ccsds.definitions.TimeSystem
Mission Elapsed Time.
META - org.orekit.files.ccsds.section.KvnStructureKey
Metadata structure.
metadata - org.orekit.files.ccsds.section.XmlStructureKey
XML metadata structure.
Metadata - Class in org.orekit.files.ccsds.section
This class gathers the meta-data present in the Navigation Data Message (ADM, ODM and TDM).
Metadata(TimeSystem) - Constructor for class org.orekit.files.ccsds.section.Metadata
Simple constructor.
MetadataKey - Enum in org.orekit.files.ccsds.section
Keys for NDM Metadata entries.
Meteo(SortedSet<CRD.MeteorologicalMeasurement>) - Constructor for class org.orekit.files.ilrs.CRD.Meteo
Constructor.
MeteorologicalConfiguration() - Constructor for class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
Empty constructor.
MeteorologicalMeasurement(AbsoluteDate, double, double, double) - Constructor for class org.orekit.files.ilrs.CRD.MeteorologicalMeasurement
Constructor.
MeteorologicalMeasurement(AbsoluteDate, double, double, double, int) - Constructor for class org.orekit.files.ilrs.CRD.MeteorologicalMeasurement
Constructor.
metersToRu(TdmMetadata, AbsoluteDate, double) - Method in class org.orekit.files.ccsds.ndm.tdm.IdentityConverter
Convert a range expressed in meters.
metersToRu(TdmMetadata, AbsoluteDate, double) - Method in interface org.orekit.files.ccsds.ndm.tdm.RangeUnitsConverter
Convert a range expressed in meters.
METHOD_NOT_AVAILABLE_WITHOUT_CENTRAL_BODY - org.orekit.errors.OrekitMessages
METHOD_NOT_AVAILABLE_WITHOUT_CENTRAL_BODY.
METRE - Static variable in class org.orekit.utils.units.Unit
Metre unit.
MF - Static variable in class org.orekit.models.earth.displacement.Tide
Mf tide.
MGO - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCategory
MEO-GEO Crossing Orbit, 2000 < hp < 31570 km, 31570 < ha < 40002 km.
MHZ_TO_HZ - Static variable in class org.orekit.estimation.measurements.gnss.AbstractDualFrequencyCombination
Mega Hertz to Hertz converter.
MICRO_ARC_SECONDS - org.orekit.data.PolynomialParser.Unit
Micro arc-seconds angles.
MICRO_M - Static variable in class org.orekit.models.earth.troposphere.TroposphericModelUtils
Micrometers unit.
MIDDLE - org.orekit.files.ccsds.ndm.tdm.IntegrationReference
Time tag in the middle of integration interval.
MidpointFieldIntegratorBuilder<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.conversion
Builder for MidpointFieldIntegrator.
MidpointFieldIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.MidpointFieldIntegratorBuilder
Constructor.
MidpointFieldIntegratorBuilder(T) - Constructor for class org.orekit.propagation.conversion.MidpointFieldIntegratorBuilder
Constructor using a "fielded" step.
MidpointIntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for MidpointIntegrator.
MidpointIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.MidpointIntegratorBuilder
Build a new instance.
MILLI_ARC_SECONDS - org.orekit.data.PolynomialParser.Unit
Milli arc-seconds angles.
MILLI_ARC_SECONDS_TO_RADIANS - Static variable in class org.orekit.utils.units.UnitsConverter
Milli arcseconds to radians converter.
MILLI_SECONDS_TO_SECONDS - Static variable in class org.orekit.utils.units.UnitsConverter
Milli seconds to seconds converter.
MIN_EPOCH - Static variable in class org.orekit.time.DateComponents
Maximum supported date.
minStep - Variable in class org.orekit.propagation.conversion.AbstractVariableStepFieldIntegratorBuilder
Minimum step size (s).
minStep - Variable in class org.orekit.propagation.conversion.AbstractVariableStepIntegratorBuilder
Minimum step size (s).
MINUS_MOMENTUM - org.orekit.frames.LocalMagneticFieldFrame.LOFBuilderVector
Negative orbital momentum vector.
MINUS_POSITION - org.orekit.frames.LocalMagneticFieldFrame.LOFBuilderVector
Negative position vector.
MINUS_VELOCITY - org.orekit.frames.LocalMagneticFieldFrame.LOFBuilderVector
Negative velocity vector.
MINUTE - Static variable in class org.orekit.utils.units.Unit
Minute unit.
minuteDuration(AbsoluteDate) - Method in class org.orekit.time.GLONASSScale
Check length of the current minute in this time scale.
minuteDuration(AbsoluteDate) - Method in interface org.orekit.time.TimeScale
Check length of the current minute in this time scale.
minuteDuration(AbsoluteDate) - Method in class org.orekit.time.UTCScale
Check length of the current minute in this time scale.
minuteDuration(FieldAbsoluteDate<T>) - Method in class org.orekit.time.GLONASSScale
Check length of the current minute in this time scale.
minuteDuration(FieldAbsoluteDate<T>) - Method in interface org.orekit.time.TimeScale
Check length of the current minute in this time scale.
minuteDuration(FieldAbsoluteDate<T>) - Method in class org.orekit.time.UTCScale
Check length of the current minute in this time scale.
MINUTES_PER_DAY - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
Time units per julian day.
minValueChanged(double, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver
Notify that a parameter minimum value has been changed.
MISMATCHED_FREQUENCIES - org.orekit.errors.OrekitMessages
MISMATCHED_FREQUENCIES.
MISS_DISTANCE - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
Norm of relative position vector at TCA.
MISSING_EARTH_ORIENTATION_PARAMETERS_BETWEEN_DATES - org.orekit.errors.OrekitMessages
MISSING_EARTH_ORIENTATION_PARAMETERS_BETWEEN_DATES.
MISSING_EARTH_ORIENTATION_PARAMETERS_BETWEEN_DATES_GAP - org.orekit.errors.OrekitMessages
MISSING_EARTH_ORIENTATION_PARAMETERS_BETWEEN_DATES_GAP.
MISSING_GRAVITY_FIELD_COEFFICIENT_IN_FILE - org.orekit.errors.OrekitMessages
MISSING_GRAVITY_FIELD_COEFFICIENT_IN_FILE.
MISSING_HEADER - org.orekit.errors.OrekitMessages
MISSING_HEADER.
MISSING_SECOND_TLE_LINE - org.orekit.errors.OrekitMessages
MISSING_SECOND_TLE_LINE.
MISSING_SERIE_J_IN_FILE - org.orekit.errors.OrekitMessages
MISSING_SERIE_J_IN_FILE.
MISSING_STATION_DATA_FOR_EPOCH - org.orekit.errors.OrekitMessages
MISSING_STATION_DATA_FOR_EPOCH.
MISSING_VELOCITY - org.orekit.errors.OrekitMessages
MISSING_VELOCITY.
missingCoefficientsAllowed() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Check if missing coefficients are allowed in the input data.
MIXED - org.orekit.files.ilrs.CRDHeader.RangeType
Mixed.
MIXED - org.orekit.files.sp3.DataUsed
Mixed data.
MIXED - org.orekit.files.sp3.SP3FileType
Mixed file.
MIXED - org.orekit.gnss.SatelliteSystem
Mixed system.
MM - Static variable in class org.orekit.gnss.metric.parser.Units
Millimetres units.
MM - Static variable in class org.orekit.models.earth.displacement.Tide
Mm tide.
MM_PER_S - Static variable in class org.orekit.gnss.metric.parser.Units
Millimetres per second units.
MM_PER_S2 - Static variable in class org.orekit.gnss.metric.parser.Units
Millimetres per square second units.
MOD_CONVENTIONS_1996 - org.orekit.frames.Predefined
MOD, IERS 1996 conventions.
MOD_CONVENTIONS_2003 - org.orekit.frames.Predefined
MOD, IERS 2003 conventions.
MOD_CONVENTIONS_2010 - org.orekit.frames.Predefined
MOD, IERS 2010 conventions.
MOD_WITHOUT_EOP_CORRECTIONS - org.orekit.frames.Predefined
MOD, IERS 1996 conventions without EOP corrections.
MODE - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Mode entry.
modelCalled(Orbit[], Map<ObservedMeasurement<?>, EstimatedMeasurement<?>>) - Method in interface org.orekit.estimation.leastsquares.ModelObserver
Notification callback for orbit changes.
ModelObserver - Interface in org.orekit.estimation.leastsquares
Observer for model calls.
MODIFIED_JULIAN_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Reference epoch for modified julian dates: 1858-11-17T00:00:00 Terrestrial Time.
MODIFIED_JULIAN_EPOCH - Static variable in class org.orekit.time.DateComponents
Reference epoch for modified julian dates: 1858-11-17.
ModifiedFrame - Class in org.orekit.files.ccsds.definitions
A reference frame created from the REF_FRAME and CENTER_NAME is a CCSDS OPM, OMM, or OEM file.
ModifiedFrame(Frame, CelestialBodyFrame, CelestialBody, String) - Constructor for class org.orekit.files.ccsds.definitions.ModifiedFrame
Create a CCSDS reference frame by changing the origin of an existing frame.
ModifiedHopfieldModel - Class in org.orekit.models.earth.troposphere
The modified Hopfield model.
ModifiedHopfieldModel() - Constructor for class org.orekit.models.earth.troposphere.ModifiedHopfieldModel
Create a new Hopfield model.
ModifiedLambdaMethod - Class in org.orekit.estimation.measurements.gnss
Decorrelation/reduction engine for Modified LAMBDA method.
ModifiedLambdaMethod() - Constructor for class org.orekit.estimation.measurements.gnss.ModifiedLambdaMethod
Empty constructor.
ModifiedSaastamoinenModel - Class in org.orekit.models.earth.troposphere
The modified Saastamoinen model.
ModifiedSaastamoinenModel(double, double, double) - Constructor for class org.orekit.models.earth.troposphere.ModifiedSaastamoinenModel
ModifiedSaastamoinenModel(double, double, double, String) - Constructor for class org.orekit.models.earth.troposphere.ModifiedSaastamoinenModel
ModifiedSaastamoinenModel(double, double, double, String, DataProvidersManager) - Constructor for class org.orekit.models.earth.troposphere.ModifiedSaastamoinenModel
ModifiedSaastamoinenModel(PressureTemperatureHumidityProvider) - Constructor for class org.orekit.models.earth.troposphere.ModifiedSaastamoinenModel
Create a new Saastamoinen model for the troposphere using the given environmental conditions and table from the reference book.
ModifiedSaastamoinenModel(PressureTemperatureHumidityProvider, String) - Constructor for class org.orekit.models.earth.troposphere.ModifiedSaastamoinenModel
Create a new Saastamoinen model for the troposphere using the given environmental conditions.
ModifiedSaastamoinenModel(PressureTemperatureHumidityProvider, String, DataProvidersManager) - Constructor for class org.orekit.models.earth.troposphere.ModifiedSaastamoinenModel
Create a new Saastamoinen model for the troposphere using the given environmental conditions.
ModifierGradientConverter - Class in org.orekit.estimation.measurements.modifiers
Converter for states and parameters arrays.
ModifierGradientConverter(SpacecraftState, int, AttitudeProvider) - Constructor for class org.orekit.estimation.measurements.modifiers.ModifierGradientConverter
Simple constructor.
modify(EstimatedMeasurement<AngularRaDec>) - Method in class org.orekit.estimation.measurements.modifiers.AberrationModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<BistaticRange>) - Method in class org.orekit.estimation.measurements.modifiers.BistaticRangeIonosphericDelayModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<BistaticRange>) - Method in class org.orekit.estimation.measurements.modifiers.BistaticRangeTroposphericDelayModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<BistaticRangeRate>) - Method in class org.orekit.estimation.measurements.modifiers.BistaticRangeRateIonosphericDelayModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<BistaticRangeRate>) - Method in class org.orekit.estimation.measurements.modifiers.BistaticRangeRateTroposphericDelayModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<InterSatellitesPhase>) - Method in class org.orekit.estimation.measurements.modifiers.InterSatellitesPhaseAmbiguityModifier
Deprecated.
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<OneWayGNSSPhase>) - Method in class org.orekit.estimation.measurements.modifiers.OneWayGNSSPhaseAmbiguityModifier
Deprecated.
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<Phase>) - Method in class org.orekit.estimation.measurements.modifiers.PhaseAmbiguityModifier
Deprecated.
 
modify(EstimatedMeasurement<Phase>) - Method in class org.orekit.estimation.measurements.modifiers.PhaseIonosphericDelayModifier
 
modify(EstimatedMeasurement<Phase>) - Method in class org.orekit.estimation.measurements.modifiers.PhaseTroposphericDelayModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<Range>) - Method in class org.orekit.estimation.measurements.modifiers.RangeIonosphericDelayModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<Range>) - Method in class org.orekit.estimation.measurements.modifiers.RangeTroposphericDelayModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<RangeRate>) - Method in class org.orekit.estimation.measurements.modifiers.RangeRateIonosphericDelayModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<RangeRate>) - Method in class org.orekit.estimation.measurements.modifiers.RangeRateTroposphericDelayModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<TDOA>) - Method in class org.orekit.estimation.measurements.modifiers.TDOAIonosphericDelayModifier
 
modify(EstimatedMeasurement<TDOA>) - Method in class org.orekit.estimation.measurements.modifiers.TDOATroposphericDelayModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<TurnAroundRange>) - Method in class org.orekit.estimation.measurements.modifiers.TurnAroundRangeIonosphericDelayModifier
 
modify(EstimatedMeasurement<TurnAroundRange>) - Method in class org.orekit.estimation.measurements.modifiers.TurnAroundRangeTroposphericDelayModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<T>) - Method in interface org.orekit.estimation.measurements.EstimationModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<T>) - Method in class org.orekit.estimation.measurements.modifiers.Bias
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<T>) - Method in class org.orekit.estimation.measurements.modifiers.DynamicOutlierFilter
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<T>, ParameterDriversProvider, AbstractGradientConverter, GroundStation, ParametricModelEffect, ParametricModelEffectGradient) - Static method in class org.orekit.estimation.measurements.modifiers.RangeModifierUtil
modify(EstimatedMeasurement<T>, ParameterDriversProvider, AbstractGradientConverter, GroundStation, ParametricModelEffect, ParametricModelEffectGradient) - Static method in class org.orekit.estimation.measurements.modifiers.RangeRateModifierUtil
modify(EstimatedMeasurement<T>, ParameterDriversProvider, AbstractGradientConverter, GroundStation, ParametricModelEffect, ParametricModelEffectGradient, EstimationModifier<T>) - Static method in class org.orekit.estimation.measurements.modifiers.RangeModifierUtil
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<T>, ParameterDriversProvider, AbstractGradientConverter, GroundStation, ParametricModelEffect, ParametricModelEffectGradient, EstimationModifier<T>) - Static method in class org.orekit.estimation.measurements.modifiers.RangeRateModifierUtil
Apply a modifier to an estimated measurement.
modifyEstimatedValue(EstimationModifier<T>, double...) - Method in class org.orekit.estimation.measurements.EstimatedMeasurementBase
Modify the estimated value.
modifyWithoutDerivatives(EstimatedMeasurementBase<AngularAzEl>) - Method in class org.orekit.estimation.measurements.modifiers.AngularIonosphericDelayModifier
 
modifyWithoutDerivatives(EstimatedMeasurementBase<AngularAzEl>) - Method in class org.orekit.estimation.measurements.modifiers.AngularRadioRefractionModifier
 
modifyWithoutDerivatives(EstimatedMeasurementBase<AngularAzEl>) - Method in class org.orekit.estimation.measurements.modifiers.AngularTroposphericDelayModifier
Deprecated.
 
modifyWithoutDerivatives(EstimatedMeasurementBase<AngularRaDec>) - Method in class org.orekit.estimation.measurements.modifiers.AberrationModifier
Apply a modifier to an estimated measurement without derivatives.
modifyWithoutDerivatives(EstimatedMeasurementBase<BistaticRange>) - Method in class org.orekit.estimation.measurements.modifiers.BistaticRangeIonosphericDelayModifier
Apply a modifier to an estimated measurement without derivatives.
modifyWithoutDerivatives(EstimatedMeasurementBase<BistaticRange>) - Method in class org.orekit.estimation.measurements.modifiers.BistaticRangeTroposphericDelayModifier
Apply a modifier to an estimated measurement without derivatives.
modifyWithoutDerivatives(EstimatedMeasurementBase<BistaticRangeRate>) - Method in class org.orekit.estimation.measurements.modifiers.BistaticRangeRateIonosphericDelayModifier
Apply a modifier to an estimated measurement without derivatives.
modifyWithoutDerivatives(EstimatedMeasurementBase<BistaticRangeRate>) - Method in class org.orekit.estimation.measurements.modifiers.BistaticRangeRateTroposphericDelayModifier
Apply a modifier to an estimated measurement without derivatives.
modifyWithoutDerivatives(EstimatedMeasurementBase<InterSatellitesOneWayRangeRate>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockInterSatellitesOneWayRangeRateModifier
Apply a modifier to an estimated measurement without derivatives.
modifyWithoutDerivatives(EstimatedMeasurementBase<InterSatellitesPhase>) - Method in class org.orekit.estimation.measurements.modifiers.InterSatellitesPhaseAmbiguityModifier
Deprecated.
Apply a modifier to an estimated measurement without derivatives.
modifyWithoutDerivatives(EstimatedMeasurementBase<InterSatellitesPhase>) - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaInterSatellitesPhaseModifier
 
modifyWithoutDerivatives(EstimatedMeasurementBase<InterSatellitesPhase>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockInterSatellitesPhaseModifier
Apply a modifier to an estimated measurement without derivatives.
modifyWithoutDerivatives(EstimatedMeasurementBase<InterSatellitesPhase>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockInterSatellitesPhaseModifier
Apply a modifier to an estimated measurement without derivatives.
modifyWithoutDerivatives(EstimatedMeasurementBase<InterSatellitesPhase>) - Method in class org.orekit.estimation.measurements.modifiers.ShapiroInterSatellitePhaseModifier
Apply a modifier to an estimated measurement without derivatives.
modifyWithoutDerivatives(EstimatedMeasurementBase<OneWayGNSSPhase>) - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaOneWayGNSSPhaseModifier
Apply a modifier to an estimated measurement without derivatives.
modifyWithoutDerivatives(EstimatedMeasurementBase<OneWayGNSSPhase>) - Method in class org.orekit.estimation.measurements.modifiers.OneWayGNSSPhaseAmbiguityModifier
Deprecated.
Apply a modifier to an estimated measurement without derivatives.
modifyWithoutDerivatives(EstimatedMeasurementBase<OneWayGNSSPhase>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockOneWayGNSSPhaseModifier
Apply a modifier to an estimated measurement without derivatives.
modifyWithoutDerivatives(EstimatedMeasurementBase<OneWayGNSSPhase>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockOneWayGNSSPhaseModifier
Apply a modifier to an estimated measurement without derivatives.
modifyWithoutDerivatives(EstimatedMeasurementBase<OneWayGNSSPhase>) - Method in class org.orekit.estimation.measurements.modifiers.ShapiroOneWayGNSSPhaseModifier
Apply a modifier to an estimated measurement without derivatives.
modifyWithoutDerivatives(EstimatedMeasurementBase<OneWayGNSSRange>) - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaOneWayGNSSRangeModifier
Apply a modifier to an estimated measurement without derivatives.
modifyWithoutDerivatives(EstimatedMeasurementBase<OneWayGNSSRange>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockOneWayGNSSRangeModifier
Apply a modifier to an estimated measurement without derivatives.
modifyWithoutDerivatives(EstimatedMeasurementBase<OneWayGNSSRange>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockOneWayGNSSRangeModifier
Apply a modifier to an estimated measurement without derivatives.
modifyWithoutDerivatives(EstimatedMeasurementBase<OneWayGNSSRange>) - Method in class org.orekit.estimation.measurements.modifiers.ShapiroOneWayGNSSRangeModifier
Apply a modifier to an estimated measurement without derivatives.
modifyWithoutDerivatives(EstimatedMeasurementBase<OneWayGNSSRangeRate>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockOneWayGNSSRangeRateModifier
Apply a modifier to an estimated measurement without derivatives.
modifyWithoutDerivatives(EstimatedMeasurementBase<Phase>) - Method in class org.orekit.estimation.measurements.modifiers.PhaseAmbiguityModifier
Deprecated.
 
modifyWithoutDerivatives(EstimatedMeasurementBase<Phase>) - Method in class org.orekit.estimation.measurements.modifiers.PhaseCentersPhaseModifier
Apply a modifier to an estimated measurement without derivatives.
modifyWithoutDerivatives(EstimatedMeasurementBase<Phase>) - Method in class org.orekit.estimation.measurements.modifiers.PhaseIonosphericDelayModifier
 
modifyWithoutDerivatives(EstimatedMeasurementBase<Phase>) - Method in class org.orekit.estimation.measurements.modifiers.PhaseTroposphericDelayModifier
Apply a modifier to an estimated measurement without derivatives.
modifyWithoutDerivatives(EstimatedMeasurementBase<Phase>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockPhaseModifier
Apply a modifier to an estimated measurement without derivatives.
modifyWithoutDerivatives(EstimatedMeasurementBase<Phase>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockPhaseModifier
Apply a modifier to an estimated measurement without derivatives.
modifyWithoutDerivatives(EstimatedMeasurementBase<Phase>) - Method in class org.orekit.estimation.measurements.modifiers.ShapiroPhaseModifier
Apply a modifier to an estimated measurement without derivatives.
modifyWithoutDerivatives(EstimatedMeasurementBase<InterSatellitesRange>) - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaInterSatellitesRangeModifier
Apply a modifier to an estimated measurement without derivatives.
modifyWithoutDerivatives(EstimatedMeasurementBase<InterSatellitesRange>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockInterSatellitesRangeModifier
Apply a modifier to an estimated measurement without derivatives.
modifyWithoutDerivatives(EstimatedMeasurementBase<InterSatellitesRange>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockInterSatellitesRangeModifier
Apply a modifier to an estimated measurement without derivatives.
modifyWithoutDerivatives(EstimatedMeasurementBase<InterSatellitesRange>) - Method in class org.orekit.estimation.measurements.modifiers.ShapiroInterSatelliteRangeModifier
Apply a modifier to an estimated measurement without derivatives.
modifyWithoutDerivatives(EstimatedMeasurementBase<Range>) - Method in class org.orekit.estimation.measurements.modifiers.PhaseCentersRangeModifier
Apply a modifier to an estimated measurement without derivatives.
modifyWithoutDerivatives(EstimatedMeasurementBase<Range>) - Method in class org.orekit.estimation.measurements.modifiers.RangeIonosphericDelayModifier
Apply a modifier to an estimated measurement without derivatives.
modifyWithoutDerivatives(EstimatedMeasurementBase<Range>) - Method in class org.orekit.estimation.measurements.modifiers.RangeTroposphericDelayModifier
Apply a modifier to an estimated measurement without derivatives.
modifyWithoutDerivatives(EstimatedMeasurementBase<Range>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockRangeModifier
Apply a modifier to an estimated measurement without derivatives.
modifyWithoutDerivatives(EstimatedMeasurementBase<Range>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockRangeModifier
Apply a modifier to an estimated measurement without derivatives.
modifyWithoutDerivatives(EstimatedMeasurementBase<Range>) - Method in class org.orekit.estimation.measurements.modifiers.ShapiroRangeModifier
Apply a modifier to an estimated measurement without derivatives.
modifyWithoutDerivatives(EstimatedMeasurementBase<RangeRate>) - Method in class org.orekit.estimation.measurements.modifiers.RangeRateIonosphericDelayModifier
Apply a modifier to an estimated measurement without derivatives.
modifyWithoutDerivatives(EstimatedMeasurementBase<RangeRate>) - Method in class org.orekit.estimation.measurements.modifiers.RangeRateTroposphericDelayModifier
Apply a modifier to an estimated measurement without derivatives.
modifyWithoutDerivatives(EstimatedMeasurementBase<RangeRate>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockRangeRateModifier
Apply a modifier to an estimated measurement without derivatives.
modifyWithoutDerivatives(EstimatedMeasurementBase<TDOA>) - Method in class org.orekit.estimation.measurements.modifiers.TDOAIonosphericDelayModifier
 
modifyWithoutDerivatives(EstimatedMeasurementBase<TDOA>) - Method in class org.orekit.estimation.measurements.modifiers.TDOATroposphericDelayModifier
Apply a modifier to an estimated measurement without derivatives.
modifyWithoutDerivatives(EstimatedMeasurementBase<TurnAroundRange>) - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaTurnAroundRangeModifier
Apply a modifier to an estimated measurement without derivatives.
modifyWithoutDerivatives(EstimatedMeasurementBase<TurnAroundRange>) - Method in class org.orekit.estimation.measurements.modifiers.TurnAroundRangeIonosphericDelayModifier
 
modifyWithoutDerivatives(EstimatedMeasurementBase<TurnAroundRange>) - Method in class org.orekit.estimation.measurements.modifiers.TurnAroundRangeTroposphericDelayModifier
Apply a modifier to an estimated measurement without derivatives.
modifyWithoutDerivatives(EstimatedMeasurementBase<T>) - Method in interface org.orekit.estimation.measurements.EstimationModifier
Apply a modifier to an estimated measurement without derivatives.
modifyWithoutDerivatives(EstimatedMeasurementBase<T>) - Method in class org.orekit.estimation.measurements.gnss.AbstractWindUp
Apply a modifier to an estimated measurement without derivatives.
modifyWithoutDerivatives(EstimatedMeasurementBase<T>) - Method in class org.orekit.estimation.measurements.modifiers.Bias
Apply a modifier to an estimated measurement without derivatives.
modifyWithoutDerivatives(EstimatedMeasurementBase<T>) - Method in class org.orekit.estimation.measurements.modifiers.OutlierFilter
Apply a modifier to an estimated measurement without derivatives.
modifyWithoutDerivatives(EstimatedMeasurementBase<T>, double, double, double, double) - Method in class org.orekit.estimation.measurements.modifiers.AbstractRelativisticClockOnBoardRangeRateModifier
Apply relativistic frequency deviation.
modifyWithoutDerivatives(EstimatedMeasurementBase<T>, GroundStation, ParametricModelEffect) - Static method in class org.orekit.estimation.measurements.modifiers.RangeModifierUtil
modifyWithoutDerivatives(EstimatedMeasurementBase<T>, GroundStation, ParametricModelEffect) - Static method in class org.orekit.estimation.measurements.modifiers.RangeRateModifierUtil
modifyWithoutDerivatives(EstimatedMeasurementBase<T>, GroundStation, ParametricModelEffect, EstimationModifier<T>) - Static method in class org.orekit.estimation.measurements.modifiers.RangeModifierUtil
Apply a modifier to an estimated measurement.
modifyWithoutDerivatives(EstimatedMeasurementBase<T>, GroundStation, ParametricModelEffect, EstimationModifier<T>) - Static method in class org.orekit.estimation.measurements.modifiers.RangeRateModifierUtil
Apply a modifier to an estimated measurement.
MODIP_GRID_NOT_LOADED - org.orekit.errors.OrekitMessages
MODIP_GRID_NOT_LOADED.
momentum(FieldVector3D<T>) - Method in class org.orekit.attitudes.FieldInertia
Compute angular momentum.
momentum(Vector3D) - Method in class org.orekit.attitudes.Inertia
Compute angular momentum.
MOMENTUM - org.orekit.attitudes.PredefinedTarget
Satellite orbital momentum.
MOMENTUM_ALPHA - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Right ascension of angular momentum vector.
MOMENTUM_ALPHA - org.orekit.files.ccsds.ndm.adm.apm.SpinStabilizedKey
Momentum right ascension entry.
MOMENTUM_DELTA - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Declination of angular momentum vector.
MOMENTUM_DELTA - org.orekit.files.ccsds.ndm.adm.apm.SpinStabilizedKey
Momentum declination entry.
monitorDetector(FieldEventDetector<T>) - Method in class org.orekit.propagation.events.FieldEventsLogger
Monitor an event detector.
monitorDetector(T) - Method in class org.orekit.propagation.events.EventsLogger
Monitor an event detector.
Month - Enum in org.orekit.time
Enumerate representing a calendar month.
MOON - org.orekit.bodies.JPLEphemeridesLoader.EphemerisType
Constant for the Moon.
MOON - org.orekit.files.ccsds.definitions.CenterName
Moon body.
MOON - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Moon.
MOON_DRACONIC_PULSATION - Static variable in class org.orekit.frames.SingleParameterFitter
Moon pulsation (one Moon draconic period).
MOON_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Moon equatorial radius: 1737400 m.
MOUNPOINT_ALREADY_CONNECTED - org.orekit.errors.OrekitMessages
MOUNPOINT_ALREADY_CONNECTED.
MRT - org.orekit.files.ccsds.definitions.TimeSystem
Mission Relative Time.
MS - org.orekit.files.rinex.clock.RinexClock.ClockDataType
Monitor measurements for the broadcast satellite clocks.
MSAS - org.orekit.files.rinex.navigation.SbasId
Multi-functional Satellite Augmentation System.
MTA - org.orekit.files.ccsds.definitions.SpacecraftBodyFrame.BaseEquipment
Magnetic Torque Assembly.
mu(double) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagatorBuilder
Sets the Earth gravity coefficient.
MU - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
Earth gravity coefficient in m³/s².
MULTIPLE_INTERPOLATOR_USED - org.orekit.errors.OrekitMessages
MULTIPLE_INTERPOLATOR_USED.
MULTIPLE_SHOOTING_UNDERCONSTRAINED - org.orekit.errors.OrekitMessages
MULTIPLE_SHOOTING_UNDERCONSTRAINED.
MultipleShooter - Class in org.orekit.utils
Multiple shooting method applicable for trajectories, in an ephemeris model.
MultipleShooter(List<SpacecraftState>, List<NumericalPropagator>, List<EpochDerivativesEquations>, double, int) - Constructor for class org.orekit.utils.MultipleShooter
Simple Constructor.
MultipleShooting - Interface in org.orekit.utils
Interface for Multiple shooting methods.
MultiplexedMeasurement - Class in org.orekit.estimation.measurements
Class multiplexing several measurements as one.
MultiplexedMeasurement(List<ObservedMeasurement<?>>) - Constructor for class org.orekit.estimation.measurements.MultiplexedMeasurement
Simple constructor.
MultiplexedMeasurementBuilder - Class in org.orekit.estimation.measurements.generation
Builder for MultiplexedMeasurement measurements.
MultiplexedMeasurementBuilder(List<MeasurementBuilder<?>>) - Constructor for class org.orekit.estimation.measurements.generation.MultiplexedMeasurementBuilder
Simple constructor.
multiply(String, Unit) - Method in class org.orekit.utils.units.Unit
Create product of units.
multiply(PolynomialFunctionMatrix) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix
Multiply the argument matrix with the current matrix.
MultiSatFixedStepHandler - Interface in org.orekit.propagation.sampling
This interface is a space-dynamics aware fixed step handler for multi-sat propagation.
MultiSatStepHandler - Interface in org.orekit.propagation.sampling
This interface is a space-dynamics aware step handler for multi-sat propagation.
MultisatStepNormalizer - Class in org.orekit.propagation.sampling
This class wraps an object implementing MultiSatFixedStepHandler into a MultiSatStepHandler.
MultisatStepNormalizer(double, MultiSatFixedStepHandler) - Constructor for class org.orekit.propagation.sampling.MultisatStepNormalizer
Simple constructor.

N

N - org.orekit.gnss.SignalCode
Beidou B1 Codeless.
N_A - org.orekit.files.ccsds.ndm.cdm.Maneuvrable
Don't know or not applicable.
N_BODY_PERTURBATIONS - org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey
N-body perturbation bodies.
N_BODY_PERTURBATIONS - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey
N-body perturbation bodies.
N_M - Static variable in class org.orekit.files.ccsds.definitions.Units
Newton metre unit.
N_M_S - Static variable in class org.orekit.files.ccsds.definitions.Units
Newton metre second unit.
N_NEIGHBORS - Static variable in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData
Size of the list.
N2 - Static variable in class org.orekit.models.earth.displacement.Tide
N₂ tide.
NADIR - org.orekit.attitudes.PredefinedTarget
Nadir.
NadirPointing - Class in org.orekit.attitudes
This class handles nadir pointing attitude provider.
NadirPointing(Frame, BodyShape) - Constructor for class org.orekit.attitudes.NadirPointing
Creates new instance.
nameChanged(String, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver
Notify that a parameter name has been changed.
NANO_M - Static variable in class org.orekit.models.earth.troposphere.TroposphericModelUtils
Nanometers unit.
NANO_TESLA - Static variable in class org.orekit.files.ccsds.definitions.Units
Nano Tesla unit.
NANO_TESLAS_TO_TESLAS - Static variable in class org.orekit.utils.units.UnitsConverter
Nano Teslas to Tesla converter.
NARROW_LANE - org.orekit.estimation.measurements.gnss.CombinationType
Narrow-lane combination.
NarrowLaneCombination - Class in org.orekit.estimation.measurements.gnss
Narrow-Lane combination.
naturalToProper(double[], GroundStation, AbsoluteDate, Frame) - Static method in class org.orekit.estimation.measurements.modifiers.AberrationModifier
Natural to proper correction for aberration of light.
naturalToProper(double[], GroundStation, AbsoluteDate, Frame, DataContext) - Static method in class org.orekit.estimation.measurements.modifiers.AberrationModifier
Natural to proper correction for aberration of light.
NAUTICAL_DAWN_DUSK_ELEVATION - Static variable in class org.orekit.propagation.events.GroundAtNightDetector
Sun elevation at nautical dawn/dusk (12° below horizon).
NAVIGATION - org.orekit.files.rinex.utils.RinexFileType
Rinex navigation (G is for Glonass navigation, in Rinex 2.X).
NavigationSystem - Enum in org.orekit.gnss.metric.ntrip
Enumerate for navigation system in DataStreamRecord.
NB_AS - Static variable in class org.orekit.gnss.rflink.gps.SubFrame4E
Number of Anti-spoofing entries.
NB_ERD - Static variable in class org.orekit.gnss.rflink.gps.SubFrame4C
Number of Estimated Range Deviations.
NB_OF_SATELLITES - org.orekit.files.rinex.section.RinexLabels
Number of satellites.
NB_PER_Y - Static variable in class org.orekit.files.ccsds.definitions.Units
#/year unit.
NB_SVH - Static variable in class org.orekit.gnss.rflink.gps.SubFrame4E
Number of SV health entries.
NB_TYPES_OF_OBSERV - org.orekit.files.rinex.section.RinexLabels
Number and types of observations.
NbsNrcSteamTable - Class in org.orekit.models.earth.weather.water
Steam table from US National Bureau of Standards (NBS) and National Research Council (NRC) of Canada.
NbsNrcSteamTable() - Constructor for class org.orekit.models.earth.weather.water.NbsNrcSteamTable
 
Ndm - Class in org.orekit.files.ccsds.ndm
CCSDS Navigation Data Message.
Ndm(List<String>, List<NdmConstituent<?, ?>>) - Constructor for class org.orekit.files.ccsds.ndm.Ndm
Simple constructor.
NDM_XML_V3_SCHEMA_LOCATION - Static variable in class org.orekit.files.ccsds.utils.generation.XmlGenerator
NDM/XML version 3 location.
NdmConstituent<H extends Header,​S extends Segment<?,​?>> - Class in org.orekit.files.ccsds.ndm
Constituents of a CCSDS Navigation Data Message.
NdmConstituent(H, List<S>, IERSConventions, DataContext) - Constructor for class org.orekit.files.ccsds.ndm.NdmConstituent
Constructor.
NdmParser - Class in org.orekit.files.ccsds.ndm
A parser for the CCSDS NDM (Navigation Data Message).
NdmParser(ParserBuilder, Function<ParseToken, List<ParseToken>>[]) - Constructor for class org.orekit.files.ccsds.ndm.NdmParser
Simple constructor.
NdmWriter - Class in org.orekit.files.ccsds.ndm
Writer for CCSDS Navigation Data Message.
NdmWriter(WriterBuilder) - Constructor for class org.orekit.files.ccsds.ndm.NdmWriter
Simple constructor.
negate() - Method in class org.orekit.attitudes.FieldInertiaAxis
Reverse the inertia axis.
negate() - Method in class org.orekit.attitudes.InertiaAxis
Reverse the inertia axis.
negate() - Method in class org.orekit.utils.FieldPVCoordinates
Get the opposite of the instance.
negate() - Method in class org.orekit.utils.PVCoordinates
Get the opposite of the instance.
NegateDetector - Class in org.orekit.propagation.events
An event detector that negates the sign on another event detector's g function.
NegateDetector(AdaptableInterval, double, int, EventHandler, EventDetector) - Constructor for class org.orekit.propagation.events.NegateDetector
Private constructor.
NegateDetector(EventDetector) - Constructor for class org.orekit.propagation.events.NegateDetector
Create a new event detector that negates an existing event detector.
NEITHER_DIRECTORY_NOR_ZIP_OR_JAR - org.orekit.errors.OrekitMessages
NEITHER_DIRECTORY_NOR_ZIP_OR_JAR.
NEPTUNE - org.orekit.bodies.JPLEphemeridesLoader.EphemerisType
Constant for Neptune.
NEPTUNE - org.orekit.files.ccsds.definitions.CenterName
Neptune body.
NEPTUNE - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Neptune.
NEQUICK_F2_FM3_NOT_LOADED - org.orekit.errors.OrekitMessages
NEQUICK_F2_FM3_NOT_LOADED.
NeQuickModel - Class in org.orekit.models.earth.ionosphere
NeQuick ionospheric delay model.
NeQuickModel(double[]) - Constructor for class org.orekit.models.earth.ionosphere.NeQuickModel
Build a new instance.
NeQuickModel(double[], TimeScale) - Constructor for class org.orekit.models.earth.ionosphere.NeQuickModel
Build a new instance.
NET - org.orekit.gnss.metric.ntrip.RecordType
Networks of data streams.
NetworkCrawler - Class in org.orekit.data
Provider for data files directly fetched from network.
NetworkCrawler(URL...) - Constructor for class org.orekit.data.NetworkCrawler
Build a data classpath crawler.
NetworkRecord - Class in org.orekit.gnss.metric.ntrip
Network record in source table.
NetworkRecord(String) - Constructor for class org.orekit.gnss.metric.ntrip.NetworkRecord
Build a data stream record by parsing a source table line.
newBlock() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.StreamingOcmWriter
Create a writer for a new OCM trajectory state history block.
newBulletinBParser(IERSConventions, ItrfVersionProvider, TimeScales) - Static method in interface org.orekit.frames.EopHistoryLoader.Parser
Create a new parser for EOP data in the Bulletin B format.
NewcombOperators - Class in org.orekit.propagation.semianalytical.dsst.utilities
Implementation of the Modified Newcomb Operators.
newEopC04Parser(IERSConventions, ItrfVersionProvider, TimeScales) - Static method in interface org.orekit.frames.EopHistoryLoader.Parser
Create a new parser for EOP data in the EOP C04 format.
newFinalsColumnsParser(IERSConventions, ItrfVersionProvider, TimeScales, boolean) - Static method in interface org.orekit.frames.EopHistoryLoader.Parser
Create a new parser for EOP data in the rapid and predicted columnar format.
newFinalsXmlParser(IERSConventions, ItrfVersionProvider, TimeScales) - Static method in interface org.orekit.frames.EopHistoryLoader.Parser
Create a new parser for EOP data in the rapid and predicted XML format.
newLine() - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Finish current line.
newLine() - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Finish current line.
newSegment() - Method in class org.orekit.files.ccsds.ndm.adm.aem.StreamingAemWriter
Create a writer for a new AEM attitude ephemeris segment.
newSegment() - Method in class org.orekit.files.ccsds.ndm.odm.oem.StreamingOemWriter
Create a writer for a new OEM ephemeris segment.
newSegment(Frame) - Method in class org.orekit.files.ilrs.StreamingCpfWriter
Create a writer for a new CPF ephemeris segment.
newTLE(FieldKeplerianOrbit<T>, FieldTLE<T>, T, TimeScale) - Static method in class org.orekit.propagation.analytical.tle.generation.TleGenerationUtil
Builds a new TLE from Keplerian parameters and a template for TLE data.
newTLE(KeplerianOrbit, TLE, double, TimeScale) - Static method in class org.orekit.propagation.analytical.tle.generation.TleGenerationUtil
Builds a new TLE from Keplerian parameters and a template for TLE data.
NEWTON - Static variable in class org.orekit.utils.units.Unit
Newton unit.
NewtonFixedBoundaryCartesianSingleShooting - Class in org.orekit.control.indirect.shooting
Class for indirect single shooting methods with Cartesian coordinates for fixed time fixed boundary.
NewtonFixedBoundaryCartesianSingleShooting(ShootingPropagationSettings, FixedTimeBoundaryOrbits, CartesianBoundaryConditionChecker) - Constructor for class org.orekit.control.indirect.shooting.NewtonFixedBoundaryCartesianSingleShooting
Constructor with boundary conditions as orbits.
NewtonFixedBoundaryCartesianSingleShooting(ShootingPropagationSettings, FixedTimeCartesianBoundaryStates, CartesianBoundaryConditionChecker) - Constructor for class org.orekit.control.indirect.shooting.NewtonFixedBoundaryCartesianSingleShooting
Constructor with boundary conditions as orbits.
NewtonianAttraction - Class in org.orekit.forces.gravity
Force model for Newtonian central body attraction.
NewtonianAttraction(double) - Constructor for class org.orekit.forces.gravity.NewtonianAttraction
Simple constructor.
next() - Method in class org.orekit.utils.TimeSpanMap.Span
Get the next time span.
next() - Method in class org.orekit.utils.TimeSpanMap.Transition
Get the next transition.
NEXT_LEAP_EPOCH - org.orekit.files.ccsds.ndm.adm.acm.AcmMetadataKey
Epoch of next leap second.
NEXT_LEAP_EPOCH - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Epoch of next leap second.
NEXT_LEAP_TAIMUTC - org.orekit.files.ccsds.ndm.adm.acm.AcmMetadataKey
Difference (TAI – UTC) in seconds incorporated at AcmMetadataKey.NEXT_LEAP_EPOCH.
NEXT_LEAP_TAIMUTC - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Difference (TAI – UTC) in seconds incorporated at OcmMetadataKey.NEXT_LEAP_EPOCH.
NEXT_MESSAGE_EPOCH - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
Scheduled UTC epoch of the next CDM associated with the event identified by CONJUNCTION_ID.
NEXT_MESSAGE_EPOCH - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Creation date of next message from a given originator.
NEXT_MESSAGE_ID - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Unique ID identifying next message from a given originator.
NICT - org.orekit.files.rinex.navigation.UtcId
UTC(NICT).
NiellMappingFunctionModel - Class in org.orekit.models.earth.troposphere
The Niell Mapping Function model for radio wavelengths.
NiellMappingFunctionModel() - Constructor for class org.orekit.models.earth.troposphere.NiellMappingFunctionModel
Builds a new instance.
NiellMappingFunctionModel(TimeScale) - Constructor for class org.orekit.models.earth.troposphere.NiellMappingFunctionModel
Builds a new instance.
NIST - org.orekit.files.rinex.navigation.UtcId
UTC(NIST).
NO - org.orekit.files.ccsds.definitions.YesNoUnknown
NO value.
NO - org.orekit.files.ccsds.ndm.cdm.Maneuvrable
Non Maneuvrable.
NO - org.orekit.files.ccsds.ndm.tdm.CorrectionApplied
Corrections have not been applied to the tracking data.
NO - org.orekit.gnss.metric.ntrip.CarrierPhase
No.
NO_CACHED_ENTRIES - org.orekit.errors.OrekitMessages
NO_CACHED_ENTRIES.
NO_DATA_GENERATED - org.orekit.errors.OrekitMessages
NO_DATA_GENERATED.
NO_DATA_IN_FILE - org.orekit.errors.OrekitMessages
NO_DATA_IN_FILE.
NO_DATA_LOADED_FOR_CELESTIAL_BODY - org.orekit.errors.OrekitMessages
NO_DATA_LOADED_FOR_CELESTIAL_BODY.
NO_EARTH_ORIENTATION_PARAMETERS - org.orekit.errors.OrekitMessages
NO_EARTH_ORIENTATION_PARAMETERS.
NO_EARTH_ORIENTATION_PARAMETERS_LOADED - org.orekit.errors.OrekitMessages
NO_EARTH_ORIENTATION_PARAMETERS_LOADED.
NO_ENTRIES_IN_IERS_UTC_TAI_HISTORY_FILE - org.orekit.errors.OrekitMessages
NO_ENTRIES_IN_IERS_UTC_TAI_HISTORY_FILE.
NO_EPOCH_IN_IONEX_HEADER - org.orekit.errors.OrekitMessages
NO_EPOCH_IN_IONEX_HEADER.
NO_GRAVITY_FIELD_DATA_LOADED - org.orekit.errors.OrekitMessages
NO_GRAVITY_FIELD_DATA_LOADED.
NO_IERS_UTC_TAI_HISTORY_DATA_LOADED - org.orekit.errors.OrekitMessages
NO_IERS_UTC_TAI_HISTORY_DATA_LOADED.
NO_INTERPOLATOR_FOR_STATE_DEFINITION - org.orekit.errors.OrekitMessages
NO_INTERPOLATOR_FOR_STATE_DEFINITION.
NO_JPL_EPHEMERIDES_BINARY_FILES_FOUND - org.orekit.errors.OrekitMessages
NO_JPL_EPHEMERIDES_BINARY_FILES_FOUND.
NO_KLOBUCHAR_ALPHA_BETA_IN_FILE - org.orekit.errors.OrekitMessages
NO_KLOBUCHAR_ALPHA_BETA_IN_FILE.
NO_LATITUDE_LONGITUDE_BONDARIES_IN_IONEX_HEADER - org.orekit.errors.OrekitMessages
NO_LATITUDE_LONGITUDE_BONDARIES_IN_IONEX_HEADER.
NO_OCEAN_TIDE_DATA_LOADED - org.orekit.errors.OrekitMessages
NO_OCEAN_TIDE_DATA_LOADED.
NO_PARAMETER - Static variable in exception org.orekit.errors.UnsupportedParameterException
String for empty parameter drivers' list.
NO_PROPAGATOR_CONFIGURED - org.orekit.errors.OrekitMessages
NO_PROPAGATOR_CONFIGURED.
NO_RANGES - org.orekit.files.ilrs.CRDHeader.RangeType
No ranges (i.e.
NO_REFERENCE_DATE_FOR_PARAMETER - org.orekit.errors.OrekitMessages
NO_REFERENCE_DATE_FOR_PARAMETER.
NO_SEM_ALMANAC_AVAILABLE - org.orekit.errors.OrekitMessages
NO_SEM_ALMANAC_AVAILABLE.
NO_SOLAR_ACTIVITY_AT_DATE - org.orekit.errors.OrekitMessages
NO_SOLAR_ACTIVITY_AT_DATE.
NO_SUCH_ITRF_FRAME - org.orekit.errors.OrekitMessages
NO_SUCH_ITRF_FRAME.
NO_TEC_DATA_IN_FILES_FOR_DATE - org.orekit.errors.OrekitMessages
NO_TEC_DATA_IN_FILES_FOR_DATE.
NO_TLE_DATA_AVAILABLE - org.orekit.errors.OrekitMessages
NO_TLE_DATA_AVAILABLE.
NO_TLE_FOR_LAUNCH_YEAR_NUMBER_PIECE - org.orekit.errors.OrekitMessages
NO_TLE_FOR_LAUNCH_YEAR_NUMBER_PIECE.
NO_TLE_FOR_OBJECT - org.orekit.errors.OrekitMessages
NO_TLE_FOR_OBJECT.
NO_UNITS - org.orekit.data.PolynomialParser.Unit
No units.
NO_UNSCENTED_TRANSFORM_CONFIGURED - org.orekit.errors.OrekitMessages
NO_UNSCENTED_TRANSFORM_CONFIGURED.
NO_VIENNA_ACOEF_OR_ZENITH_DELAY_IN_FILE - org.orekit.errors.OrekitMessages
NO_VIENNA_ACOEF_OR_ZENITH_DELAY_IN_FILE.
NO_YUMA_ALMANAC_AVAILABLE - org.orekit.errors.OrekitMessages
NO_YUMA_ALMANAC_AVAILABLE.
NodeDetector - Class in org.orekit.propagation.events
Finder for node crossing events.
NodeDetector(double, Orbit, Frame) - Constructor for class org.orekit.propagation.events.NodeDetector
Build a new instance.
NodeDetector(Frame) - Constructor for class org.orekit.propagation.events.NodeDetector
Build a new instance.
NodeDetector(Orbit, Frame) - Constructor for class org.orekit.propagation.events.NodeDetector
Build a new instance.
NodeDetector(AdaptableInterval, double, int, EventHandler, Frame) - Constructor for class org.orekit.propagation.events.NodeDetector
Deprecated.
as of 12.2
NodeDetector(EventDetectionSettings, EventHandler, Frame) - Constructor for class org.orekit.propagation.events.NodeDetector
Protected constructor with full parameters.
NON_CHRONOLOGICAL_DATES_FOR_OBSERVATIONS - org.orekit.errors.OrekitMessages
NON_CHRONOLOGICAL_DATES_FOR_OBSERVATIONS.
NON_CHRONOLOGICAL_DATES_IN_FILE - org.orekit.errors.OrekitMessages
NON_CHRONOLOGICAL_DATES_IN_FILE.
NON_CHRONOLOGICALLY_SORTED_ENTRIES - org.orekit.errors.OrekitMessages
NON_CHRONOLOGICALLY_SORTED_ENTRIES.
NON_COPLANAR_POINTS - org.orekit.errors.OrekitMessages
NON_COPLANAR_POINTS.
NON_DIFFERENT_DATES_FOR_OBSERVATIONS - org.orekit.errors.OrekitMessages
NON_DIFFERENT_DATES_FOR_OBSERVATIONS.
NON_EXISTENT_DATE - org.orekit.errors.OrekitMessages
NON_EXISTENT_DATE.
NON_EXISTENT_DAY_NUMBER_IN_YEAR - org.orekit.errors.OrekitMessages
NON_EXISTENT_DAY_NUMBER_IN_YEAR.
NON_EXISTENT_GEOMAGNETIC_MODEL - org.orekit.errors.OrekitMessages
NON_EXISTENT_GEOMAGNETIC_MODEL.
NON_EXISTENT_HMS_TIME - org.orekit.errors.OrekitMessages
NON_EXISTENT_HMS_TIME.
NON_EXISTENT_MONTH - org.orekit.errors.OrekitMessages
NON_EXISTENT_MONTH.
NON_EXISTENT_TIME - org.orekit.errors.OrekitMessages
NON_EXISTENT_TIME.
NON_EXISTENT_WEEK_DATE - org.orekit.errors.OrekitMessages
NON_EXISTENT_WEEK_DATE.
NON_EXISTENT_YEAR_MONTH_DAY - org.orekit.errors.OrekitMessages
NON_EXISTENT_YEAR_MONTH_DAY.
NON_PSEUDO_INERTIAL_FRAME - org.orekit.errors.OrekitMessages
NON_PSEUDO_INERTIAL_FRAME.
NON_PSEUDO_INERTIAL_FRAME_NOT_SUITABLE_AS_REFERENCE_FOR_INERTIAL_FORCES - org.orekit.errors.OrekitMessages
NON_PSEUDO_INERTIAL_FRAME_NOT_SUITABLE_AS_REFERENCE_FOR_INERTIAL_FORCES.
NON_RESETABLE_STATE - org.orekit.errors.OrekitMessages
NON_RESETABLE_STATE.
nonCentralPart(AbsoluteDate, Vector3D, double) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Compute the non-central part of the gravity field.
NONE - org.orekit.files.ccsds.ndm.adm.acm.RateElementsType
No rates.
NONE - org.orekit.files.ccsds.ndm.odm.ocm.ShadowModel
No shadow.
NONE - org.orekit.forces.maneuvers.Control3DVectorCostType
Zero cost (free control).
NONE - org.orekit.gnss.metric.ntrip.Authentication
None.
NONE - Static variable in class org.orekit.utils.units.Unit
No unit.
NONOPERATIONAL - org.orekit.files.ccsds.ndm.odm.ocm.OpsStatus
Non-operational object.
NORAD_CAT_ID - org.orekit.files.ccsds.ndm.odm.omm.OmmTleKey
NORAD Catalog Number.
NORMAL_POINT - org.orekit.files.ilrs.CRDHeader.DataType
Normal point.
normalize() - Method in class org.orekit.utils.FieldPVCoordinates
Normalize the position part of the instance.
normalize() - Method in class org.orekit.utils.PVCoordinates
Normalize the position part of the instance.
normalize(FieldOrbit<T>, FieldOrbit<T>) - Method in enum org.orekit.orbits.OrbitType
Normalize one orbit with respect to a reference one.
normalize(Orbit, Orbit) - Method in enum org.orekit.orbits.OrbitType
Normalize one orbit with respect to a reference one.
normalizeCovarianceMatrix(RealMatrix, double[]) - Static method in class org.orekit.estimation.sequential.KalmanEstimatorUtil
Normalize a covariance matrix.
NORMALIZED_EQUATORIAL_RADIUS - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
Equatorial radius rescaled (1.0).
NormalizedSphericalHarmonicsProvider - Interface in org.orekit.forces.gravity.potential
Interface used to provide normalized spherical harmonics coefficients.
NormalizedSphericalHarmonicsProvider.NormalizedSphericalHarmonics - Interface in org.orekit.forces.gravity.potential
The normalized geopotential coefficients at a specific instance in time.
NormBasedCartesianConditionChecker - Class in org.orekit.control.indirect.shooting.boundary
Class defining convergence criterion on the norm of relative position and velocity vectors, with absolute tolerances.
NormBasedCartesianConditionChecker(int, double, double) - Constructor for class org.orekit.control.indirect.shooting.boundary.NormBasedCartesianConditionChecker
Constructor.
NORTH - org.orekit.attitudes.PredefinedTarget
North direction.
NORTH - org.orekit.models.earth.displacement.PsdCorrection.Axis
North axis.
NORTH_POLE - Static variable in class org.orekit.bodies.GeodeticPoint
North pole.
NORTHERN - org.orekit.orbits.LibrationOrbitFamily
Northern.
NOT_A_DIRECTORY - org.orekit.errors.OrekitMessages
NOT_A_DIRECTORY.
NOT_A_JPL_EPHEMERIDES_BINARY_FILE - org.orekit.errors.OrekitMessages
NOT_A_JPL_EPHEMERIDES_BINARY_FILE.
NOT_A_MARSHALL_SOLAR_ACTIVITY_FUTURE_ESTIMATION_FILE - org.orekit.errors.OrekitMessages
NOT_A_MARSHALL_SOLAR_ACTIVITY_FUTURE_ESTIMATION_FILE.
NOT_A_SUPPORTED_HATANAKA_COMPRESSED_FILE - org.orekit.errors.OrekitMessages
NOT_A_SUPPORTED_HATANAKA_COMPRESSED_FILE.
NOT_A_SUPPORTED_IERS_DATA_FILE - org.orekit.errors.OrekitMessages
NOT_A_SUPPORTED_IERS_DATA_FILE.
NOT_A_SUPPORTED_SEM_ALMANAC_FILE - org.orekit.errors.OrekitMessages
NOT_A_SUPPORTED_SEM_ALMANAC_FILE.
NOT_A_SUPPORTED_UNIX_COMPRESSED_FILE - org.orekit.errors.OrekitMessages
NOT_A_SUPPORTED_UNIX_COMPRESSED_FILE.
NOT_A_SUPPORTED_YUMA_ALMANAC_FILE - org.orekit.errors.OrekitMessages
NOT_A_SUPPORTED_YUMA_ALMANAC_FILE.
NOT_ENOUGH_ATTITUDE_PROVIDERS - org.orekit.errors.OrekitMessages
NOT_ENOUGH_ATTITUDE_PROVIDERS.
NOT_ENOUGH_CACHED_NEIGHBORS - org.orekit.errors.OrekitMessages
NOT_ENOUGH_CACHED_NEIGHBORS.
NOT_ENOUGH_DATA - org.orekit.errors.OrekitMessages
NOT_ENOUGH_DATA.
NOT_ENOUGH_GNSS_FOR_DOP - org.orekit.errors.OrekitMessages
NOT_ENOUGH_GNSS_FOR_DOP.
NOT_ENOUGH_PROPAGATORS - org.orekit.errors.OrekitMessages
NOT_ENOUGH_PROPAGATORS.
NOT_POSITIVE_SPACECRAFT_MASS - org.orekit.errors.OrekitMessages
NOT_POSITIVE_SPACECRAFT_MASS.
NOT_STRICTLY_POSITIVE - org.orekit.errors.OrekitMessages
NOT_STRICTLY_POSITIVE.
NOT_TLE_LINES - org.orekit.errors.OrekitMessages
NOT_TLE_LINES.
NOT_VALID_INTERNATIONAL_DESIGNATOR - org.orekit.errors.OrekitMessages
NOT_VALID_INTERNATIONAL_DESIGNATOR.
notCombine(EventDetector) - Static method in class org.orekit.propagation.events.BooleanDetector
Create a new event detector that negates the g function of another detector.
notCombine(FieldEventDetector<T>) - Static method in class org.orekit.propagation.events.FieldBooleanDetector
Create a new event detector that negates the g function of another detector.
notifyResetters(FieldSpacecraftState<T>, boolean) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers
Notify resetters.
notifyResetters(SpacecraftState, boolean) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers
Notify resetters.
NOVEMBER - org.orekit.time.Month
November.
NptRangeMeasurement(AbsoluteDate, double, int, double, String) - Constructor for class org.orekit.files.ilrs.CRD.NptRangeMeasurement
Constructor.
NptRangeMeasurement(AbsoluteDate, double, int, double, String, double, int, double, double, double, double, double, int) - Constructor for class org.orekit.files.ilrs.CRD.NptRangeMeasurement
Constructor.
NRLMSISE00 - Class in org.orekit.models.earth.atmosphere
This class implements the mathematical representation of the 2001 Naval Research Laboratory Mass Spectrometer and Incoherent Scatter Radar Exosphere (NRLMSISE-00) of the MSIS® class model.
NRLMSISE00(NRLMSISE00InputParameters, PVCoordinatesProvider, BodyShape) - Constructor for class org.orekit.models.earth.atmosphere.NRLMSISE00
Constructor.
NRLMSISE00(NRLMSISE00InputParameters, PVCoordinatesProvider, BodyShape, TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.NRLMSISE00
Constructor.
NRLMSISE00.FieldOutput<T extends CalculusFieldElement<T>> - Class in org.orekit.models.earth.atmosphere
This class is a placeholder for the computed densities and temperatures.
NRLMSISE00InputParameters - Interface in org.orekit.models.earth.atmosphere
Container for solar activity data, compatible with NRLMSISE-00 atmosphere model.
NS - Static variable in class org.orekit.gnss.metric.parser.Units
Nanoseconds units.
NsgfV00Filter - Class in org.orekit.files.sp3
Filter for some non-official files from CDDIS.
NsgfV00Filter() - Constructor for class org.orekit.files.sp3.NsgfV00Filter
Simple constructor.
NsgfV00Filter(String, Function<String, String>) - Constructor for class org.orekit.files.sp3.NsgfV00Filter
Simple constructor.
NSKey(int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey
Simple constructor.
NSO - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCategory
Navigation Satellites Orbit 50° < i < 70°, 18100 < hp < 24300 km, 18100 < ha < 4300 km.
nSteps - Variable in class org.orekit.propagation.conversion.AbstractLimitedVariableStepFieldIntegratorBuilder
Number of steps.
NSW_INERTIAL - org.orekit.files.ccsds.definitions.OrbitRelativeFrame
Nadir, Sun, Normal (X towards nadir, Y as close to Sun as possible).
NSW_ROTATING - org.orekit.files.ccsds.definitions.OrbitRelativeFrame
Nadir, Sun, Normal (X towards nadir, Y as close to Sun as possible).
NtripClient - Class in org.orekit.gnss.metric.ntrip
Source table for ntrip streams retrieval.
NtripClient(String, int) - Constructor for class org.orekit.gnss.metric.ntrip.NtripClient
Build a client for NTRIP.
NTSC - org.orekit.files.rinex.navigation.UtcId
UTC(NTSC).
NTW - org.orekit.frames.LOFType
Constant for Transverse Velocity Normal coordinate system (Y axis aligned with velocity, Z axis aligned with orbital momentum).
NTW_INERTIAL - org.orekit.files.ccsds.definitions.OrbitRelativeFrame
Transverse Velocity Normal coordinate system (Y towards velocity, Z towards momentum).
NTW_INERTIAL - org.orekit.frames.LOFType
Constant for Transverse Velocity Normal coordinate system considered inertial (Y axis aligned with velocity, Z axis aligned with orbital momentum).
NTW_ROTATING - org.orekit.files.ccsds.definitions.OrbitRelativeFrame
Transverse Velocity Normal coordinate system (Y towards velocity, Z towards momentum).
NULL_ARGUMENT - org.orekit.errors.OrekitMessages
NULL_ARGUMENT.
NULL_CORRECTION - Static variable in class org.orekit.frames.PoleCorrection
Null correction (xp = 0, yp = 0).
NULL_PARENT_FOR_FRAME - org.orekit.errors.OrekitMessages
NULL_PARENT_FOR_FRAME.
NUMBER_SENSOR_NOISE_COVARIANCE - org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationSensorKey
Number of noise elements.
NUMBER_STATES - org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationKey
Number of states.
NUMBER_STATES - org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadataKey
Number of data states included.
numberOfCandidates() - Method in interface org.orekit.estimation.measurements.gnss.AmbiguityAcceptance
Get the number of candidate solutions to search for.
numberOfCandidates() - Method in class org.orekit.estimation.measurements.gnss.SimpleRatioAmbiguityAcceptance
Get the number of candidate solutions to search for.
numberOfObsTypes(SatelliteSystem) - Method in class org.orekit.files.rinex.clock.RinexClock
Get the number of observation types for a given system.
NumericalPropagator - Class in org.orekit.propagation.numerical
This class propagates orbits using numerical integration.
NumericalPropagator(ODEIntegrator) - Constructor for class org.orekit.propagation.numerical.NumericalPropagator
Create a new instance of NumericalPropagator, based on orbit definition mu.
NumericalPropagator(ODEIntegrator, AttitudeProvider) - Constructor for class org.orekit.propagation.numerical.NumericalPropagator
Create a new instance of NumericalPropagator, based on orbit definition mu.
NumericalPropagatorBuilder - Class in org.orekit.propagation.conversion
Builder for numerical propagator.
NumericalPropagatorBuilder(Orbit, ODEIntegratorBuilder, PositionAngleType, double) - Constructor for class org.orekit.propagation.conversion.NumericalPropagatorBuilder
Build a new instance.
NumericalPropagatorBuilder(Orbit, ODEIntegratorBuilder, PositionAngleType, double, AttitudeProvider) - Constructor for class org.orekit.propagation.conversion.NumericalPropagatorBuilder
Build a new instance.
NUTATION - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Nutation angle entry.
NUTATION - org.orekit.files.ccsds.ndm.adm.apm.SpinStabilizedKey
Nutation angle entry.
NUTATION_PER - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Nutation period entry.
NUTATION_PER - org.orekit.files.ccsds.ndm.adm.apm.SpinStabilizedKey
Nutation period entry.
NUTATION_PHASE - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Nutation phase entry.
NUTATION_PHASE - org.orekit.files.ccsds.ndm.adm.apm.SpinStabilizedKey
Nutation phase entry.
NUTATION_VEL - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Nutation velocity entry.
NUTATION_VEL - org.orekit.files.ccsds.ndm.adm.apm.SpinStabilizedKey
Nutation velocity entry.

O

O1 - Static variable in class org.orekit.models.earth.displacement.Tide
O₁ tide.
OBJECT - org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey
Object to which data apply.
OBJECT_DESIGNATOR - org.orekit.files.ccsds.ndm.adm.acm.AcmMetadataKey
Unique satellite identification designator for the object.
OBJECT_DESIGNATOR - org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey
Satellite catalog designator for object.
OBJECT_DESIGNATOR - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Unique satellite identification designator for the object.
OBJECT_ID - org.orekit.files.ccsds.ndm.adm.AdmCommonMetadataKey
Object ID entry.
OBJECT_ID - org.orekit.files.ccsds.ndm.odm.CommonMetadataKey
Object ID entry.
OBJECT_NAME - org.orekit.files.ccsds.ndm.adm.AdmMetadataKey
Object name entry.
OBJECT_NAME - org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey
Spacecraft name for the object.
OBJECT_NAME - org.orekit.files.ccsds.ndm.odm.OdmMetadataKey
Object name entry.
OBJECT_TYPE - org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey
Object Type.
OBJECT_TYPE - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Type of object.
ObjectType - Enum in org.orekit.files.ccsds.ndm.odm.ocm
Object type used in CCSDS Orbit Comprehensive Messages.
OBLATE_FLATTENING - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey
Central body oblate spheroid oblateness.
OBS_AVAILABLE - org.orekit.files.ccsds.ndm.cdm.ODParametersKey
The number of observations available for the OD of the object.
OBS_AVAILABLE - org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey
Number of observations available within the actual OD span.
OBS_BEFORE_NEXT_MESSAGE - org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey
Flag indicating whether new tracking observations are anticipated prior to the issue of the next CDM associated with the event specified by CONJUNCTION_ID.
OBS_SCALE_FACTOR - org.orekit.files.rinex.section.RinexLabels
Observations scale factor.
OBS_USED - org.orekit.files.ccsds.ndm.cdm.ODParametersKey
The number of observations accepted for the OD of the object.
OBS_USED - org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey
Number of observations accepted within the actual OD span.
ObservableSatellite - Class in org.orekit.estimation.measurements
Class modeling a satellite that can be observed.
ObservableSatellite(int) - Constructor for class org.orekit.estimation.measurements.ObservableSatellite
Simple constructor.
observation - org.orekit.files.ccsds.ndm.tdm.TdmDataKey
Observation wrapper.
Observation - Class in org.orekit.files.ccsds.ndm.tdm
The Observation class contains the data from an observation line.
Observation(ObservationType, AbsoluteDate, double) - Constructor for class org.orekit.files.ccsds.ndm.tdm.Observation
Simple constructor.
OBSERVATION - org.orekit.files.rinex.utils.RinexFileType
Rinex Observation.
ObservationData - Class in org.orekit.files.rinex.observation
Observation Data.
ObservationData(ObservationType, double, int, int) - Constructor for class org.orekit.files.rinex.observation.ObservationData
Simple constructor.
ObservationDataSet - Class in org.orekit.files.rinex.observation
Observation Data set.
ObservationDataSet(SatInSystem, AbsoluteDate, int, double, List<ObservationData>) - Constructor for class org.orekit.files.rinex.observation.ObservationDataSet
Simple constructor.
ObservationsBlock - Class in org.orekit.files.ccsds.ndm.tdm
The Observations Block class contain metadata and the list of observation data lines.
ObservationsBlock() - Constructor for class org.orekit.files.ccsds.ndm.tdm.ObservationsBlock
ObservationsBlock constructor.
ObservationTimeScale - Enum in org.orekit.gnss
Observation time scales.
ObservationType - Enum in org.orekit.files.ccsds.ndm.tdm
Keys for TDM observations entries.
ObservationType - Enum in org.orekit.gnss
Enumerate for all the Observation Types for Rinex 2 and 3.
ObservedMeasurement<T extends ObservedMeasurement<T>> - Interface in org.orekit.estimation.measurements
Interface for measurements used for orbit determination.
OBSERVER_AGENCY - org.orekit.files.rinex.section.RinexLabels
Observer agency.
OccultationEngine - Class in org.orekit.utils
Computation engine for occultation events.
OccultationEngine(ExtendedPVCoordinatesProvider, double, OneAxisEllipsoid) - Constructor for class org.orekit.utils.OccultationEngine
Build a new occultation engine.
OccultationEngine.FieldOccultationAngles<T extends CalculusFieldElement<T>> - Class in org.orekit.utils
Container for occultation angles.
OccultationEngine.OccultationAngles - Class in org.orekit.utils
Container for occultation angles.
OCEAN_TIDE_DATA_DEGREE_ORDER_LIMITS - org.orekit.errors.OrekitMessages
OCEAN_TIDE_DATA_DEGREE_ORDER_LIMITS.
OCEAN_TIDE_LOAD_DEFORMATION_LIMITS - org.orekit.errors.OrekitMessages
OCEAN_TIDE_LOAD_DEFORMATION_LIMITS.
OCEAN_TIDES_MODEL - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey
Ocean tides model.
OceanLoadDeformationCoefficients - Enum in org.orekit.forces.gravity.potential
Supported Ocean load Deformation coefficients (Love numbers k'i).
OceanLoading - Class in org.orekit.models.earth.displacement
Modeling of displacement of reference points due to ocean loading.
OceanLoading(OneAxisEllipsoid, OceanLoadingCoefficients) - Constructor for class org.orekit.models.earth.displacement.OceanLoading
Simple constructor.
OceanLoadingCoefficients - Class in org.orekit.models.earth.displacement
Site specific coefficients for ocean loading.
OceanLoadingCoefficients(String, GeodeticPoint, Tide[][], double[][], double[][], double[][], double[][], double[][], double[][]) - Constructor for class org.orekit.models.earth.displacement.OceanLoadingCoefficients
Simple constructor.
OceanLoadingCoefficientsBLQFactory - Class in org.orekit.models.earth.displacement
Factory for ocean loading coefficients, using Onsala Space Observatory files in BLQ format.
OceanLoadingCoefficientsBLQFactory(String) - Constructor for class org.orekit.models.earth.displacement.OceanLoadingCoefficientsBLQFactory
Simple constructor.
OceanLoadingCoefficientsBLQFactory(String, DataProvidersManager) - Constructor for class org.orekit.models.earth.displacement.OceanLoadingCoefficientsBLQFactory
This constructor allows specification of the source of the BLQ auxiliary data files.
OceanLoadingCoefficientsBlqParser - Class in org.orekit.models.earth.displacement
Parser for ocean loading coefficients, using Onsala Space Observatory files in BLQ format.
OceanLoadingCoefficientsBlqParser() - Constructor for class org.orekit.models.earth.displacement.OceanLoadingCoefficientsBlqParser
 
OceanTides - Class in org.orekit.forces.gravity
Ocean tides force model.
OceanTides(Frame, double, double, boolean, double, int, int, int, IERSConventions, UT1Scale) - Constructor for class org.orekit.forces.gravity.OceanTides
Simple constructor.
OceanTides(Frame, double, double, boolean, double, int, int, int, IERSConventions, UT1Scale, GravityFields) - Constructor for class org.orekit.forces.gravity.OceanTides
Simple constructor.
OceanTides(Frame, double, double, int, int, IERSConventions, UT1Scale) - Constructor for class org.orekit.forces.gravity.OceanTides
Simple constructor.
OceanTidesReader - Class in org.orekit.forces.gravity.potential
Reader for ocean tides coefficients.
OceanTidesReader(String) - Constructor for class org.orekit.forces.gravity.potential.OceanTidesReader
Simple constructor.
OceanTidesWave - Class in org.orekit.forces.gravity.potential
Container for ocen tides coefficients for one tide wave.
OceanTidesWave(int, int, int, double[][][]) - Constructor for class org.orekit.forces.gravity.potential.OceanTidesWave
Simple constructor.
Ocm - Class in org.orekit.files.ccsds.ndm.odm.ocm
This class gathers the informations present in the Orbit Comprehensive Message (OCM).
Ocm(OdmHeader, List<Segment<OcmMetadata, OcmData>>, IERSConventions, DataContext, double) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.Ocm
Simple constructor.
OCM_DATA_ELEMENTS - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
List of elements of information data blocks included in this message.
OcmData - Class in org.orekit.files.ccsds.ndm.odm.ocm
Data container for Orbit Comprehensive Messages.
OcmData(List<TrajectoryStateHistory>, OrbitPhysicalProperties, List<OrbitCovarianceHistory>, List<OrbitManeuverHistory>, Perturbations, OrbitDetermination, UserDefined) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.OcmData
Simple constructor.
OcmDataSubStructureKey - Enum in org.orekit.files.ccsds.ndm.odm.ocm
Keywords for OCM data sub-structure.
OcmElements - Enum in org.orekit.files.ccsds.ndm.odm.ocm
Data elements types used in CCSDS Orbit Comprehensive Messages.
OcmMetadata - Class in org.orekit.files.ccsds.ndm.odm.ocm
OcmMetadata(DataContext) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Create a new meta-data.
OcmMetadataKey - Enum in org.orekit.files.ccsds.ndm.odm.ocm
Keys for OCM container entries.
OcmParser - Class in org.orekit.files.ccsds.ndm.odm.ocm
A parser for the CCSDS OCM (Orbit Comprehensive Message).
OcmParser(IERSConventions, double, double, boolean, DataContext, double, ParsedUnitsBehavior, Function<ParseToken, List<ParseToken>>[]) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser
Complete constructor.
OcmSatelliteEphemeris - Class in org.orekit.files.ccsds.ndm.odm.ocm
OCM ephemeris blocks for a single satellite.
OcmSatelliteEphemeris(String, double, List<TrajectoryStateHistory>) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.OcmSatelliteEphemeris
Create a container for the set of ephemeris blocks in the file that pertain to a single satellite.
OcmWriter - Class in org.orekit.files.ccsds.ndm.odm.ocm
Writer for CCSDS Orbit Comprehensive Message.
OcmWriter(IERSConventions, double, double, DataContext) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.OcmWriter
Complete constructor.
OCTOBER - org.orekit.time.Month
October.
od - org.orekit.files.ccsds.ndm.odm.ocm.OcmDataSubStructureKey
Orbit determination section.
OD - org.orekit.files.ccsds.ndm.odm.ocm.OcmDataSubStructureKey
Orbit determination section.
OD - org.orekit.files.ccsds.ndm.odm.ocm.OcmElements
Orbit determination.
OD_CONFIDENCE - org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey
Confidence metric.
OD_EPOCH - org.orekit.files.ccsds.ndm.cdm.ODParametersKey
The epoch of the orbit determination used for this message (UTC).
OD_EPOCH - org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey
Time tag for orbit determination solved-for state.
OD_EPOCH_EIGINT - org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey
Positional error ellipsoid 1σ intermediate eigenvalue at the epoch of OD.
OD_EPOCH_EIGMAJ - org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey
Positional error ellipsoid 1σ major eigenvalue at the epoch of OD.
OD_EPOCH_EIGMIN - org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey
Positional error ellipsoid 1σ minor eigenvalue at the epoch of OD.
OD_ID - org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey
Identification number.
OD_MAX_PRED_EIGMAJ - org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey
Maximum predicted major eigenvalue of 1σ positional error ellipsoid over entire time span of the OCM.
OD_METHOD - org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey
Orbit determination method.
OD_MIN_PRED_EIGMIN - org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey
Minimum predicted minor eigenvalue of 1σ positional error ellipsoid over entire time span of the OCM.
OD_PREV_ID - org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey
Identification of previous orbit determination.
ODEIntegratorBuilder - Interface in org.orekit.propagation.conversion
This interface is the top-level abstraction to build first order integrators for propagators conversion.
ODM_MSG_LINK - org.orekit.files.ccsds.ndm.adm.acm.AcmMetadataKey
Unique identifier of Orbit Data Message linked to this Attitude Data Message.
ODM_MSG_LINK - org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey
Unique identifier of Orbit Data Message(s) that are linked (relevant) to this Conjunction Data Message.
OdmCommonMetadata - Class in org.orekit.files.ccsds.ndm.odm
Common metadata for Orbit Parameter/Ephemeris/Mean Messages.
OdmCommonMetadata() - Constructor for class org.orekit.files.ccsds.ndm.odm.OdmCommonMetadata
Simple constructor.
OdMethodFacade - Class in org.orekit.files.ccsds.definitions
Facade in front of several orbit determination methods in CCSDS messages.
OdMethodFacade(String, OdMethodType, String) - Constructor for class org.orekit.files.ccsds.definitions.OdMethodFacade
Simple constructor.
OdMethodType - Enum in org.orekit.files.ccsds.definitions
Type of orbit determination method used in CCSDS Orbit Comprehensive Messages.
OdmHeader - Class in org.orekit.files.ccsds.ndm.odm
Header of a CCSDS Orbit Data Message.
OdmHeader() - Constructor for class org.orekit.files.ccsds.ndm.odm.OdmHeader
Constructor.
OdmMetadata - Class in org.orekit.files.ccsds.ndm.odm
This class gathers the meta-data present in the Orbital Data Message (ODM).
OdmMetadata(TimeSystem) - Constructor for class org.orekit.files.ccsds.ndm.odm.OdmMetadata
Simple constructor.
OdmMetadataKey - Enum in org.orekit.files.ccsds.ndm.odm
Keys for ODM metadata entries.
OdmParser<T extends NdmConstituent<OdmHeader,​?>,​P extends OdmParser<T,​?>> - Class in org.orekit.files.ccsds.ndm.odm
Common parser for Orbit Parameter/Ephemeris/Mean/Comprehensive Messages.
OdmParser(String, String, IERSConventions, boolean, DataContext, AbsoluteDate, double, ParsedUnitsBehavior, Function<ParseToken, List<ParseToken>>[]) - Constructor for class org.orekit.files.ccsds.ndm.odm.OdmParser
Complete constructor.
odParameters - org.orekit.files.ccsds.ndm.cdm.XmlSubStructureKey
OD Parameters section.
ODParameters - Class in org.orekit.files.ccsds.ndm.cdm
Container for OD parameters data block.
ODParameters() - Constructor for class org.orekit.files.ccsds.ndm.cdm.ODParameters
Simple constructor.
ODParametersKey - Enum in org.orekit.files.ccsds.ndm.cdm
Keys for CDM OD parameters entries.
ODParametersWriter - Class in org.orekit.files.ccsds.ndm.cdm
Writer for OD parameters data block for CCSDS Conjunction Data Messages.
OEB_INT - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
Intermediate physical dimension of Optimally Enclosing Box.
OEB_INT - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Dimensions of Optimally Enclosing Box along Y-OEB (i.e intermediate).
OEB_MAX - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
Maximum physical dimension of Optimally Enclosing Box.
OEB_MAX - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Dimensions of Optimally Enclosing Box along X-OEB (i.e max).
OEB_MIN - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
Minium physical dimension of Optimally Enclosing Box.
OEB_MIN - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Dimensions of Optimally Enclosing Box along Z-OEB (i.e min).
OEB_PARENT_FRAME - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
Optimally Enclosing Box parent reference frame.
OEB_PARENT_FRAME - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Optimally Enclosing Box parent reference frame.
OEB_PARENT_FRAME_EPOCH - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
Optimally Enclosing Box parent reference frame epoch.
OEB_PARENT_FRAME_EPOCH - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Optimally Enclosing Box parent reference frame epoch.
OEB_Q1 - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
Quaternion defining Optimally Enclosing Box (first vectorial component).
OEB_Q1 - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Quaternion defining Optimally Enclosing Box (first vectorial component).
OEB_Q2 - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
Quaternion defining Optimally Enclosing Box (second vectorial component).
OEB_Q2 - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Quaternion defining Optimally Enclosing Box (second vectorial component).
OEB_Q3 - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
Quaternion defining Optimally Enclosing Box (third vectorial component).
OEB_Q3 - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Quaternion defining Optimally Enclosing Box (third vectorial component).
OEB_QC - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
Quaternion defining Optimally Enclosing Box (scalar component).
OEB_QC - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Quaternion defining Optimally Enclosing Box (scalar component).
Oem - Class in org.orekit.files.ccsds.ndm.odm.oem
This class stores all the information of the OEM File parsed by OEMParser.
Oem(OdmHeader, List<OemSegment>, IERSConventions, DataContext, double) - Constructor for class org.orekit.files.ccsds.ndm.odm.oem.Oem
Simple constructor.
OemData - Class in org.orekit.files.ccsds.ndm.odm.oem
The Ephemerides data blocks class contain list of orbital data points.
OemData() - Constructor for class org.orekit.files.ccsds.ndm.odm.oem.OemData
EphemeridesBlock constructor.
OemMetadata - Class in org.orekit.files.ccsds.ndm.odm.oem
Metadata for Orbit Ephemeris Messages.
OemMetadata(int) - Constructor for class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata
Simple constructor.
OemMetadataKey - Enum in org.orekit.files.ccsds.ndm.odm.oem
Keys for OEM container entries.
OemParser - Class in org.orekit.files.ccsds.ndm.odm.oem
A parser for the CCSDS OEM (Orbit Ephemeris Message).
OemParser(IERSConventions, boolean, DataContext, AbsoluteDate, double, int, ParsedUnitsBehavior, Function<ParseToken, List<ParseToken>>[]) - Constructor for class org.orekit.files.ccsds.ndm.odm.oem.OemParser
Complete constructor.
OemSatelliteEphemeris - Class in org.orekit.files.ccsds.ndm.odm.oem
OEM ephemeris blocks for a single satellite.
OemSatelliteEphemeris(String, double, List<OemSegment>) - Constructor for class org.orekit.files.ccsds.ndm.odm.oem.OemSatelliteEphemeris
Create a container for the set of ephemeris blocks in the file that pertain to a single satellite.
OemSegment - Class in org.orekit.files.ccsds.ndm.odm.oem
The Ephemerides Blocks class contain metadata, the list of ephemerides data lines and optional covariance matrices (and their metadata).
OemSegment(OemMetadata, OemData, double) - Constructor for class org.orekit.files.ccsds.ndm.odm.oem.OemSegment
Simple constructor.
OemWriter - Class in org.orekit.files.ccsds.ndm.odm.oem
A writer for Orbit Ephemeris Message (OEM) files.
OemWriter(IERSConventions, DataContext, AbsoluteDate) - Constructor for class org.orekit.files.ccsds.ndm.odm.oem.OemWriter
Constructor used to create a new OEM writer configured with the necessary parameters to successfully fill in all required fields that aren't part of a standard object.
of(double) - Static method in interface org.orekit.propagation.events.AdaptableInterval
Method creating a constant interval provider.
of(double) - Static method in interface org.orekit.propagation.events.FieldAdaptableInterval
Method creating a constant interval provider.
of(Collection<? extends OffsetModel>, BiFunction<? super IERSConventions, ? super TimeScales, ? extends Collection<? extends EOPEntry>>) - Static method in interface org.orekit.time.TimeScales
Create a set of time scales where all the data is loaded from the given functions.
of(Field<T>, KinematicTransform) - Static method in interface org.orekit.frames.FieldKinematicTransform
Create a new kinematic transform from a non-Field version.
of(Frame) - Static method in class org.orekit.attitudes.FrameAlignedProvider
Creates an attitude provider aligned with the given frame.
of(TLE, Frame) - Static method in class org.orekit.propagation.conversion.averaging.SGP4OrbitalState
Static constructor.
of(AbsoluteDate, Rotation) - Static method in interface org.orekit.frames.StaticTransform
Create a new static transform from a rotation and zero translation.
of(AbsoluteDate, Rotation, Vector3D) - Static method in interface org.orekit.frames.KinematicTransform
Create a new kinematic transform from a rotation and zero, constant translation.
of(AbsoluteDate, Vector3D) - Static method in interface org.orekit.frames.StaticTransform
Create a new static transform from a translation and rotation.
of(AbsoluteDate, Vector3D, Rotation) - Static method in interface org.orekit.frames.StaticTransform
Create a new static transform from a translation and rotation.
of(AbsoluteDate, PVCoordinates) - Static method in interface org.orekit.frames.KinematicTransform
Create a new kinematic transform from a translation and its rate.
of(AbsoluteDate, PVCoordinates, Rotation, Vector3D) - Static method in interface org.orekit.frames.KinematicTransform
Create a new kinematic transform from a translation and rotation.
of(FieldAbsoluteDate<T>, FieldRotation<T>) - Static method in interface org.orekit.frames.FieldStaticTransform
Create a new static transform from a rotation and zero translation.
of(FieldAbsoluteDate<T>, FieldRotation<T>, FieldVector3D<T>) - Static method in interface org.orekit.frames.FieldKinematicTransform
Create a new kinematic transform from a rotation and zero, constant translation.
of(FieldAbsoluteDate<T>, FieldVector3D<T>) - Static method in interface org.orekit.frames.FieldStaticTransform
Create a new static transform from a translation and rotation.
of(FieldAbsoluteDate<T>, FieldVector3D<T>, FieldRotation<T>) - Static method in interface org.orekit.frames.FieldStaticTransform
Create a new static transform from a translation and rotation.
of(FieldAbsoluteDate<T>, StaticTransform) - Static method in interface org.orekit.frames.FieldStaticTransform
Create a new static transform from an FieldAbsoluteDate and a StaticTransform.
of(FieldAbsoluteDate<T>, FieldPVCoordinates<T>) - Static method in interface org.orekit.frames.FieldKinematicTransform
Create a new kinematic transform from a translation and its rate.
of(FieldAbsoluteDate<T>, FieldPVCoordinates<T>, FieldRotation<T>, FieldVector3D<T>) - Static method in interface org.orekit.frames.FieldKinematicTransform
Create a new kinematic transform from a translation and rotation.
of(TimeScales, Supplier<Frame>) - Static method in interface org.orekit.frames.Frames
Create a set of frames from the given data.
of(TimeScales, CelestialBodies) - Static method in interface org.orekit.frames.Frames
Create a set of frames from the given data.
OFF - org.orekit.files.ccsds.definitions.OnOff
Off status.
offset(StaticTransform, StaticTransform) - Method in class org.orekit.estimation.measurements.modifiers.PhaseCentersOffsetComputer
Compute distance offset to be added to the distance between antennas reference points.
offset(AbsoluteDate) - Method in class org.orekit.files.ccsds.definitions.TimeConverter
Generate relative offset.
OFFSET_SUFFIX - Static variable in class org.orekit.estimation.measurements.GroundStation
Suffix for ground station position and clock offset parameters names.
offsetFrom(AbsoluteDate, TimeScale) - Method in class org.orekit.time.AbsoluteDate
Compute the apparent clock offset between two instant in the perspective of a specific time scale.
offsetFrom(DateTimeComponents) - Method in class org.orekit.time.DateTimeComponents
Compute the seconds offset between two instances.
offsetFrom(DateTimeComponents, TimeUnit) - Method in class org.orekit.time.DateTimeComponents
Compute the seconds offset between two instances.
offsetFrom(FieldAbsoluteDate<T>, TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate
Compute the apparent clock offset between two instant in the perspective of a specific time scale.
offsetFromBoundary(Vector3D, double, VisibilityTrigger) - Method in class org.orekit.geometry.fov.CircularFieldOfView
Get the offset of target body with respect to the Field Of View Boundary.
offsetFromBoundary(Vector3D, double, VisibilityTrigger) - Method in class org.orekit.geometry.fov.EllipticalFieldOfView
Get the offset of target body with respect to the Field Of View Boundary.
offsetFromBoundary(Vector3D, double, VisibilityTrigger) - Method in interface org.orekit.geometry.fov.FieldOfView
Get the offset of target body with respect to the Field Of View Boundary.
offsetFromBoundary(Vector3D, double, VisibilityTrigger) - Method in class org.orekit.geometry.fov.PolygonalFieldOfView
Get the offset of target body with respect to the Field Of View Boundary.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.ClockTimeScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.ConstantOffsetTimeScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.GLONASSScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.GMSTScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.SatelliteClockScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.TCBScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.TCGScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.TDBScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in interface org.orekit.time.TimeScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.UT1Scale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.UTCScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.ClockTimeScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.ConstantOffsetTimeScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.GLONASSScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.GMSTScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.SatelliteClockScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.TCBScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.TCGScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.TDBScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(FieldAbsoluteDate<T>) - Method in interface org.orekit.time.TimeScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.UT1Scale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.UTCScale
Get the offset to convert locations from TAIScale to instance.
OffsetModel - Class in org.orekit.time
TAI UTC offset model.
OffsetModel(DateComponents, int) - Constructor for class org.orekit.time.OffsetModel
Constructor for a constant offset model.
OffsetModel(DateComponents, int, double, double) - Constructor for class org.orekit.time.OffsetModel
Constructor for a linear offset model.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.ConstantOffsetTimeScale
Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.GLONASSScale
Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.SatelliteClockScale
Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in interface org.orekit.time.TimeScale
Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.UTCScale
Get the offset to convert locations from instance to TAIScale.
OHM - Static variable in class org.orekit.utils.units.Unit
Ohm unit.
omega - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
final perigee argument.
omega - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
final perigee argument.
omgdot - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
common parameter for perigee argument (omega) computation.
omgdot - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
common parameter for perigee argument (omega) computation.
Omm - Class in org.orekit.files.ccsds.ndm.odm.omm
This class gathers the informations present in the Orbital Mean-Elements Message (OMM).
Omm(OdmHeader, List<Segment<OmmMetadata, OmmData>>, IERSConventions, DataContext) - Constructor for class org.orekit.files.ccsds.ndm.odm.omm.Omm
Simple constructor.
OmmData - Class in org.orekit.files.ccsds.ndm.odm.omm
Container for Orbit Mean-elements Message data.
OmmData(KeplerianElements, SpacecraftParameters, OmmTle, CartesianCovariance, UserDefined, double) - Constructor for class org.orekit.files.ccsds.ndm.odm.omm.OmmData
Simple constructor.
OmmMetadata - Class in org.orekit.files.ccsds.ndm.odm.omm
Metadata for Orbit Mean Messages.
OmmMetadata() - Constructor for class org.orekit.files.ccsds.ndm.odm.omm.OmmMetadata
Empty constructor.
OmmMetadataKey - Enum in org.orekit.files.ccsds.ndm.odm.omm
Keys for OMM container entries.
OmmParser - Class in org.orekit.files.ccsds.ndm.odm.omm
A parser for the CCSDS OMM (Orbiter Mean-Elements Message).
OmmParser(IERSConventions, boolean, DataContext, AbsoluteDate, double, double, ParsedUnitsBehavior, Function<ParseToken, List<ParseToken>>[]) - Constructor for class org.orekit.files.ccsds.ndm.odm.omm.OmmParser
Complete constructor.
OmmTle - Class in org.orekit.files.ccsds.ndm.odm.omm
Container for TLE data.
OmmTle() - Constructor for class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
Create an empty data set.
OmmTleKey - Enum in org.orekit.files.ccsds.ndm.odm.omm
Keys for TLE entries.
OmmWriter - Class in org.orekit.files.ccsds.ndm.odm.omm
Writer for CCSDS Orbit Mean Mean-Elements Message.
OmmWriter(IERSConventions, DataContext, AbsoluteDate) - Constructor for class org.orekit.files.ccsds.ndm.odm.omm.OmmWriter
Complete constructor.
ON - org.orekit.files.ccsds.definitions.OnOff
On status.
OnBoardAntennaInterSatellitesPhaseModifier - Class in org.orekit.estimation.measurements.modifiers
On-board antenna offset effect on inter-satellites phase measurements.
OnBoardAntennaInterSatellitesPhaseModifier(Vector3D, Vector3D) - Constructor for class org.orekit.estimation.measurements.modifiers.OnBoardAntennaInterSatellitesPhaseModifier
Simple constructor.
OnBoardAntennaInterSatellitesPhaseModifier(FrequencyPattern, FrequencyPattern) - Constructor for class org.orekit.estimation.measurements.modifiers.OnBoardAntennaInterSatellitesPhaseModifier
Simple constructor.
OnBoardAntennaInterSatellitesRangeModifier - Class in org.orekit.estimation.measurements.modifiers
On-board antenna offset effect on inter-satellites range measurements.
OnBoardAntennaInterSatellitesRangeModifier(Vector3D, Vector3D) - Constructor for class org.orekit.estimation.measurements.modifiers.OnBoardAntennaInterSatellitesRangeModifier
Simple constructor.
OnBoardAntennaInterSatellitesRangeModifier(FrequencyPattern, FrequencyPattern) - Constructor for class org.orekit.estimation.measurements.modifiers.OnBoardAntennaInterSatellitesRangeModifier
Simple constructor.
OnBoardAntennaOneWayGNSSPhaseModifier - Class in org.orekit.estimation.measurements.modifiers
On-board antenna offset effect on one-way GNSS phase measurements.
OnBoardAntennaOneWayGNSSPhaseModifier(Vector3D, Vector3D, AttitudeProvider) - Constructor for class org.orekit.estimation.measurements.modifiers.OnBoardAntennaOneWayGNSSPhaseModifier
Simple constructor.
OnBoardAntennaOneWayGNSSPhaseModifier(FrequencyPattern, FrequencyPattern, AttitudeProvider) - Constructor for class org.orekit.estimation.measurements.modifiers.OnBoardAntennaOneWayGNSSPhaseModifier
Simple constructor.
OnBoardAntennaOneWayGNSSRangeModifier - Class in org.orekit.estimation.measurements.modifiers
On-board antenna offset effect on one-way GNSS range measurements.
OnBoardAntennaOneWayGNSSRangeModifier(Vector3D, Vector3D, AttitudeProvider) - Constructor for class org.orekit.estimation.measurements.modifiers.OnBoardAntennaOneWayGNSSRangeModifier
Simple constructor.
OnBoardAntennaOneWayGNSSRangeModifier(FrequencyPattern, FrequencyPattern, AttitudeProvider) - Constructor for class org.orekit.estimation.measurements.modifiers.OnBoardAntennaOneWayGNSSRangeModifier
Simple constructor.
OnBoardAntennaTurnAroundRangeModifier - Class in org.orekit.estimation.measurements.modifiers
On-board antenna offset effect on turn around range measurements.
OnBoardAntennaTurnAroundRangeModifier(Vector3D) - Constructor for class org.orekit.estimation.measurements.modifiers.OnBoardAntennaTurnAroundRangeModifier
Simple constructor.
OnBoardCommonParametersWithDerivatives - Class in org.orekit.estimation.measurements.gnss
Common intermediate parameters used to estimate measurements where receiver is a satellite.
OnBoardCommonParametersWithDerivatives(SpacecraftState, Map<String, Integer>, Gradient, Gradient, Gradient, Gradient, Gradient, TimeStampedFieldPVCoordinates<Gradient>, TimeStampedFieldPVCoordinates<Gradient>) - Constructor for class org.orekit.estimation.measurements.gnss.OnBoardCommonParametersWithDerivatives
Simple constructor.
OnBoardCommonParametersWithoutDerivatives - Class in org.orekit.estimation.measurements.gnss
Common intermediate parameters used to estimate measurements where receiver is a satellite.
OnBoardCommonParametersWithoutDerivatives(SpacecraftState, double, double, double, double, double, TimeStampedPVCoordinates, TimeStampedPVCoordinates) - Constructor for class org.orekit.estimation.measurements.gnss.OnBoardCommonParametersWithoutDerivatives
Simple constructor.
onDate(AbsoluteDate) - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
Get the normalized spherical harmonic coefficients at a specific instance in time.
onDate(AbsoluteDate) - Method in interface org.orekit.forces.gravity.potential.NormalizedSphericalHarmonicsProvider
Get the normalized spherical harmonic coefficients at a specific instance in time.
onDate(AbsoluteDate) - Method in interface org.orekit.forces.gravity.potential.RawSphericalHarmonicsProvider
Get the raw spherical harmonic coefficients on a specific date.
onDate(AbsoluteDate) - Method in interface org.orekit.forces.gravity.potential.UnnormalizedSphericalHarmonicsProvider
Get the un-normalized spherical harmonic coefficients at a specific instance in time.
ONE - Static variable in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities
1 represented as a polynomial.
ONE - Static variable in class org.orekit.utils.units.Unit
Dimensionless unit.
ONE_NORM - org.orekit.forces.maneuvers.Control3DVectorCostType
1-norm.
ONE_PER_ER - Static variable in class org.orekit.files.ccsds.definitions.Units
Earth radii reciprocal unit.
ONE_PER_S - Static variable in class org.orekit.files.ccsds.definitions.Units
Seconds reciprocal unit.
ONE_THIRD - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
Constant 1.0 / 3.0.
ONE_WAY - org.orekit.files.ccsds.ndm.tdm.RangeMode
Special value used in delta-DOR.
ONE_WAY - org.orekit.files.ilrs.CRDHeader.RangeType
One-way ranging.
OneAxisEllipsoid - Class in org.orekit.bodies
Modeling of a one-axis ellipsoid.
OneAxisEllipsoid(double, double, Frame) - Constructor for class org.orekit.bodies.OneAxisEllipsoid
Simple constructor.
OneDVariation - Class in org.orekit.gnss.antenna
Interpolator for 1D phase center variation data.
OneDVariation(double, double, double[]) - Constructor for class org.orekit.gnss.antenna.OneDVariation
Simple constructor.
oneWayDistanceModification(EstimatedMeasurementBase<T>) - Method in class org.orekit.estimation.measurements.modifiers.PhaseCentersGroundReceiverBaseModifier
Compute distance modification for one way measurement.
oneWayDistanceModification(EstimatedMeasurementBase<T>) - Method in class org.orekit.estimation.measurements.modifiers.PhaseCentersInterSatellitesBaseModifier
Compute distance modification for one way measurement.
oneWayDistanceModification(EstimatedMeasurementBase<T>) - Method in class org.orekit.estimation.measurements.modifiers.PhaseCentersOneWayGNSSBaseModifier
Compute distance modification for one way measurement.
OneWayGNSSPhase - Class in org.orekit.estimation.measurements.gnss
One-way GNSS phase measurement.
OneWayGNSSPhase(PVCoordinatesProvider, double, AbsoluteDate, double, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.gnss.OneWayGNSSPhase
OneWayGNSSPhase(PVCoordinatesProvider, String, QuadraticClockModel, AbsoluteDate, double, double, double, double, ObservableSatellite, AmbiguityCache) - Constructor for class org.orekit.estimation.measurements.gnss.OneWayGNSSPhase
Simple constructor.
OneWayGNSSPhaseAmbiguityModifier - Class in org.orekit.estimation.measurements.modifiers
Deprecated.
as of 12.1 ambiguity is managed directly by raw measurements OneWayGNSSPhase
OneWayGNSSPhaseAmbiguityModifier(int, double) - Constructor for class org.orekit.estimation.measurements.modifiers.OneWayGNSSPhaseAmbiguityModifier
Deprecated.
Constructor.
OneWayGNSSPhaseBuilder - Class in org.orekit.estimation.measurements.generation
Builder for OneWayGNSSPhase measurements.
OneWayGNSSPhaseBuilder(CorrelatedRandomVectorGenerator, ObservableSatellite, ObservableSatellite, ToDoubleFunction<AbsoluteDate>, double, double, double) - Constructor for class org.orekit.estimation.measurements.generation.OneWayGNSSPhaseBuilder
OneWayGNSSPhaseBuilder(CorrelatedRandomVectorGenerator, ObservableSatellite, ObservableSatellite, QuadraticClockModel, double, double, double, AmbiguityCache) - Constructor for class org.orekit.estimation.measurements.generation.OneWayGNSSPhaseBuilder
Simple constructor.
OneWayGNSSRange - Class in org.orekit.estimation.measurements.gnss
One-way GNSS range measurement.
OneWayGNSSRange(PVCoordinatesProvider, double, AbsoluteDate, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.gnss.OneWayGNSSRange
Simple constructor.
OneWayGNSSRange(PVCoordinatesProvider, QuadraticClockModel, AbsoluteDate, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.gnss.OneWayGNSSRange
Simple constructor.
OneWayGNSSRangeBuilder - Class in org.orekit.estimation.measurements.generation
Builder for OneWayGNSSRange measurements.
OneWayGNSSRangeBuilder(CorrelatedRandomVectorGenerator, ObservableSatellite, ObservableSatellite, ToDoubleFunction<AbsoluteDate>, double, double) - Constructor for class org.orekit.estimation.measurements.generation.OneWayGNSSRangeBuilder
Simple constructor.
OneWayGNSSRangeRate - Class in org.orekit.estimation.measurements.gnss
One-way GNSS range rate measurement.
OneWayGNSSRangeRate(PVCoordinatesProvider, double, AbsoluteDate, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.gnss.OneWayGNSSRangeRate
Simple constructor.
OneWayGNSSRangeRate(PVCoordinatesProvider, QuadraticClockModel, AbsoluteDate, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.gnss.OneWayGNSSRangeRate
Simple constructor.
OneWayGNSSRangeRateBuilder - Class in org.orekit.estimation.measurements.generation
Builder for OneWayGNSSRangeRate measurements.
OneWayGNSSRangeRateBuilder(CorrelatedRandomVectorGenerator, ObservableSatellite, ObservableSatellite, double, double) - Constructor for class org.orekit.estimation.measurements.generation.OneWayGNSSRangeRateBuilder
Simple constructor.
OnOff - Enum in org.orekit.files.ccsds.definitions
On/Off status for various elements.
ONSTATION - org.orekit.files.ccsds.ndm.odm.ocm.OrbitElementsType
Geosynchronous on-station tailored set (a, ex, ey, ix, iy, λ).
ooA - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext
1 / A .
ooA - Variable in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext
1 / A .
ooAB - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext
1 / (A * B) .
ooAB - Variable in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext
1 / (A * B) .
ooBpo - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext
1 / (1 + B) .
ooBpo - Variable in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext
1 / (1 + B) .
ooMu - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext
1 / μ .
ooMu - Variable in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext
1 / μ .
OP - org.orekit.files.rinex.navigation.UtcId
UTC(OP).
openOnce() - Method in interface org.orekit.data.DataSource.ReaderOpener
Open the stream once.
openOnce() - Method in interface org.orekit.data.DataSource.StreamOpener
Open the stream once.
openReaderOnce() - Method in interface org.orekit.data.DataSource.Opener
Open a characters stream reader once.
openStreamOnce() - Method in interface org.orekit.data.DataSource.Opener
Open a bytes stream once.
OPERATIONAL - org.orekit.files.ccsds.ndm.odm.ocm.OpsStatus
Operational object.
OPERATOR - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Operator of the space object.
OPERATOR_CONTACT_POSITION - org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey
Contact position of the owner/operator of the object.
OPERATOR_EMAIL - org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey
Email address of the contact position for the object.
OPERATOR_ORGANIZATION - org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey
Contact organization of the object.
OPERATOR_PHONE - org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey
Phone number of the contact position for the object.
Opm - Class in org.orekit.files.ccsds.ndm.odm.opm
This class gathers the informations present in the Orbital Parameter Message (OPM).
Opm(OdmHeader, List<Segment<OdmCommonMetadata, OpmData>>, IERSConventions, DataContext, double) - Constructor for class org.orekit.files.ccsds.ndm.odm.opm.Opm
Simple constructor.
OpmData - Class in org.orekit.files.ccsds.ndm.odm.opm
Container for Orbit Parameter Message data.
OpmData(StateVector, KeplerianElements, SpacecraftParameters, CartesianCovariance, List<Maneuver>, UserDefined, double) - Constructor for class org.orekit.files.ccsds.ndm.odm.opm.OpmData
Simple constructor.
OpmParser - Class in org.orekit.files.ccsds.ndm.odm.opm
A parser for the CCSDS OPM (Orbit Parameter Message).
OpmParser(IERSConventions, boolean, DataContext, AbsoluteDate, double, double, ParsedUnitsBehavior, Function<ParseToken, List<ParseToken>>[]) - Constructor for class org.orekit.files.ccsds.ndm.odm.opm.OpmParser
Complete constructor.
OpmWriter - Class in org.orekit.files.ccsds.ndm.odm.opm
Writer for CCSDS Orbit Parameter Message.
OpmWriter(IERSConventions, DataContext, AbsoluteDate) - Constructor for class org.orekit.files.ccsds.ndm.odm.opm.OpmWriter
Complete constructor.
OPS_STATUS - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Operational status.
OpsStatus - Enum in org.orekit.files.ccsds.ndm.odm.ocm
Operational status used in CCSDS Orbit Comprehensive Messages.
ORB - org.orekit.files.ccsds.ndm.odm.ocm.OcmElements
Trajectory state time history (orbit).
ORB_AVERAGING - org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadataKey
Type of averaging (Osculating, mean Brouwer, other...).
ORB_REVNUM - org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadataKey
Integer orbit revolution number entry.
ORB_REVNUM_BASIS - org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadataKey
Basis for orbit revolution number entry.
Orbit - Class in org.orekit.orbits
This class handles orbital parameters.
Orbit(Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.Orbit
Default constructor.
Orbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.Orbit
Set the orbit from Cartesian parameters.
ORBIT - org.orekit.files.sp3.DataUsed
Orbit data.
ORBIT_A_E_MISMATCH_WITH_CONIC_TYPE - org.orekit.errors.OrekitMessages
ORBIT_A_E_MISMATCH_WITH_CONIC_TYPE.
ORBIT_AND_ATTITUDE_DATES_MISMATCH - org.orekit.errors.OrekitMessages
ORBIT_AND_ATTITUDE_DATES_MISMATCH.
ORBIT_ANOMALY_OUT_OF_HYPERBOLIC_RANGE - org.orekit.errors.OrekitMessages
ORBIT_ANOMALY_OUT_OF_HYPERBOLIC_RANGE.
ORBIT_CATEGORY - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Orbit category.
ORBIT_CENTER - org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey
Central body for Object 1 and 2.
ORBIT_TYPE_NOT_ALLOWED - org.orekit.errors.OrekitMessages
ORBIT_TYPE_NOT_ALLOWED.
OrbitBlender - Class in org.orekit.orbits
Orbit blender.
OrbitBlender(SmoothStepFactory.SmoothStepFunction, Propagator, Frame) - Constructor for class org.orekit.orbits.OrbitBlender
Default constructor.
OrbitCategory - Enum in org.orekit.files.ccsds.ndm.odm.ocm
Orbit category used in CCSDS Orbit Comprehensive Messages.
OrbitCorrection - Class in org.orekit.gnss.metric.messages.common
Container for SSR orbit correction data.
OrbitCorrection(double, double, double, double, double, double) - Constructor for class org.orekit.gnss.metric.messages.common.OrbitCorrection
Constructor.
OrbitCovariance - Class in org.orekit.files.ccsds.ndm.odm.ocm
Covariance entry.
OrbitCovariance(OrbitElementsType, Ordering, AbsoluteDate, String[], int) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovariance
Simple constructor.
OrbitCovarianceHistory - Class in org.orekit.files.ccsds.ndm.odm.ocm
Covariance history.
OrbitCovarianceHistory(OrbitCovarianceHistoryMetadata, List<OrbitCovariance>) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistory
Simple constructor.
OrbitCovarianceHistoryMetadata - Class in org.orekit.files.ccsds.ndm.odm.ocm
Metadata for covariance history.
OrbitCovarianceHistoryMetadata(AbsoluteDate) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata
Simple constructor.
OrbitCovarianceHistoryMetadataKey - Enum in org.orekit.files.ccsds.ndm.odm.ocm
OrbitDetermination - Class in org.orekit.files.ccsds.ndm.odm.ocm
Orbit determination data.
OrbitDetermination() - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Simple constructor.
OrbitDeterminationKey - Enum in org.orekit.files.ccsds.ndm.odm.ocm
Keys for orbit determination data entries.
OrbitElementsType - Enum in org.orekit.files.ccsds.ndm.odm.ocm
Orbit element set type used in CCSDS Orbit Comprehensive Messages.
OrbitHermiteInterpolator - Class in org.orekit.orbits
Class using a Hermite interpolator to interpolate orbits.
OrbitHermiteInterpolator(int, double, Frame, CartesianDerivativesFilter) - Constructor for class org.orekit.orbits.OrbitHermiteInterpolator
Constructor.
OrbitHermiteInterpolator(int, Frame) - Constructor for class org.orekit.orbits.OrbitHermiteInterpolator
Constructor with : Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of position and two time derivatives during interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).
OrbitHermiteInterpolator(int, Frame, CartesianDerivativesFilter) - Constructor for class org.orekit.orbits.OrbitHermiteInterpolator
Constructor with default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s).
OrbitHermiteInterpolator(Frame) - Constructor for class org.orekit.orbits.OrbitHermiteInterpolator
Constructor with : Default number of interpolation points of DEFAULT_INTERPOLATION_POINTS Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of position and two time derivatives during interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).
OrbitManeuver - Class in org.orekit.files.ccsds.ndm.odm.ocm
Maneuver entry.
OrbitManeuver() - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Build an uninitialized maneuver.
OrbitManeuverHistory - Class in org.orekit.files.ccsds.ndm.odm.ocm
Maneuver history.
OrbitManeuverHistory(OrbitManeuverHistoryMetadata, List<OrbitManeuver>) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistory
Simple constructor.
OrbitManeuverHistoryMetadata - Class in org.orekit.files.ccsds.ndm.odm.ocm
Metadata for maneuver history.
OrbitManeuverHistoryMetadata(AbsoluteDate) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Simple constructor.
OrbitManeuverHistoryMetadataKey - Enum in org.orekit.files.ccsds.ndm.odm.ocm
Keys for maneuver history container entries.
OrbitPhysicalProperties - Class in org.orekit.files.ccsds.ndm.odm.ocm
Spacecraft physical properties.
OrbitPhysicalProperties(AbsoluteDate) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Simple constructor.
OrbitPhysicalPropertiesKey - Enum in org.orekit.files.ccsds.ndm.odm.ocm
Keys for physical properties data entries.
OrbitRelativeFrame - Enum in org.orekit.files.ccsds.definitions
Frames used in CCSDS Orbit Data Messages.
ORBITS_MUS_MISMATCH - org.orekit.errors.OrekitMessages
ORBITS_MUS_MISMATCH.
OrbitType - Enum in org.orekit.orbits
Enumerate for Orbit and FieldOrbit parameters types.
orCombine(Collection<? extends EventDetector>) - Static method in class org.orekit.propagation.events.BooleanDetector
Create a new event detector that is the logical OR of the given event detectors.
orCombine(Collection<? extends FieldEventDetector<T>>) - Static method in class org.orekit.propagation.events.FieldBooleanDetector
Create a new event detector that is the logical OR of the given event detectors.
orCombine(EventDetector...) - Static method in class org.orekit.propagation.events.BooleanDetector
Create a new event detector that is the logical OR of the given event detectors.
orCombine(FieldEventDetector<T>...) - Static method in class org.orekit.propagation.events.FieldBooleanDetector
Create a new event detector that is the logical OR of the given event detectors.
Ordering - Enum in org.orekit.files.ccsds.ndm.odm.ocm
Keys for OrbitCovariance elements ordering.
OREKIT_DATA_PATH - Static variable in class org.orekit.data.DataProvidersManager
Name of the property defining the root directories or zip/jar files path for default configuration.
OrekitAttitudeEphemerisFile - Class in org.orekit.files.general
A class for encapsulating Orekit propagators within an AttitudeEphemerisFile complaint object that makes for easy serialization to external ephemeris formats like AEM.
OrekitAttitudeEphemerisFile() - Constructor for class org.orekit.files.general.OrekitAttitudeEphemerisFile
Standard default constructor.
OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment - Class in org.orekit.files.general
Ephemeris segment.
OrekitAttitudeEphemerisFile.OrekitSatelliteAttitudeEphemeris - Class in org.orekit.files.general
Inner class of OrekitAttitudeEphemerisFile that defines the OrekitAttitudeEphemerisFile.OrekitSatelliteAttitudeEphemeris corresponding object for this ephemeris type.
OrekitAttitudeEphemerisSegment(List<TimeStampedAngularCoordinates>, String, int, Frame, AngularDerivativesFilter) - Constructor for class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment
Constructor for OrekitAttitudeEphemerisSegment.
OrekitConfiguration - Class in org.orekit.utils
Utility class for setting global configuration parameters.
OrekitEphemerisFile - Class in org.orekit.files.general
A class for encapsulating Orekit propagators within an EphemerisFile complaint object that makes for easy serialization to external ephemeris formats like OEM.
OrekitEphemerisFile() - Constructor for class org.orekit.files.general.OrekitEphemerisFile
Standard default constructor.
OrekitEphemerisFile.OrekitEphemerisSegment - Class in org.orekit.files.general
Ephemeris segment.
OrekitEphemerisFile.OrekitSatelliteEphemeris - Class in org.orekit.files.general
Inner class of OrekitEphemerisFile that defines the OrekitEphemerisFile.OrekitSatelliteEphemeris corresponding object for this ephemeris type.
OrekitEphemerisSegment(List<TimeStampedPVCoordinates>, Frame, double, int) - Constructor for class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
constructor for OrekitEphemerisSegment.
OrekitException - Exception in org.orekit.errors
This class is the base class for all specific exceptions thrown by the Orekit classes.
OrekitException(Throwable, Localizable, Object...) - Constructor for exception org.orekit.errors.OrekitException
Simple constructor.
OrekitException(Localizable, Object...) - Constructor for exception org.orekit.errors.OrekitException
Simple constructor.
OrekitException(Localizable, Throwable) - Constructor for exception org.orekit.errors.OrekitException
Simple constructor.
OrekitException(MathRuntimeException) - Constructor for exception org.orekit.errors.OrekitException
Simple constructor.
OrekitException(OrekitException) - Constructor for exception org.orekit.errors.OrekitException
Copy constructor.
OrekitFixedStepHandler - Interface in org.orekit.propagation.sampling
This interface is a space-dynamics aware fixed size step handler.
OrekitIllegalArgumentException - Exception in org.orekit.errors
Extension of IllegalArgumentException with localized message.
OrekitIllegalArgumentException(Localizable, Object...) - Constructor for exception org.orekit.errors.OrekitIllegalArgumentException
Create an exception with localized message.
OrekitIllegalStateException - Exception in org.orekit.errors
Extension of IllegalStateException with localized message.
OrekitIllegalStateException(Localizable, Object...) - Constructor for exception org.orekit.errors.OrekitIllegalStateException
Create an exception with localized message.
OrekitInternalError - Exception in org.orekit.errors
Extension of Runtime with localized message for internal errors only.
OrekitInternalError(Throwable) - Constructor for exception org.orekit.errors.OrekitInternalError
Create an exception with localized message.
OrekitIOException - Exception in org.orekit.errors
Extension of IOException with localized message.
OrekitIOException(Localizable, Object...) - Constructor for exception org.orekit.errors.OrekitIOException
Create an exception with localized message.
OrekitMessages - Enum in org.orekit.errors
Enumeration for localized messages formats.
OrekitParseException - Exception in org.orekit.errors
Extension of ParseException with localized message.
OrekitParseException(Localizable, Object...) - Constructor for exception org.orekit.errors.OrekitParseException
Create an exception with localized message.
OrekitSatelliteAttitudeEphemeris(String) - Constructor for class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitSatelliteAttitudeEphemeris
Standard constructor for building the satellite Ephemeris object.
OrekitSatelliteEphemeris(String) - Constructor for class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
Standard constructor for building the satellite Ephemeris object.
OrekitStepHandler - Interface in org.orekit.propagation.sampling
This interface is a space-dynamics aware step handler.
OrekitStepInterpolator - Interface in org.orekit.propagation.sampling
This interface is a space-dynamics aware step interpolator.
OrekitStepNormalizer - Class in org.orekit.propagation.sampling
This class wraps an object implementing OrekitFixedStepHandler into a OrekitStepHandler.
OrekitStepNormalizer(double, OrekitFixedStepHandler) - Constructor for class org.orekit.propagation.sampling.OrekitStepNormalizer
Simple constructor.
org.orekit.annotation - package org.orekit.annotation
This package is the top level package for Orekit's specific annotations.
org.orekit.attitudes - package org.orekit.attitudes
This package provides classes to represent simple attitudes.
org.orekit.bodies - package org.orekit.bodies
This package provides interface to represent the position and geometry of space objects such as stars, planets or asteroids.
org.orekit.compiler.plugin - package org.orekit.compiler.plugin
This package provides elements to handle data context plugin.
org.orekit.control - package org.orekit.control
This package provides routines to perform optimal control within the frame of orbital mechanics.
org.orekit.control.indirect - package org.orekit.control.indirect
This package provides routines to perform so-called indirect optimal control within the frame of orbital mechanics.
org.orekit.control.indirect.adjoint - package org.orekit.control.indirect.adjoint
This package provides routines to model the adjoint dynamics as in the Pontryagin Maximum Principle, as used in indirect control.
org.orekit.control.indirect.adjoint.cost - package org.orekit.control.indirect.adjoint.cost
This package provides routines to model the control cost in adjoint equations as in the Pontryagin Maximum Principle.
org.orekit.control.indirect.shooting - package org.orekit.control.indirect.shooting
This package provides routines to solve indirect optimal control within the frame of orbital mechanics, using shooting methods.
org.orekit.control.indirect.shooting.boundary - package org.orekit.control.indirect.shooting.boundary
This package provides classes relative to the boundary conditions for indirect shooting.
org.orekit.control.indirect.shooting.propagation - package org.orekit.control.indirect.shooting.propagation
This package provides classes relative to the propagation part of indirect shooting.
org.orekit.data - package org.orekit.data
This package provide base classes for exploring the configured data directory tree and read external data that can be used by the library.
org.orekit.errors - package org.orekit.errors
This package provides classes to generate and handle exceptions.
org.orekit.estimation - package org.orekit.estimation
This package is the top level package for orbit determination.
org.orekit.estimation.iod - package org.orekit.estimation.iod
This package provides initial orbit determination methods.
org.orekit.estimation.leastsquares - package org.orekit.estimation.leastsquares
The leastsquares package provides an implementation of a batch least squares estimator engine to perform an orbit determination.
org.orekit.estimation.measurements - package org.orekit.estimation.measurements
The measurements package defines everything that is related to orbit determination measurements.
org.orekit.estimation.measurements.filtering - package org.orekit.estimation.measurements.filtering
This package provides measurement pre-processing filters.
org.orekit.estimation.measurements.generation - package org.orekit.estimation.measurements.generation
This package provides Orbit Determination measurements generation.
org.orekit.estimation.measurements.gnss - package org.orekit.estimation.measurements.gnss
This package provides methods to handle GNSS measurements.
org.orekit.estimation.measurements.modifiers - package org.orekit.estimation.measurements.modifiers
This package provides measurement modifier.
org.orekit.estimation.sequential - package org.orekit.estimation.sequential
The sequential package provides an implementation of a Kalman Filter engine to perform an orbit determination.
org.orekit.files - package org.orekit.files
Top level package for various parsers.
org.orekit.files.ccsds - package org.orekit.files.ccsds
This package is gathers sub-packages providing parsers/writers for various CCSDS messages.
org.orekit.files.ccsds.definitions - package org.orekit.files.ccsds.definitions
This package contains definitions for CCSDS objects (frames, time systems...).
org.orekit.files.ccsds.ndm - package org.orekit.files.ccsds.ndm
This package contains the base hierarchy for CCSDS ADM, ODM and TDM.
org.orekit.files.ccsds.ndm.adm - package org.orekit.files.ccsds.ndm.adm
This package contains class managing CCSDS Attitude Data Message.
org.orekit.files.ccsds.ndm.adm.acm - package org.orekit.files.ccsds.ndm.adm.acm
This package contains class managing CCSDS Attitude Comprehensive Message.
org.orekit.files.ccsds.ndm.adm.aem - package org.orekit.files.ccsds.ndm.adm.aem
This package contains class managing CCSDS Attitude Ephemeris Message.
org.orekit.files.ccsds.ndm.adm.apm - package org.orekit.files.ccsds.ndm.adm.apm
This package contains class managing CCSDS Attitude Parameter Message.
org.orekit.files.ccsds.ndm.cdm - package org.orekit.files.ccsds.ndm.cdm
This package contains class managing CCSDS Conjunction Data Message.
org.orekit.files.ccsds.ndm.odm - package org.orekit.files.ccsds.ndm.odm
This package contains class managing CCSDS Orbit Data Message.
org.orekit.files.ccsds.ndm.odm.ocm - package org.orekit.files.ccsds.ndm.odm.ocm
This package contains class managing CCSDS Orbit Comprehensive Message.
org.orekit.files.ccsds.ndm.odm.oem - package org.orekit.files.ccsds.ndm.odm.oem
This package contains class managing CCSDS Orbit Ephemeris Message.
org.orekit.files.ccsds.ndm.odm.omm - package org.orekit.files.ccsds.ndm.odm.omm
This package contains class managing CCSDS Orbit Mean-Elements Message.
org.orekit.files.ccsds.ndm.odm.opm - package org.orekit.files.ccsds.ndm.odm.opm
This package contains class managing CCSDS Orbit Parameter Message.
org.orekit.files.ccsds.ndm.tdm - package org.orekit.files.ccsds.ndm.tdm
This package contains class managing CCSDS Tracking Data Message.
org.orekit.files.ccsds.section - package org.orekit.files.ccsds.section
This package contains class managing the sections in CCSDS Messages.
org.orekit.files.ccsds.utils - package org.orekit.files.ccsds.utils
This package contains utilities shared by many CCSDS messages parsers/writers.
org.orekit.files.ccsds.utils.generation - package org.orekit.files.ccsds.utils.generation
This package contains utilities for CCSDS messages generation.
org.orekit.files.ccsds.utils.lexical - package org.orekit.files.ccsds.utils.lexical
This package contains utilities for CCSDS messages lexical analysis.
org.orekit.files.ccsds.utils.parsing - package org.orekit.files.ccsds.utils.parsing
This package contains classes related to the processing of parse tokens using the state design pattern.
org.orekit.files.general - package org.orekit.files.general
This package provides interfaces for orbit file representations and corresponding parsers.
org.orekit.files.ilrs - package org.orekit.files.ilrs
This package provides parsers for laser ranging data stored in CDR and CPF formats.
org.orekit.files.rinex - package org.orekit.files.rinex
This package is gathers sub-packages providing parsers/writers for various RINEX files.
org.orekit.files.rinex.clock - package org.orekit.files.rinex.clock
This package provides classes related to navigation clock files.
org.orekit.files.rinex.navigation - package org.orekit.files.rinex.navigation
This package provides classes related to RINEX navigation files.
org.orekit.files.rinex.observation - package org.orekit.files.rinex.observation
This package provides classes related to RINEX observation files.
org.orekit.files.rinex.section - package org.orekit.files.rinex.section
This package contains class managing the sections in RINEX files.
org.orekit.files.rinex.utils - package org.orekit.files.rinex.utils
This package contains utilities shared by many RINEX parsers/writers.
org.orekit.files.rinex.utils.parsing - package org.orekit.files.rinex.utils.parsing
This package contains classes related to the parsing of RINEX files.
org.orekit.files.sinex - package org.orekit.files.sinex
This package provides classes related to station data.
org.orekit.files.sp3 - package org.orekit.files.sp3
This package provides a parser for orbit data stored in SP3 format.
org.orekit.files.stk - package org.orekit.files.stk
This package provides a parser for STK ephemeris files.
org.orekit.forces - package org.orekit.forces
This package provides the interface for force models that will be used by the NumericalPropagator, as well as some classical spacecraft models for surface forces (spherical, box and solar array ...).
org.orekit.forces.drag - package org.orekit.forces.drag
This package provides all drag-related forces.
org.orekit.forces.empirical - package org.orekit.forces.empirical
This package provides empirical forces.
org.orekit.forces.gravity - package org.orekit.forces.gravity
This package provides all gravity-related forces.
org.orekit.forces.gravity.potential - package org.orekit.forces.gravity.potential
This package provides classes to read gravity field files and supports several different formats.
org.orekit.forces.inertia - package org.orekit.forces.inertia
This package provides inertial force model.
org.orekit.forces.maneuvers - package org.orekit.forces.maneuvers
This package provides models of simple maneuvers.
org.orekit.forces.maneuvers.jacobians - package org.orekit.forces.maneuvers.jacobians
Generators for columns of Jacobian matrices related to maneuver parameters.
org.orekit.forces.maneuvers.propulsion - package org.orekit.forces.maneuvers.propulsion
This package provides propulsion models intended to be used with class Maneuver.
org.orekit.forces.maneuvers.trigger - package org.orekit.forces.maneuvers.trigger
This package provides maneuver triggers' models intended to be used with class Maneuver.
org.orekit.forces.radiation - package org.orekit.forces.radiation
This package provides all radiation pressure related forces.
org.orekit.frames - package org.orekit.frames
This package provides classes to handle frames and transforms between them.
org.orekit.frames.encounter - package org.orekit.frames.encounter
Package specific to encounter local orbital frame.
org.orekit.geometry.fov - package org.orekit.geometry.fov
This package provides classes for representing a spacecraft sensor Field Of View.
org.orekit.gnss - package org.orekit.gnss
This package provides classes related to GNSS applications.
org.orekit.gnss.antenna - package org.orekit.gnss.antenna
This package provides classes related to receiver and satellites antenna modeling.
org.orekit.gnss.attitude - package org.orekit.gnss.attitude
This package provides classes related to navigation satellites attitude modeling.
org.orekit.gnss.metric - package org.orekit.gnss.metric
This package provides classes related to IGS binary formats.
org.orekit.gnss.metric.messages - package org.orekit.gnss.metric.messages
This package provides all supported IGS binary messages.
org.orekit.gnss.metric.messages.common - package org.orekit.gnss.metric.messages.common
This package contains utility classes relate to RTCM ephemeris messages.
org.orekit.gnss.metric.messages.rtcm - package org.orekit.gnss.metric.messages.rtcm
This package provides all supported RTCM messages.
org.orekit.gnss.metric.messages.rtcm.correction - package org.orekit.gnss.metric.messages.rtcm.correction
This package provides all supported RTCM correction messages.
org.orekit.gnss.metric.messages.rtcm.ephemeris - package org.orekit.gnss.metric.messages.rtcm.ephemeris
This package provides all supported RTCM ephemeris messages.
org.orekit.gnss.metric.messages.ssr - package org.orekit.gnss.metric.messages.ssr
This package provides all supported IGS SSR messages.
org.orekit.gnss.metric.messages.ssr.igm - package org.orekit.gnss.metric.messages.ssr.igm
This package provides all supported IGS Generic SSR Message types.
org.orekit.gnss.metric.messages.ssr.subtype - package org.orekit.gnss.metric.messages.ssr.subtype
This package provides all supported IGS SSR Sub-Type Message.
org.orekit.gnss.metric.ntrip - package org.orekit.gnss.metric.ntrip
This package provides streams reading from ntrip casters.
org.orekit.gnss.metric.parser - package org.orekit.gnss.metric.parser
This package provides the top level MessagesParser class that can extract messages from binary containers like ByteArrayEncodedMessages or {link org.orekit.metric.gnss.ssr.parser.InputStreamEncodedMessages InputStreamEncodedMessages}.
org.orekit.gnss.rflink - package org.orekit.gnss.rflink
This package provides classes related to RF-links binary formats.
org.orekit.gnss.rflink.gps - package org.orekit.gnss.rflink.gps
This package provides classes related to GPS RF-links binary formats.
org.orekit.models - package org.orekit.models
Top level package for physical models.
org.orekit.models.earth - package org.orekit.models.earth
This package provides models that simulate certain physical phenomena of Earth and the near-Earth environment.
org.orekit.models.earth.atmosphere - package org.orekit.models.earth.atmosphere
This package provides the atmosphere model interface and several implementations.
org.orekit.models.earth.atmosphere.data - package org.orekit.models.earth.atmosphere.data
This package provides classes to get atmospheric data, including solar flux and planetary geomagnetic indices.
org.orekit.models.earth.displacement - package org.orekit.models.earth.displacement
This package provides models computing reference points displacements on Earth surface.
org.orekit.models.earth.ionosphere - package org.orekit.models.earth.ionosphere
This package provides models that simulate the impact of the ionosphere.
org.orekit.models.earth.tessellation - package org.orekit.models.earth.tessellation
This package provides ways to do tessellation and sampling of zones of interest over an ellipsoid surface.
org.orekit.models.earth.troposphere - package org.orekit.models.earth.troposphere
This package provides models that simulate the impact of the troposphere.
org.orekit.models.earth.weather - package org.orekit.models.earth.weather
This package provides models that simulate global weather conditions on Earth.
org.orekit.models.earth.weather.water - package org.orekit.models.earth.weather.water
This package provides models that convert between relative humidity and partial water pressure.
org.orekit.orbits - package org.orekit.orbits
This package provides classes to represent orbits.
org.orekit.propagation - package org.orekit.propagation
Propagation
org.orekit.propagation.analytical - package org.orekit.propagation.analytical
Top level package for analytical propagators.
org.orekit.propagation.analytical.gnss - package org.orekit.propagation.analytical.gnss
This package provides classes to propagate GNSS orbits.
org.orekit.propagation.analytical.gnss.data - package org.orekit.propagation.analytical.gnss.data
This package provides classes related to navigation data containing in GNSS almanacs and navigation messages.
org.orekit.propagation.analytical.intelsat - package org.orekit.propagation.analytical.intelsat
This package provides classes to propagate Intelsat's 11 elements.
org.orekit.propagation.analytical.tle - package org.orekit.propagation.analytical.tle
This package provides classes to read and extrapolate tle's.
org.orekit.propagation.analytical.tle.generation - package org.orekit.propagation.analytical.tle.generation
This package provides classes related to TLE generation.
org.orekit.propagation.conversion - package org.orekit.propagation.conversion
This package provides tools to convert a given propagator or a set of SpacecraftState into another propagator.
org.orekit.propagation.conversion.averaging - package org.orekit.propagation.conversion.averaging
This package wraps methods from various (semi)analytical models in Orekit to convert back and forth between an averaged orbital state and an osculating one.
org.orekit.propagation.conversion.averaging.converters - package org.orekit.propagation.conversion.averaging.converters
This package wraps conversions from an osculating orbit to an averaged state according to a given theory (usually via a fixed-point algorithm using the inverse conversion).
org.orekit.propagation.conversion.averaging.elements - package org.orekit.propagation.conversion.averaging.elements
This package contains data classes representing averaged orbital elements (not time-stamped and in any theory compatible with this choice of coordinates).
org.orekit.propagation.events - package org.orekit.propagation.events
This package provides interfaces and classes dealing with events occurring during propagation.
org.orekit.propagation.events.handlers - package org.orekit.propagation.events.handlers
This package provides an interface and classes dealing with events occurrence only.
org.orekit.propagation.events.intervals - package org.orekit.propagation.events.intervals
This package provides built-in implementations of AdaptableInterval.
org.orekit.propagation.integration - package org.orekit.propagation.integration
Utilities for integration-based propagators (both numerical and semi-analytical).
org.orekit.propagation.numerical - package org.orekit.propagation.numerical
Top level package for numerical propagators.
org.orekit.propagation.numerical.cr3bp - package org.orekit.propagation.numerical.cr3bp
Top level package for CR3BP Models used with a numerical propagator.
org.orekit.propagation.sampling - package org.orekit.propagation.sampling
This package provides interfaces and classes dealing with step handling during propagation.
org.orekit.propagation.semianalytical - package org.orekit.propagation.semianalytical
Top level package for semi-analytical propagators.
org.orekit.propagation.semianalytical.dsst - package org.orekit.propagation.semianalytical.dsst
This package provides an implementation of the Draper Semi-analytical Satellite Theory (DSST).
org.orekit.propagation.semianalytical.dsst.forces - package org.orekit.propagation.semianalytical.dsst.forces
This package provides force models for Draper Semi-analytical Satellite Theory (DSST).
org.orekit.propagation.semianalytical.dsst.utilities - package org.orekit.propagation.semianalytical.dsst.utilities
This package provides utilities for Draper Semi-analytical Satellite Theory (DSST).
org.orekit.propagation.semianalytical.dsst.utilities.hansen - package org.orekit.propagation.semianalytical.dsst.utilities.hansen
This package provides Hansen coefficient related utilities for Draper Semi-analytical Satellite Theory (DSST).
org.orekit.ssa - package org.orekit.ssa
Top level package for various space situational awareness fields as well as associated evaluation metrics.
org.orekit.ssa.collision.shorttermencounter.probability.twod - package org.orekit.ssa.collision.shorttermencounter.probability.twod
Package specific to calculus assuming a 2D short-term encounter model.
org.orekit.ssa.metrics - package org.orekit.ssa.metrics
This package stores space situational awareness evaluation metrics.
org.orekit.time - package org.orekit.time
This independent package provides classes to handle epochs, time scales, and to compare instants together.
org.orekit.utils - package org.orekit.utils
This package provides useful objects.
org.orekit.utils.units - package org.orekit.utils.units
This package provides very basic handling of units.
ORIGINATOR - org.orekit.files.ccsds.section.HeaderKey
Creating agency or operator.
ORIGINATOR_ADDRESS - org.orekit.files.ccsds.ndm.adm.acm.AcmMetadataKey
Address of Programmatic Point Of Contact at originator.
ORIGINATOR_ADDRESS - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Address of Programmatic Point Of Contact at originator.
ORIGINATOR_EMAIL - org.orekit.files.ccsds.ndm.adm.acm.AcmMetadataKey
Email address of Programmatic Point Of Contact at originator.
ORIGINATOR_EMAIL - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Email address of Programmatic Point Of Contact at originator.
ORIGINATOR_PHONE - org.orekit.files.ccsds.ndm.adm.acm.AcmMetadataKey
Phone number of Programmatic Point Of Contact at originator.
ORIGINATOR_PHONE - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Phone number of Programmatic Point Of Contact at originator.
ORIGINATOR_POC - org.orekit.files.ccsds.ndm.adm.acm.AcmMetadataKey
Programmatic Point Of Contact at originator.
ORIGINATOR_POC - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Programmatic Point Of Contact at originator.
ORIGINATOR_POSITION - org.orekit.files.ccsds.ndm.adm.acm.AcmMetadataKey
Position of Programmatic Point Of Contact at originator.
ORIGINATOR_POSITION - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Position of Programmatic Point Of Contact at originator.
OrphanFrame - Class in org.orekit.frames
Prototype frame that can be built from leaf to roots and later attached to a tree.
OrphanFrame(String) - Constructor for class org.orekit.frames.OrphanFrame
Simple constructor.
OSCULATING - org.orekit.propagation.PropagationType
Osculating propagation.
osculatingDerivative(AbsoluteDate) - Method in class org.orekit.utils.SecularAndHarmonic
Get fitted osculating derivative.
osculatingSecondDerivative(AbsoluteDate) - Method in class org.orekit.utils.SecularAndHarmonic
Get fitted osculating second derivative.
OsculatingToAveragedConverter<T extends AveragedOrbitalState> - Interface in org.orekit.propagation.conversion.averaging.converters
Interface for osculating-to-averaged converters.
OsculatingToBrouwerLyddaneConverter - Class in org.orekit.propagation.conversion.averaging.converters
Class for osculating-to-averaged conversion according to Brouwer-Lyddane theory.
OsculatingToBrouwerLyddaneConverter(double, int, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.conversion.averaging.converters.OsculatingToBrouwerLyddaneConverter
Constructor.
OsculatingToBrouwerLyddaneConverter(UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.conversion.averaging.converters.OsculatingToBrouwerLyddaneConverter
Constructor with default parameters for fixed-point algorithm.
OsculatingToDSST6X0Converter - Class in org.orekit.propagation.conversion.averaging.converters
Class for osculating-to-averaged conversion according to DSST theory, using 6 zonal harmonics as the only perturbations.
OsculatingToDSST6X0Converter(double, int, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.conversion.averaging.converters.OsculatingToDSST6X0Converter
Constructor.
OsculatingToDSST6X0Converter(UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.conversion.averaging.converters.OsculatingToDSST6X0Converter
Constructor with default parameters for fixed-point algorithm.
OsculatingToEcksteinHechlerConverter - Class in org.orekit.propagation.conversion.averaging.converters
Class for osculating-to-averaged conversion according to Eckstein-Hechler theory.
OsculatingToEcksteinHechlerConverter(double, int, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.conversion.averaging.converters.OsculatingToEcksteinHechlerConverter
Constructor.
OsculatingToEcksteinHechlerConverter(UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.conversion.averaging.converters.OsculatingToEcksteinHechlerConverter
Constructor with default parameters for fixed-point algorithm.
OsculatingToMeanElementsConverter - Class in org.orekit.propagation.conversion
This class converts osculating orbital elements into mean elements.
OsculatingToMeanElementsConverter(SpacecraftState, int, Propagator, double) - Constructor for class org.orekit.propagation.conversion.OsculatingToMeanElementsConverter
Constructor.
OsculatingToSGP4Converter - Class in org.orekit.propagation.conversion.averaging.converters
Class for osculating-to-averaged conversion according to "SGP4" theory, meant as the set of models associated to Two-Line Elements.
OsculatingToSGP4Converter() - Constructor for class org.orekit.propagation.conversion.averaging.converters.OsculatingToSGP4Converter
Constructor with default data context.
OsculatingToSGP4Converter(double, int, double, DataContext) - Constructor for class org.orekit.propagation.conversion.averaging.converters.OsculatingToSGP4Converter
Constructor.
OsculatingToSGP4Converter(DataContext) - Constructor for class org.orekit.propagation.conversion.averaging.converters.OsculatingToSGP4Converter
Constructor with default parameters for fixed-point algorithm.
osculatingValue(AbsoluteDate) - Method in class org.orekit.utils.SecularAndHarmonic
Get fitted osculating value.
OTHER - org.orekit.files.ccsds.ndm.odm.ocm.ManBasis
Other bases.
OTHER - org.orekit.files.ccsds.ndm.odm.ocm.ObjectType
Other.
OTHER - org.orekit.files.sp3.SP3OrbitType
other type, defined by SP3 file producing agency.
OUT_OF_RANGE_BODY_EPHEMERIDES_DATE - org.orekit.errors.OrekitMessages
OUT_OF_RANGE_BODY_EPHEMERIDES_DATE.
OUT_OF_RANGE_DATE - org.orekit.errors.OrekitMessages
OUT_OF_RANGE_DATE.
OUT_OF_RANGE_DERIVATION_ORDER - org.orekit.errors.OrekitMessages
OUT_OF_RANGE_DERIVATION_ORDER.
OUT_OF_RANGE_EPHEMERIDES_DATE_AFTER - org.orekit.errors.OrekitMessages
OUT_OF_RANGE_EPHEMERIDES_DATE_AFTER.
OUT_OF_RANGE_EPHEMERIDES_DATE_BEFORE - org.orekit.errors.OrekitMessages
OUT_OF_RANGE_EPHEMERIDES_DATE_BEFORE.
OUT_OF_RANGE_SECONDS_NUMBER - org.orekit.errors.OrekitMessages
OUT_OF_RANGE_SECONDS_NUMBER.
OUT_OF_RANGE_SECONDS_NUMBER_DETAIL - org.orekit.errors.OrekitMessages
OUT_OF_RANGE_SECONDS_NUMBER_DETAIL.
OUT_OF_RANGE_TIME_TRANSFORM - org.orekit.errors.OrekitMessages
OUT_OF_RANGE_TIME_TRANSFORM.
OutlierFilter<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.modifiers
Modifier that sets estimated measurement weight to 0 if residual is too far from expected domain.
OutlierFilter(int, double) - Constructor for class org.orekit.estimation.measurements.modifiers.OutlierFilter
Simple constructor.
outputField(TimeConverter, OrbitManeuver) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
Output one maneuver field.
OUTSIDE_CONE_TOUCHING_POLYGON_AT_VERTICES - org.orekit.geometry.fov.PolygonalFieldOfView.DefiningConeType
Constant for cones outside polygons and touching it at polygon vertices.
OWNER - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Owner of the space object.

P

P - org.orekit.gnss.SignalCode
GPS P (AS off) / GLONASS P / QZSS L5P / Beidou Pilot codes.
P1 - org.orekit.gnss.ObservationType
Pseudorange GPS L1 / GLONASS G1 for Rinex2.
P1 - Static variable in class org.orekit.models.earth.displacement.Tide
P₁ tide.
P2 - org.orekit.gnss.ObservationType
Pseudorange GPS L2 / GLONASS G2 for Rinex2.
PA - Static variable in enum org.orekit.orbits.OrbitType
Name for perigee argument.
Panel - Class in org.orekit.forces
Base class representing one panel of a satellite.
Panel(double, boolean, double, double, double, double) - Constructor for class org.orekit.forces.Panel
Simple constructor.
PARAMETER_NOT_SET - org.orekit.errors.OrekitMessages
PARAMETER_NOT_SET.
PARAMETER_PERIODS_HAS_ALREADY_BEEN_SET - org.orekit.errors.OrekitMessages
PARAMETER_PERIODS_HAS_ALREADY_BEEN_SET.
PARAMETER_WITH_SEVERAL_ESTIMATED_VALUES - org.orekit.errors.OrekitMessages
PARAMETER_WITH_SEVERAL_ESTIMATED_VALUES.
ParameterDrivenDateIntervalDetector - Class in org.orekit.propagation.events
Detector for date intervals that may be offset thanks to parameter drivers.
ParameterDrivenDateIntervalDetector(String, AbsoluteDate, double) - Constructor for class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector
Build a new instance.
ParameterDrivenDateIntervalDetector(String, AbsoluteDate, AbsoluteDate) - Constructor for class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector
Build a new instance.
ParameterDrivenDateIntervalDetector(AdaptableInterval, double, int, EventHandler, DateDriver, DateDriver, DateDriver, ParameterDriver) - Constructor for class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector
Protected constructor with full parameters.
ParameterDriver - Class in org.orekit.utils
Class allowing to drive the value of a parameter.
ParameterDriver(String, double, double, double, double) - Constructor for class org.orekit.utils.ParameterDriver
Simple constructor.
ParameterDriver(String, TimeSpanMap<String>, TimeSpanMap<Double>, double, double, double, double) - Constructor for class org.orekit.utils.ParameterDriver
Create a new instance from another parameterDriver informations for example (useful for ParameterDriversList.DelegatingDriver)) At construction, the parameter new is configured as not selected, the reference date is set to null.
ParameterDriversList - Class in org.orekit.utils
Class managing several parameter drivers, taking care of duplicated names.
ParameterDriversList() - Constructor for class org.orekit.utils.ParameterDriversList
Creates an empty list.
ParameterDriversList.DelegatingDriver - Class in org.orekit.utils
Specialized driver delegating to several other managing the same parameter name.
ParameterDriversProvider - Interface in org.orekit.utils
Provider for parameters drivers.
ParameterFunction - Interface in org.orekit.utils
Interface representing a scalar function depending on a ParameterDriver.
ParameterObserver - Interface in org.orekit.utils
Interface for observing parameters changes.
ParametricAcceleration - Class in org.orekit.forces.empirical
This class implements a parametric acceleration.
ParametricAcceleration(Vector3D, boolean, AccelerationModel) - Constructor for class org.orekit.forces.empirical.ParametricAcceleration
Simple constructor.
ParametricAcceleration(Vector3D, AttitudeProvider, AccelerationModel) - Constructor for class org.orekit.forces.empirical.ParametricAcceleration
Simple constructor.
ParametricModelEffect - Interface in org.orekit.estimation.measurements.modifiers
Functional interface for parametric models.
ParametricModelEffectGradient - Interface in org.orekit.estimation.measurements.modifiers
Functional interface for parametric models.
PARITY_SIZE - Static variable in class org.orekit.gnss.rflink.gps.SubFrame
Size of parity field.
parse(boolean, boolean, RotationOrder, boolean, ContextBinding, String[]) - Method in enum org.orekit.files.ccsds.ndm.adm.AttitudeType
Get the angular coordinates corresponding to the attitude data.
parse(BufferedReader, String) - Method in class org.orekit.files.rinex.clock.RinexClockParser
Parse an IGS clock file from a stream.
parse(InputStream) - Method in class org.orekit.files.rinex.clock.RinexClockParser
Parse an IGS clock file from an input stream using the UTF-8 charset.
parse(InputStream, String) - Method in class org.orekit.data.PoissonSeriesParser
Parse a stream.
parse(InputStream, String) - Method in class org.orekit.data.SimpleTimeStampedTableParser
Parse a stream.
parse(InputStream, String) - Method in interface org.orekit.frames.EopHistoryLoader.Parser
Parse EOP from the given input stream.
parse(InputStream, String) - Method in class org.orekit.time.AGILeapSecondFilesLoader.Parser
Load UTC-TAI offsets entries read from some file.
parse(InputStream, String) - Method in class org.orekit.time.TAIUTCDatFilesLoader.Parser
Load UTC-TAI offsets entries read from some file.
parse(InputStream, String) - Method in class org.orekit.time.UTCTAIHistoryFilesLoader.Parser
Load UTC-TAI offsets entries read from some file.
parse(InputStream, String) - Method in interface org.orekit.time.UTCTAIOffsetsLoader.Parser
Parse leap seconds from the input stream.
parse(String) - Method in class org.orekit.data.PolynomialParser
Parse a polynomial expression.
parse(String) - Static method in enum org.orekit.files.ccsds.definitions.CelestialBodyFrame
Parse a CCSDS frame.
parse(String) - Static method in class org.orekit.files.ccsds.definitions.OdMethodFacade
Parse a string from OCM.
parse(String) - Static method in class org.orekit.files.ccsds.definitions.PocMethodFacade
Parse a string from CDM.
parse(String) - Static method in class org.orekit.files.ccsds.definitions.SpacecraftBodyFrame
Build an instance from a normalized descriptor.
parse(String) - Method in class org.orekit.files.ccsds.definitions.TimeConverter
Parse a relative or absolute date.
parse(String) - Static method in enum org.orekit.files.ccsds.definitions.TimeSystem
Parse a value from a key=value entry.
parse(String) - Method in class org.orekit.files.rinex.clock.RinexClockParser
Parse an IGS clock file from a file on the local file system.
parse(String) - Static method in enum org.orekit.files.sp3.SP3FileType
Parse the string to get the data used.
parse(String) - Static method in enum org.orekit.files.stk.STKEphemerisFile.STKCoordinateSystem
Parses a coordinate system from a string.
parse(String) - Static method in class org.orekit.utils.units.Unit
Parse a unit.
parse(String, String, char) - Static method in enum org.orekit.files.sp3.DataUsed
Parse the string to get the data used.
parse(String, IERSConventions, boolean, DataContext, boolean, boolean, boolean) - Static method in class org.orekit.files.ccsds.definitions.FrameFacade
Simple constructor.
parse(DataSource) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmParser
Parse an attitude ephemeris file from a data source.
parse(DataSource) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser
Parse an attitude ephemeris file from a data source.
parse(DataSource) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser
Parse an ephemeris file from a data source.
parse(DataSource) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser
Parse an ephemeris file from a data source.
parse(DataSource) - Method in interface org.orekit.files.general.AttitudeEphemerisFileParser
Parse an attitude ephemeris file from a data source.
parse(DataSource) - Method in interface org.orekit.files.general.EphemerisFileParser
Parse an ephemeris file from a data source.
parse(DataSource) - Method in class org.orekit.files.ilrs.CPFParser
Parse an ephemeris file from a data source.
parse(DataSource) - Method in class org.orekit.files.ilrs.CRDParser
Parse a CRD file.
parse(DataSource) - Method in class org.orekit.files.rinex.clock.RinexClockParser
Parse an IGS clock file from a DataSource.
parse(DataSource) - Method in class org.orekit.files.rinex.navigation.RinexNavigationParser
Parse RINEX navigation messages.
parse(DataSource) - Method in class org.orekit.files.rinex.observation.RinexObservationParser
Parse RINEX observations messages.
parse(DataSource) - Method in class org.orekit.files.sp3.SP3Parser
 
parse(DataSource) - Method in class org.orekit.files.stk.STKEphemerisFileParser
 
parse(DataSource) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficientsBlqParser
Parse a BLQ file.
parse(EncodedMessage) - Static method in class org.orekit.gnss.rflink.gps.SubFrame
Builder for sub-frames.
parse(EncodedMessage, boolean) - Method in class org.orekit.gnss.metric.parser.MessagesParser
Parse one message.
parse(EncodedMessage, int) - Method in interface org.orekit.gnss.metric.parser.MessageType
Parse an encoded message.
parseCCSDSCalendarSegmentedTimeCode(byte, byte[]) - Static method in class org.orekit.time.AbsoluteDate
Build an instance from a CCSDS Calendar Segmented Time Code (CCS).
parseCCSDSCalendarSegmentedTimeCode(byte, byte[]) - Method in class org.orekit.time.FieldAbsoluteDate
Build an instance from a CCSDS Calendar Segmented Time Code (CCS).
parseCCSDSCalendarSegmentedTimeCode(byte, byte[], TimeScale) - Static method in class org.orekit.time.AbsoluteDate
Build an instance from a CCSDS Calendar Segmented Time Code (CCS).
parseCCSDSCalendarSegmentedTimeCode(byte, byte[], TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate
Build an instance from a CCSDS Calendar Segmented Time Code (CCS).
parseCCSDSDaySegmentedTimeCode(byte, byte[], DateComponents) - Static method in class org.orekit.time.AbsoluteDate
Build an instance from a CCSDS Day Segmented Time Code (CDS).
parseCCSDSDaySegmentedTimeCode(byte, byte[], DateComponents, TimeScale) - Static method in class org.orekit.time.AbsoluteDate
Build an instance from a CCSDS Day Segmented Time Code (CDS).
parseCCSDSDaySegmentedTimeCode(Field<T>, byte, byte[], DateComponents) - Static method in class org.orekit.time.FieldAbsoluteDate
Build an instance from a CCSDS Day Segmented Time Code (CDS).
parseCCSDSDaySegmentedTimeCode(Field<T>, byte, byte[], DateComponents, TimeScale) - Static method in class org.orekit.time.FieldAbsoluteDate
Build an instance from a CCSDS Day Segmented Time Code (CDS).
parseCCSDSUnsegmentedTimeCode(byte, byte, byte[], AbsoluteDate) - Static method in class org.orekit.time.AbsoluteDate
Build an instance from a CCSDS Unsegmented Time Code (CUC).
parseCCSDSUnsegmentedTimeCode(byte, byte, byte[], AbsoluteDate, AbsoluteDate) - Static method in class org.orekit.time.AbsoluteDate
Build an instance from a CCSDS Unsegmented Time Code (CUC).
parseCCSDSUnsegmentedTimeCode(Field<T>, byte, byte, byte[], FieldAbsoluteDate<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Build an instance from a CCSDS Unsegmented Time Code (CUC).
parseCCSDSUnsegmentedTimeCode(Field<T>, byte, byte, byte[], FieldAbsoluteDate<T>, FieldAbsoluteDate<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Build an instance from a CCSDS Unsegmented Time Code (CUC).
parseClockDataType(String) - Static method in enum org.orekit.files.rinex.clock.RinexClock.ClockDataType
Parse a string to get the time system.
parseCoefficient(String, Flattener, double[], int, int, String, String) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Parse a coefficient.
parseComment(int, String, RinexFile<?>) - Static method in class org.orekit.files.rinex.utils.parsing.RinexUtils
Parse a comment.
parseDate(String) - Static method in class org.orekit.time.DateComponents
Parse a string in ISO-8601 format to build a date.
parseDateTime(String) - Static method in class org.orekit.time.DateTimeComponents
Parse a string in ISO-8601 format to build a date/time.
ParsedMessage - Class in org.orekit.gnss.metric.messages
Abstract base class for decoded IGS messages.
ParsedMessage(int) - Constructor for class org.orekit.gnss.metric.messages.ParsedMessage
Simple constructor.
parseDouble(String) - Static method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Parse a double from a string.
parseDouble(String, int, int) - Static method in class org.orekit.files.rinex.utils.parsing.RinexUtils
Parse a double value.
ParsedUnitsBehavior - Enum in org.orekit.files.ccsds.ndm
Behavior adopted for units that have been parsed from a CCSDS message.
parseInt(String, int, int) - Static method in class org.orekit.files.rinex.utils.parsing.RinexUtils
Parse an integer value.
parseMessage(DataSource) - Method in interface org.orekit.files.ccsds.utils.lexical.MessageParser
Parse a data source.
parseMessage(DataSource) - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser
Parse a data source.
parseMessageNumber(EncodedMessage) - Method in class org.orekit.gnss.metric.parser.IgsSsrMessagesParser
Parse the message number.
parseMessageNumber(EncodedMessage) - Method in class org.orekit.gnss.metric.parser.MessagesParser
Parse the message number.
parseMessageNumber(EncodedMessage) - Method in class org.orekit.gnss.metric.parser.RtcmMessagesParser
Parse the message number.
parseMonth(String) - Static method in enum org.orekit.time.Month
Parse the string to get the month.
parseOneLetterCode(String) - Static method in enum org.orekit.gnss.TimeSystem
Parse a string to get the time system.
parseProgramRunByDate(String, int, String, TimeScales, RinexBaseHeader) - Static method in class org.orekit.files.rinex.utils.parsing.RinexUtils
Parse program, run/by and date.
Parser - Class in org.orekit.utils.units
Parser for units.
Parser() - Constructor for class org.orekit.time.AGILeapSecondFilesLoader.Parser
Simple constructor.
Parser() - Constructor for class org.orekit.time.TAIUTCDatFilesLoader.Parser
Simple constructor.
Parser() - Constructor for class org.orekit.time.UTCTAIHistoryFilesLoader.Parser
Simple constructor.
ParserBuilder - Class in org.orekit.files.ccsds.ndm
Builder for all CCSDS Message files parsers.
ParserBuilder() - Constructor for class org.orekit.files.ccsds.ndm.ParserBuilder
Simple constructor.
ParserBuilder(DataContext) - Constructor for class org.orekit.files.ccsds.ndm.ParserBuilder
Simple constructor.
parseRinexFileType(String) - Static method in enum org.orekit.files.rinex.utils.RinexFileType
Parse the string to get the type.
parseSatelliteSystem(String) - Static method in enum org.orekit.gnss.SatelliteSystem
Parse a string to get the satellite system.
parseSatelliteSystemWithGPSDefault(String) - Static method in enum org.orekit.gnss.SatelliteSystem
Parse a string to get the satellite system.
parseSatelliteType(String) - Static method in enum org.orekit.gnss.antenna.SatelliteType
Parse a string to get the satellite type.
parseString(String, int, int) - Static method in class org.orekit.files.rinex.utils.parsing.RinexUtils
Parse a string value.
parseTime(String) - Static method in class org.orekit.time.TimeComponents
Parse a string in ISO-8601 format to build a time.
parseTimeSystem(String) - Static method in enum org.orekit.gnss.TimeSystem
Parse a string to get the time system.
ParseToken - Class in org.orekit.files.ccsds.utils.lexical
Token occurring during CCSDS file parsing.
ParseToken(TokenType, String, String, Unit, int, String) - Constructor for class org.orekit.files.ccsds.utils.lexical.ParseToken
Simple constructor.
ParseToken.BooleanConsumer - Interface in org.orekit.files.ccsds.utils.lexical
Interface representing instance methods that consume boolean values.
ParseToken.CenterConsumer - Interface in org.orekit.files.ccsds.utils.lexical
Interface representing instance methods that consume center values.
ParseToken.CenterListConsumer - Interface in org.orekit.files.ccsds.utils.lexical
Interface representing instance methods that consume center lists.
ParseToken.CharConsumer - Interface in org.orekit.files.ccsds.utils.lexical
Interface representing instance methods that consume character values.
ParseToken.DateConsumer - Interface in org.orekit.files.ccsds.utils.lexical
Interface representing instance methods that consume date values.
ParseToken.DoubleArrayConsumer - Interface in org.orekit.files.ccsds.utils.lexical
Interface representing instance methods that consume double array.
ParseToken.DoubleConsumer - Interface in org.orekit.files.ccsds.utils.lexical
Interface representing instance methods that consume double values.
ParseToken.DoublyIndexedDoubleConsumer - Interface in org.orekit.files.ccsds.utils.lexical
Interface representing instance methods that consume doubly-indexed double values.
ParseToken.EnumConsumer<T extends Enum<T>> - Interface in org.orekit.files.ccsds.utils.lexical
Interface representing instance methods that consume enum values.
ParseToken.EnumListConsumer<T extends Enum<T>> - Interface in org.orekit.files.ccsds.utils.lexical
Interface representing instance methods that consume lists of enum values.
ParseToken.FrameConsumer - Interface in org.orekit.files.ccsds.utils.lexical
Interface representing instance methods that consume frame values.
ParseToken.IndexedDoubleArrayConsumer - Interface in org.orekit.files.ccsds.utils.lexical
Interface representing instance methods that consume indexed double array values.
ParseToken.IndexedDoubleConsumer - Interface in org.orekit.files.ccsds.utils.lexical
Interface representing instance methods that consume indexed double values.
ParseToken.IndexedIntConsumer - Interface in org.orekit.files.ccsds.utils.lexical
Interface representing instance methods that consume indexed integer values.
ParseToken.IndexedStringConsumer - Interface in org.orekit.files.ccsds.utils.lexical
Interface representing instance methods that consume indexed string values.
ParseToken.IntConsumer - Interface in org.orekit.files.ccsds.utils.lexical
Interface representing instance methods that consume integer values.
ParseToken.IntegerArrayConsumer - Interface in org.orekit.files.ccsds.utils.lexical
Interface representing instance methods that consume integer array.
ParseToken.LabeledDoubleConsumer - Interface in org.orekit.files.ccsds.utils.lexical
Interface representing instance methods that consume labeled double values.
ParseToken.ManeuvrableConsumer - Interface in org.orekit.files.ccsds.utils.lexical
Interface representing instance methods that consume Maneuvrable values.
ParseToken.RotationOrderConsumer - Interface in org.orekit.files.ccsds.utils.lexical
Interface representing instance methods that consume otation order values.
ParseToken.StringConsumer - Interface in org.orekit.files.ccsds.utils.lexical
Interface representing instance methods that consume string values.
ParseToken.StringListConsumer - Interface in org.orekit.files.ccsds.utils.lexical
Interface representing instance methods that consume lists of strings values.
ParseToken.TimeSystemConsumer - Interface in org.orekit.files.ccsds.utils.lexical
Interface representing instance methods that consume time systems values.
ParseToken.UnitListConsumer - Interface in org.orekit.files.ccsds.utils.lexical
Interface representing instance methods that consume units lists values.
ParseToken.VectorConsumer - Interface in org.orekit.files.ccsds.utils.lexical
Interface representing instance methods that consume vector values.
parseTwoLettersCode(String) - Static method in enum org.orekit.gnss.TimeSystem
Parse a string to get the time system.
parseType(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.AttitudeType
Parse an attitude type.
parseType(String) - Static method in enum org.orekit.files.sp3.SP3OrbitType
Parse a string to get the type.
parseUtcId(String) - Static method in enum org.orekit.files.rinex.navigation.UtcId
Parse a string to get the UTC id.
parseVersionFileTypeSatelliteSystem(String, String, RinexBaseHeader, double...) - Static method in class org.orekit.files.rinex.utils.parsing.RinexUtils
Parse version, file type and satellite system.
PARTIALLY_OPERATIONAL - org.orekit.files.ccsds.ndm.odm.ocm.OpsStatus
partially operational object.
PARTICIPANT_1 - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
First participant entry.
PARTICIPANT_2 - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Second participant entry.
PARTICIPANT_3 - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Third participant entry.
PARTICIPANT_4 - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Fourth participant entry.
PARTICIPANT_5 - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Fifth participant entry.
PASCAL - Static variable in class org.orekit.utils.units.Unit
Pascal unit.
PAST_INFINITY - Static variable in class org.orekit.time.AbsoluteDate
Dummy date at infinity in the past direction.
PATERA_2001 - org.orekit.files.ccsds.definitions.PocMethodType
Patera 2001 method.
PATERA_2003 - org.orekit.files.ccsds.definitions.PocMethodType
Patera 2003 method.
PATERA_2005 - org.orekit.files.ccsds.definitions.PocMethodType
Patera 2005 method.
PATERA_2005 - org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethodType
Probability of collision computing method described in :"PATERA, Russell P.
Patera2005 - Class in org.orekit.ssa.collision.shorttermencounter.probability.twod
Compute the probability of collision using the method described in :"PATERA, Russell P.
Patera2005() - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.Patera2005
Default constructor built with the following trapezoid integrator: Minimal iteration count of 5 Maximum iteration count of 50000 .
Patera2005(UnivariateIntegrator, int) - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.Patera2005
Customizable constructor.
PATH - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Path entry.
PATH_1 - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Path 1 entry.
PATH_2 - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Path 2 entry.
pathDelay(double, double, double[]) - Method in class org.orekit.models.earth.ionosphere.EstimatedIonosphericModel
Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(double, GeodeticPoint, double[], AbsoluteDate) - Method in interface org.orekit.models.earth.troposphere.DiscreteTroposphericModel
Deprecated.
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(double, GeodeticPoint, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.EstimatedTroposphericModel
Deprecated.
pathDelay(double, GeodeticPoint, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.FixedTroposphericDelay
Deprecated.
pathDelay(double, GeodeticPoint, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.MariniMurrayModel
Deprecated.
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(double, GeodeticPoint, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.MendesPavlisModel
Deprecated.
pathDelay(double, GeodeticPoint, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.ModifiedSaastamoinenModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(double, GeodeticPoint, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.SaastamoinenModel
Deprecated.
pathDelay(double, GeodeticPoint, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
Deprecated.
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(double, GeodeticPoint, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.ViennaOneModel
Deprecated.
pathDelay(double, GeodeticPoint, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.ViennaThreeModel
Deprecated.
pathDelay(FieldSpacecraftState<T>, TopocentricFrame, double, T[]) - Method in class org.orekit.models.earth.ionosphere.EstimatedIonosphericModel
Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(FieldSpacecraftState<T>, TopocentricFrame, double, T[]) - Method in class org.orekit.models.earth.ionosphere.GlobalIonosphereMapModel
 
pathDelay(FieldSpacecraftState<T>, TopocentricFrame, double, T[]) - Method in interface org.orekit.models.earth.ionosphere.IonosphericModel
Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(FieldSpacecraftState<T>, TopocentricFrame, double, T[]) - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoModel
Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(FieldSpacecraftState<T>, TopocentricFrame, double, T[]) - Method in class org.orekit.models.earth.ionosphere.NeQuickModel
 
pathDelay(FieldSpacecraftState<T>, TopocentricFrame, double, T[]) - Method in class org.orekit.models.earth.ionosphere.SsrVtecIonosphericModel
Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(SpacecraftState, TopocentricFrame, double, double[]) - Method in class org.orekit.models.earth.ionosphere.EstimatedIonosphericModel
Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(SpacecraftState, TopocentricFrame, double, double[]) - Method in class org.orekit.models.earth.ionosphere.GlobalIonosphereMapModel
 
pathDelay(SpacecraftState, TopocentricFrame, double, double[]) - Method in interface org.orekit.models.earth.ionosphere.IonosphericModel
Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(SpacecraftState, TopocentricFrame, double, double[]) - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoModel
Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(SpacecraftState, TopocentricFrame, double, double[]) - Method in class org.orekit.models.earth.ionosphere.NeQuickModel
 
pathDelay(SpacecraftState, TopocentricFrame, double, double[]) - Method in class org.orekit.models.earth.ionosphere.SsrVtecIonosphericModel
Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(AbsoluteDate, GeodeticPoint, double, double, double, double[]) - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoModel
Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(FieldAbsoluteDate<T>, FieldGeodeticPoint<T>, T, T, double, T[]) - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoModel
Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(FieldTrackingCoordinates<T>, FieldGeodeticPoint<T>, FieldPressureTemperatureHumidity<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.AbstractVienna
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(FieldTrackingCoordinates<T>, FieldGeodeticPoint<T>, FieldPressureTemperatureHumidity<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.AskneNordiusModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(FieldTrackingCoordinates<T>, FieldGeodeticPoint<T>, FieldPressureTemperatureHumidity<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.CanonicalSaastamoinenModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(FieldTrackingCoordinates<T>, FieldGeodeticPoint<T>, FieldPressureTemperatureHumidity<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.ConstantTroposphericModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(FieldTrackingCoordinates<T>, FieldGeodeticPoint<T>, FieldPressureTemperatureHumidity<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.EstimatedModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(FieldTrackingCoordinates<T>, FieldGeodeticPoint<T>, FieldPressureTemperatureHumidity<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.FixedTroposphericDelay
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(FieldTrackingCoordinates<T>, FieldGeodeticPoint<T>, FieldPressureTemperatureHumidity<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.MariniMurray
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(FieldTrackingCoordinates<T>, FieldGeodeticPoint<T>, FieldPressureTemperatureHumidity<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.MendesPavlisModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(FieldTrackingCoordinates<T>, FieldGeodeticPoint<T>, FieldPressureTemperatureHumidity<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.ModifiedHopfieldModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(FieldTrackingCoordinates<T>, FieldGeodeticPoint<T>, FieldPressureTemperatureHumidity<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.ModifiedSaastamoinenModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(FieldTrackingCoordinates<T>, FieldGeodeticPoint<T>, FieldPressureTemperatureHumidity<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(FieldTrackingCoordinates<T>, FieldGeodeticPoint<T>, FieldPressureTemperatureHumidity<T>, T[], FieldAbsoluteDate<T>) - Method in interface org.orekit.models.earth.troposphere.TroposphericModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(FieldTrackingCoordinates<T>, FieldGeodeticPoint<T>, FieldPressureTemperatureHumidity<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.TroposphericModelAdapter
Deprecated.
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(TrackingCoordinates, GeodeticPoint, PressureTemperatureHumidity, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.AbstractVienna
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(TrackingCoordinates, GeodeticPoint, PressureTemperatureHumidity, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.AskneNordiusModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(TrackingCoordinates, GeodeticPoint, PressureTemperatureHumidity, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.CanonicalSaastamoinenModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(TrackingCoordinates, GeodeticPoint, PressureTemperatureHumidity, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.ConstantTroposphericModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(TrackingCoordinates, GeodeticPoint, PressureTemperatureHumidity, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.EstimatedModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(TrackingCoordinates, GeodeticPoint, PressureTemperatureHumidity, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.FixedTroposphericDelay
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(TrackingCoordinates, GeodeticPoint, PressureTemperatureHumidity, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.MariniMurray
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(TrackingCoordinates, GeodeticPoint, PressureTemperatureHumidity, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.MendesPavlisModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(TrackingCoordinates, GeodeticPoint, PressureTemperatureHumidity, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.ModifiedHopfieldModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(TrackingCoordinates, GeodeticPoint, PressureTemperatureHumidity, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.ModifiedSaastamoinenModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(TrackingCoordinates, GeodeticPoint, PressureTemperatureHumidity, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(TrackingCoordinates, GeodeticPoint, PressureTemperatureHumidity, double[], AbsoluteDate) - Method in interface org.orekit.models.earth.troposphere.TroposphericModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(TrackingCoordinates, GeodeticPoint, PressureTemperatureHumidity, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.TroposphericModelAdapter
Deprecated.
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(T, double, T[]) - Method in class org.orekit.models.earth.ionosphere.EstimatedIonosphericModel
Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(T, FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in interface org.orekit.models.earth.troposphere.DiscreteTroposphericModel
Deprecated.
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(T, FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.EstimatedTroposphericModel
Deprecated.
pathDelay(T, FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.FixedTroposphericDelay
Deprecated.
pathDelay(T, FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.MariniMurrayModel
Deprecated.
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(T, FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.MendesPavlisModel
Deprecated.
pathDelay(T, FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.ModifiedSaastamoinenModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(T, FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.SaastamoinenModel
Deprecated.
pathDelay(T, FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
Deprecated.
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(T, FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.ViennaOneModel
Deprecated.
pathDelay(T, FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.ViennaThreeModel
Deprecated.
PATTERN_DATETIME_DELIMITER_REGEX - Static variable in class org.orekit.files.ilrs.CRDHeader
Pattern of delimiter of datetime.
PATTERN_NAN - Static variable in class org.orekit.files.ilrs.CRD
Pattern of "NaN".
PAYLOAD - org.orekit.files.ccsds.ndm.odm.ocm.ObjectType
Payload.
PC - org.orekit.files.ccsds.ndm.cdm.ScreenType
Collision probability type.
PC_MAX - org.orekit.files.ccsds.ndm.cdm.ScreenType
Maximum collision probability type.
PC_N0 - org.orekit.files.ccsds.ndm.tdm.ObservationType
Data: Carrier power to noise spectral density ratio (Pc/No) [dBHz].
PERCENT - Static variable in class org.orekit.utils.units.Unit
Percentage unit.
PERCENTS_TO_UNIT - Static variable in class org.orekit.utils.units.UnitsConverter
Percents to units converter.
PerfectClockModel - Class in org.orekit.time
Clock model for perfect clock with constant zero offset.
PerfectClockModel() - Constructor for class org.orekit.time.PerfectClockModel
 
PERIAPSIS_ALTITUDE - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
The distance of the closest point in the objects orbit above the equatorial radius of the central body.
perige - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
perigee, expressed in KM and ALTITUDE.
perige - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
perigee, expressed in KM and ALTITUDE.
permutation(int, double) - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Perform one symmetric permutation involving rows/columns k0 and k0+1.
pert - org.orekit.files.ccsds.ndm.odm.ocm.OcmDataSubStructureKey
Perturbations parameters section.
PERT - org.orekit.files.ccsds.ndm.odm.ocm.OcmDataSubStructureKey
Perturbations parameters section.
PERT - org.orekit.files.ccsds.ndm.odm.ocm.OcmElements
Perturbations.
Perturbations - Class in org.orekit.files.ccsds.ndm.odm.ocm
Perturbation parameters.
Perturbations(CelestialBodies) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Simple constructor.
PerturbationsKey - Enum in org.orekit.files.ccsds.ndm.odm.ocm
Keys for perturbations data entries.
Phase - Class in org.orekit.estimation.measurements.gnss
Class modeling a phase measurement from a ground station.
Phase(GroundStation, AbsoluteDate, double, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.gnss.Phase
Phase(GroundStation, AbsoluteDate, double, double, double, double, ObservableSatellite, AmbiguityCache) - Constructor for class org.orekit.estimation.measurements.gnss.Phase
Simple constructor.
PHASE_MINUS_CODE - org.orekit.estimation.measurements.gnss.CombinationType
Phase minus code combination.
PhaseAmbiguityModifier - Class in org.orekit.estimation.measurements.modifiers
Deprecated.
as of 12.1 ambiguity is managed directly by raw measurements Phase
PhaseAmbiguityModifier(int, double) - Constructor for class org.orekit.estimation.measurements.modifiers.PhaseAmbiguityModifier
Deprecated.
Constructor.
PhaseBias - Class in org.orekit.gnss.metric.messages.common
Container for phase bias data.
PhaseBias(int, boolean, int, int, double) - Constructor for class org.orekit.gnss.metric.messages.common.PhaseBias
Constructor.
PhaseBuilder - Class in org.orekit.estimation.measurements.gnss
Builder for Phase measurements.
PhaseBuilder(CorrelatedRandomVectorGenerator, GroundStation, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.gnss.PhaseBuilder
PhaseBuilder(CorrelatedRandomVectorGenerator, GroundStation, double, double, double, ObservableSatellite, AmbiguityCache) - Constructor for class org.orekit.estimation.measurements.gnss.PhaseBuilder
Simple constructor.
PhaseCentersGroundReceiverBaseModifier<T extends GroundReceiverMeasurement<T>> - Class in org.orekit.estimation.measurements.modifiers
Ground and on-board antennas offsets effect on range measurements.
PhaseCentersGroundReceiverBaseModifier(FrequencyPattern, FrequencyPattern) - Constructor for class org.orekit.estimation.measurements.modifiers.PhaseCentersGroundReceiverBaseModifier
Simple constructor.
PhaseCentersInterSatellitesBaseModifier<T extends AbstractMeasurement<T>> - Class in org.orekit.estimation.measurements.modifiers
On-board antenna offset effect on inter-satellites phase measurements.
PhaseCentersInterSatellitesBaseModifier(FrequencyPattern, FrequencyPattern) - Constructor for class org.orekit.estimation.measurements.modifiers.PhaseCentersInterSatellitesBaseModifier
Simple constructor.
PhaseCentersOffsetComputer - Class in org.orekit.estimation.measurements.modifiers
Compute phase centers offset on an emitter-receiver link.
PhaseCentersOffsetComputer(FrequencyPattern, FrequencyPattern) - Constructor for class org.orekit.estimation.measurements.modifiers.PhaseCentersOffsetComputer
Simple constructor.
PhaseCentersOneWayGNSSBaseModifier<T extends AbstractMeasurement<T>> - Class in org.orekit.estimation.measurements.modifiers
On-board antenna offset effect on inter-satellites phase measurements.
PhaseCentersOneWayGNSSBaseModifier(FrequencyPattern, FrequencyPattern, AttitudeProvider) - Constructor for class org.orekit.estimation.measurements.modifiers.PhaseCentersOneWayGNSSBaseModifier
Simple constructor.
PhaseCentersPhaseModifier - Class in org.orekit.estimation.measurements.modifiers
Ground and on-board antennas offsets effect on phase measurements.
PhaseCentersPhaseModifier(FrequencyPattern, FrequencyPattern) - Constructor for class org.orekit.estimation.measurements.modifiers.PhaseCentersPhaseModifier
Simple constructor.
PhaseCentersRangeModifier - Class in org.orekit.estimation.measurements.modifiers
Ground and on-board antennas offsets effect on range measurements.
PhaseCentersRangeModifier(FrequencyPattern, FrequencyPattern) - Constructor for class org.orekit.estimation.measurements.modifiers.PhaseCentersRangeModifier
Simple constructor.
PhaseCenterVariationFunction - Interface in org.orekit.gnss.antenna
Model for antennas phase center variations.
PhaseIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical phase measurement with ionospheric delay.
PhaseIonosphericDelayModifier(IonosphericModel, double) - Constructor for class org.orekit.estimation.measurements.modifiers.PhaseIonosphericDelayModifier
Constructor.
PhaseMinusCodeCombination - Class in org.orekit.estimation.measurements.gnss
Phase minus Code combination.
PhaseMinusCodeCycleSlipDetector - Class in org.orekit.estimation.measurements.gnss
Phase minus code cycle slip detectors.
PhaseMinusCodeCycleSlipDetector(double, double, int, int) - Constructor for class org.orekit.estimation.measurements.gnss.PhaseMinusCodeCycleSlipDetector
Polynomial single frequency cycle-slip detector Constructor.
PhaseShiftCorrection - Class in org.orekit.files.rinex.observation
Phase Shift corrections.
PhaseShiftCorrection(SatelliteSystem, ObservationType, double, List<SatInSystem>) - Constructor for class org.orekit.files.rinex.observation.PhaseShiftCorrection
Simple constructor.
PhaseTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical phase measurement with tropospheric delay.
PhaseTroposphericDelayModifier(DiscreteTroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.PhaseTroposphericDelayModifier
Deprecated.
PhaseTroposphericDelayModifier(TroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.PhaseTroposphericDelayModifier
Constructor.
phys - org.orekit.files.ccsds.ndm.adm.acm.AcmDataSubStructureKey
Physical properties section.
phys - org.orekit.files.ccsds.ndm.odm.ocm.OcmDataSubStructureKey
Physical properties section.
PHYS - org.orekit.files.ccsds.ndm.adm.acm.AcmDataSubStructureKey
Physical properties section.
PHYS - org.orekit.files.ccsds.ndm.adm.acm.AcmElements
Physical characteristics.
PHYS - org.orekit.files.ccsds.ndm.odm.ocm.OcmDataSubStructureKey
Physical properties section.
PHYS - org.orekit.files.ccsds.ndm.odm.ocm.OcmElements
Physical characteristics.
PLANNED - org.orekit.files.ccsds.ndm.odm.ocm.ManBasis
Currently planned future maneuver.
PLUS_MOMENTUM - org.orekit.frames.LocalMagneticFieldFrame.LOFBuilderVector
Positive orbital momentum vector.
PLUS_POSITION - org.orekit.frames.LocalMagneticFieldFrame.LOFBuilderVector
Positive position vector.
PLUS_VELOCITY - org.orekit.frames.LocalMagneticFieldFrame.LOFBuilderVector
Positive velocity vector.
PLUTO - org.orekit.bodies.JPLEphemeridesLoader.EphemerisType
Constant for Pluto.
PLUTO - org.orekit.files.ccsds.definitions.CenterName
Pluto body.
PLUTO - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Pluto.
PocMethodFacade - Class in org.orekit.files.ccsds.definitions
Facade in front of several probability of collision methods in CCSDS messages.
PocMethodFacade(String, PocMethodType) - Constructor for class org.orekit.files.ccsds.definitions.PocMethodFacade
Simple constructor.
PocMethodType - Enum in org.orekit.files.ccsds.definitions
Type of probability of collision method used in CCSDS Conjunction Data Messages.
POINCARE - org.orekit.files.ccsds.ndm.odm.ocm.OrbitElementsType
Canonical counterpart of equinoctial 6-element set (λM=M+ω+Ω, gp, hp, Lp, Gp, Hp).
POINT_INSIDE_ELLIPSOID - org.orekit.errors.OrekitMessages
POINT_INSIDE_ELLIPSOID.
pointAt(double) - Method in class org.orekit.bodies.Ellipse
Get a point of the 2D ellipse.
pointAt(T) - Method in class org.orekit.bodies.FieldEllipse
Get a point of the 2D ellipse.
pointAtDistance(double) - Method in class org.orekit.bodies.Loxodrome
Calculate the point at the specified distance from the origin point along the loxodrome.
pointAtDistance(double, double, double) - Method in class org.orekit.frames.TopocentricFrame
Compute the point observed from the station at some specified distance.
PointingPanel - Class in org.orekit.forces
Class representing one panel of a satellite, roughly pointing towards some target.
PointingPanel(Vector3D, ExtendedPVCoordinatesProvider, double, double, double, double, double) - Constructor for class org.orekit.forces.PointingPanel
Simple constructor.
pointOnLimb(FieldVector3D<T>, FieldVector3D<T>) - Method in class org.orekit.bodies.Ellipsoid
Find a point on ellipsoid limb, as seen by an external observer.
pointOnLimb(Vector3D, Vector3D) - Method in class org.orekit.bodies.Ellipsoid
Find a point on ellipsoid limb, as seen by an external observer.
PoissonSeries - Class in org.orekit.data
Class representing a Poisson series for nutation or ephemeris computations.
PoissonSeries(PolynomialNutation, Map<Long, SeriesTerm>) - Constructor for class org.orekit.data.PoissonSeries
Build a Poisson series from an IERS table file.
PoissonSeries.CompiledSeries - Interface in org.orekit.data
This interface represents a fast evaluator for Poisson series.
PoissonSeriesParser - Class in org.orekit.data
Parser for Poisson series files.
PoissonSeriesParser(int) - Constructor for class org.orekit.data.PoissonSeriesParser
Build a parser for a Poisson series from an IERS table file.
POLAR_TRAJECTORY - org.orekit.errors.OrekitMessages
POLAR_TRAJECTORY.
PoleCorrection - Class in org.orekit.frames
Simple container class for pole correction parameters.
PoleCorrection(double, double) - Constructor for class org.orekit.frames.PoleCorrection
Simple constructor.
PolygonalFieldOfView - Class in org.orekit.geometry.fov
Class representing a spacecraft sensor Field Of View with polygonal shape.
PolygonalFieldOfView(Vector3D, PolygonalFieldOfView.DefiningConeType, Vector3D, double, int, double) - Constructor for class org.orekit.geometry.fov.PolygonalFieldOfView
Build Field Of View with a regular polygon shape.
PolygonalFieldOfView(SphericalPolygonsSet, double) - Constructor for class org.orekit.geometry.fov.PolygonalFieldOfView
Build a new instance.
PolygonalFieldOfView.DefiningConeType - Enum in org.orekit.geometry.fov
Enumerate for cone/polygon relative position.
PolynomialAccelerationModel - Class in org.orekit.forces.empirical
Polynomial acceleration model.
PolynomialAccelerationModel(String, AbsoluteDate, int) - Constructor for class org.orekit.forces.empirical.PolynomialAccelerationModel
Simple constructor.
PolynomialFunctionMatrix - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen
A quadratic matrix of PolynomialFunction.
PolynomialNutation - Class in org.orekit.data
Polynomial nutation function.
PolynomialNutation(double...) - Constructor for class org.orekit.data.PolynomialNutation
Build a polynomial from its coefficients.
PolynomialParser - Class in org.orekit.data
Parser for polynomials in IERS tables.
PolynomialParser(char, PolynomialParser.Unit) - Constructor for class org.orekit.data.PolynomialParser
Simple constructor.
PolynomialParser.Unit - Enum in org.orekit.data
Unit for the coefficients.
PolynomialThrustSegment - Class in org.orekit.forces.maneuvers.propulsion
One polynomial segment of a thrust profile.
PolynomialThrustSegment(AbsoluteDate, PolynomialFunction, PolynomialFunction, PolynomialFunction) - Constructor for class org.orekit.forces.maneuvers.propulsion.PolynomialThrustSegment
Simple constructor.
POS_VEL_BASE_ACCURACY - Static variable in class org.orekit.files.sp3.SP3Utils
Base for general position/velocity accuracy.
POS_X - Static variable in enum org.orekit.orbits.OrbitType
Name for position along X.
POS_Y - Static variable in enum org.orekit.orbits.OrbitType
Name for position along Y.
POS_Z - Static variable in enum org.orekit.orbits.OrbitType
Name for position along Z.
Position - Class in org.orekit.estimation.measurements
Class modeling a position only measurement.
Position(AbsoluteDate, Vector3D, double[][], double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.Position
Constructor with full covariance matrix and all inputs.
Position(AbsoluteDate, Vector3D, double[], double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.Position
Constructor with one vector for the standard deviation.
Position(AbsoluteDate, Vector3D, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.Position
Constructor with one double for the standard deviation.
POSITION_ACCURACY_UNIT - Static variable in class org.orekit.files.sp3.SP3Utils
Position accuracy unit.
POSITION_UNIT - Static variable in class org.orekit.files.sp3.SP3Utils
Position unit.
PositionAngleBased - Interface in org.orekit.orbits
This interface represent orbit-like trajectory whose definition is based on a so-called position angle.
PositionAngleDetector - Class in org.orekit.propagation.events
Detector for in-orbit position angle.
PositionAngleDetector(double, double, OrbitType, PositionAngleType, double) - Constructor for class org.orekit.propagation.events.PositionAngleDetector
Build a detector.
PositionAngleDetector(OrbitType, PositionAngleType, double) - Constructor for class org.orekit.propagation.events.PositionAngleDetector
Build a new detector.
PositionAngleDetector(AdaptableInterval, double, int, EventHandler, OrbitType, PositionAngleType, double) - Constructor for class org.orekit.propagation.events.PositionAngleDetector
Protected constructor with full parameters.
PositionAngleType - Enum in org.orekit.orbits
Enumerate for true, eccentric and mean position angles.
PositionBuilder - Class in org.orekit.estimation.measurements.generation
Builder for Position measurements.
PositionBuilder(CorrelatedRandomVectorGenerator, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.PositionBuilder
Simple constructor.
positionShiftedBy(double) - Method in class org.orekit.utils.PVCoordinates
Get a time-shifted position.
positionShiftedBy(T) - Method in class org.orekit.utils.FieldPVCoordinates
Get a time-shifted position.
POSITIVE_FLOW_RATE - org.orekit.errors.OrekitMessages
POSITIVE_FLOW_RATE.
PostSeismicDeformation - Class in org.orekit.models.earth.displacement
Modeling of displacement of one reference point due to post-seismic effects.
PostSeismicDeformation(GeodeticPoint, TimeSpanMap<List<PsdCorrection>>) - Constructor for class org.orekit.models.earth.displacement.PostSeismicDeformation
Simple constructor.
PotentialCoefficientsReader - Class in org.orekit.forces.gravity.potential
This abstract class represents a Gravitational Potential Coefficients file reader.
PotentialCoefficientsReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Simple constructor.
PotentialCoefficientsReader(String, boolean, TimeScale) - Constructor for class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Simple constructor.
power(String, Fraction) - Method in class org.orekit.utils.units.Unit
Create power of unit.
PowerTerm - Class in org.orekit.utils.units
A container for a term with associated power.
PQW_INERTIAL - org.orekit.files.ccsds.definitions.OrbitRelativeFrame
Perifocal coordinate system (X towards periapsis, Z towards momentum).
PR_N0 - org.orekit.files.ccsds.ndm.tdm.ObservationType
Data: Ranging power to noise spectral density ratio (Pr/No) [dBHz].
PREAMBLE_VALUE - Static variable in class org.orekit.gnss.rflink.gps.SubFrame
TLM preamble.
Predefined - Enum in org.orekit.frames
Predefined frames provided by Frames.
PredefinedTarget - Enum in org.orekit.attitudes
Predefined targets for AlignedAndConstrained.
PredictedEOPHistory - Class in org.orekit.frames
This class extends an EOPHistory for some weeks using fitting.
PredictedEOPHistory(EOPHistory, double, EOPFitter) - Constructor for class org.orekit.frames.PredictedEOPHistory
Simple constructor.
predictPositionVelocity(double, Vector3D, Vector3D, double) - Static method in class org.orekit.orbits.KeplerianMotionCartesianUtility
Method to propagate position and velocity according to Keplerian dynamics.
predictPositionVelocity(T, FieldVector3D<T>, FieldVector3D<T>, T) - Static method in class org.orekit.orbits.KeplerianMotionCartesianUtility
Method to propagate position and velocity according to Keplerian dynamics.
PREFIX - Static variable in class org.orekit.estimation.measurements.gnss.AmbiguityDriver
Prefix for parameter drivers names.
PREFIX - Static variable in class org.orekit.forces.maneuvers.jacobians.MassDepletionDelay
Prefix for state name.
prepareComments(List<RinexComment>) - Method in class org.orekit.files.rinex.observation.RinexObservationWriter
Prepare comments to be emitted at specified lines.
prepareData() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmParser
Prepare data for parsing.
prepareData() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser
Prepare data for parsing.
prepareData() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser
Prepare data for parsing.
prepareData() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmParser
Prepare data for parsing.
prepareData() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser
Prepare data for parsing.
prepareData() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser
Prepare data for parsing.
prepareData() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser
Prepare data for parsing.
prepareData() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser
Prepare data for parsing.
prepareData() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser
Prepare data for parsing.
prepareData() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser
Prepare data for parsing.
prepareHeader() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmParser
Prepare header for parsing.
prepareHeader() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser
Prepare header for parsing.
prepareHeader() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser
Prepare header for parsing.
prepareHeader() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmParser
Prepare header for parsing.
prepareHeader() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser
Prepare header for parsing.
prepareHeader() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser
Prepare header for parsing.
prepareHeader() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser
Prepare header for parsing.
prepareHeader() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser
Prepare header for parsing.
prepareHeader() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser
Prepare header for parsing.
prepareHeader() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser
Prepare header for parsing.
prepareMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmParser
Prepare metadata for parsing.
prepareMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser
Prepare metadata for parsing.
prepareMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser
Prepare metadata for parsing.
prepareMetadata() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmParser
Prepare metadata for parsing.
prepareMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser
Prepare metadata for parsing.
prepareMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser
Prepare metadata for parsing.
prepareMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser
Prepare metadata for parsing.
prepareMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser
Prepare metadata for parsing.
prepareMetadata() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser
Prepare metadata for parsing.
prepareMetadata() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser
Prepare metadata for parsing.
PRESSURE - org.orekit.files.ccsds.ndm.tdm.ObservationType
Data: Pressure [hPa].
PressureTemperature - Class in org.orekit.models.earth.weather
Container for pressure and temperature.
PressureTemperature(double, double, double) - Constructor for class org.orekit.models.earth.weather.PressureTemperature
Simple constructor.
PressureTemperatureHumidity - Class in org.orekit.models.earth.weather
Container for pressure, temperature, and humidity.
PressureTemperatureHumidity(double, double, double, double, double, double) - Constructor for class org.orekit.models.earth.weather.PressureTemperatureHumidity
Simple constructor.
PressureTemperatureHumidityProvider - Interface in org.orekit.models.earth.weather
Interface for providing weather parameters.
previous() - Method in class org.orekit.utils.TimeSpanMap.Span
Get the previous time span.
previous() - Method in class org.orekit.utils.TimeSpanMap.Transition
Get the previous transition.
PREVIOUS_MESSAGE_EPOCH - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
UTC epoch of the previous CDM issued for the event identified by CONJUNCTION_ID.
PREVIOUS_MESSAGE_EPOCH - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Creation date of previous message from a given originator.
PREVIOUS_MESSAGE_ID - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
ID of previous CDM issued for event identified by CONJUNCTION_ID.
PREVIOUS_MESSAGE_ID - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Unique ID identifying previous message from a given originator.
PRM_MSG_LINK - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Unique identifier of Pointing Request Message linked to this Orbit Data Message.
PRN_NB_OF_OBS - org.orekit.files.rinex.section.RinexLabels
PRN and number of observations .
ProbabilityOfCollision - Class in org.orekit.ssa.metrics
Container for values relative to the probability of collision : Value of the probability of collision. Name of the method with which it was computed. Upper and lower limit of the value if the method provides them (such as Laas2015 for example). Flag defining if the probability was maximized in any way (such as Alfriend1999Max for example).
ProbabilityOfCollision(double, double, double, String, boolean) - Constructor for class org.orekit.ssa.metrics.ProbabilityOfCollision
Constructor.
ProbabilityOfCollision(double, String) - Constructor for class org.orekit.ssa.metrics.ProbabilityOfCollision
Constructor with default values of 0 for the upper/lower limits and default false flag for maximum probability.
ProbabilityOfCollision(double, String, boolean) - Constructor for class org.orekit.ssa.metrics.ProbabilityOfCollision
Constructor with default values of 0 for the upper and lower limits.
process(String, ContextBinding, OrbitManeuver, int, String) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
Process one field.
process(ParseToken) - Method in interface org.orekit.files.ccsds.utils.lexical.MessageParser
Process a parse token.
process(ParseToken) - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser
Process a parse token.
process(ParseToken, AcmParser) - Method in enum org.orekit.files.ccsds.ndm.adm.acm.AcmDataSubStructureKey
Process one token.
process(ParseToken, AcmParser, ContextBinding, AttitudeDetermination) - Method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationKey
Process an token.
process(ParseToken, CdmParser) - Method in enum org.orekit.files.ccsds.ndm.cdm.XmlSubStructureKey
Process one token.
process(ParseToken, OcmParser) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.OcmDataSubStructureKey
Process one token.
process(ParseToken, ContextBinding, AcmMetadata) - Method in enum org.orekit.files.ccsds.ndm.adm.acm.AcmMetadataKey
Process an token.
process(ParseToken, ContextBinding, AttitudeCovarianceHistoryMetadata) - Method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadataKey
Process an token.
process(ParseToken, ContextBinding, AttitudeDeterminationSensor) - Method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationSensorKey
Process an token.
process(ParseToken, ContextBinding, AttitudeManeuver) - Method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuverKey
Process an token.
process(ParseToken, ContextBinding, AttitudePhysicalProperties) - Method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalPropertiesKey
Process an token.
process(ParseToken, ContextBinding, AttitudeStateHistoryMetadata) - Method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadataKey
Process an token.
process(ParseToken, ContextBinding, AdmMetadata) - Method in enum org.orekit.files.ccsds.ndm.adm.AdmCommonMetadataKey
Process one token.
process(ParseToken, ContextBinding, AdmMetadata) - Method in enum org.orekit.files.ccsds.ndm.adm.AdmMetadataKey
Process one token.
process(ParseToken, ContextBinding, AemMetadata) - Method in enum org.orekit.files.ccsds.ndm.adm.aem.AemMetadataKey
Process an token.
process(ParseToken, ContextBinding, AttitudeEntry) - Method in enum org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Process an token.
process(ParseToken, ContextBinding, AngularVelocity) - Method in enum org.orekit.files.ccsds.ndm.adm.apm.AngularVelocityKey
Process one token.
process(ParseToken, ContextBinding, ApmQuaternion, ParseToken.DateConsumer) - Method in enum org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternionKey
Process one token.
process(ParseToken, ContextBinding, Euler) - Method in enum org.orekit.files.ccsds.ndm.adm.apm.EulerKey
Process one token.
process(ParseToken, ContextBinding, Inertia) - Method in enum org.orekit.files.ccsds.ndm.adm.apm.InertiaKey
Process an token.
process(ParseToken, ContextBinding, Maneuver) - Method in enum org.orekit.files.ccsds.ndm.adm.apm.ManeuverKey
Process one token.
process(ParseToken, ContextBinding, SpinStabilized) - Method in enum org.orekit.files.ccsds.ndm.adm.apm.SpinStabilizedKey
Process one token.
process(ParseToken, ContextBinding, AdditionalCovarianceMetadata) - Method in enum org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadataKey
Process one token.
process(ParseToken, ContextBinding, AdditionalParameters) - Method in enum org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
Process one token.
process(ParseToken, ContextBinding, CdmHeader) - Method in enum org.orekit.files.ccsds.ndm.cdm.CdmHeaderKey
Process an token.
process(ParseToken, ContextBinding, CdmMetadata) - Method in enum org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey
Process an token.
process(ParseToken, ContextBinding, CdmRelativeMetadata) - Method in enum org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
Process one token.
process(ParseToken, ContextBinding, ODParameters) - Method in enum org.orekit.files.ccsds.ndm.cdm.ODParametersKey
Process one token.
process(ParseToken, ContextBinding, RTNCovariance) - Method in enum org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Process one token.
process(ParseToken, ContextBinding, SigmaEigenvectorsCovariance) - Method in enum org.orekit.files.ccsds.ndm.cdm.SigmaEigenvectorsCovarianceKey
Process one token.
process(ParseToken, ContextBinding, StateVector) - Method in enum org.orekit.files.ccsds.ndm.cdm.StateVectorKey
Process one token.
process(ParseToken, ContextBinding, XYZCovariance) - Method in enum org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Process one token.
process(ParseToken, ContextBinding, CartesianCovariance) - Method in enum org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey
Process one token.
process(ParseToken, ContextBinding, KeplerianElements) - Method in enum org.orekit.files.ccsds.ndm.odm.KeplerianElementsKey
Process one token.
process(ParseToken, ContextBinding, OcmMetadata) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Process an token.
process(ParseToken, ContextBinding, OrbitCovarianceHistoryMetadata) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadataKey
Process an token.
process(ParseToken, ContextBinding, OrbitDetermination) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey
Process an token.
process(ParseToken, ContextBinding, OrbitManeuverHistoryMetadata) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey
Process an token.
process(ParseToken, ContextBinding, OrbitPhysicalProperties) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Process an token.
process(ParseToken, ContextBinding, Perturbations) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey
Process an token.
process(ParseToken, ContextBinding, TrajectoryStateHistoryMetadata) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadataKey
Process an token.
process(ParseToken, ContextBinding, OdmCommonMetadata) - Method in enum org.orekit.files.ccsds.ndm.odm.CommonMetadataKey
Process one token.
process(ParseToken, ContextBinding, OdmMetadata) - Method in enum org.orekit.files.ccsds.ndm.odm.OdmMetadataKey
Process one token.
process(ParseToken, ContextBinding, OemMetadata) - Method in enum org.orekit.files.ccsds.ndm.odm.oem.OemMetadataKey
Process an token.
process(ParseToken, ContextBinding, OmmMetadata) - Method in enum org.orekit.files.ccsds.ndm.odm.omm.OmmMetadataKey
Process one token.
process(ParseToken, ContextBinding, OmmTle) - Method in enum org.orekit.files.ccsds.ndm.odm.omm.OmmTleKey
Process one token.
process(ParseToken, ContextBinding, Maneuver) - Method in enum org.orekit.files.ccsds.ndm.odm.opm.ManeuverKey
Process one token.
process(ParseToken, ContextBinding, SpacecraftParameters) - Method in enum org.orekit.files.ccsds.ndm.odm.SpacecraftParametersKey
Process one token.
process(ParseToken, ContextBinding, StateVector) - Method in enum org.orekit.files.ccsds.ndm.odm.StateVectorKey
Process one token.
process(ParseToken, ContextBinding, ObservationsBlock) - Method in enum org.orekit.files.ccsds.ndm.tdm.TdmDataKey
Process one token.
process(ParseToken, ContextBinding, RangeUnitsConverter, TdmMetadata, ObservationsBlock) - Method in enum org.orekit.files.ccsds.ndm.tdm.ObservationType
Process an observation line.
process(ParseToken, ContextBinding, TdmMetadata) - Method in enum org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Process an token.
process(ParseToken, ContextBinding, Header) - Method in enum org.orekit.files.ccsds.section.HeaderKey
Process an token.
process(ParseToken, ContextBinding, Metadata) - Method in enum org.orekit.files.ccsds.section.MetadataKey
Process an token.
process(ParseToken, AbstractConstituentParser<?, ?, ?>) - Method in enum org.orekit.files.ccsds.section.KvnStructureKey
Process an token.
process(ParseToken, AbstractConstituentParser<?, ?, ?>) - Method in enum org.orekit.files.ccsds.section.XmlStructureKey
Process an token.
processAsBoolean(ParseToken.BooleanConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as a boolean.
processAsCenter(ParseToken.CenterConsumer, CelestialBodies) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as a body center.
processAsCenterList(ParseToken.CenterListConsumer, CelestialBodies) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as a body center list.
processAsDate(ParseToken.DateConsumer, ContextBinding) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as a date.
processAsDouble(Unit, ParsedUnitsBehavior, ParseToken.DoubleConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as a double.
processAsDoubleArray(Unit, ParsedUnitsBehavior, ParseToken.DoubleArrayConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as an array of doubles.
processAsDoublyIndexedDouble(int, int, Unit, ParsedUnitsBehavior, ParseToken.DoublyIndexedDoubleConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as a doubly-indexed double.
processAsEnum(Class<T>, ParseToken.EnumConsumer<T>) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as an enum.
processAsEnumsList(Class<T>, ParseToken.EnumListConsumer<T>) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as a list of enums.
processAsFrame(ParseToken.FrameConsumer, ContextBinding, boolean, boolean, boolean) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as a frame.
processAsFreeTextList(ParseToken.StringListConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as a list of free-text strings.
processAsFreeTextString(ParseToken.StringConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as free text string.
processAsIndexedDouble(int, Unit, ParsedUnitsBehavior, ParseToken.IndexedDoubleConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as an indexed double.
processAsIndexedDoubleArray(int, Unit, ParsedUnitsBehavior, ParseToken.IndexedDoubleArrayConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as an indexed double array.
processAsIndexedInteger(int, ParseToken.IndexedIntConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as an indexed integer.
processAsIndexedNormalizedString(int, ParseToken.IndexedStringConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as an indexed normalized string.
processAsIndexedUppercaseString(int, ParseToken.IndexedStringConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as an indexed normalized uppercase string.
processAsInteger(ParseToken.IntConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as an integer.
processAsIntegerArray(ParseToken.IntegerArrayConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as an array of integers.
processAsIntegerArrayNoSpace(ParseToken.IntegerArrayConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as an array of integers.
processAsLabeledDouble(char, Unit, ParsedUnitsBehavior, ParseToken.LabeledDoubleConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as a labeled double.
processAsManeuvrableEnum(ParseToken.ManeuvrableConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content of the Maneuvrable enum.
processAsNormalizedCharacter(ParseToken.CharConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as a normalized character.
processAsNormalizedList(ParseToken.StringListConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as a list of normalized strings.
processAsNormalizedString(ParseToken.StringConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as a normalized string.
processAsRotationOrder(ParseToken.RotationOrderConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as a rotation sequence.
processAsTimeSystem(ParseToken.TimeSystemConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as a time system.
processAsUnitList(ParseToken.UnitListConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as a list of units.
processAsUppercaseList(ParseToken.StringListConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as a list of normalized uppercase strings.
processAsUppercaseString(ParseToken.StringConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as a normalized uppercase string.
processAsVector(Unit, ParsedUnitsBehavior, ParseToken.VectorConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as a vector.
PROCESSED - org.orekit.estimation.measurements.EstimatedMeasurementBase.Status
Status for processed measurements.
ProcessingState - Interface in org.orekit.files.ccsds.utils.parsing
Interface for processing parsing tokens for CCSDS NDM files.
processMeasurements(Iterable<ObservedMeasurement<?>>) - Method in class org.orekit.estimation.sequential.KalmanEstimator
Process several measurements.
processMeasurements(Iterable<ObservedMeasurement<?>>) - Method in class org.orekit.estimation.sequential.UnscentedKalmanEstimator
Process several measurements.
processMeasurements(List<ObservedMeasurement<?>>) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimator
Process a single measurement.
processMeasurements(List<ObservedMeasurement<?>>) - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanEstimator
Process a single measurement.
processMeasurements(List<ObservedMeasurement<?>>, ExtendedKalmanFilter<MeasurementDecorator>) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Process a single measurement.
processMeasurements(List<ObservedMeasurement<?>>, UnscentedKalmanFilter<MeasurementDecorator>) - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel
Process measurements.
processToken(ParseToken) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmHeaderProcessingState
Process one token.
processToken(ParseToken) - Method in class org.orekit.files.ccsds.section.HeaderProcessingState
Process one token.
processToken(ParseToken) - Method in class org.orekit.files.ccsds.section.KvnStructureProcessingState
Process one token.
processToken(ParseToken) - Method in class org.orekit.files.ccsds.section.XmlStructureProcessingState
Process one token.
processToken(ParseToken) - Method in class org.orekit.files.ccsds.utils.parsing.ErrorState
Process one token.
processToken(ParseToken) - Method in interface org.orekit.files.ccsds.utils.parsing.ProcessingState
Process one token.
ProfileThrustPropulsionModel - Class in org.orekit.forces.maneuvers.propulsion
Thrust propulsion model based on segmented profile.
ProfileThrustPropulsionModel(TimeSpanMap<PolynomialThrustSegment>, double, Control3DVectorCostType, String) - Constructor for class org.orekit.forces.maneuvers.propulsion.ProfileThrustPropulsionModel
Generic constructor.
PROGRAM - org.orekit.files.rinex.section.RinexLabels
Generating program and emiting agency.
projectOntoCollisionPlane(FieldVector3D<T>) - Method in interface org.orekit.frames.encounter.EncounterLOF
Project given vector expressed in this encounter local orbital frame onto the collision plane.
projectOntoCollisionPlane(Vector3D) - Method in interface org.orekit.frames.encounter.EncounterLOF
Project given vector expressed in this encounter local orbital frame onto the collision plane.
projectOntoCollisionPlane(FieldMatrix<T>) - Method in interface org.orekit.frames.encounter.EncounterLOF
Project given matrix expressed in this encounter local orbital frame onto the collision plane defined by this same encounter local orbital frame.
projectOntoCollisionPlane(RealMatrix) - Method in interface org.orekit.frames.encounter.EncounterLOF
Project given matrix expressed in this encounter local orbital frame onto the collision plane.
projectToBoundary(Vector3D) - Method in class org.orekit.geometry.fov.CircularFieldOfView
Find the direction on Field Of View Boundary closest to a line of sight.
projectToBoundary(Vector3D) - Method in class org.orekit.geometry.fov.EllipticalFieldOfView
Find the direction on Field Of View Boundary closest to a line of sight.
projectToBoundary(Vector3D) - Method in interface org.orekit.geometry.fov.FieldOfView
Find the direction on Field Of View Boundary closest to a line of sight.
projectToBoundary(Vector3D) - Method in class org.orekit.geometry.fov.PolygonalFieldOfView
Find the direction on Field Of View Boundary closest to a line of sight.
projectToEllipse(FieldVector2D<T>) - Method in class org.orekit.bodies.FieldEllipse
Find the closest ellipse point.
projectToEllipse(Vector2D) - Method in class org.orekit.bodies.Ellipse
Find the closest ellipse point.
projectToEllipse(TimeStampedFieldPVCoordinates<T>) - Method in class org.orekit.bodies.FieldEllipse
Project position-velocity-acceleration on an ellipse.
projectToEllipse(TimeStampedPVCoordinates) - Method in class org.orekit.bodies.Ellipse
Project position-velocity-acceleration on an ellipse.
projectToGround(Vector3D, AbsoluteDate, Frame) - Method in interface org.orekit.bodies.BodyShape
Project a point to the ground.
projectToGround(Vector3D, AbsoluteDate, Frame) - Method in class org.orekit.bodies.OneAxisEllipsoid
Project a point to the ground.
projectToGround(Vector3D, AbsoluteDate, Frame) - Method in class org.orekit.models.earth.Geoid
 
projectToGround(TimeStampedPVCoordinates, Frame) - Method in interface org.orekit.bodies.BodyShape
Project a moving point to the ground.
projectToGround(TimeStampedPVCoordinates, Frame) - Method in class org.orekit.bodies.OneAxisEllipsoid
Project a moving point to the ground.
projectToGround(TimeStampedPVCoordinates, Frame) - Method in class org.orekit.models.earth.Geoid
 
propagate(AbsoluteDate) - Method in class org.orekit.propagation.AbstractPropagator
Propagate towards a target date.
propagate(AbsoluteDate) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Propagate towards a target date.
propagate(AbsoluteDate) - Method in class org.orekit.propagation.numerical.GLONASSNumericalPropagator
Propagate towards a target date.
propagate(AbsoluteDate) - Method in interface org.orekit.propagation.Propagator
Propagate towards a target date.
propagate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Propagate from a start date towards a target date.
propagate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Propagate from a start date towards a target date.
propagate(AbsoluteDate, AbsoluteDate) - Method in interface org.orekit.propagation.Propagator
Propagate from a start date towards a target date.
propagate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.propagation.PropagatorsParallelizer
Propagate from a start date towards a target date.
propagate(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator
Propagate towards a target date.
propagate(FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.FieldPropagator
Propagate towards a target date.
propagate(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Propagate towards a target date.
propagate(FieldAbsoluteDate<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Propagate from a start date towards a target date.
propagate(FieldAbsoluteDate<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.FieldPropagator
Propagate from a start date towards a target date.
propagate(FieldAbsoluteDate<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Propagate from a start date towards a target date.
PROPAGATE - org.orekit.files.ccsds.ndm.odm.oem.InterpolationMethod
Propagation.
propagateInEcef(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator
Gets the PVCoordinates of the GLONASS SV in ECEF frame.
propagateInEcef(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator
Gets the PVCoordinates of the GNSS SV in ECEF frame.
propagateInEcef(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator
Gets the PVCoordinates of the GNSS SV in ECEF frame.
propagateInEcef(AbsoluteDate) - Method in class org.orekit.propagation.analytical.intelsat.IntelsatElevenElementsPropagator
Converts the Intelsat's 11 elements into Position/Velocity coordinates in ECEF.
propagateInEcef(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElementsPropagator
Converts the Intelsat's 11 elements into Position/Velocity coordinates in ECEF.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.files.general.EphemerisSegmentPropagator
 
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AdapterPropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
 
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.Ephemeris
Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.intelsat.IntelsatElevenElementsPropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.KeplerianPropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Extrapolate an orbit up to a specific target date.
propagateOrbit(FieldAbsoluteDate<T>, T[]) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(FieldAbsoluteDate<T>, T[]) - Method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(FieldAbsoluteDate<T>, T[]) - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(FieldAbsoluteDate<T>, T[]) - Method in class org.orekit.propagation.analytical.FieldKeplerianPropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(FieldAbsoluteDate<T>, T[]) - Method in class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElementsPropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(FieldAbsoluteDate<T>, T[]) - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(FieldAbsoluteDate<T>, T[]) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
Extrapolate an orbit up to a specific target date.
PropagationType - Enum in org.orekit.propagation
Enumerate to define the propagation type used by the propagator.
Propagator - Interface in org.orekit.propagation
This interface provides a way to propagate an orbit at any time.
PROPAGATOR - org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadataKey
Orbit propagator used to generate this trajectory.
PROPAGATOR_BUILDER_NOT_CLONEABLE - org.orekit.errors.OrekitMessages
PROPAGATOR_BUILDER_NOT_CLONEABLE.
PropagatorBuilder - Interface in org.orekit.propagation.conversion
This interface is the top-level abstraction to build propagators for conversion.
PropagatorConverter - Interface in org.orekit.propagation.conversion
This interface is the top-level abstraction for propagators conversions.
PropagatorsParallelizer - Class in org.orekit.propagation
This class provides a way to propagate simultaneously several orbits.
PropagatorsParallelizer(List<Propagator>, double, MultiSatFixedStepHandler) - Constructor for class org.orekit.propagation.PropagatorsParallelizer
Simple constructor.
PropagatorsParallelizer(List<Propagator>, MultiSatStepHandler) - Constructor for class org.orekit.propagation.PropagatorsParallelizer
Simple constructor.
properToNatural(double[], GroundStation, AbsoluteDate, Frame) - Static method in class org.orekit.estimation.measurements.modifiers.AberrationModifier
Proper to natural correction for aberration of light.
properToNatural(double[], GroundStation, AbsoluteDate, Frame, DataContext) - Static method in class org.orekit.estimation.measurements.modifiers.AberrationModifier
Proper to natural correction for aberration of light.
PropulsionModel - Interface in org.orekit.forces.maneuvers.propulsion
Generic interface for a propulsion model used in a Maneuver.
PsdCorrection - Class in org.orekit.models.earth.displacement
Model for post-seismic deformation corrections.
PsdCorrection(PsdCorrection.Axis, PsdCorrection.TimeEvolution, AbsoluteDate, double, double) - Constructor for class org.orekit.models.earth.displacement.PsdCorrection
Simple constructor.
PsdCorrection.Axis - Enum in org.orekit.models.earth.displacement
Enumerate for correction axis.
PsdCorrection.TimeEvolution - Enum in org.orekit.models.earth.displacement
Enumerate for correction time evolution.
PSEUDO_RANGE - org.orekit.gnss.MeasurementType
Pseudo-range measurement.
put(String, double[]) - Method in class org.orekit.utils.DoubleArrayDictionary
Add an entry.
put(String, double[]) - Method in class org.orekit.utils.FieldArrayDictionary
Add an entry.
put(String, T[]) - Method in class org.orekit.utils.FieldArrayDictionary
Add an entry.
putAll(Map<String, double[]>) - Method in class org.orekit.utils.DoubleArrayDictionary
Put all the entries from the map in the dictionary.
putAll(Map<String, T[]>) - Method in class org.orekit.utils.FieldArrayDictionary
Put all the entries from the map in the dictionary.
putAll(DoubleArrayDictionary) - Method in class org.orekit.utils.DoubleArrayDictionary
Put all the entries from another dictionary.
putAll(FieldArrayDictionary<T>) - Method in class org.orekit.utils.FieldArrayDictionary
Put all the entries from another dictionary.
PV - Class in org.orekit.estimation.measurements
Class modeling a position-velocity measurement.
PV(AbsoluteDate, Vector3D, Vector3D, double[][], double[][], double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.PV
Constructor with 2 smaller covariance matrices.
PV(AbsoluteDate, Vector3D, Vector3D, double[][], double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.PV
Constructor with full covariance matrix and all inputs.
PV(AbsoluteDate, Vector3D, Vector3D, double[], double[], double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.PV
Constructor with two vectors for the standard deviations.
PV(AbsoluteDate, Vector3D, Vector3D, double[], double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.PV
Constructor with one vector for the standard deviations.
PV(AbsoluteDate, Vector3D, Vector3D, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.PV
Constructor with two double for the standard deviations.
PVBuilder - Class in org.orekit.estimation.measurements.generation
Builder for PV measurements.
PVBuilder(CorrelatedRandomVectorGenerator, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.PVBuilder
Simple constructor.
PVCoordinates - Class in org.orekit.utils
Simple container for Position/Velocity/Acceleration triplets.
PVCoordinates() - Constructor for class org.orekit.utils.PVCoordinates
Simple constructor.
PVCoordinates(double, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates
Multiplicative constructor.
PVCoordinates(double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates
Linear constructor.
PVCoordinates(double, PVCoordinates, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates
Linear constructor.
PVCoordinates(double, PVCoordinates, double, PVCoordinates, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates
Linear constructor.
PVCoordinates(FieldVector3D<U>) - Constructor for class org.orekit.utils.PVCoordinates
Builds a PVCoordinates triplet from a FieldVector3D<Derivative>.
PVCoordinates(Vector3D) - Constructor for class org.orekit.utils.PVCoordinates
Builds PV coordinates with the givne position, zero velocity, and zero acceleration.
PVCoordinates(Vector3D, Vector3D) - Constructor for class org.orekit.utils.PVCoordinates
Builds a PVCoordinates triplet with zero acceleration.
PVCoordinates(Vector3D, Vector3D, Vector3D) - Constructor for class org.orekit.utils.PVCoordinates
Builds a PVCoordinates triplet.
PVCoordinates(PVCoordinates, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates
Subtractive constructor.
PVCoordinatesProvider - Interface in org.orekit.utils
Interface for PV coordinates providers.
PZ90_11 - org.orekit.frames.Predefined
PZ-90.11 frame.

Q

Q - org.orekit.gnss.SignalCode
GPS Q / GLONASS Q / Galileo Q / SBAS Q / QZSS Q / Beidou Q codes.
Q_DIR - org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternionKey
Rotation direction entry.
Q_DOT - org.orekit.files.ccsds.ndm.adm.acm.RateElementsType
Quaternion derivatives.
Q_FRAME_A - org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternionKey
First reference frame entry (ADM V1 only).
Q_FRAME_B - org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternionKey
Second reference frame entry (ADM V1 only).
Q_METHOD - org.orekit.files.ccsds.definitions.AdMethodType
Q-method.
Q1 - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Quaternion first vectorial component.
Q1 - org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternionKey
First component of the vector part of the quaternion entry.
Q1 - Static variable in class org.orekit.models.earth.displacement.Tide
Q₁ tide.
Q1_DOT - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Quaternion first vectorial component.
Q1_DOT - org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternionKey
First component of the vector part of the quaternion derivative entry.
Q2 - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Quaternion second vectorial component.
Q2 - org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternionKey
Second component of the vector part of the quaternion entry.
Q2_DOT - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Quaternion second vectorial component.
Q2_DOT - org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternionKey
Second component of the vector part of the quaternion derivative entry.
Q22 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
Q22.
Q3 - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Quaternion third vectorial component.
Q3 - org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternionKey
Third component of the vector part of the quaternion entry.
Q3_DOT - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Quaternion third vectorial component.
Q3_DOT - org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternionKey
Third component of the vector part of the quaternion derivative entry.
Q31 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
Q31.
Q33 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
Q33.
QC - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Quaternion scalar component.
QC - org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternionKey
Scalar part of the quaternion entry.
QC_DOT - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Quaternion scalar component.
QC_DOT - org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternionKey
Scalar part of the quaternion derivative entry.
QOMS2T - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
QOMS2T.
QSW - org.orekit.files.ccsds.definitions.OrbitRelativeFrame
Another name for Radial, Transverse (along-track) and Normal (X towards zenith, Z towards momentum).
QSW - org.orekit.frames.LOFType
Constant for QSW frame (X axis aligned with position, Z axis aligned with orbital momentum).
QSW_INERTIAL - org.orekit.frames.LOFType
Constant for QSW frame considered inertial (X axis aligned with position, Z axis aligned with orbital momentum).
QuadraticClockModel - Class in org.orekit.estimation.measurements
Quadratic clock model.
QuadraticClockModel(AbsoluteDate, double, double, double) - Constructor for class org.orekit.estimation.measurements.QuadraticClockModel
Simple constructor.
QuadraticClockModel(ParameterDriver, ParameterDriver, ParameterDriver) - Constructor for class org.orekit.estimation.measurements.QuadraticClockModel
Simple constructor.
QuadraticFieldClockModel<T extends CalculusFieldElement<T>> - Class in org.orekit.estimation.measurements
Quadratic clock model.
QuadraticFieldClockModel(FieldAbsoluteDate<T>, T, T, T) - Constructor for class org.orekit.estimation.measurements.QuadraticFieldClockModel
Simple constructor.
quaternion - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Quaternion sub-sub-section.
quaternion - org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternionKey
Quaternion wrapping element in XML files.
QUATERNION - org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceType
Quaternion.
QUATERNION - org.orekit.files.ccsds.ndm.adm.acm.AttitudeElementsType
Quaternion.
QUATERNION - org.orekit.files.ccsds.ndm.adm.AttitudeType
Quaternion.
QUATERNION_ANGVEL - org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceType
Quaternion and angular velocities.
QUATERNION_ANGVEL - org.orekit.files.ccsds.ndm.adm.AttitudeType
Quaternion and angular velocity.
QUATERNION_DERIVATIVE - org.orekit.files.ccsds.ndm.adm.AttitudeType
Quaternion and derivatives.
QUATERNION_EULER_RATES - org.orekit.files.ccsds.ndm.adm.AttitudeType
Quaternion and Euler angles rates (only in ADM V1).
QUATERNION_GYROBIAS - org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceType
Quaternion and gyro biases.
QUATERNION_TYPE - org.orekit.files.ccsds.ndm.adm.aem.AemMetadataKey
Placement of the scalar component in quaternion entry.
quaternionAngVel - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Quaternion/angular velocity sub-section.
quaternionDerivative - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Quaternion/derivative sub-section.
quaternionDot - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Quaternion rate sub-sub-section.
quaternionDot - org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternionKey
Quaternion derivative wrapping element in XML files.
quaternionEphemeris - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Quaternion state sub-section.
quaternionEulerRate - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Quaternion/rate sub-section (only for ADM V1).
quaternionRate - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Quaternion rate sub-sub-section(only for ADM V1).
quaternionRate - org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternionKey
Quaternion derivative wrapping element in XML files (ADM V1 only).
quaternionState - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Quaternion state sub-section (only for ADM V1).
QUEST - org.orekit.files.ccsds.definitions.AdMethodType
QUaternion ESTimator.
QZS - org.orekit.files.rinex.navigation.IonosphericCorrectionType
QZSSS α/β.
QZS - org.orekit.gnss.metric.ntrip.NavigationSystem
QZNSS.
QZS - org.orekit.gnss.ObservationTimeScale
QZSS time scale.
QZSS - org.orekit.files.sp3.SP3FileType
QZSS only file.
QZSS - org.orekit.gnss.antenna.SatelliteType
QZSS Block I (Michibiki-1).
QZSS - org.orekit.gnss.SatelliteSystem
Quasi-Zenith Satellite System system.
QZSS - org.orekit.gnss.TimeSystem
Quasi-Zenith System.
QZSS_2A - org.orekit.gnss.antenna.SatelliteType
QZSS Block II (Michibiki-2).
QZSS_2G - org.orekit.gnss.antenna.SatelliteType
QZSS Block II GEO (Michibiki-3).
QZSS_2I - org.orekit.gnss.antenna.SatelliteType
QZSS Block II IGSO (Michibiki-2,4).
QZSS_AV - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
Value of the earth's rotation rate in rad/s for QZSS user.
QZSS_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Reference epoch for QZSS weeks: 1980-01-06T00:00:00 QZSS time.
QZSS_EPOCH - Static variable in class org.orekit.time.DateComponents
Reference epoch for QZSS weeks: 1980-01-06.
QZSS_MU - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
WGS 84 value of the Earth's universal gravitational parameter for QZSS user in m³/s².
QZSS_WEEK_NB - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
Number of weeks in the QZSS cycle.
QZSSAlmanac - Class in org.orekit.propagation.analytical.gnss.data
This class holds a QZSS almanac as read from YUMA files.
QZSSAlmanac() - Constructor for class org.orekit.propagation.analytical.gnss.data.QZSSAlmanac
Constructor.
QZSSCivilianNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data
Container for data contained in a QZSS navigation message.
QZSSCivilianNavigationMessage(boolean) - Constructor for class org.orekit.propagation.analytical.gnss.data.QZSSCivilianNavigationMessage
Constructor.
QZSSLegacyNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data
Container for data contained in a QZSS navigation message.
QZSSLegacyNavigationMessage() - Constructor for class org.orekit.propagation.analytical.gnss.data.QZSSLegacyNavigationMessage
Constructor.
QZSSScale - Class in org.orekit.time
QZSS time scale.

R

R01 - org.orekit.gnss.Frequency
GLONASS, "G1" (1602 MHZ).
R02 - org.orekit.gnss.Frequency
GLONASS, "G2" (1246 MHz).
R03 - org.orekit.gnss.Frequency
GLONASS, "G3" (1202.025 MHz).
R04 - org.orekit.gnss.Frequency
GLONASS, "G1a" (1600.995 MHZ).
R06 - org.orekit.gnss.Frequency
GLONASS, "G2a" (1248.06 MHz).
RA_OF_ASC_NODE - org.orekit.files.ccsds.ndm.odm.KeplerianElementsKey
Orbit right ascension of ascending node.
RAAN - Static variable in enum org.orekit.orbits.OrbitType
Name for right ascension of ascending node.
RADEC - org.orekit.files.ccsds.ndm.tdm.AngleType
right ascension, declination.
RADIAN - Static variable in class org.orekit.utils.units.Unit
Radian unit.
RADIANS - org.orekit.data.PolynomialParser.Unit
Radians angles.
RadiationForceModel - Interface in org.orekit.forces.radiation
Interface for radiation-related force models.
radiationPressureAcceleration(FieldSpacecraftState<T>, FieldVector3D<T>, T[]) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Compute the acceleration due to radiation pressure.
radiationPressureAcceleration(FieldSpacecraftState<T>, FieldVector3D<T>, T[]) - Method in class org.orekit.forces.radiation.IsotropicRadiationClassicalConvention
Compute the acceleration due to radiation pressure.
radiationPressureAcceleration(FieldSpacecraftState<T>, FieldVector3D<T>, T[]) - Method in class org.orekit.forces.radiation.IsotropicRadiationCNES95Convention
Compute the acceleration due to radiation pressure.
radiationPressureAcceleration(FieldSpacecraftState<T>, FieldVector3D<T>, T[]) - Method in class org.orekit.forces.radiation.IsotropicRadiationSingleCoefficient
Compute the acceleration due to radiation pressure.
radiationPressureAcceleration(FieldSpacecraftState<T>, FieldVector3D<T>, T[]) - Method in interface org.orekit.forces.radiation.RadiationSensitive
Compute the acceleration due to radiation pressure.
radiationPressureAcceleration(SpacecraftState, Vector3D, double[]) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Compute the acceleration due to radiation pressure.
radiationPressureAcceleration(SpacecraftState, Vector3D, double[]) - Method in class org.orekit.forces.radiation.IsotropicRadiationClassicalConvention
Compute the acceleration due to radiation pressure.
radiationPressureAcceleration(SpacecraftState, Vector3D, double[]) - Method in class org.orekit.forces.radiation.IsotropicRadiationCNES95Convention
Compute the acceleration due to radiation pressure.
radiationPressureAcceleration(SpacecraftState, Vector3D, double[]) - Method in class org.orekit.forces.radiation.IsotropicRadiationSingleCoefficient
Compute the acceleration due to radiation pressure.
radiationPressureAcceleration(SpacecraftState, Vector3D, double[]) - Method in interface org.orekit.forces.radiation.RadiationSensitive
Compute the acceleration due to radiation pressure.
RadiationPressureModel - Class in org.orekit.forces.radiation
Class representing a light-induced radiation pressure force, by leveraging on a given flux model.
RadiationPressureModel(LightFluxModel, RadiationSensitive) - Constructor for class org.orekit.forces.radiation.RadiationPressureModel
Constructor.
RadiationSensitive - Interface in org.orekit.forces.radiation
Interface for spacecraft that are sensitive to radiation pressure forces.
RadioWave - Interface in org.orekit.gnss
Top level interface for radio waves.
radiusCorrection(double) - Method in enum org.orekit.propagation.events.VisibilityTrigger
Apply radius correction.
Range - Class in org.orekit.estimation.measurements
Class modeling a range measurement from a ground station.
Range(GroundStation, boolean, AbsoluteDate, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.Range
Simple constructor.
RANGE - org.orekit.files.ccsds.ndm.tdm.ObservationType
Data: Range value [km, s or RU].
RANGE_MODE - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Range mode entry.
RANGE_MODULUS - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Range modulus entry (beware the unit is Range Units here).
RANGE_UNITS - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Range units entry.
RangeBuilder - Class in org.orekit.estimation.measurements.generation
Builder for Range measurements.
RangeBuilder(CorrelatedRandomVectorGenerator, GroundStation, boolean, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.RangeBuilder
Simple constructor.
rangeErrorIonosphericModel(GroundStation, FieldSpacecraftState<T>, T[]) - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeIonosphericDelayModifier
Compute the measurement error due to Ionosphere.
rangeErrorIonosphericModel(GroundStation, SpacecraftState) - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeIonosphericDelayModifier
Compute the measurement error due to Ionosphere.
rangeErrorTroposphericModel(GroundStation, FieldSpacecraftState<T>, T[]) - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeTroposphericDelayModifier
Compute the measurement error due to Troposphere.
rangeErrorTroposphericModel(GroundStation, SpacecraftState) - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeTroposphericDelayModifier
Compute the measurement error due to Troposphere.
RangeIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical range measurement with ionospheric delay.
RangeIonosphericDelayModifier(IonosphericModel, double) - Constructor for class org.orekit.estimation.measurements.modifiers.RangeIonosphericDelayModifier
Constructor.
RangeMeasurement(AbsoluteDate, double, int) - Constructor for class org.orekit.files.ilrs.CRD.RangeMeasurement
Constructor.
RangeMeasurement(AbsoluteDate, double, int, double) - Constructor for class org.orekit.files.ilrs.CRD.RangeMeasurement
Constructor.
RangeMeasurement(AbsoluteDate, double, int, double, String) - Constructor for class org.orekit.files.ilrs.CRD.RangeMeasurement
Constructor.
RangeMode - Enum in org.orekit.files.ccsds.ndm.tdm
Type of range tones.
RangeModifierUtil - Class in org.orekit.estimation.measurements.modifiers
Utility class modifying theoretical range measurement.
RangeRate - Class in org.orekit.estimation.measurements
Class modeling one-way or two-way range rate measurement between two vehicles.
RangeRate(GroundStation, AbsoluteDate, double, double, double, boolean, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.RangeRate
Simple constructor.
RangeRateBuilder - Class in org.orekit.estimation.measurements.generation
Builder for RangeRate measurements.
RangeRateBuilder(CorrelatedRandomVectorGenerator, GroundStation, boolean, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.RangeRateBuilder
Simple constructor.
rangeRateErrorIonosphericModel(GroundStation, FieldSpacecraftState<T>, T[]) - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeRateIonosphericDelayModifier
Compute the measurement error due to Ionosphere.
rangeRateErrorIonosphericModel(GroundStation, FieldSpacecraftState<T>, T[]) - Method in class org.orekit.estimation.measurements.modifiers.RangeRateIonosphericDelayModifier
Compute the measurement error due to Ionosphere.
rangeRateErrorIonosphericModel(GroundStation, SpacecraftState) - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeRateIonosphericDelayModifier
Compute the measurement error due to Ionosphere.
rangeRateErrorIonosphericModel(GroundStation, SpacecraftState) - Method in class org.orekit.estimation.measurements.modifiers.RangeRateIonosphericDelayModifier
Compute the measurement error due to Ionosphere.
rangeRateErrorTroposphericModel(GroundStation, FieldSpacecraftState<T>, T[]) - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeRateTroposphericDelayModifier
Compute the measurement error due to Troposphere.
rangeRateErrorTroposphericModel(GroundStation, FieldSpacecraftState<T>, T[]) - Method in class org.orekit.estimation.measurements.modifiers.RangeRateTroposphericDelayModifier
Compute the measurement error due to Troposphere.
rangeRateErrorTroposphericModel(GroundStation, SpacecraftState) - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeRateTroposphericDelayModifier
Compute the measurement error due to Troposphere.
rangeRateErrorTroposphericModel(GroundStation, SpacecraftState) - Method in class org.orekit.estimation.measurements.modifiers.RangeRateTroposphericDelayModifier
Compute the measurement error due to Troposphere.
RangeRateIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical range-rate measurement with ionospheric delay.
RangeRateIonosphericDelayModifier(IonosphericModel, double, boolean) - Constructor for class org.orekit.estimation.measurements.modifiers.RangeRateIonosphericDelayModifier
Constructor.
RangeRateModifierUtil - Class in org.orekit.estimation.measurements.modifiers
Utility class modifying theoretical range-rate measurement.
RangeRateTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical range-rate measurements with tropospheric delay.
RangeRateTroposphericDelayModifier(DiscreteTroposphericModel, boolean) - Constructor for class org.orekit.estimation.measurements.modifiers.RangeRateTroposphericDelayModifier
RangeRateTroposphericDelayModifier(TroposphericModel, boolean) - Constructor for class org.orekit.estimation.measurements.modifiers.RangeRateTroposphericDelayModifier
Constructor.
RangeSupplement(AbsoluteDate, String, double, double, double, double, double) - Constructor for class org.orekit.files.ilrs.CRD.RangeSupplement
Constructor.
RangeTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical range measurement with tropospheric delay.
RangeTroposphericDelayModifier(DiscreteTroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.RangeTroposphericDelayModifier
Deprecated.
RangeTroposphericDelayModifier(TroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.RangeTroposphericDelayModifier
Constructor.
RangeUnits - Enum in org.orekit.files.ccsds.ndm.tdm
Units of the range observable.
RangeUnitsConverter - Interface in org.orekit.files.ccsds.ndm.tdm
Interface for converting Range Units to meters.
RAPID_DATA_PREDICTION_COLUMNS_1980_FILENAME - Static variable in class org.orekit.frames.FramesFactory
Default regular expression for the Rapid Data and Prediction EOP columns files (IAU1980 compatibles).
RAPID_DATA_PREDICTION_COLUMNS_2000_FILENAME - Static variable in class org.orekit.frames.FramesFactory
Default regular expression for the Rapid Data and Prediction EOP columns files (IAU2000 compatibles).
RATE_FRAME - org.orekit.files.ccsds.ndm.adm.aem.AemMetadataKey
Reference frame for Euler rates.
RATE_FRAME - org.orekit.files.ccsds.ndm.adm.apm.EulerKey
Reference frame for rate entry (ADM V1 only).
RATE_PROCESS_NOISE_STDDEV - org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationKey
Process noise standard deviation if AttitudeDeterminationKey.RATE_STATES is RateElementsType.ANGVEL.
RATE_STATES - org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationKey
Attitude rate states.
RATE_TYPE - org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadataKey
Attitude rate element set type.
RateElementsType - Enum in org.orekit.files.ccsds.ndm.adm.acm
Attitude rate element set type used in CCSDS Attitude Comprehensive Messages.
rateFrameIsA() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Check if rates are specified in frame A.
rateFrameIsA() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler
Check if rates are specified in frame A.
RAW - org.orekit.files.ccsds.ndm.tdm.DataQuality
No quality check occurred.
RAW - org.orekit.gnss.metric.ntrip.DataFormat
RAW.
RAW_LINE - org.orekit.files.ccsds.utils.lexical.TokenType
Raw line token.
rawDataIsBinary() - Method in interface org.orekit.data.DataSource.Opener
Check if the raw data is binary.
RawSphericalHarmonicsProvider - Interface in org.orekit.forces.gravity.potential
Interface used to provide raw spherical harmonics coefficients.
RawSphericalHarmonicsProvider.RawSphericalHarmonics - Interface in org.orekit.forces.gravity.potential
The raw spherical harmonics at a particular instant.
rawToSI(RangeUnitsConverter, TdmMetadata, AbsoluteDate, double) - Method in enum org.orekit.files.ccsds.ndm.tdm.ObservationType
Convert a measurement to SI units.
RCS - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
Typical (50th percentile) radar cross-section.
RCS - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Typical (50th percentile) radar cross-section.
RCS - org.orekit.files.ccsds.ndm.tdm.ObservationType
Data: Radar Cross section [m²].
RCS_MAX - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
Maximum radar cross-section.
RCS_MAX - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Maximum radar cross-section.
RCS_MIN - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
Minimum radar cross-section.
RCS_MIN - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Minimum radar cross-section.
RCV_CLOCK_OFFS_APPL - org.orekit.files.rinex.section.RinexLabels
Indicator of receiver clock offset application.
RDM_MSG_LINK - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Unique identifier of Reentry Data Message linked to this Orbit Data Message.
read(char[], int, int) - Method in class org.orekit.data.LineOrientedFilteringReader
readGravityField(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Read a gravity field coefficients provider from the first supported file.
readGravityField(int, int) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
Read a gravity field coefficients provider from the first supported file.
REC_NB_TYPE_VERS - org.orekit.files.rinex.section.RinexLabels
Receiver number, type and version.
RecallLastOccurrence - Class in org.orekit.propagation.events.handlers
Event handler wrapping another, arbitrary one whilst remembering date of last detection.
RecallLastOccurrence(EventHandler) - Constructor for class org.orekit.propagation.events.handlers.RecallLastOccurrence
Constructor.
RECEIVE - org.orekit.files.ccsds.ndm.tdm.TimetagReference
Reference at receive time.
RECEIVE_BAND - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Receive band entry.
RECEIVE_DELAY_1 - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
First receive delay entry.
RECEIVE_DELAY_2 - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Second receive delay entry.
RECEIVE_DELAY_3 - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Third receive delay entry.
RECEIVE_DELAY_4 - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Fourth receive delay entry.
RECEIVE_DELAY_5 - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Fifth receive delay entry.
RECEIVE_FREQ - org.orekit.files.ccsds.ndm.tdm.ObservationType
Data: Received frequency [Hz].
RECEIVE_FREQ_1 - org.orekit.files.ccsds.ndm.tdm.ObservationType
Data: Received frequencies [Hz].
RECEIVE_FREQ_2 - org.orekit.files.ccsds.ndm.tdm.ObservationType
Received frequency 2.
RECEIVE_FREQ_3 - org.orekit.files.ccsds.ndm.tdm.ObservationType
Received frequency 3.
RECEIVE_FREQ_4 - org.orekit.files.ccsds.ndm.tdm.ObservationType
Received frequency 4.
RECEIVE_FREQ_5 - org.orekit.files.ccsds.ndm.tdm.ObservationType
Received frequency 5.
RECEIVE_PHASE_CT_1 - org.orekit.files.ccsds.ndm.tdm.ObservationType
Data: phase cycle count at receiver.
RECEIVE_PHASE_CT_2 - org.orekit.files.ccsds.ndm.tdm.ObservationType
Data: phase cycle count at receiver.
RECEIVE_PHASE_CT_3 - org.orekit.files.ccsds.ndm.tdm.ObservationType
Data: phase cycle count at receiver.
RECEIVE_PHASE_CT_4 - org.orekit.files.ccsds.ndm.tdm.ObservationType
Data: phase cycle count at receiver.
RECEIVE_PHASE_CT_5 - org.orekit.files.ccsds.ndm.tdm.ObservationType
Data: phase cycle count at receiver.
RECEIVED_ONLY - org.orekit.files.ilrs.CRDHeader.RangeType
Received times only.
Receiver(String, String, double, double, double) - Constructor for class org.orekit.files.rinex.clock.RinexClock.Receiver
Constructor.
ReceiverAntenna - Class in org.orekit.gnss.antenna
GNSS receiver antenna model.
ReceiverAntenna(String, String, Map<Frequency, FrequencyPattern>, String) - Constructor for class org.orekit.gnss.antenna.ReceiverAntenna
Simple constructor.
receiverToInert(EstimatedMeasurementBase<InterSatellitesPhase>) - Method in class org.orekit.estimation.measurements.gnss.InterSatellitesWindUp
Compute rotation from receiver to inertial frame.
receiverToInert(EstimatedMeasurementBase<Phase>) - Method in class org.orekit.estimation.measurements.gnss.WindUp
Compute rotation from receiver to inertial frame.
receiverToInert(EstimatedMeasurementBase<T>) - Method in class org.orekit.estimation.measurements.gnss.AbstractWindUp
Compute rotation from receiver to inertial frame.
RECOMMENDED_OD_SPAN - org.orekit.files.ccsds.ndm.cdm.ODParametersKey
The recommended OD time span calculated for the object.
RECOMMENDED_OD_SPAN - org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey
Time span of observation recommended for the OD of the object.
Record - Class in org.orekit.gnss.metric.ntrip
Record in source table.
Record(String) - Constructor for class org.orekit.gnss.metric.ntrip.Record
Build a record by parsing a source table line.
RecordAndContinue - Class in org.orekit.propagation.events.handlers
Handler that will record every time an event occurs and always return Action.CONTINUE.
RecordAndContinue() - Constructor for class org.orekit.propagation.events.handlers.RecordAndContinue
Create a new handler using an ArrayList to store events.
RecordAndContinue(List<RecordAndContinue.Event>) - Constructor for class org.orekit.propagation.events.handlers.RecordAndContinue
Create a handler using the given collection to store events.
RecordAndContinue.Event - Class in org.orekit.propagation.events.handlers
A single event detected during propagation.
RecordType - Enum in org.orekit.gnss.metric.ntrip
Enumerate for record types in sourcetable.
recoverAmbiguities() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Recover ambiguities prior to the Z-transformation.
recoverAmbiguities() - Method in class org.orekit.estimation.measurements.gnss.IntegerBootstrapping
Recover ambiguities prior to the Z-transformation.
reduction() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Perform LAMBDA reduction.
reduction() - Method in class org.orekit.estimation.measurements.gnss.LambdaMethod
Perform LAMBDA reduction.
reduction() - Method in class org.orekit.estimation.measurements.gnss.ModifiedLambdaMethod
Perform MLAMBDA reduction.
REDUCTION_THEORY - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey
Reduction theory used for precession and nutation modeling.
REENTRY_MODE - org.orekit.files.ccsds.ndm.odm.ocm.OpsStatus
Object in reentry mode.
REF_FRAME - org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey
Name of the reference frame, in which state vector data are given.
REF_FRAME - org.orekit.files.ccsds.ndm.odm.CommonMetadataKey
Name of the reference frame in which the state vector and optional Keplerian element data are given.
REF_FRAME_A - org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationKey
Reference frame defining the starting point of the transformation.
REF_FRAME_A - org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadataKey
Reference frame defining the starting point of the transformation.
REF_FRAME_A - org.orekit.files.ccsds.ndm.adm.aem.AemMetadataKey
First reference frame.
REF_FRAME_A - org.orekit.files.ccsds.ndm.adm.apm.AngularVelocityKey
First reference frame entry.
REF_FRAME_A - org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternionKey
First reference frame entry.
REF_FRAME_A - org.orekit.files.ccsds.ndm.adm.apm.EulerKey
First reference frame entry.
REF_FRAME_A - org.orekit.files.ccsds.ndm.adm.apm.SpinStabilizedKey
First reference frame entry.
REF_FRAME_B - org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationKey
Reference frame defining the end point of the transformation.
REF_FRAME_B - org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadataKey
Reference frame defining the end point of the transformation.
REF_FRAME_B - org.orekit.files.ccsds.ndm.adm.aem.AemMetadataKey
Second reference frame.
REF_FRAME_B - org.orekit.files.ccsds.ndm.adm.apm.AngularVelocityKey
Second reference frame entry.
REF_FRAME_B - org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternionKey
Second reference frame entry.
REF_FRAME_B - org.orekit.files.ccsds.ndm.adm.apm.EulerKey
Second reference frame entry.
REF_FRAME_B - org.orekit.files.ccsds.ndm.adm.apm.SpinStabilizedKey
Second reference frame entry.
REF_FRAME_EPOCH - org.orekit.files.ccsds.ndm.odm.CommonMetadataKey
Epoch of reference frame, if not intrinsic to the definition of the reference frame.
REFERENCE_FRAME - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
reference frame entry.
ReferenceClock(String, String, double, AbsoluteDate, AbsoluteDate) - Constructor for class org.orekit.files.rinex.clock.RinexClock.ReferenceClock
Constructor.
referenceDateChanged(AbsoluteDate, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver
Notify that a parameter reference date has been changed.
ReferenceEllipsoid - Class in org.orekit.models.earth
A Reference Ellipsoid for use in geodesy.
ReferenceEllipsoid(double, double, Frame, double, double) - Constructor for class org.orekit.models.earth.ReferenceEllipsoid
Creates a new geodetic Reference Ellipsoid from four defining parameters.
referenceValueChanged(double, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver
Notify that a parameter reference value has been changed.
REFLECTANCE - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
Typical (50th percentile) coefficient of reflectance.
REFLECTANCE - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Typical (50th percentile) coefficient of reflectance.
REFLECTION_COEFFICIENT - Static variable in interface org.orekit.forces.radiation.RadiationSensitive
Parameter name for reflection coefficient.
refuseFurtherComments() - Method in class org.orekit.files.ccsds.section.CommentsContainer
Set flag to refuse further comments.
RegionCode - Enum in org.orekit.files.rinex.navigation
Enumerate for region code.
registerAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Register an attitude provider.
registerAttitudeProvider(AttitudeProvider) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Register an attitude provider.
registerAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTJ2SquaredClosedForm
Register an attitude provider.
registerAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction
Register an attitude provider.
registerAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Register an attitude provider.
registerAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Register an attitude provider.
registerAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Register an attitude provider.
registerSwitchEvents(Field<T>, FieldPropagator<T>) - Method in class org.orekit.attitudes.AttitudesSequence
Register all wrapped switch events to the propagator.
registerSwitchEvents(Propagator) - Method in class org.orekit.attitudes.AttitudesSequence
Register all wrapped switch events to the propagator.
RegularXmlTokenBuilder - Class in org.orekit.files.ccsds.utils.lexical
Regular builder using XML elements names and content for tokens.
RegularXmlTokenBuilder() - Constructor for class org.orekit.files.ccsds.utils.lexical.RegularXmlTokenBuilder
Simple constructor.
reinitializeBegin(FieldOrekitStepInterpolator<T>) - Method in class org.orekit.propagation.events.FieldEventState
Reinitialize the beginning of the step.
reinitializeBegin(OrekitStepInterpolator) - Method in class org.orekit.propagation.events.EventState
Reinitialize the beginning of the step.
REJECTED - org.orekit.estimation.measurements.EstimatedMeasurementBase.Status
Status for rejected measurements.
RELATIVE_POSITION_N - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
The N component of Object2’s position relative to Object1’s position in the Radial/Transverse/Normal coordinate frame.
RELATIVE_POSITION_R - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
The R component of Object2’s position relative to Object1’s position in the Radial/Transverse/Normal coordinate frame.
RELATIVE_POSITION_T - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
The T component of Object2’s position relative to Object1’s position in the Radial/Transverse/Normal coordinate frame.
RELATIVE_SPEED - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
Norm of relative velocity vector at TCA.
RELATIVE_VELOCITY_N - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
The N component of Object2’s velocity relative to Object1’s veloity in the Radial/Transverse/Normal coordinate frame.
RELATIVE_VELOCITY_R - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
The R component of Object2’s velocity relative to Object1’s veloity in the Radial/Transverse/Normal coordinate frame.
RELATIVE_VELOCITY_T - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
The T component of Object2’s velocity relative to Object1’s veloity in the Radial/Transverse/Normal coordinate frame.
RelativeDistanceDetector - Class in org.orekit.propagation.events
Detector of specific value for the distance relative to another trajectory (using the Euclidean norm).
RelativeDistanceDetector(AdaptableInterval, double, int, EventHandler, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.RelativeDistanceDetector
Deprecated.
as of 12.2
RelativeDistanceDetector(EventDetectionSettings, EventHandler, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.RelativeDistanceDetector
Constructor.
RelativeDistanceDetector(PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.RelativeDistanceDetector
Constructor with default values.
relativeHumidity(double, double, double) - Method in interface org.orekit.models.earth.weather.water.WaterVaporPressureProvider
Compute relative humidity.
relativeHumidity(T, T, T) - Method in interface org.orekit.models.earth.weather.water.WaterVaporPressureProvider
Compute relative humidity.
relativeMetadataData - org.orekit.files.ccsds.ndm.cdm.XmlSubStructureKey
Relative Metadata section.
relativeStateVector - org.orekit.files.ccsds.ndm.cdm.XmlSubStructureKey
Relative Metadata section.
RelativisticClockInterSatellitesOneWayRangeRateModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical range-rate measurement with relativistic frequency deviation.
RelativisticClockInterSatellitesOneWayRangeRateModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticClockInterSatellitesOneWayRangeRateModifier
Simple constructor.
RelativisticClockInterSatellitesPhaseModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical inter-satellites phase measurement with relativistic clock correction.
RelativisticClockInterSatellitesPhaseModifier() - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticClockInterSatellitesPhaseModifier
Simple constructor.
RelativisticClockInterSatellitesRangeModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical inter-satellites range measurement with relativistic clock correction.
RelativisticClockInterSatellitesRangeModifier() - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticClockInterSatellitesRangeModifier
Simple constructor.
RelativisticClockOneWayGNSSPhaseModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical one-way GNSS phase measurement with relativistic clock correction.
RelativisticClockOneWayGNSSPhaseModifier() - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticClockOneWayGNSSPhaseModifier
Simple constructor.
RelativisticClockOneWayGNSSRangeModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical one-way GNSS range measurement with relativistic clock correction.
RelativisticClockOneWayGNSSRangeModifier() - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticClockOneWayGNSSRangeModifier
Simple constructor.
RelativisticClockOneWayGNSSRangeRateModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical range-rate measurement with relativistic frequency deviation.
RelativisticClockOneWayGNSSRangeRateModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticClockOneWayGNSSRangeRateModifier
Simple constructor.
RelativisticClockPhaseModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical phase measurement with relativistic clock correction.
RelativisticClockPhaseModifier() - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticClockPhaseModifier
Simple constructor.
RelativisticClockRangeModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical range measurement with relativistic clock correction.
RelativisticClockRangeModifier() - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticClockRangeModifier
Simple constructor.
RelativisticClockRangeRateModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical range-rate measurement with relativistic frequency deviation.
RelativisticClockRangeRateModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticClockRangeRateModifier
Simple constructor.
relativisticCorrection(EstimatedMeasurementBase<?>) - Method in class org.orekit.estimation.measurements.modifiers.AbstractRelativisticClockModifier
Computes the relativistic clock correction.
RelativisticJ2ClockInterSatellitesPhaseModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical inter-satellites phase measurements with relativistic J2 clock correction.
RelativisticJ2ClockInterSatellitesPhaseModifier(double, double, double) - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockInterSatellitesPhaseModifier
Modifier constructor.
RelativisticJ2ClockInterSatellitesRangeModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical inter-satellites range measurements with relativistic J2 clock correction.
RelativisticJ2ClockInterSatellitesRangeModifier(double, double, double) - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockInterSatellitesRangeModifier
Modifier constructor.
RelativisticJ2ClockOneWayGNSSPhaseModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical one-way phase measurements with relativistic J2 clock correction.
RelativisticJ2ClockOneWayGNSSPhaseModifier(double, double, double) - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockOneWayGNSSPhaseModifier
Modifier constructor.
RelativisticJ2ClockOneWayGNSSRangeModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying one-way GNSS range theoretical measurements with relativistic J2 clock correction.
RelativisticJ2ClockOneWayGNSSRangeModifier(double, double, double) - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockOneWayGNSSRangeModifier
Modifier constructor.
RelativisticJ2ClockPhaseModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical phase measurements with relativistic J2 clock correction.
RelativisticJ2ClockPhaseModifier(double, double, double) - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockPhaseModifier
Modifier constructor.
RelativisticJ2ClockRangeModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical range measurements with relativistic J2 clock correction.
RelativisticJ2ClockRangeModifier(double, double, double) - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockRangeModifier
Modifier constructor.
relativisticJ2Correction(EstimatedMeasurementBase<?>) - Method in class org.orekit.estimation.measurements.modifiers.AbstractRelativisticJ2ClockModifier
Computes the relativistic J2 clock time delay correction.
Relativity - Class in org.orekit.forces.gravity
Post-Newtonian correction force due to general relativity.
Relativity(double) - Constructor for class org.orekit.forces.gravity.Relativity
Create a force model to add post-Newtonian acceleration corrections to an Earth orbit.
remove(String) - Method in class org.orekit.utils.DoubleArrayDictionary
Remove an entry.
remove(String) - Method in class org.orekit.utils.FieldArrayDictionary
remove an entry.
remove(FieldOrekitFixedStepHandler<T>) - Method in class org.orekit.propagation.sampling.FieldStepHandlerMultiplexer
Remove a handler.
remove(FieldOrekitStepHandler<T>) - Method in class org.orekit.propagation.sampling.FieldStepHandlerMultiplexer
Remove a handler.
remove(OrekitFixedStepHandler) - Method in class org.orekit.propagation.sampling.StepHandlerMultiplexer
Remove a handler.
remove(OrekitStepHandler) - Method in class org.orekit.propagation.sampling.StepHandlerMultiplexer
Remove a handler.
removeForceModels() - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Remove all perturbing force models from the global perturbation model.
removeForceModels() - Method in class org.orekit.propagation.numerical.NumericalPropagator
Remove all force models (except central attraction).
removeForceModels() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Remove all perturbing force models from the global perturbation model (except central attraction).
removeForceModels() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Remove all perturbing force models from the global perturbation model (except central attraction).
removeObserver(ParameterObserver) - Method in class org.orekit.utils.ParameterDriver
Remove an observer.
removeProvider(DataProvider) - Method in class org.orekit.data.DataProvidersManager
Remove one provider.
removeRates() - Method in class org.orekit.orbits.CircularOrbit
Create a new instance such that PositionAngleBased.hasRates() is false.
removeRates() - Method in class org.orekit.orbits.EquinoctialOrbit
Create a new instance such that PositionAngleBased.hasRates() is false.
removeRates() - Method in class org.orekit.orbits.FieldCircularOrbit
Create a new instance such that PositionAngleBased.hasRates() is false.
removeRates() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Create a new instance such that PositionAngleBased.hasRates() is false.
removeRates() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Create a new instance such that PositionAngleBased.hasRates() is false.
removeRates() - Method in class org.orekit.orbits.KeplerianOrbit
Create a new instance such that PositionAngleBased.hasRates() is false.
removeRates() - Method in interface org.orekit.orbits.PositionAngleBased
Create a new instance such that PositionAngleBased.hasRates() is false.
removeSolution() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Remove spurious solution.
replaceObserver(ParameterObserver, ParameterObserver) - Method in class org.orekit.utils.ParameterDriver
Replace an observer.
requiresDenseOutput() - Method in class org.orekit.propagation.sampling.FieldOrekitStepNormalizer
Determines whether this handler needs dense output.
rescale(boolean, Flattener, Flattener, TimeDependentHarmonic[]) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Rescale coefficients arrays.
rescale(double, boolean, Flattener, Flattener, double[]) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Rescale coefficients arrays.
RESERVED - org.orekit.propagation.analytical.gnss.data.BeidouSatelliteType
Reserved.
reset(FileFormat) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmParser
Reset parser to initial state before parsing.
reset(FileFormat) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser
Reset parser to initial state before parsing.
reset(FileFormat) - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser
Reset parser to initial state before parsing.
reset(FileFormat) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmParser
Reset parser to initial state before parsing.
reset(FileFormat) - Method in class org.orekit.files.ccsds.ndm.NdmParser
Reset parser to initial state before parsing.
reset(FileFormat) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser
Reset parser to initial state before parsing.
reset(FileFormat) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser
Reset parser to initial state before parsing.
reset(FileFormat) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser
Reset parser to initial state before parsing.
reset(FileFormat) - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser
Reset parser to initial state before parsing.
reset(FileFormat) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser
Reset parser to initial state before parsing.
reset(FileFormat) - Method in interface org.orekit.files.ccsds.utils.lexical.MessageParser
Reset parser to initial state before parsing.
reset(FileFormat, ProcessingState) - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser
Reset parser to initial state before parsing.
resetActiveProvider(AttitudeProvider) - Method in class org.orekit.attitudes.AttitudesSequence
Reset the active provider.
ResetDerivativesOnEvent - Class in org.orekit.propagation.events.handlers
Event handler which will always return stop as a state.
ResetDerivativesOnEvent() - Constructor for class org.orekit.propagation.events.handlers.ResetDerivativesOnEvent
 
resetFiltersToDefault() - Method in class org.orekit.data.DataProvidersManager
Reset all filters to default.
resetFitting(AbsoluteDate, double...) - Method in class org.orekit.utils.SecularAndHarmonic
Reset fitting.
resetInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Reset the propagator initial state.
resetInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Reset the propagator initial state.
resetInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.analytical.FieldKeplerianPropagator
Reset the propagator initial state.
resetInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElementsPropagator
Reset the propagator initial state.
resetInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
Reset the propagator initial state.
resetInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator
Reset the propagator initial state.
resetInitialState(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.FieldPropagator
Reset the propagator initial state.
resetInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
Reset the propagator initial state.
resetInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Reset the propagator initial state.
resetInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Reset the initial state.
resetInitialState(FieldSpacecraftState<T>, PropagationType) - Method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Reset the propagator initial state.
resetInitialState(FieldSpacecraftState<T>, PropagationType) - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Reset the propagator initial state.
resetInitialState(FieldSpacecraftState<T>, PropagationType) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Reset initial state with a given propagation type.
resetInitialState(FieldSpacecraftState<T>, PropagationType) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Reset initial state with a given propagation type.
resetInitialState(FieldSpacecraftState<T>, PropagationType, double, int) - Method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Reset the propagator initial state.
resetInitialState(FieldSpacecraftState<T>, PropagationType, double, int) - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.files.general.EphemerisSegmentPropagator
 
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.AbstractPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.AdapterPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
 
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.Ephemeris
Try (and fail) to reset the initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.intelsat.IntelsatElevenElementsPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.KeplerianPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in interface org.orekit.propagation.Propagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Reset the initial state.
resetInitialState(SpacecraftState, PropagationType) - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState, PropagationType) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState, PropagationType) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Reset initial state with a given propagation type.
resetInitialState(SpacecraftState, PropagationType) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Reset initial state with a given propagation type.
resetInitialState(SpacecraftState, PropagationType, double, int) - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState, PropagationType, double, int) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Reset the propagator initial state.
resetIntermediateState(FieldSpacecraftState<T>, boolean) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Reset an intermediate state.
resetIntermediateState(FieldSpacecraftState<T>, boolean) - Method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Reset an intermediate state.
resetIntermediateState(FieldSpacecraftState<T>, boolean) - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Reset an intermediate state.
resetIntermediateState(FieldSpacecraftState<T>, boolean) - Method in class org.orekit.propagation.analytical.FieldKeplerianPropagator
Reset an intermediate state.
resetIntermediateState(FieldSpacecraftState<T>, boolean) - Method in class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElementsPropagator
Reset an intermediate state.
resetIntermediateState(FieldSpacecraftState<T>, boolean) - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
Reset an intermediate state.
resetIntermediateState(FieldSpacecraftState<T>, boolean) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
Reset an intermediate state.
resetIntermediateState(FieldSpacecraftState<T>, boolean, double, int) - Method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Reset an intermediate state.
resetIntermediateState(FieldSpacecraftState<T>, boolean, double, int) - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.files.general.EphemerisSegmentPropagator
 
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.AdapterPropagator
Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
 
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.Ephemeris
Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator
Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator
Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator
Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.intelsat.IntelsatElevenElementsPropagator
Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.KeplerianPropagator
Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean, double, int) - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean, double, int) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Reset an intermediate state.
resetOrbit(Orbit) - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Reset the orbit in the propagator builder.
resetOrbit(Orbit) - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
Reset the orbit in the propagator builder.
resetOrbit(Orbit, PropagationType) - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder
Reset the orbit in the propagator builder.
resetState(EventDetector, SpacecraftState) - Method in class org.orekit.attitudes.AttitudesSequence.Switch
Reset the state prior to continue propagation.
resetState(EventDetector, SpacecraftState) - Method in interface org.orekit.propagation.events.handlers.EventHandler
Reset the state prior to continue propagation.
resetState(EventDetector, SpacecraftState) - Method in class org.orekit.propagation.events.handlers.EventMultipleHandler
Reset the state prior to continue propagation.
resetState(EventDetector, SpacecraftState) - Method in class org.orekit.propagation.events.handlers.RecallLastOccurrence
Reset the state prior to continue propagation.
resetState(FieldEventDetector<T>, FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.events.handlers.FieldEventHandler
Reset the state prior to continue propagation.
resetState(FieldEventDetector<T>, FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.handlers.FieldRecallLastOccurrence
Reset the state prior to continue propagation.
resetState(FieldSpacecraftState<T>) - Method in interface org.orekit.forces.maneuvers.trigger.FieldManeuverTriggersResetter
Reset state as a maneuver triggers.
resetState(SpacecraftState) - Method in class org.orekit.forces.maneuvers.jacobians.TriggerDate
Reset state as a maneuver triggers.
resetState(SpacecraftState) - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggersResetter
Reset state as a maneuver triggers.
ResidualFilter<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.filtering
Residual pre-processing filter.
ResidualFilter(double) - Constructor for class org.orekit.estimation.measurements.filtering.ResidualFilter
Constructor.
RESIDUALS_ACCEPTED - org.orekit.files.ccsds.ndm.cdm.ODParametersKey
The percentage of residuals accepted in the OD of the object (from 0 to 100).
restrictStep(FieldSpacecraftState<T>, FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.sampling.FieldOrekitStepInterpolator
Create a new restricted version of the instance.
restrictStep(SpacecraftState, SpacecraftState) - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator
Create a new restricted version of the instance.
REV_AT_EPOCH - org.orekit.files.ccsds.ndm.odm.omm.OmmTleKey
Revolution number.
REV_PER_DAY - Static variable in class org.orekit.files.ccsds.definitions.Units
Revolutions per day unit.
REV_PER_DAY2_SCALED - Static variable in class org.orekit.files.ccsds.definitions.Units
Scaled revolutions per square day unit.
REV_PER_DAY3_SCALED - Static variable in class org.orekit.files.ccsds.definitions.Units
Scaled revolutions per cubic day divieded by 6 unit.
revert() - Method in class org.orekit.utils.AngularCoordinates
Revert a rotation/rotation rate/ rotation acceleration triplet.
revert() - Method in class org.orekit.utils.FieldAngularCoordinates
Revert a rotation / rotation rate / rotation acceleration triplet.
revert() - Method in class org.orekit.utils.TimeStampedAngularCoordinates
Revert a rotation/rotation rate pair.
revert() - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates
Revert a rotation/rotation rate pair.
RevisedChaoMappingFunction - Class in org.orekit.models.earth.troposphere
Chao mapping function for radio wavelengths.
RevisedChaoMappingFunction() - Constructor for class org.orekit.models.earth.troposphere.RevisedChaoMappingFunction
Builds a new instance.
REVOLUTION - Static variable in class org.orekit.utils.units.Unit
Revolution unit.
RHUMIDITY - org.orekit.files.ccsds.ndm.tdm.ObservationType
Data: Relative humidity [%].
RIC - org.orekit.files.ccsds.definitions.OrbitRelativeFrame
Another name for Radial, Transverse (along-track) and Normal (X towards zenith, Z towards momentum).
RichardsonExpansion - Class in org.orekit.orbits
Class implementing the Third-Order Richardson Expansion.
RichardsonExpansion(CR3BPSystem, LagrangianPoints) - Constructor for class org.orekit.orbits.RichardsonExpansion
Simple Constructor.
RINEX - org.orekit.gnss.metric.ntrip.DataFormat
RINEX.
RinexBaseHeader - Class in org.orekit.files.rinex.section
Base container for Rinex headers.
RinexBaseHeader(RinexFileType) - Constructor for class org.orekit.files.rinex.section.RinexBaseHeader
Simple constructor.
RinexClock - Class in org.orekit.files.rinex.clock
Represents a parsed clock file from the IGS.
RinexClock(Function<? super String, ? extends Frame>) - Constructor for class org.orekit.files.rinex.clock.RinexClock
Constructor.
RinexClock.ClockDataLine - Class in org.orekit.files.rinex.clock
Clock data for a single station.
RinexClock.ClockDataType - Enum in org.orekit.files.rinex.clock
Clock data type.
RinexClock.Receiver - Class in org.orekit.files.rinex.clock
Represents a receiver or a satellite with its position in the considered frame.
RinexClock.ReferenceClock - Class in org.orekit.files.rinex.clock
Represents a reference clock with its validity time span.
RinexClockParser - Class in org.orekit.files.rinex.clock
A parser for the clock file from the IGS.
RinexClockParser() - Constructor for class org.orekit.files.rinex.clock.RinexClockParser
Create a clock file parser using default values.
RinexClockParser(Function<? super String, ? extends Frame>) - Constructor for class org.orekit.files.rinex.clock.RinexClockParser
Create a clock file parser and specify the frame builder.
RinexClockParser(Function<? super String, ? extends Frame>, TimeScales) - Constructor for class org.orekit.files.rinex.clock.RinexClockParser
Constructor, build the IGS clock file parser.
RinexComment - Class in org.orekit.files.rinex.section
Container for comment in RINEX file.
RinexComment(int, String) - Constructor for class org.orekit.files.rinex.section.RinexComment
Simple constructor.
RinexFile<T extends RinexBaseHeader> - Class in org.orekit.files.rinex
Container for Rinex file.
RinexFile(T) - Constructor for class org.orekit.files.rinex.RinexFile
Simple constructor.
RinexFileType - Enum in org.orekit.files.rinex.utils
Enumerate for RINEX files types.
RinexLabels - Enum in org.orekit.files.rinex.section
Labels for Rinex files.
RinexNavigation - Class in org.orekit.files.rinex.navigation
Represents a parsed RINEX navigation messages files.
RinexNavigation() - Constructor for class org.orekit.files.rinex.navigation.RinexNavigation
Constructor.
RinexNavigationHeader - Class in org.orekit.files.rinex.navigation
Header for Rinex Navigation.
RinexNavigationHeader() - Constructor for class org.orekit.files.rinex.navigation.RinexNavigationHeader
Simple constructor.
RinexNavigationParser - Class in org.orekit.files.rinex.navigation
Parser for RINEX navigation messages files.
RinexNavigationParser() - Constructor for class org.orekit.files.rinex.navigation.RinexNavigationParser
Constructor.
RinexNavigationParser(TimeScales) - Constructor for class org.orekit.files.rinex.navigation.RinexNavigationParser
Constructor.
RinexObservation - Class in org.orekit.files.rinex.observation
Container for Rinex observation file.
RinexObservation() - Constructor for class org.orekit.files.rinex.observation.RinexObservation
Simple constructor.
RinexObservationHeader - Class in org.orekit.files.rinex.observation
Container for Rinex observation file header.
RinexObservationHeader() - Constructor for class org.orekit.files.rinex.observation.RinexObservationHeader
Simple constructor.
RinexObservationParser - Class in org.orekit.files.rinex.observation
Parser for Rinex measurements files.
RinexObservationParser() - Constructor for class org.orekit.files.rinex.observation.RinexObservationParser
Simple constructor.
RinexObservationParser(TimeScales) - Constructor for class org.orekit.files.rinex.observation.RinexObservationParser
Create a RINEX loader/parser with the given source of RINEX auxiliary data files.
RinexObservationWriter - Class in org.orekit.files.rinex.observation
Writer for Rinex observation file.
RinexObservationWriter(Appendable, String) - Constructor for class org.orekit.files.rinex.observation.RinexObservationWriter
Simple constructor.
RinexUtils - Class in org.orekit.files.rinex.utils.parsing
Utilities for RINEX various messages files.
ROCKET_BODY - org.orekit.files.ccsds.ndm.odm.ocm.ObjectType
Rocket body.
ROOT - Static variable in class org.orekit.files.ccsds.ndm.adm.acm.Acm
Root element for XML messages.
ROOT - Static variable in class org.orekit.files.ccsds.ndm.adm.aem.Aem
Root element for XML files.
ROOT - Static variable in class org.orekit.files.ccsds.ndm.adm.apm.Apm
Root element for XML files.
ROOT - Static variable in class org.orekit.files.ccsds.ndm.cdm.Cdm
Root element for XML files.
ROOT - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.Ocm
Root element for XML messages.
ROOT - Static variable in class org.orekit.files.ccsds.ndm.odm.oem.Oem
Root element for XML files.
ROOT - Static variable in class org.orekit.files.ccsds.ndm.odm.omm.Omm
Root element for XML files.
ROOT - Static variable in class org.orekit.files.ccsds.ndm.odm.opm.Opm
Root element for XML files.
ROOT - Static variable in class org.orekit.files.ccsds.ndm.tdm.Tdm
Root element for XML files.
ROOT22 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
ROOT22.
ROOT32 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
ROOT32.
ROOT44 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
ROOT44.
ROOT52 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
ROOT52.
ROOT54 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
ROOT54.
rotationAngles - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Rotation angles sub-sub-section (only for ADM V1).
rotationAngles - org.orekit.files.ccsds.ndm.adm.apm.EulerKey
Rotation angles wrapping element in XML files (ADM V1 only).
rotationFromInertial(Field<T>, FieldAbsoluteDate<T>, FieldPVCoordinates<T>) - Method in interface org.orekit.frames.encounter.EncounterLOF
Get the rotation from inertial frame to local orbital frame.
rotationFromInertial(Field<T>, FieldAbsoluteDate<T>, FieldPVCoordinates<T>) - Method in class org.orekit.frames.LocalMagneticFieldFrame
Get the rotation from inertial frame to local orbital frame.
rotationFromInertial(Field<T>, FieldAbsoluteDate<T>, FieldPVCoordinates<T>) - Method in interface org.orekit.frames.LOF
Get the rotation from inertial frame to local orbital frame.
rotationFromInertial(Field<T>, FieldAbsoluteDate<T>, FieldPVCoordinates<T>) - Method in enum org.orekit.frames.LOFType
Get the rotation from inertial frame to local orbital frame.
rotationFromInertial(Field<T>, FieldPVCoordinates<T>) - Method in class org.orekit.frames.encounter.AbstractEncounterLOF
Get the rotation from inertial to this encounter local orbital frame.
rotationFromInertial(Field<T>, FieldPVCoordinates<T>) - Method in interface org.orekit.frames.encounter.EncounterLOF
Get the rotation from inertial to this encounter local orbital frame.
rotationFromInertial(Field<T>, FieldPVCoordinates<T>) - Method in enum org.orekit.frames.LOFType
Get the rotation from inertial frame to local orbital frame.
rotationFromInertial(Field<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>) - Method in class org.orekit.frames.encounter.DefaultEncounterLOF
Get the rotation from inertial to this encounter local orbital frame.
rotationFromInertial(Field<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>) - Method in interface org.orekit.frames.encounter.EncounterLOF
Get the rotation from inertial to this encounter local orbital frame.
rotationFromInertial(Field<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>) - Method in class org.orekit.frames.encounter.ValsecchiEncounterFrame
Get the rotation from inertial to this encounter local orbital frame.
rotationFromInertial(AbsoluteDate, PVCoordinates) - Method in interface org.orekit.frames.encounter.EncounterLOF
Get the rotation from inertial frame to local orbital frame.
rotationFromInertial(AbsoluteDate, PVCoordinates) - Method in class org.orekit.frames.LocalMagneticFieldFrame
Get the rotation from inertial frame to local orbital frame.
rotationFromInertial(AbsoluteDate, PVCoordinates) - Method in interface org.orekit.frames.LOF
Get the rotation from inertial frame to local orbital frame.
rotationFromInertial(AbsoluteDate, PVCoordinates) - Method in enum org.orekit.frames.LOFType
Get the rotation from inertial frame to local orbital frame.
rotationFromInertial(PVCoordinates) - Method in class org.orekit.frames.encounter.AbstractEncounterLOF
Get the rotation from inertial to this encounter local orbital frame.
rotationFromInertial(PVCoordinates) - Method in interface org.orekit.frames.encounter.EncounterLOF
Get the rotation from inertial to this encounter local orbital frame.
rotationFromInertial(PVCoordinates) - Method in enum org.orekit.frames.LOFType
Get the rotation from inertial frame to local orbital frame.
rotationFromInertial(PVCoordinates, PVCoordinates) - Method in class org.orekit.frames.encounter.DefaultEncounterLOF
Get the rotation from inertial to this encounter local orbital frame.
rotationFromInertial(PVCoordinates, PVCoordinates) - Method in interface org.orekit.frames.encounter.EncounterLOF
Get the rotation from inertial to this encounter local orbital frame.
rotationFromInertial(PVCoordinates, PVCoordinates) - Method in class org.orekit.frames.encounter.ValsecchiEncounterFrame
Get the rotation from inertial to this encounter local orbital frame.
rotationFromLOF(Field<T>, LOF, FieldAbsoluteDate<T>, FieldPVCoordinates<T>) - Method in interface org.orekit.frames.LOF
Get the rotation from input local orbital frame to the instance.
rotationFromLOF(Field<T>, LOFType, FieldPVCoordinates<T>) - Method in enum org.orekit.frames.LOFType
Get the rotation from input local orbital frame to the instance.
rotationFromLOF(LOF, AbsoluteDate, PVCoordinates) - Method in interface org.orekit.frames.LOF
Get the rotation from input local orbital frame to the instance.
rotationFromLOF(LOFType, PVCoordinates) - Method in enum org.orekit.frames.LOFType
Get the rotation from input local orbital frame to the instance.
rotationFromLOFInToLOFOut(Field<T>, LOF, LOF, FieldAbsoluteDate<T>, FieldPVCoordinates<T>) - Static method in interface org.orekit.frames.LOF
Get the rotation from input to output local orbital frame.
rotationFromLOFInToLOFOut(LOF, LOF, AbsoluteDate, PVCoordinates) - Static method in interface org.orekit.frames.LOF
Get the rotation from input to output local orbital frame.
rotationRates - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Rotation rates sub-sub-section (only for ADM V1).
rotationRates - org.orekit.files.ccsds.ndm.adm.apm.EulerKey
Rotation rates wrapping element in XML files (ADM V1 only).
rotationShiftedBy(double) - Method in class org.orekit.utils.AngularCoordinates
Get a time-shifted rotation.
rotationShiftedBy(T) - Method in class org.orekit.utils.FieldAngularCoordinates
Get a time-shifted rotation.
RotationXmlTokenBuilder - Class in org.orekit.files.ccsds.ndm.adm
Builder for rotation angles and rates.
RotationXmlTokenBuilder() - Constructor for class org.orekit.files.ccsds.ndm.adm.RotationXmlTokenBuilder
Simple constructor.
roundIfNeeded(int, int) - Method in class org.orekit.time.DateTimeComponents
Round this date-time to the given precision if needed to prevent rounding up to an invalid seconds number.
ROW_DIM - Static variable in class org.orekit.propagation.AbstractStateCovarianceInterpolator
Default row dimension for position-velocity state covariance.
RSW - org.orekit.files.ccsds.definitions.OrbitRelativeFrame
Another name for Radial, Transverse (along-track) and Normal.
RSW_INERTIAL - org.orekit.files.ccsds.definitions.OrbitRelativeFrame
Another name for Radial, Transverse (along-track) and Normal (X towards zenith, Z towards momentum).
RSW_ROTATING - org.orekit.files.ccsds.definitions.OrbitRelativeFrame
Another name for Radial, Transverse (along-track) and Normal (X towards zenith, Z towards momentum).
RTCA - org.orekit.gnss.metric.ntrip.DataFormat
RTCA.
RTCM - org.orekit.gnss.metric.ntrip.Type
RTCM.
RTCM_1019 - org.orekit.gnss.metric.parser.RtcmMessageType
GPS Ephemeris message.
RTCM_1020 - org.orekit.gnss.metric.parser.RtcmMessageType
GLONASS Ephemeris message.
RTCM_1042 - org.orekit.gnss.metric.parser.RtcmMessageType
Beidou Ephemeris message.
RTCM_1044 - org.orekit.gnss.metric.parser.RtcmMessageType
QZSS Ephemeris message.
RTCM_1045 - org.orekit.gnss.metric.parser.RtcmMessageType
Galileo F/NAV Ephemeris message.
RTCM_1057 - org.orekit.gnss.metric.parser.RtcmMessageType
GPS Orbit Correction.
RTCM_1058 - org.orekit.gnss.metric.parser.RtcmMessageType
GPS Clock Correction.
RTCM_1060 - org.orekit.gnss.metric.parser.RtcmMessageType
GPS Combined Orbit and Clock Correction.
RTCM_1063 - org.orekit.gnss.metric.parser.RtcmMessageType
GLONASS Orbit Correction.
RTCM_1064 - org.orekit.gnss.metric.parser.RtcmMessageType
GLONASS Clock Correction.
RTCM_1066 - org.orekit.gnss.metric.parser.RtcmMessageType
GLONASS Combined Orbit and Clock Correction.
RTCM_1240 - org.orekit.gnss.metric.parser.RtcmMessageType
Galileo Orbit Correction Message.
RTCM_1241 - org.orekit.gnss.metric.parser.RtcmMessageType
Galileo Clock Correction Message.
RTCM_1243 - org.orekit.gnss.metric.parser.RtcmMessageType
Galileo Combined Orbit and Clock Correction Message.
RTCM_2 - org.orekit.gnss.metric.ntrip.DataFormat
RTCM 2.x.
RTCM_3 - org.orekit.gnss.metric.ntrip.DataFormat
RTCM 3.x.
RTCM_SAPOS - org.orekit.gnss.metric.ntrip.DataFormat
RTCM SAPOS.
Rtcm1019 - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris
RTCM 1019 message: GPS Satellite Ephemeris Data.
Rtcm1019(int, Rtcm1019Data) - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019
Constructor.
Rtcm1019Data - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris
Container for RTCM 1019 data.
Rtcm1019Data() - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data
Constructor.
Rtcm1020 - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris
RTCM 1020 message: Glonass Satellite Ephemeris Data.
Rtcm1020(int, Rtcm1020Data) - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020
Constructor.
Rtcm1020Data - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris
Container for RTCM 1020 data.
Rtcm1020Data() - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Constructor.
Rtcm1042 - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris
RTCM 1042 message: Beidou Satellite Ephemeris Data.
Rtcm1042(int, Rtcm1042Data) - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1042
Constructor.
Rtcm1042Data - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris
Container for RTCM 1042 data.
Rtcm1042Data() - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1042Data
Constructor.
Rtcm1044 - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris
RTCM 1044 message: QZSS Satellite Ephemeris Data.
Rtcm1044(int, Rtcm1044Data) - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044
Constructor.
Rtcm1044Data - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris
Container for RTCM 1044 data.
Rtcm1044Data() - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data
Constructor.
Rtcm1045 - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris
RTCM 1045 message: Galileo F/NAV Satellite Ephemeris Data.
Rtcm1045(int, Rtcm1045Data) - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1045
Constructor.
Rtcm1045Data - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris
Container for RTCM 1045 data.
Rtcm1045Data() - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1045Data
Constructor.
Rtcm1057 - Class in org.orekit.gnss.metric.messages.rtcm.correction
RTCM 1057 message: GPS Orbit Correction Message.
Rtcm1057(int, RtcmOrbitCorrectionHeader, List<RtcmOrbitCorrectionData>) - Constructor for class org.orekit.gnss.metric.messages.rtcm.correction.Rtcm1057
Constructor.
Rtcm1058 - Class in org.orekit.gnss.metric.messages.rtcm.correction
RTCM 1057 message: GPS Clock Correction Message.
Rtcm1058(int, RtcmCorrectionHeader, List<RtcmClockCorrectionData>) - Constructor for class org.orekit.gnss.metric.messages.rtcm.correction.Rtcm1058
Constructor.
Rtcm1060 - Class in org.orekit.gnss.metric.messages.rtcm.correction
RTCM 1060 message: GPS Combined Orbit and Clock Correction Message.
Rtcm1060(int, RtcmOrbitCorrectionHeader, List<RtcmCombinedCorrectionData>) - Constructor for class org.orekit.gnss.metric.messages.rtcm.correction.Rtcm1060
Constructor.
Rtcm1063 - Class in org.orekit.gnss.metric.messages.rtcm.correction
RTCM 1063 message: GLONASS Orbit Correction Message.
Rtcm1063(int, RtcmOrbitCorrectionHeader, List<RtcmOrbitCorrectionData>) - Constructor for class org.orekit.gnss.metric.messages.rtcm.correction.Rtcm1063
Constructor.
Rtcm1064 - Class in org.orekit.gnss.metric.messages.rtcm.correction
RTCM 1064 message: GLONASS Clock Correction Message.
Rtcm1064(int, RtcmCorrectionHeader, List<RtcmClockCorrectionData>) - Constructor for class org.orekit.gnss.metric.messages.rtcm.correction.Rtcm1064
Constructor.
Rtcm1066 - Class in org.orekit.gnss.metric.messages.rtcm.correction
RTCM 1066 message: GLONASS Combined Orbit and Clock Correction Message.
Rtcm1066(int, RtcmOrbitCorrectionHeader, List<RtcmCombinedCorrectionData>) - Constructor for class org.orekit.gnss.metric.messages.rtcm.correction.Rtcm1066
Constructor.
Rtcm1240 - Class in org.orekit.gnss.metric.messages.rtcm.correction
RTCM 1240 message: Galileo Orbit Correction Message.
Rtcm1240(int, RtcmOrbitCorrectionHeader, List<RtcmOrbitCorrectionData>) - Constructor for class org.orekit.gnss.metric.messages.rtcm.correction.Rtcm1240
Constructor.
Rtcm1241 - Class in org.orekit.gnss.metric.messages.rtcm.correction
RTCM 1241 message: Galileo Clock Correction Message.
Rtcm1241(int, RtcmCorrectionHeader, List<RtcmClockCorrectionData>) - Constructor for class org.orekit.gnss.metric.messages.rtcm.correction.Rtcm1241
Constructor.
Rtcm1243 - Class in org.orekit.gnss.metric.messages.rtcm.correction
RTCM 1242 message: Combined Galileo Clock Correction Message.
Rtcm1243(int, RtcmOrbitCorrectionHeader, List<RtcmCombinedCorrectionData>) - Constructor for class org.orekit.gnss.metric.messages.rtcm.correction.Rtcm1243
Constructor.
RtcmClockCorrectionData - Class in org.orekit.gnss.metric.messages.rtcm.correction
Container for common data in RTCM clock correction message type.
RtcmClockCorrectionData() - Constructor for class org.orekit.gnss.metric.messages.rtcm.correction.RtcmClockCorrectionData
Constructor.
RtcmCombinedCorrectionData - Class in org.orekit.gnss.metric.messages.rtcm.correction
Container for common data in RTCM combined corrections message type.
RtcmCombinedCorrectionData() - Constructor for class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCombinedCorrectionData
Constructor.
RtcmCorrectionData - Class in org.orekit.gnss.metric.messages.rtcm.correction
Container for common data in RTCM corrections message type.
RtcmCorrectionData() - Constructor for class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionData
Constructor.
RtcmCorrectionHeader - Class in org.orekit.gnss.metric.messages.rtcm.correction
Container for common data in RTCM Correction Message type header.
RtcmCorrectionHeader() - Constructor for class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionHeader
Constructor.
RtcmCorrectionMessage<H extends RtcmCorrectionHeader,​D extends RtcmCorrectionData> - Class in org.orekit.gnss.metric.messages.rtcm.correction
The RTCM Correction Message types provide elements to calculate GNSS satellite corrections.
RtcmCorrectionMessage(int, SatelliteSystem, H, List<D>) - Constructor for class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionMessage
Constructor.
RtcmData - Class in org.orekit.gnss.metric.messages.rtcm
Container for common data in RTCM message.
RtcmData() - Constructor for class org.orekit.gnss.metric.messages.rtcm.RtcmData
Empty constructor.
RtcmDataField - Enum in org.orekit.gnss.metric.parser
Enum containing all intermediate level data fields that can be parsed to build a RTCM message.
RtcmEphemerisData - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris
Container for common data in RTCM ephemeris message type.
RtcmEphemerisData() - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.RtcmEphemerisData
Constructor.
RtcmEphemerisMessage<D extends RtcmEphemerisData> - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris
Base class for RTCM ephemeris messages.
RtcmEphemerisMessage(int, D) - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.RtcmEphemerisMessage
Constructor.
RtcmMessage<D extends RtcmData> - Class in org.orekit.gnss.metric.messages.rtcm
Base class for RTCM messages.
RtcmMessage(int, List<D>) - Constructor for class org.orekit.gnss.metric.messages.rtcm.RtcmMessage
Constructor.
RtcmMessagesParser - Class in org.orekit.gnss.metric.parser
Parser for RTCM encoded messages.
RtcmMessagesParser(List<Integer>) - Constructor for class org.orekit.gnss.metric.parser.RtcmMessagesParser
Constructor.
RtcmMessageType - Enum in org.orekit.gnss.metric.parser
Enum containing the supported RTCM messages types.
RtcmOrbitCorrectionData - Class in org.orekit.gnss.metric.messages.rtcm.correction
Container for common data in RTCM orbit correction message type.
RtcmOrbitCorrectionData() - Constructor for class org.orekit.gnss.metric.messages.rtcm.correction.RtcmOrbitCorrectionData
Constructor.
RtcmOrbitCorrectionHeader - Class in org.orekit.gnss.metric.messages.rtcm.correction
Container for common data in RTCM Orbit Correction Message type header.
RtcmOrbitCorrectionHeader() - Constructor for class org.orekit.gnss.metric.messages.rtcm.correction.RtcmOrbitCorrectionHeader
Constructor.
RTN - org.orekit.files.ccsds.definitions.OrbitRelativeFrame
Radial, Transverse (along-track) and Normal (X towards zenith, Z towards momentum).
RTN - org.orekit.files.ccsds.ndm.cdm.ScreenVolumeFrame
Radial Transverse Normal frame.
RTNCovariance - Class in org.orekit.files.ccsds.ndm.cdm
Container for RTN covariance matrix data.
RTNCovariance() - Constructor for class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Simple constructor.
RTNCovarianceKey - Enum in org.orekit.files.ccsds.ndm.cdm
Keys for CDM covariance matrix entries.
RTNCovarianceWriter - Class in org.orekit.files.ccsds.ndm.cdm
Writer for RTN covariance matrix data block for CCSDS Conjunction Data Messages.
RU - org.orekit.files.ccsds.ndm.tdm.RangeUnits
Range in "Range Units" with changing frequency.
run() - Method in class org.orekit.gnss.metric.ntrip.StreamMonitor
ruToMeters(TdmMetadata, AbsoluteDate, double) - Method in class org.orekit.files.ccsds.ndm.tdm.IdentityConverter
Convert a range expressed in Range Units.
ruToMeters(TdmMetadata, AbsoluteDate, double) - Method in interface org.orekit.files.ccsds.ndm.tdm.RangeUnitsConverter
Convert a range expressed in Range Units.
RW - org.orekit.files.ccsds.definitions.SpacecraftBodyFrame.BaseEquipment
Reaction Wheel.

S

s - org.orekit.files.ccsds.ndm.tdm.RangeUnits
Range in seconds.
S - org.orekit.gnss.SignalCode
GPS L1C (D), L2C (M) / QZSS L1C (D), L2C (M) and S codes.
S - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
S.
S_2FASX4 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
S_2FASX4.
S_3FASX6 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
S_3FASX6.
S_FASX2 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
S_FASX2.
S_G22 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
S_G22.
S_G32 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
S_G32.
S_G44 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
S_G44.
S_G52 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
S_G52.
S_G54 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
S_G54.
S0 - org.orekit.gnss.ObservationType
Signal-strength for Rinex3.
S01 - org.orekit.gnss.Frequency
SBAS L1 (1575.42 MHz).
S05 - org.orekit.gnss.Frequency
SBAS L5 (1176.45 MHz).
S1 - org.orekit.gnss.ObservationType
Doppler GPS L1 / GLONASS G1 / Galileo E2-L1-E1 / SBAS L1 for Rinex2.
S1A - org.orekit.gnss.ObservationType
Signal-strength Galileo E1 A / Beidou B1 B1A for Rinex3.
S1B - org.orekit.gnss.ObservationType
Signal-strength Galileo E1 I/NAV OS/CS/SoL / QZSS geo signal for Rinex3.
S1C - org.orekit.gnss.ObservationType
Signal-strength GPS L1 C/A / GLONASS G1 C/A / Galileo E1 C / SBAS L1 C/A / QZSS L1 C/A for Rinex3.
S1D - org.orekit.gnss.ObservationType
Signal-strength Beidou B1 Data for Rinex3.
S1E - org.orekit.gnss.ObservationType
Signal-strength QZSS L1 C/B for Rinex3.
S1I - org.orekit.gnss.ObservationType
Signal-strength Beidou B1 I for Rinex3.
S1L - org.orekit.gnss.ObservationType
Signal-strength GPS L1 L1C(P) / QZSS L1 L1C(P) for Rinex3, Beidou B1A for Rinex3.03.
S1M - org.orekit.gnss.ObservationType
Signal-strength GPS L2 M for Rinex3.
S1N - org.orekit.gnss.ObservationType
Signal-strength GPS L1 codeless / Beidou B1 codeless for Rinex3.
S1P - org.orekit.gnss.ObservationType
Signal-strength GPS L2 P(AS off) / GLONASS G2 P / Beidou B1 Pilot for Rinex3.
S1S - org.orekit.gnss.ObservationType
Signal-strength GPS L1 L1C(D) / QZSS L1 L1C(D) for Rinex3, Beidou B1A for Rinex3.03.
S1W - org.orekit.gnss.ObservationType
Signal-strength GPS L1 Z-tracking and similar (AS on) for Rinex3.
S1X - org.orekit.gnss.ObservationType
Signal-strength GPS L1 L1C (D+P) / Galileo E1 B+C / QZSS L1 L1C(D+P) / Beidou B1 Data+Pilot for Rinex3.
S1Y - org.orekit.gnss.ObservationType
Signal-strength GPS L1 Y for Rinex3.
S1Z - org.orekit.gnss.ObservationType
Signal-strength Galileo E1 C1Z A+B+C / QZSS L1 L1-SAIF for Rinex3, Beidou B1A for Rinex3.03.
S2 - org.orekit.gnss.ObservationType
Signal Strength GPS L2 / GLONASS G2 / Beidou B02 for Rinex2.
S2 - Static variable in class org.orekit.models.earth.displacement.Tide
S₂ tide.
S2C - org.orekit.gnss.ObservationType
Signal-strength GPS L2 C/A / GLONASS G2 C/A for Rinex3.
S2D - org.orekit.gnss.ObservationType
Signal-strength GPS L1(C/A)+(P2-P1) (semi-codeless) for Rinex3.
S2I - org.orekit.gnss.ObservationType
Signal-strength Beidou B1 I for Rinex3.03.
S2L - org.orekit.gnss.ObservationType
Signal-strength GPS L2 L2C(L) / QZSS L2 L2C(2) for Rinex3.
S2M - org.orekit.gnss.ObservationType
Signal-strength GPS L2 M for Rinex3.
S2N - org.orekit.gnss.ObservationType
Signal-strength GPS L2 codeless for Rinex3.
S2P - org.orekit.gnss.ObservationType
Signal-strength GPS L2 P(AS off) / GLONASS G2 P for Rinex3.
S2Q - org.orekit.gnss.ObservationType
Signal-strength Beidou B1 Q for Rinex3.03.
S2S - org.orekit.gnss.ObservationType
Signal-strength GPS L2 L2C(M) / QZSS L2 L2C(M) for Rinex3.
S2W - org.orekit.gnss.ObservationType
Signal-strength GPS L2 Z-tracking and similar (AS on) for Rinex3.
S2X - org.orekit.gnss.ObservationType
Signal-strength GPS L2 L2C (M+L) / QZSS L2 L2C(M+L) for Rinex3, Beidou B1 I+Q for Rinex3.03.
S2Y - org.orekit.gnss.ObservationType
Signal-strength GPS L2 Y for Rinex3.
S3I - org.orekit.gnss.ObservationType
Signal-strength GLONASS G3 I for Rinex3.
S3Q - org.orekit.gnss.ObservationType
Signal-strength GLONASS G3 Q for Rinex3.
S3X - org.orekit.gnss.ObservationType
Signal-strength GLONASS G3 I+Q for Rinex3.
s4 - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
s* new value for the contant s.
s4 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
s* new value for the contant s.
S4A - org.orekit.gnss.ObservationType
Signal-strength GLONASS G1a L1OCd for Rinex3.
S4B - org.orekit.gnss.ObservationType
Signal-strength GLONASS G1a L1OCp for Rinex3.
S4X - org.orekit.gnss.ObservationType
Signal-strength GLONASS G1a L1OCd+L1OCd for Rinex3.
S5 - org.orekit.gnss.ObservationType
Signal Strength GPS L5 / Galileo E5a / SBAS L5 for Rinex2.
S5A - org.orekit.gnss.ObservationType
Signal-strength IRNSS L5 A for Rinex3.
S5B - org.orekit.gnss.ObservationType
Signal-strength IRNSS L5 B for Rinex3.
S5C - org.orekit.gnss.ObservationType
Signal-strength IRNSS L5 C for Rinex3.
S5D - org.orekit.gnss.ObservationType
Signal-strength QZSS L5 D / Beidou B2a Data for Rinex3.
S5I - org.orekit.gnss.ObservationType
Signal-strength GPS L5 I/ Galileo E5a F/NAV OS / SBAS L5 I / QZSS L5 I for Rinex3.
S5P - org.orekit.gnss.ObservationType
Signal-strength QZSS L5 P / Beidou B2a Pilot for Rinex3.
S5Q - org.orekit.gnss.ObservationType
Signal-strength GPS L5 Q/ Galileo E5a Q / SBAS L5 Q / QZSS L5 Q for Rinex3.
S5X - org.orekit.gnss.ObservationType
Signal-strength GPS L5 I+Q/ Galileo E5a I+Q / SBAS L5 I+Q / QZSS L5 I+Q / IRNSS L5 B+C / Beidou B2a Data+Pilot for Rinex3.
S5Z - org.orekit.gnss.ObservationType
Signal-strength QZSS L5 D+P for Rinex3.
S6 - org.orekit.gnss.ObservationType
Signal Strength Galileo E6 / Beidou B03 for Rinex2.
S6A - org.orekit.gnss.ObservationType
Signal-strength Galileo E6 A PRS / GLONASS G2a L2CSI/ Beidou B3A for Rinex3.
S6B - org.orekit.gnss.ObservationType
Signal-strength Galileo E6 B C/NAV CS / GLONASS G2a L2OCp for Rinex3.
S6C - org.orekit.gnss.ObservationType
Signal-strength Galileo E6 C no data for Rinex3.
S6D - org.orekit.gnss.ObservationType
Signal-strength Beidou B3A for Rinex3.
S6E - org.orekit.gnss.ObservationType
Signal-strength QZSS L6E for Rinex3.
S6I - org.orekit.gnss.ObservationType
Signal-strength Beidou B3 I for Rinex3.
S6L - org.orekit.gnss.ObservationType
Signal-strength QZSS LEX(6) L for Rinex3.
S6P - org.orekit.gnss.ObservationType
Signal-strength Beidou B3A for Rinex3.
S6Q - org.orekit.gnss.ObservationType
Signal-strength Beidou B3 Q for Rinex3.
S6S - org.orekit.gnss.ObservationType
Signal-strength QZSS LEX(6) S for Rinex3.
S6X - org.orekit.gnss.ObservationType
Signal-strength Galileo E6 B+C / QZSS LEX(6) S+L / Beidou B3 I+Q / GLONASS G2a L2CSI+L2OCp for Rinex3.
S6Z - org.orekit.gnss.ObservationType
Signal-strength Galileo E6 A+B+C / QZSS L6(D+E) / Beidou B3A for Rinex3.
S7 - org.orekit.gnss.ObservationType
Signal Strength Galileo E5b / Beidou B02 for Rinex2.
S7D - org.orekit.gnss.ObservationType
Signal-strength Beidou B2b Data for Rinex3.
S7I - org.orekit.gnss.ObservationType
Signal-strength Galileo E5b I I/NAV OS/CS/SoL / Beidou B2 I for Rinex3.
S7P - org.orekit.gnss.ObservationType
Signal-strength Beidou B2b Pilot for Rinex3.
S7Q - org.orekit.gnss.ObservationType
Signal-strength Galileo Q no data / Beidou B2 Q for Rinex3.
S7X - org.orekit.gnss.ObservationType
Signal-strength Galileo E5b I+Q / Beidou B2 I+Q for Rinex3.
S7Z - org.orekit.gnss.ObservationType
Signal-strength Beidou B2b Data+Pilot for Rinex3.
S8 - org.orekit.gnss.ObservationType
Signal Strength Galileo E5a+b for Rinex2.
S8D - org.orekit.gnss.ObservationType
Signal-strength Beidou B2(B2a+B2b) Data for Rinex3.
S8I - org.orekit.gnss.ObservationType
Signal-strength Galileo E5(E5a+E5b) I for Rinex3.
S8P - org.orekit.gnss.ObservationType
Signal-strength Beidou B2(B2a+B2b) Pilot for Rinex3.
S8Q - org.orekit.gnss.ObservationType
Signal-strength Galileo E5(E5a+E5b) for Rinex3.
S8X - org.orekit.gnss.ObservationType
Signal-strength Galileo E5(E5a+E5b) I+Q / Beidou B2(B2a+B2b) Data+Pilot for Rinex3.
S9A - org.orekit.gnss.ObservationType
Signal-strength IRNSS S A for Rinex3.
S9B - org.orekit.gnss.ObservationType
Signal-strength IRNSS S B for Rinex3.
S9C - org.orekit.gnss.ObservationType
Signal-strength IRNSS S C for Rinex3.
S9X - org.orekit.gnss.ObservationType
Signal-strength IRNSS S B+C for Rinex3.
SA - org.orekit.files.ccsds.definitions.SpacecraftBodyFrame.BaseEquipment
Solar Array.
SA - org.orekit.gnss.ObservationType
Signal-strength GPS L1 C/A / GLONASS G1 C/A for Rinex2.
SaastamoinenModel - Class in org.orekit.models.earth.troposphere
Deprecated.
as of 12.1, replaced by ModifiedSaastamoinenModel
SaastamoinenModel(double, double, double) - Constructor for class org.orekit.models.earth.troposphere.SaastamoinenModel
Deprecated.
Create a new Saastamoinen model for the troposphere using the given environmental conditions and table from the reference book.
SaastamoinenModel(double, double, double, String) - Constructor for class org.orekit.models.earth.troposphere.SaastamoinenModel
Deprecated.
Create a new Saastamoinen model for the troposphere using the given environmental conditions.
SaastamoinenModel(double, double, double, String, DataProvidersManager) - Constructor for class org.orekit.models.earth.troposphere.SaastamoinenModel
Deprecated.
Create a new Saastamoinen model for the troposphere using the given environmental conditions.
SACCSA - org.orekit.files.rinex.navigation.SbasId
Soluciόn de Aumentaciόn para Caribe, Centro y Sudamérica.
sameDimension(Unit) - Method in class org.orekit.utils.units.Unit
Check if a unit has the same dimension as another unit.
sameDimensionSI() - Method in class org.orekit.utils.units.Unit
Create the SI unit with same dimension.
sample(SphericalPolygonsSet, double, double) - Method in class org.orekit.models.earth.tessellation.EllipsoidTessellator
Sample a zone of interest into a grid sample of geodetic points.
SAMPLED_ENGIEERING - org.orekit.files.ilrs.CRDHeader.DataType
Sampled engineering.
SampledClockModel - Class in org.orekit.time
Offset clock model backed up by a sample.
SampledClockModel(List<ClockOffset>, int) - Constructor for class org.orekit.time.SampledClockModel
Simple constructor.
SAPOS_ADV - org.orekit.gnss.metric.ntrip.DataFormat
SAPOS-AdV.
SATELLITE_COLLIDED_WITH_TARGET - org.orekit.errors.OrekitMessages
SATELLITE_COLLIDED_WITH_TARGET.
SATELLITE_LASER_RANGING - org.orekit.files.sp3.DataUsed
Satellite Laser Ranging.
SatelliteAntenna - Class in org.orekit.gnss.antenna
GNSS satellite antenna model.
SatelliteAntenna(String, String, Map<Frequency, FrequencyPattern>, SatelliteSystem, int, SatelliteType, int, String, AbsoluteDate, AbsoluteDate) - Constructor for class org.orekit.gnss.antenna.SatelliteAntenna
Simple constructor.
SatelliteClockScale - Class in org.orekit.time
Scale for on-board clock.
SatelliteClockScale(String, AbsoluteDate, TimeScale, double, double) - Constructor for class org.orekit.time.SatelliteClockScale
Create a linear model for satellite clock.
SatelliteSystem - Enum in org.orekit.gnss
Enumerate for satellite system.
SatelliteType - Enum in org.orekit.gnss.antenna
Enumerate for satellite types.
SatInSystem - Class in org.orekit.gnss
Container for satellite system and PRN.
SatInSystem(SatelliteSystem, int) - Constructor for class org.orekit.gnss.SatInSystem
Simple constructor.
SATURN - org.orekit.bodies.JPLEphemeridesLoader.EphemerisType
Constant for Saturn.
SATURN - org.orekit.files.ccsds.definitions.CenterName
Saturn body.
SATURN - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Saturn.
SB - org.orekit.gnss.ObservationType
Signal-strength GPS L1C for Rinex2.
SBAS - org.orekit.files.sp3.SP3FileType
SBAS only file.
SBAS - org.orekit.gnss.metric.ntrip.NavigationSystem
SBAS.
SBAS - org.orekit.gnss.SatelliteSystem
SBAS system.
SBAS - org.orekit.gnss.TimeSystem
SBAS.
SBAS_MU - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
WGS 84 value of the Earth's universal gravitational parameter for SBAS user in m³/s².
SbasId - Enum in org.orekit.files.rinex.navigation
Enumerate for the SBAS ids.
SBASNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data
Container for data contained in a SBAS navigation message.
SBASNavigationMessage() - Constructor for class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage
Constructor.
SBASOrbitalElements - Interface in org.orekit.propagation.analytical.gnss.data
This interface provides the minimal set of orbital elements needed by the SBASPropagator.
SBASPropagator - Class in org.orekit.propagation.analytical.gnss
This class aims at propagating a SBAS orbit from SBASOrbitalElements.
SBASPropagatorBuilder - Class in org.orekit.propagation.analytical.gnss
This nested class aims at building a SBASPropagator.
SBASPropagatorBuilder(SBASOrbitalElements) - Constructor for class org.orekit.propagation.analytical.gnss.SBASPropagatorBuilder
Initializes the builder.
SBASPropagatorBuilder(SBASOrbitalElements, Frames) - Constructor for class org.orekit.propagation.analytical.gnss.SBASPropagatorBuilder
Initializes the builder.
SC - org.orekit.gnss.ObservationType
Signal-strength GPS L2C for Rinex2.
SC_BODY - org.orekit.files.ccsds.definitions.SpacecraftBodyFrame.BaseEquipment
Spacecraft Body.
scale(double, Orbit) - Method in enum org.orekit.orbits.OrbitType
Compute scaling factor for parameters drivers.
scale(String, double) - Method in class org.orekit.utils.units.Unit
Scale a unit.
SCALE_DEFAULT - Static variable in class org.orekit.propagation.analytical.tle.generation.FixedPointTleGenerationAlgorithm
Default value for scale.
scaleChanged(double, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver
Notify that a parameter scale has been changed.
ScaledConstantThrustPropulsionModel - Class in org.orekit.forces.maneuvers.propulsion
Thrust propulsion model with parameters (for estimation) represented by scale factors on the X, Y and Z axis of the spacecraft frame.
ScaledConstantThrustPropulsionModel(double, double, Vector3D, String) - Constructor for class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel
Constructor with min/max deviation for the scale factors.
scaledIncrement(double, DoubleArrayDictionary.Entry) - Method in class org.orekit.utils.DoubleArrayDictionary.Entry
Increment the value with another scaled entry.
scaledIncrement(double, FieldArrayDictionary.Entry) - Method in class org.orekit.utils.FieldArrayDictionary.Entry
Increment the value with another scaled entry.
scaledIncrement(T, FieldArrayDictionary.Entry) - Method in class org.orekit.utils.FieldArrayDictionary.Entry
Increment the value with another scaled entry.
ScaleFactorCorrection - Class in org.orekit.files.rinex.observation
Scale Factor to be applied.
ScaleFactorCorrection(double, List<ObservationType>) - Constructor for class org.orekit.files.rinex.observation.ScaleFactorCorrection
Simple constructor.
Scheduler<T extends ObservedMeasurement<T>> - Interface in org.orekit.estimation.measurements.generation
Interface for generating measurements sequences.
SCLK - org.orekit.files.ccsds.definitions.TimeSystem
Spacecraft Clock.
SCLK_OFFSET_AT_EPOCH - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Spacecraft clock count at OcmMetadataKey.EPOCH_TZERO.
SCLK_SEC_PER_SI_SEC - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Number of clock seconds occurring during one SI second.
SCREEN_ENTRY_TIME - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
The time in UTC when Object2 enters the screening volume.
SCREEN_EXIT_TIME - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
The time in UTC when Object2 exits the screening volume.
SCREEN_PC_THRESHOLD - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
The collision probability screening threshold used to identify this conjunction.
SCREEN_TYPE - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
The type of screening to be used.
SCREEN_VOLUME_FRAME - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
Name of the Object1 centered reference frame in which the screening volume data are given.
SCREEN_VOLUME_RADIUS - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
The radius of the screening volume.
SCREEN_VOLUME_SHAPE - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
Shape of the screening volume.
SCREEN_VOLUME_X - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
The R or T (depending on if RTN or TVN is selected) component size of the screening volume in the SCREEN_VOLUME_FRAME.
SCREEN_VOLUME_Y - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
The T or V (depending on if RTN or TVN is selected) component size of the screening volume in the SCREEN_VOLUME_FRAME.
SCREEN_VOLUME_Z - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
The N component size of the screening volume in the SCREEN_VOLUME_FRAME.
SCREENING_DATA_SOURCE - org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadataKey
The source (or origin) of the specific orbital data for this object.
ScreenType - Enum in org.orekit.files.ccsds.ndm.cdm
Screening type options allowed in CCSDS Conjunction Data Messages.
ScreenVolumeFrame - Enum in org.orekit.files.ccsds.ndm.cdm
Screening volume frame possibilities used in CCSDS Conjunction Data Messages.
ScreenVolumeShape - Enum in org.orekit.files.ccsds.ndm.cdm
Screening volume shape possibilities used in CCSDS Conjunction Data Messages.
SD - org.orekit.gnss.ObservationType
Signal-strength GLONASS G2 for Rinex2.
SDCM - org.orekit.files.rinex.navigation.SbasId
System for Differential Corrections and Monitoring.
SDP4 - Static variable in class org.orekit.propagation.analytical.tle.FieldTLE
Identifier for SDP4 type of ephemeris.
SDP4 - Static variable in class org.orekit.propagation.analytical.tle.TLE
Identifier for SDP4 type of ephemeris.
SDP8 - Static variable in class org.orekit.propagation.analytical.tle.FieldTLE
Identifier for SDP8 type of ephemeris.
SDP8 - Static variable in class org.orekit.propagation.analytical.tle.TLE
Identifier for SDP8 type of ephemeris.
SECOND - Static variable in class org.orekit.utils.units.Unit
Second unit.
Section - Interface in org.orekit.files.ccsds.section
Top level interface for all CCSDS message sections.
SecularAndHarmonic - Class in org.orekit.utils
Class for fitting evolution of osculating orbital parameters.
SecularAndHarmonic(int, double...) - Constructor for class org.orekit.utils.SecularAndHarmonic
Simple constructor.
SEDR - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
The amount of energy being removed from the object’s orbit by atmospheric drag.
SEDR - org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey
Specific Energy Dissipation Rate.
SEFI_COLLISION_PROBABILITY - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
The space environment fragmentation impact (SEFI) adjusted estimate of collision probability that Object1 and Object2 will collide.
SEFI_COLLISION_PROBABILITY_METHOD - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
The method that was used to calculate the space environment fragmentation impact collision probability.
SEFI_FRAGMENTATION_MODEL - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
The Space environment fragmentation model used.
segment - org.orekit.files.ccsds.ndm.cdm.XmlSubStructureKey
Segment structure.
segment - org.orekit.files.ccsds.section.XmlStructureKey
Segment structure.
Segment<M extends Metadata,​D extends Data> - Class in org.orekit.files.ccsds.section
NDM segments are (Metadata, Data) pairs.
Segment(M, D) - Constructor for class org.orekit.files.ccsds.section.Segment
Constructor.
SegmentWriter() - Constructor for class org.orekit.files.ccsds.ndm.adm.aem.StreamingAemWriter.SegmentWriter
Empty constructor.
SegmentWriter() - Constructor for class org.orekit.files.ccsds.ndm.odm.oem.StreamingOemWriter.SegmentWriter
Empty constructor.
select(DataSource) - Static method in class org.orekit.files.ccsds.utils.lexical.LexicalAnalyzerSelector
Select a LexicalAnalyzer for a DataSource based on content.
select(Unit, Unit) - Method in enum org.orekit.files.ccsds.ndm.ParsedUnitsBehavior
Select the unit to use for interpreting parsed value.
selectDates(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.time.BurstSelector
Select dates within an interval.
selectDates(AbsoluteDate, AbsoluteDate) - Method in interface org.orekit.time.DatesSelector
Select dates within an interval.
selectDates(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.time.FixedStepSelector
Select dates within an interval.
selectExtrapolator(FieldTLE<T>, AttitudeProvider, T, Frame, T[]) - Static method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
Selects the extrapolator to use with the selected TLE.
selectExtrapolator(FieldTLE<T>, AttitudeProvider, T, T[]) - Static method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
Selects the extrapolator to use with the selected TLE.
selectExtrapolator(FieldTLE<T>, Frame, T[]) - Static method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
Selects the extrapolator to use with the selected TLE.
selectExtrapolator(FieldTLE<T>, T[]) - Static method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
Selects the extrapolator to use with the selected TLE.
selectExtrapolator(TLE) - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator
Selects the extrapolator to use with the selected TLE.
selectExtrapolator(TLE, AttitudeProvider, double) - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator
Selects the extrapolator to use with the selected TLE.
selectExtrapolator(TLE, AttitudeProvider, double, Frame) - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator
Selects the extrapolator to use with the selected TLE.
selectExtrapolator(TLE, Frame) - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator
Selects the extrapolator to use with the selected TLE.
selectExtrapolator(TLE, Frame, AttitudeProvider) - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator
Selects the extrapolator to use with the selected TLE.
selectionChanged(boolean, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver
Notify that a parameter selection status has been changed.
selectPredefined(int, int) - Static method in enum org.orekit.frames.HelmertTransformation.Predefined
Select a predefined transform between two years.
selectTransformer(Transformer, double, boolean) - Method in enum org.orekit.propagation.events.FilterType
Get next function transformer in the specified direction.
SEMI_CIRCLE - Static variable in class org.orekit.gnss.metric.parser.Units
Semi-circles units.
SEMI_MAJOR_AXIS - org.orekit.files.ccsds.ndm.odm.KeplerianElementsKey
Orbit semi-major axis.
SemiAnalyticalKalmanEstimator - Class in org.orekit.estimation.sequential
Implementation of an Extended Semi-analytical Kalman Filter (ESKF) to perform orbit determination.
SemiAnalyticalKalmanEstimator(MatrixDecomposer, DSSTPropagatorBuilder, CovarianceMatrixProvider, ParameterDriversList, CovarianceMatrixProvider) - Constructor for class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimator
Kalman filter estimator constructor (package private).
SemiAnalyticalKalmanEstimatorBuilder - Class in org.orekit.estimation.sequential
Builder for a Semi-analytical Kalman Filter.
SemiAnalyticalKalmanEstimatorBuilder() - Constructor for class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimatorBuilder
Default constructor.
SemiAnalyticalKalmanModel - Class in org.orekit.estimation.sequential
Process model to use with a SemiAnalyticalKalmanEstimator.
SemiAnalyticalKalmanModel(DSSTPropagatorBuilder, CovarianceMatrixProvider, ParameterDriversList, CovarianceMatrixProvider) - Constructor for class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Kalman process model constructor (package private).
SemiAnalyticalMeasurementHandler - Class in org.orekit.estimation.sequential
SemiAnalyticalMeasurementHandler(SemiAnalyticalProcess, KalmanFilter<MeasurementDecorator>, List<ObservedMeasurement<?>>, AbsoluteDate) - Constructor for class org.orekit.estimation.sequential.SemiAnalyticalMeasurementHandler
Simple constructor.
SemiAnalyticalMeasurementHandler(SemiAnalyticalProcess, KalmanFilter<MeasurementDecorator>, List<ObservedMeasurement<?>>, AbsoluteDate, boolean) - Constructor for class org.orekit.estimation.sequential.SemiAnalyticalMeasurementHandler
Simple constructor.
SemiAnalyticalProcess - Interface in org.orekit.estimation.sequential
SemiAnalyticalUnscentedKalmanEstimator - Class in org.orekit.estimation.sequential
Implementation of an Unscented Semi-analytical Kalman filter (USKF) to perform orbit determination.
SemiAnalyticalUnscentedKalmanEstimatorBuilder - Class in org.orekit.estimation.sequential
Builder for an Unscented Semi-analytical Kalman filter estimator.
SemiAnalyticalUnscentedKalmanEstimatorBuilder() - Constructor for class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanEstimatorBuilder
Default constructor.
SemiAnalyticalUnscentedKalmanModel - Class in org.orekit.estimation.sequential
Class defining the process model dynamics to use with a SemiAnalyticalUnscentedKalmanEstimator.
SemiAnalyticalUnscentedKalmanModel(DSSTPropagatorBuilder, CovarianceMatrixProvider, ParameterDriversList, CovarianceMatrixProvider) - Constructor for class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel
Unscented Kalman process model constructor (package private).
SEMParser - Class in org.orekit.gnss
This class reads SEM almanac files and provides GPS almanacs.
SEMParser(String) - Constructor for class org.orekit.gnss.SEMParser
Simple constructor.
SEMParser(String, DataProvidersManager, TimeScales) - Constructor for class org.orekit.gnss.SEMParser
Create a SEM loader/parser with the given source of SEM auxiliary data files.
SENSOR - org.orekit.files.ccsds.definitions.SpacecraftBodyFrame.BaseEquipment
Sensor.
SENSOR - org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationKey
Sensor block sub-structure.
SENSOR_FREQUENCY - org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationSensorKey
Frequency of sensor data.
SENSOR_NOISE_STDDEV - org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationSensorKey
Standard deviation of sensor noises.
SENSOR_NUMBER - org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationSensorKey
Sensor number.
SENSOR_USED - org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationSensorKey
Sensor used.
SENSORS - org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey
Description of sensors used.
SENSORS_N - org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey
Number of sensors used.
SEPTEMBER - org.orekit.time.Month
September.
SEQUENTIAL - org.orekit.files.ccsds.ndm.tdm.TrackingMode
Sequential mode, applies to range, Doppler, angles and line-of-sighe ionosphere calibration.
SequentialBatchLSEstimator - Class in org.orekit.estimation.leastsquares
Sequential least squares estimator for orbit determination.
SequentialBatchLSEstimator(SequentialGaussNewtonOptimizer, PropagatorBuilder...) - Constructor for class org.orekit.estimation.leastsquares.SequentialBatchLSEstimator
Simple constructor.
SessionStatistics(String, double, double, double, double, int) - Constructor for class org.orekit.files.ilrs.CRD.SessionStatistics
Constructor.
setA(double) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Set the orbit semi-major axis.
setA(int, double) - Method in class org.orekit.files.ccsds.ndm.odm.StateVector
Set acceleration component.
setA0(double) - Method in class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage
Set the constant term of the offset.
setA1(double) - Method in class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage
set the linear term of the offset.
setA2(double) - Method in class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage
Set the quadratic term of the offset.
setA2b(boolean) - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints
Set rotation direction.
setAcceleration(int, double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Set acceleration component.
setAccelerationDirectionSigma(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Set one σ angular off-nominal acceleration direction.
setAccelerationInterpolation(OnOff) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Set interpolation mode between current and next acceleration line.
setAccelerationMagnitudeSigma(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Set one σ percent error on acceleration magnitude.
setAccuracy(int, double) - Method in class org.orekit.files.sp3.SP3Header
Set the accuracy.
setAccuracyProvider(AccuracyProvider) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.RtcmEphemerisData
Set the accuracy provider of the ephemeris message.
setAcmDataElements(List<AcmElements>) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata
Set the list of elements of information data blocks included in this message.
setActualOdSpan(double) - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters
Set the actual OD time based on the observations available and the RECOMMENDED_OD_SPAN.
setActualOdSpan(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set actual time span used for the OD of the object.
setActuatorUsed(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver
Set actuator used.
setAdditionalParametersBlock(AdditionalParameters) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmData
Set the additional parameters logical block.
setAdmMessageLink(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the Unique identifier of Attitude Data Message linked to this Orbit Data Message.
setAdmMsgLink(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set the unique identifier of Attitude Data Message(s) that are linked (relevant) to this Conjunction Data Message.
setADot(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage
Setter for the change rate in semi-major axis.
setADot(double) - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage
Setter for the change rate in semi-major axis.
setAe(double) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Set the central body reference radius.
setAf0(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Setter for the SV Clock Bias Correction Coefficient (s).
setAf1(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Setter for the SV Clock Drift Correction Coefficient (s/s).
setAf2(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Setter for the Drift Rate Correction Coefficient (s/s²).
setAgency(String) - Method in class org.orekit.files.sp3.SP3Header
Set the agency string for this SP3 file.
setAgencyName(String) - Method in class org.orekit.files.rinex.clock.RinexClock
Setter for the agency name.
setAgencyName(String) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Setter for the agency name.
setAGf0(double) - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage
Setter for the SV clock bias.
setAGf1(double) - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage
Setter for the SV relative frequency.
setAGoM(double) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
Set the SGP4-XP solar radiation pressure-like coefficient Aγ/m.
setAi0(double) - Method in class org.orekit.files.rinex.navigation.IonosphereNequickGMessage
Set aᵢ₀.
setAi1(double) - Method in class org.orekit.files.rinex.navigation.IonosphereNequickGMessage
Set aᵢ₁.
setAi2(double) - Method in class org.orekit.files.rinex.navigation.IonosphereNequickGMessage
Set aᵢ₂.
setAlbedoGridSize(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set albedo grid size.
setAlbedoModel(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set albedo model.
setAlphaI(int, double) - Method in class org.orekit.files.rinex.navigation.IonosphereBDGIMMessage
Set one α coefficient.
setAlphaI(int, double) - Method in class org.orekit.files.rinex.navigation.IonosphereKlobucharMessage
Set one α coefficient.
setAltCovRefFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set the name of the reference frame in which the alternate covariance data are given.
setAltCovType(AltCovarianceType) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set the flag indicating the type of alternate covariance information provided.
setAlternateNames(List<String>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the alternate names for this space object.
setAmplifierBandwidth(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Set the amplifier bandwidth.
setAmplifierGain(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Set the amplifier gain.
setAmplifierInUse(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Set the amplifier in use.
setAnalysisCenterID(String) - Method in class org.orekit.files.rinex.clock.RinexClock
Setter for the analysis center ID.
setAnalysisCenterName(String) - Method in class org.orekit.files.rinex.clock.RinexClock
Setter for the analysis center name.
setAngleType(AngleType) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the angleType.
setAngularThreshold(double) - Method in class org.orekit.bodies.OneAxisEllipsoid
Set the angular convergence threshold.
setAngvelFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Set frame in which angular velocities are specified.
setAngVelX(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.AngularVelocity
Set the angular velocity around X axis (rad/s).
setAngVelY(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.AngularVelocity
Set the angular velocity around Y axis (rad/s).
setAngVelZ(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.AngularVelocity
Set the angular velocity around Z axis (rad/s).
setAnomaly(double) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Set the orbit anomaly.
setAnomalyType(PositionAngleType) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Set the type of anomaly.
setAntennaAzimuth(double) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Set the azimuth of the zero direction of a fixed antenna.
setAntennaBSight(Vector3D) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Set the antenna B.Sight.
setAntennaHeight(double) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Set the antenna height.
setAntennaNumber(String) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Set the number of the antenna.
setAntennaPhaseCenter(Vector3D) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Set the antenna phasecenter.
setAntennaReferencePoint(Vector3D) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Set the position of antenna reference point for antenna on vehicle.
setAntennaType(String) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Set the type of the antenna.
setAntennaZeroDirection(Vector3D) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Set the zero direction of antenna.
setAODC(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouLegacyNavigationMessage
Setter for the age of data clock.
setAODE(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouLegacyNavigationMessage
Setter for the age of data ephemeris.
setApoapsisAltitude(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Set the distance of the furthest point in the objects orbit above the equatorial radius of the central body.
setApplicableWavelength(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Set the applicable wavelength.
setAppliedVoltage(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Set the applied voltage.
setApproachAngle(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the approach angle computed between Objects 1 and 2 in the RTN coordinate frame relative to object 1.
setApproxPos(Vector3D) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Set the Approximate Marker Position.
setAreAdditionalDataAvailable(boolean) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Set the flag indicating if additional parameters are in the message.
setAreaDRG(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Set the effective area of the object exposed to atmospheric drag.
setAreaPC(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Set the actual area of the object.
setAreaPCMax(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Set the maximum area for the object to be used to compute the collision probability.
setAreaPCMin(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Get the minimum area of the object to be used to compute the collision probability.
setAreaSRP(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Set the effective area of the object exposed to solar radiation pressure.
setAtmosphericModel(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set name of atmospheric model.
setAtmosphericModel(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set name of atmospheric model.
setAttBasis(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata
Set basis of this attitude state time history data.
setAttBasisID(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata
Set identification number of the orbit determination or simulation upon which this attitude is based.
setAttID(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata
Set attitude identification number.
setAttitudeActuatorType(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Set the type of actuator for attitude control.
setAttitudeControlAccuracy(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Set the accuracy of attitude control.
setAttitudeControlMode(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Set the attitude control mode.
setAttitudeKnowledgeAccuracy(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Set the accuracy of attitude knowledge.
setAttitudePointingAccuracy(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Set the overall accuracy of spacecraft to maintain attitude.
setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.AbstractPropagator
Set attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Set the attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.FieldAbstractPropagator
Set attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in interface org.orekit.propagation.FieldPropagator
Set attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Set attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Set attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.integration.FieldStateMapper
Setter for the attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Set attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.integration.StateMapper
Set the attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in interface org.orekit.propagation.Propagator
Set attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Set attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Set attitude provider.
setAttitudeStates(AttitudeElementsType) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination
Set attitude states.
setAttitudeType(AttitudeElementsType) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata
Set attitude element set type.
setAttitudeType(AttitudeType) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Set the format of the data lines in the message.
setAttPrevID(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata
Set identification number of previous attitude.
setBeamDivergence(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
Set the beam divergence.
setBeginTime(double) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver
Set start time of actual maneuver, relative to t₀.
setBeidouNavigationMessage(BeidouLegacyNavigationMessage) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1042Data
Set the Beidou navigation message.
setBeidouToc(double) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1042Data
Set the Beidou time of clock.
setBetaI(int, double) - Method in class org.orekit.files.rinex.navigation.IonosphereKlobucharMessage
Set one β coefficient.
setBGDE1E5a(double) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage
Setter for the E1/E5a broadcast group delay (s).
setBGDE5bE1(double) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage
Setter for the E5b/E1 broadcast group delay (s).
setBiasMode(String) - Method in class org.orekit.files.sinex.DcbDescription
Set the bias mode.
setBN(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Set the GLONASS Bn Word.
setBolDv(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Set the total ΔV capability at beginning of life.
setBStar(double) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
Set the SGP/SGP4 drag-like coefficient.
setBTerm(double) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
Set the SGP4-XP drag-like coefficient.
setBusModel(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Set the bus model name.
setC1cCodePhaseBias(double) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Set the code phase bias correction for GLONASS ObservationType.C1C signal.
setC1pCodePhaseBias(double) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Set the code phase bias correction for GLONASS ObservationType.C1P signal.
setC2cCodePhaseBias(double) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Set the code phase bias correction for GLONASS ObservationType.C2C signal.
setC2pCodePhaseBias(double) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Set the code phase bias correction for GLONASS ObservationType.C2P signal.
setCacheSlotsNumber(int) - Static method in class org.orekit.utils.OrekitConfiguration
Set the number of slots to use in caches.
setCatalogName(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata
Set the specification of satellite catalog source.
setCatalogName(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set the satellite catalog name used for object.
setCatalogName(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the specification of satellite catalog source.
setCDAreaOverMass(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Set the object’s Cd x A/m used to propagate the state vector and covariance to TCA.
setCdmMessageLink(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the Unique identifier of Conjunction Data Message linked to this Orbit Data Message.
setCdrgdrg(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [7,7] in covariance matrix (with index starting at 1).
setCdrgdrg(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set the object [7,7] in covariance matrix (with index starting at 1).
setCdrgn(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [7,3] in covariance matrix (with index starting at 1).
setCdrgndot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [7,6] in covariance matrix (with index starting at 1).
setCdrgr(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [7,1] in covariance matrix (with index starting at 1).
setCdrgrdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [7,4] in covariance matrix (with index starting at 1).
setCdrgt(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [7,2] in covariance matrix (with index starting at 1).
setCdrgtdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [7,5] in covariance matrix (with index starting at 1).
setCdrgx(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set the object [7,1] in covariance matrix (with index starting at 1).
setCdrgxdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set the object [7,4] in covariance matrix (with index starting at 1).
setCdrgy(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set the object [7,2] in covariance matrix (with index starting at 1).
setCdrgydot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set the object [7,5] in covariance matrix (with index starting at 1).
setCdrgz(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set the object [7,3] in covariance matrix (with index starting at 1).
setCdrgzdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set the object [7,6] in covariance matrix (with index starting at 1).
setCelestialSource(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the source and version of celestial body (e.g.
setCenter(BodyFacade) - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata
Set the body at origin of reference frame.
setCenter(BodyFacade) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Set the origin of reference frame.
setCenter(BodyFacade) - Method in class org.orekit.files.ccsds.ndm.odm.OdmCommonMetadata
Set the origin of reference frame.
setCenterMass(Vector3D) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Set the current center of mass of vehicle in body fixed coordinate system.
setCenterOfMassOffset(double) - Method in class org.orekit.files.ilrs.CPFHeader
Set the approximate center of mass to reflector offset.
setCenterOfPressure(Vector3D) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalProperties
Set the location of center of pressure.
setCenterOfPressureReferenceFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalProperties
Set reference frame for center of pressure.
setCentralBodyRotation(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set central body angular rotation rate.
setCic(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Setter for te Cic parameter.
setCis(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Setter for the Cis parameter.
setClassification(String) - Method in class org.orekit.files.ccsds.section.Header
Set the classification/caveats.
setClassificationType(char) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
Set the classification type.
setClkOffset(int) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Deprecated.
setClockBase(double) - Method in class org.orekit.files.sp3.SP3Header
Set the base for clock/clock-rate accuracy.
setClockCorrection(ClockCorrection) - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmClockCorrectionData
Set the clock correction data.
setClockCorrection(ClockCorrection) - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCombinedCorrectionData
Set the clock correction data.
setClockCorrection(ClockCorrection) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm02Data
Set the clock correction data.
setClockCorrection(ClockCorrection) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Data
Set the clock correction data.
setClockOffsetApplied(boolean) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Set the application flag for realtime-derived receiver clock offset.
setClosedOrbitConstraint(boolean) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPMultipleShooter
Set the constraint of a closed orbit or not.
setCndotn(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [6,3] in covariance matrix (with index starting at 1).
setCndotndot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [6,6] in covariance matrix (with index starting at 1).
setCndotr(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [6,1] in covariance matrix (with index starting at 1).
setCndotrdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [6,4] in covariance matrix (with index starting at 1).
setCndott(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [6,2] in covariance matrix (with index starting at 1).
setCndottdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [6,5] in covariance matrix (with index starting at 1).
setCnm(double[][]) - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data
Set the cosine parameters of spherical harmonics expansion of degree N and order M.
setCnn(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [3,3] in covariance matrix (with index starting at 1).
setCnr(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [3,1] in covariance matrix (with index starting at 1).
setCnt(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [3,2] in covariance matrix (with index starting at 1).
setCollisionPercentile(int[]) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the array of 1 to n elements indicating the percentile(s) for which estimates of the collision probability are provided in the COLLISION_PROBABILITY variable.
setCollisionProbability(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the probability (between 0.0 and 1.0) that Object1 and Object2 will collide.
setCollisionProbaMethod(PocMethodFacade) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the method that was used to calculate the collision probability.
setComments(List<String>) - Method in class org.orekit.files.ccsds.section.CommentsContainer
Set the comments.
setComparator(Comparator<IntegerLeastSquareSolution>) - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Set a custom comparator for integer least square solutions comparison.
setComponents(String[]) - Method in class org.orekit.files.ilrs.CRDConfiguration.SystemConfiguration
Set the components (config ids) for system configuration.
setConfidence(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set confidence metric.
setConfigurationId(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.BaseConfiguration
Set the configuration ID.
setConfigurationRecords(CRDConfiguration) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
Set the configuration records for the current data block.
setConjunctionId(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the Originator’s ID that uniquely identifies the conjunction to which the message refers.
setConsiderN(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set number of consider parameters.
setConsiderParameters(List<String>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set description of consider parameters.
setConstellation(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the name of the constellation this space object belongs to.
setContext(ContextBinding) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter
Reset context binding.
setContext(ContextBinding) - Method in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter
Reset context binding.
setContinuousEstimation(boolean) - Method in class org.orekit.utils.ParameterDriver
Set parameter estimation to continuous, by default step estimation.
setConvergenceChecker(ConvergenceChecker<LeastSquaresProblem.Evaluation>) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Set a custom convergence checker.
setConvergenceRMS(double) - Method in class org.orekit.utils.SecularAndHarmonic
Set RMS for convergence.
setCoordinateSystem(String) - Method in class org.orekit.files.sp3.SP3Header
Set the coordinate system used for the orbit entries.
setCorrectionAberrationDiurnal(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the diurnal aberration correction.
setCorrectionAberrationYearly(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the yearly aberration correction.
setCorrectionAngle1(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the correctionAngle1.
setCorrectionAngle2(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the correctionAngle2.
setCorrectionDoppler(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the correctionDoppler.
setCorrectionMagnitude(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the magnitude correction.
setCorrectionRcs(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the radar cross section correction.
setCorrectionReceive(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the correctionReceive.
setCorrectionsApplied(CorrectionApplied) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the correctionApplied.
setCorrectionTransmit(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the correctionTransmit.
setCountry(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the name of the country where the space object owner is based.
setCovarianceMatrixBlock(RTNCovariance) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmData
Set the additional covariance metadata logical block.
setCovarianceMatrixEntry(int, int, double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set an entry in the RTN covariance matrix.
setCovarianceMatrixEntry(int, int, double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set an entry in the XYZ covariance matrix.
setCovarianceMatrixEntry(int, int, double) - Method in class org.orekit.files.ccsds.ndm.odm.CartesianCovariance
Set an entry in the Position/Velocity covariance matrix.
setCovarianceMethod(CovarianceMethod) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set the method name used to calculate covariance during OD.
setCovarianceSource(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set the source of the covariance data.
setCovarianceType(AttitudeCovarianceType) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination
Set type of attitude error state.
setCovBasis(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadata
Set basis of this covariance time history data.
setCovBasis(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata
Set basis of this covariance time history data.
setCovBasisID(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadata
Set identification number of the orbit determination or simulation upon which this covariance is based.
setCovBasisID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata
Set identification number of the orbit determination or simulation upon which this covariance is based.
setCovConfidence(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Set the measure of the confidence in the covariance errors matching reality.
setCovConfidence(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata
Set the measure of confidence in covariance error matching reality.
setCovConfidenceMethod(String) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Set the method used for the calculation of COV_CONFIDENCE.
setCovFrameEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata
Set epoch of the covariance reference frame.
setCovID(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadata
Set covariance identification number.
setCovID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata
Set covariance identification number.
setCovNextID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata
Set identification number of next covariance.
setCovOrdering(Ordering) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata
Set covariance ordering.
setCovPrevID(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadata
Set identification number of previous covariance.
setCovPrevID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata
Set identification number of previous covariance.
setCovReferenceFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadata
Set reference frame of the covariance.
setCovReferenceFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata
Set reference frame of the covariance.
setCovScaleMax(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata
Set the maximum scale factor to apply to achieve realism.
setCovScaleMin(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata
Set the minimum scale factor to apply to achieve realism.
setCovType(AttitudeCovarianceType) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadata
Set covariance element set type.
setCovType(OrbitElementsType) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata
Set covariance element set type.
setCovUnits(List<Unit>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata
Set covariance element set units.
setCRAreaOverMass(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Set the object’s Cr x A/m used to propagate the state vector and covariance to TCA.
setCrc(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Setter for the Crc parameter.
setCrdotn(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [4, 3] in covariance matrix (with index starting at 1).
setCrdotr(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [4,1] in covariance matrix (with index starting at 1).
setCrdotrdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [4, 4] in covariance matrix (with index starting at 1).
setCrdott(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [4, 2] in covariance matrix (with index starting at 1).
setCreationDate(AbsoluteDate) - Method in class org.orekit.files.ccsds.section.Header
Set the message creation date and time in UTC.
setCreationDate(AbsoluteDate) - Method in class org.orekit.files.rinex.clock.RinexClock
Setter for the creation date.
setCreationDate(AbsoluteDate) - Method in class org.orekit.files.rinex.section.RinexBaseHeader
Setter for the creation date.
setCreationDateComponents(DateTimeComponents) - Method in class org.orekit.files.rinex.section.RinexBaseHeader
Setter for the creation date as a string.
setCreationDateString(String) - Method in class org.orekit.files.rinex.clock.RinexClock
Setter for the creation date as a string.
setCreationTimeString(String) - Method in class org.orekit.files.rinex.clock.RinexClock
Setter for the creation time as a string.
setCreationTimeZone(String) - Method in class org.orekit.files.rinex.section.RinexBaseHeader
Setter for the creation time zone.
setCreationTimeZoneString(String) - Method in class org.orekit.files.rinex.clock.RinexClock
Setter for the creation time zone.
setCrr(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [1,1] in covariance matrix (with index starting at 1).
setCrs(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Setter for the Crs parameter.
setCrsIndicator(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01Header
Set the Global/Regional CRS Indicator.
setCrsIndicator(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Header
Set the Global/Regional CRS Indicator.
setcScaleFactor(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadata
Set the (median) suggested covariance scale factor.
setcScaleFactorMax(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadata
set the maximum suggested covariance scale factor.
setcScaleFactorMin(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadata
Set the minimum suggested covariance scale factor.
setCsig3eigvec3(double[]) - Method in class org.orekit.files.ccsds.ndm.cdm.SigmaEigenvectorsCovariance
Set the Sigma/Eigenvectors Covariance data.
setCsrpdrg(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [8,7] in covariance matrix (with index starting at 1).
setCsrpdrg(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set the object [8,7] in covariance matrix (with index starting at 1).
setCsrpn(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [8,3] in covariance matrix (with index starting at 1).
setCsrpndot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [8,6] in covariance matrix (with index starting at 1).
setCsrpr(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [8,1] in covariance matrix (with index starting at 1).
setCsrprdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [8,4] in covariance matrix (with index starting at 1).
setCsrpsrp(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [8,8] in covariance matrix (with index starting at 1).
setCsrpsrp(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set the object [8,8] in covariance matrix (with index starting at 1).
setCsrpt(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [8,2] in covariance matrix (with index starting at 1).
setCsrptdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [8,5] in covariance matrix (with index starting at 1).
setCsrpx(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set the object [8,1] in covariance matrix (with index starting at 1).
setCsrpxdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set the object [8,4] in covariance matrix (with index starting at 1).
setCsrpy(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set the object [8,2] in covariance matrix (with index starting at 1).
setCsrpydot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set the object [8,5] in covariance matrix (with index starting at 1).
setCsrpz(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set the object [8,3] in covariance matrix (with index starting at 1).
setCsrpzdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set the object [8,6] in covariance matrix (with index starting at 1).
setCtdotn(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [5,3] in covariance matrix (with index starting at 1).
setCtdotr(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [5,1] in covariance matrix (with index starting at 1).
setCtdotrdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [5,4] in covariance matrix (with index starting at 1).
setCtdott(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [5,2] in covariance matrix (with index starting at 1).
setCtdottdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [5,5] in covariance matrix (with index starting at 1).
setCthrdrg(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [9,7] in covariance matrix (with index starting at 1).
setCthrdrg(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set the object [9,7] in covariance matrix (with index starting at 1).
setCthrn(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [9,3] in covariance matrix (with index starting at 1).
setCthrndot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [9,6] in covariance matrix (with index starting at 1).
setCthrr(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [9,1] in covariance matrix (with index starting at 1).
setCthrrdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [9,4] in covariance matrix (with index starting at 1).
setCthrsrp(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [9,8] in covariance matrix (with index starting at 1).
setCthrsrp(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set the object [9,8] in covariance matrix (with index starting at 1).
setCthrt(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [9,2] in covariance matrix (with index starting at 1).
setCthrtdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [9,5] in covariance matrix (with index starting at 1).
setCthrthr(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [9,9] in covariance matrix (with index starting at 1).
setCthrthr(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set the object [9,9] in covariance matrix (with index starting at 1).
setCthrx(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set the object [9,1] in covariance matrix (with index starting at 1).
setCthrxdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set the object [9,4] in covariance matrix (with index starting at 1).
setCthry(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set the object [9,2] in covariance matrix (with index starting at 1).
setCthrydot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set the object [9,5] in covariance matrix (with index starting at 1).
setCthrz(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set the object [9,3] in covariance matrix (with index starting at 1).
setCthrzdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set the object [9,6] in covariance matrix (with index starting at 1).
setCtr(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [2,1] in covariance matrix (with index starting at 1).
setCtt(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [2,2] in covariance matrix (with index starting at 1).
setCuc(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Setter for the Cuc parameter.
setCus(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Setter for the Cus parameter.
setCxdotx(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set the object [4,1] in covariance matrix (with index starting at 1).
setCxdotxdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set the object [4, 4] in covariance matrix (with index starting at 1).
setCxdoty(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set the object [4, 2] in covariance matrix (with index starting at 1).
setCxdotz(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set the object [4, 3] in covariance matrix (with index starting at 1).
setCxx(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set the object [1,1] in covariance matrix (with index starting at 1).
setCydotx(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set the object [5,1] in covariance matrix (with index starting at 1).
setCydotxdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set the object [5,4] in covariance matrix (with index starting at 1).
setCydoty(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set the object [5,2] in covariance matrix (with index starting at 1).
setCydotydot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set the object [5,5] in covariance matrix (with index starting at 1).
setCydotz(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set the object [5,3] in covariance matrix (with index starting at 1).
setCyx(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set the object [2,1] in covariance matrix (with index starting at 1).
setCyy(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set the object [2,2] in covariance matrix (with index starting at 1).
setCzdotx(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set the object [6,1] in covariance matrix (with index starting at 1).
setCzdotxdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set the object [6,4] in covariance matrix (with index starting at 1).
setCzdoty(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set the object [6,2] in covariance matrix (with index starting at 1).
setCzdotydot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set the object [6,5] in covariance matrix (with index starting at 1).
setCzdotz(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set the object [6,3] in covariance matrix (with index starting at 1).
setCzdotzdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set the object [6,6] in covariance matrix (with index starting at 1).
setCzx(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set the object [3,1] in covariance matrix (with index starting at 1).
setCzy(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set the object [3,2] in covariance matrix (with index starting at 1).
setCzz(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Set the object [3,3] in covariance matrix (with index starting at 1).
setDarkCount(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Set the dark count.
setDataQuality(DataQuality) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the dataQuality.
setDataReleaseFlag(int) - Method in class org.orekit.files.ilrs.CRDHeader
Set the flag indicating the data release.
setDataSource(int) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage
Setter for the data source.
setDataType(int) - Method in class org.orekit.files.ilrs.CRDHeader
Set the data type.
setDataTypes(List<String>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set observation data types used.
setDataTypes(List<ObservationType>) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the data types in the data section.
setDataUsed(List<DataUsed>) - Method in class org.orekit.files.sp3.SP3Header
Set the data used indicator for this SP3 file.
setDate(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Set date.
setDate(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Setter for the reference date of the ephemeris.
setDate(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Setter for the reference epoch.
setDateAndTime(String) - Method in class org.orekit.files.ilrs.CRDHeader
Set the string value of date and time.
setDayFraction(double) - Method in class org.orekit.files.sp3.SP3Header
Set the day fraction for this SP3 file.
setDcBodyFrame(SpacecraftBodyFrame) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Set spacecraft body frame in which OrbitManeuverHistoryMetadata.getDcBodyTrigger() is specified.
setDcBodyTrigger(Vector3D) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Set direction in body frame for triggering duty cycle.
setDcExecStart(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Set the start time of initial duty cycle-based maneuver execution.
setDcExecStop(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Set the end time of final duty cycle-based maneuver execution.
setDcMaxCycles(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Set the maximum number of "ON" duty cycles.
setDcMinCycles(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Set the minimum number of "ON" duty cycles.
setDcPhaseStartAngle(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Set phase angle of pulse start.
setDcPhaseStopAngle(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Set phase angle of pulse stop.
setDcpSensitivityVectorPosition(double[]) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadata
Set the DCP sensitivity vector (position errors at TCA).
setDcpSensitivityVectorVelocity(double[]) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadata
Set the DCP sensitivity vector (velocity errors at TCA).
setDcRefDir(Vector3D) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Set reference direction for triggering duty cycle.
setDcRefTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Set duty cycle thrust reference time.
setDcTimePulseDuration(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Set duty cycle pulse "ON" duration.
setDcTimePulsePeriod(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Set duty cycle elapsed time between start of a pulse and start of next pulse.
setDcType(DutyCycleType) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Set type of duty cycle.
setDcWindowClose(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Set the end time of duty cycle-based maneuver window.
setDcWindowOpen(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Set the start time of duty cycle-based maneuver window.
setDefault(LazyLoadedDataContext) - Static method in interface org.orekit.data.DataContext
Set the default data context that is used to implement Orekit's static factories.
setDefinedTimeSystem(TimeSystem) - Method in class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage
Set the time system defined by this message.
setDeltaInc(double) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac
Sets the the correction of orbit reference inclination at reference time.
setDeltaMass(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver
Set mass change during maneuver.
setDeltaMass(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Set mass change.
setDeltaMass(double) - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver
Set mass change during maneuver (value is < 0).
setDeltaN(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Setter for the delta of satellite mean motion.
setDeltaN0Dot(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage
Setter for change rate in Δn₀.
setDeltaN0Dot(double) - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage
Setter for change rate in Δn₀.
setDeltaSqrtA(double) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac
Sets the difference between the square root of the semi-major axis and the square root of the nominal semi-major axis.
setDeltaTN(double) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Set the deltaTauN value.
setDensityForecastUncertainty(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadata
Set the atmospheric density forecast error.
setDeployDirSigma(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Set one σ angular off-nominal deployment vector direction.
setDeployDv(int, double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Set velocity increment component of deployed "child" object.
setDeployDvCda(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Set typical (50th percentile) product of drag coefficient times cross-sectional area of deployed "child" object.
setDeployDvRatio(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Set ratio of child-to-host ΔV vectors.
setDeployDvSigma(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Set one σ percent error on deployment ΔV magnitude.
setDeployId(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Set identifier of resulting "child" object deployed from this host.
setDeployMass(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Set decrement in host mass as a result of deployment.
setDescription(DcbDescription) - Method in class org.orekit.files.sinex.DcbSatellite
Set the data contained in "DCB/DESCRIPTION" block of the Sinex file.
setDescription(DcbDescription) - Method in class org.orekit.files.sinex.DcbStation
Set the data contained in "DCB/DESCRIPTION" block of the Sinex file.
setDetectorId(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Set the detector configuration ID.
setDetectorType(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Set the detector type.
setDeterminationMethod(String) - Method in class org.orekit.files.sinex.DcbDescription
Set the determination mode used to generate the bias results.
setDockedWith(List<String>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Set the other space objects this object is docked to.
setDoi(String) - Method in class org.orekit.files.rinex.section.RinexBaseHeader
Setter for the Digital Object Information.
setDomes(String) - Method in class org.orekit.files.sinex.Station
Set the DOMES number.
setDopplerCountBias(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Set the Doppler count bias.
setDopplerCountRollover(boolean) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Set the indicator for Doppler count rollover.
setDopplerCountScale(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Set the Doppler count Scale.
setDragArea(double) - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters
Set the drag area.
setDragCoeff(double) - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters
Set the drag coefficient.
setDragCoefficient(double) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalProperties
Set the the drag coefficient.
setDragCoefficient(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Set the the nominal drag coefficient.
setDragConstantArea(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Set the attitude-independent drag cross-sectional area, not already into attitude-dependent area along OEB.
setDragUncertainty(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Set the drag coefficient 1σ uncertainty.
setDryMass(double) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalProperties
Set the mass without propellant.
setDryMass(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Set the mass without propellant.
setDuration(double) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver
Set duration.
setDuration(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver
Set duration (value is 0 for impulsive maneuver).
setDuration(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Set duration.
setDuration(double) - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver
Set duration (value is 0 for impulsive maneuver).
setDut1(double) - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage
Set the ΔUT₁.
setDut1Dot(double) - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage
Set the ΔUT₁ first derivative.
setDut1DotDot(double) - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage
Set the ΔUT₁ second derivative.
setDv(int, double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Set velocity increment component.
setDV(int, double) - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver
Set velocity increment component.
setDvDirSigma(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Set one σ angular off-nominal ΔV direction.
setDvMagSigma(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Set one σ percent error on ΔV magnitude.
setE(double) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Set the orbit eccentricity.
setE(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Setter the eccentricity.
setEarthTides(YesNoUnknown) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set Enum YesNoUnknown that indicates if Earth and ocean tides are taken into account or not.
setEccentricities(Vector2D) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Set the eccentricities of antenna center.
setEccRefSystem(Station.ReferenceSystem) - Method in class org.orekit.files.sinex.Station
Set the reference system used to define the eccentricity vector (local or cartesian).
setElem(int, int, PolynomialFunction) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix
Set an element of the matrix.
setElementSetNo(int) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
Set the element set number for this satellite.
setEn(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the GLONASS En Word.
setEnabled(boolean) - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Enable or disable a measurement.
setEnabled(boolean) - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
Enable or disable a measurement.
setEndEpoch(AbsoluteDate) - Method in class org.orekit.files.ilrs.ILRSHeader
Set the ending epoch (UTC).
setEndTagSeen(boolean) - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser
Set the flag for XML end tag.
setEndTime(double) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver
Set end time of actual maneuver, relative to t₀.
setEOPContinuityThreshold(double) - Static method in class org.orekit.frames.FramesFactory
Set the threshold to check EOP continuity.
setEOPContinuityThreshold(double) - Method in class org.orekit.frames.LazyLoadedEop
Set the threshold to check EOP continuity.
setEOPContinuityThreshold(double) - Method in class org.orekit.frames.LazyLoadedFrames
Set the threshold to check EOP continuity.
setEopSource(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the source and version of Earth Orientation Parameters.
setEphemerisNames(Map<Integer, String>) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the external ephemeris names for participants.
setEphemerisType(int) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
Set the ephemeris type.
setEphemName(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set the name of external ephemeris used for OD.
setEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.CartesianCovariance
Set matrix epoch.
setEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Set epoch of state vector, Keplerian elements and covariance matrix data.
setEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set time tag for orbit determination solved-for state.
setEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.StateVector
Set epoch of state vector, Keplerian elements and covariance matrix data.
setEpoch(AbsoluteDate) - Method in class org.orekit.files.sinex.Station
Set the coordinates reference epoch.
setEpoch(AbsoluteDate) - Method in class org.orekit.files.sp3.SP3Header
Set the epoch of the SP3 file.
setEpochDelayCorrection(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration
Set the epoch delay correction.
setEpochEigenInt(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set positional error ellipsoid 1σ intermediate eigenvalue at the epoch of OD.
setEpochEigenMaj(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set positional error ellipsoid 1σ major eigenvalue at the epoch of OD.
setEpochEigenMin(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set positional error ellipsoid 1σ minor eigenvalue at the epoch of OD.
setEpochFreedom(int, boolean) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPMultipleShooter
Set the epoch of a patch point to free or not.
setEpochFreedom(int, boolean) - Method in class org.orekit.utils.AbstractMultipleShooting
Set the epoch of a patch point to free or not.
setEpochIdentifier(int) - Method in class org.orekit.files.ilrs.CRDHeader
Set the epoch identifier.
setEpochIgnition(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver
Set epoch ignition.
setEpochInterval(double) - Method in class org.orekit.files.sp3.SP3Header
Set the epoch interval for this SP3 file.
setEpochStart(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver
Set epoch start.
setEpochT0(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata
Set the epoch to which all relative times are referenced in data blocks.
setEpochT0(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the epoch to which all relative times are referenced in data blocks.
setEpochTime1s(double) - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionHeader
Set the Epoch Time 1s.
setEpochToc(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Setter for the time of clock epoch.
setEpochToc(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Setter for the time of clock epoch.
setEpsilon(double) - Method in class org.orekit.propagation.conversion.averaging.converters.FixedPointOsculatingToAveragedConverter
Setter for epsilon.
setEquatorialRadius(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set oblate spheroid equatorial radius of central body.
setEstimatedValue(double...) - Method in class org.orekit.estimation.measurements.EstimatedMeasurementBase
Set the estimated value.
setEulerRotSeq(RotationOrder) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination
Set the rotation order for Euler angles.
setEulerRotSeq(RotationOrder) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata
Set the rotation order for Euler angles.
setEulerRotSeq(RotationOrder) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Set the rotation order for Euler angles.
setEulerRotSeq(RotationOrder) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler
Set the rotation order for Euler angles.
setEvaluationsCounter(Incrementor) - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel
Set the counter for evaluations.
setExternalClockReference(String) - Method in class org.orekit.files.rinex.clock.RinexClock
Setter for the external clock reference.
setExternalSignalProcessing(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Set the external signal processing.
setFallback(ProcessingState) - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser
Set fallback processing state.
setField(int, int, int, int, int[]) - Method in class org.orekit.gnss.rflink.gps.SubFrame
Set a field.
setField(int, int, int, int, int, int, int, int[]) - Method in class org.orekit.gnss.rflink.gps.SubFrame
Set a field.
setFilter(CartesianDerivativesFilter) - Method in class org.orekit.files.ilrs.CPF
Set the derivatives filter.
setFilter(CartesianDerivativesFilter) - Method in class org.orekit.files.sp3.SP3Header
Set the derivatives filter.
setFitInterval(int) - Method in class org.orekit.propagation.analytical.gnss.data.LegacyNavigationMessage
Setter for the fit interval.
setFix(int, int, double, double, double, double, double) - Method in class org.orekit.gnss.metric.ntrip.NtripClient
Set GPS fix data to send as NMEA sentence to Ntrip caster if required.
setFixedF10P7(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set fixed (time invariant) value of the Solar Flux Unit daily proxy F10.7.
setFixedF10P7Mean(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set fixed (time invariant) value of the Solar Flux Unit 81-day running center-average proxy F10.7.
setFixedGeomagneticAp(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set fixed (time invariant) value of the planetary 3-hour-range geomagnetic index aₚ.
setFixedGeomagneticDst(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set fixed (time invariant) value of the planetary 1-hour-range geomagnetic index Dst.
setFixedGeomagneticKp(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set fixed (time invariant) value of the planetary 3-hour-range geomagnetic index Kₚ.
setFixedM10P7(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set fixed (time invariant) value of the Solar Flux daily proxy M10.7.
setFixedM10P7Mean(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set fixed (time invariant) value of the Solar Flux 81-day running center-average proxy M10.7.
setFixedS10P7(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set fixed (time invariant) value of the Solar Flux daily proxy S10.7.
setFixedS10P7Mean(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set fixed (time invariant) value of the Solar Flux 81-day running center-average proxy S10.7.
setFixedY10P7(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set fixed (time invariant) value of the Solar Flux daily proxy Y10.7.
setFixedY10P7Mean(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set fixed (time invariant) value of the Solar Flux 81-day running center-average proxy Y10.7.
setFlags(int) - Method in class org.orekit.files.rinex.navigation.IonosphereNequickGMessage
Set the disturbance flags.
setFormat(String) - Method in class org.orekit.files.ilrs.ILRSHeader
Set the file format.
setFormatVersion(double) - Method in class org.orekit.files.ccsds.section.Header
Set the CCSDS NDM (ADM, ODM or TDM) format version.
setFormatVersion(double) - Method in class org.orekit.files.rinex.clock.RinexClock
Setter for the format version.
setFormatVersion(double) - Method in class org.orekit.files.rinex.section.RinexBaseHeader
Setter for the format version.
setFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.adm.apm.AngularVelocity
Set frame in which angular velocities are specified.
setFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Inertia
Set frame in which inertia is specified.
setFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver
Set Coordinate system for the torque vector.
setFrameA(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints
Set frame A.
setFrameB(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints
Set frame B.
setFrameEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.OdmCommonMetadata
Set epoch of reference frame, if not intrinsic to the definition of the reference frame.
setFrameEpochString(String) - Method in class org.orekit.files.ccsds.ndm.odm.OdmCommonMetadata
Set epoch of reference frame, if not intrinsic to the definition of the reference frame.
setFrameName(String) - Method in class org.orekit.files.rinex.clock.RinexClock
Setter for the frame name.
setFreqOffset(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the freqOffset.
setFrequencyNumber(double) - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage
Setter for the frequency number.
setFrequencySource(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration
Set the frequency source.
setFT(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Set the GLONASS FT Word.
setGalileoDataValidityStatus(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1045Data
Set the Galileo data validity status.
setGalileoNavigationMessage(GalileoNavigationMessage) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1045Data
Set the Galileo navigation message.
setGalileoToc(double) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1045Data
Set the Galileo time of clock.
setGammaN(double) - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage
Setter for the SV relative frequency bias.
setGdop(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set generalize Dilution Of Precision.
setGlonassNavigationMessage(GLONASSNavigationMessage) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Set the Glonass navigation message.
setGm(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set gravitational coefficient of attracting body.
setGnssIod(int) - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCombinedCorrectionData
Set the GNSS IOD.
setGnssIod(int) - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmOrbitCorrectionData
Set the GNSS IOD.
setGnssIod(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01Data
Set the GNSS IOD.
setGnssIod(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Data
Set the GNSS IOD.
setGpsCodeOnL2(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data
Set the GPS code on L2.
setGpsFitInterval(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data
Set the GPS fit interval.
setGpsL2PDataFlag(boolean) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data
Set the GPS L2 P-code data flag.
setGpsNavigationMessage(GPSLegacyNavigationMessage) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data
Set the GPS navigation message.
setGpsToc(double) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data
Set the GPS time of clock.
setGpsWeek(int) - Method in class org.orekit.files.sp3.SP3Header
Set the GPS week of the SP3 file.
setGravitationalAssist(BodyFacade) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Set the origin of gravitational assist.
setGravityModel(String, int, int) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set gravity model.
setGravityModel(String, int, int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set gravity model.
setGroupDelayDifference(double) - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage
Set group delay difference.
setHandlers(List<EventHandler>) - Method in class org.orekit.propagation.events.handlers.EventMultipleHandler
Change handlers list with user input.
setHbr(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Set the object hard body radius.
setHeader(H) - Method in class org.orekit.files.ccsds.ndm.NdmConstituent
Set the header.
setHeader(CRDHeader) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
Set the header for the current data block.
setHealth(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Setter for the health status.
setHealth(int) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouAlmanac
Sets the health status.
setHealth(int) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage
Setter for health.
setHealth(int) - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac
Sets the health status.
setHealth(int) - Method in class org.orekit.propagation.analytical.gnss.data.QZSSAlmanac
Sets the health status.
setHealthAvailabilityIndicator(boolean) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Set the flag indicating if GLONASS almanac health is available.
setHealthE1(int) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac
Sets the E1-B/C signal health status.
setHealthE5a(int) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac
Sets the E5a signal health status.
setHealthE5b(int) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac
Sets the E5b signal health status.
setHealthFlags(double) - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage
Set health flag.
setHeightIonosphericLayer(double) - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data
Set the height of the ionospheric layer.
setHighRateClockCorrection(double) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm04Data
Set the high rate clock correction to be added to the polynomial clock correction.
setHumiSensorManufacturer(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
Set the humidity sensor manufacturer.
setHumiSensorModel(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
Set the humidity sensor model.
setHumiSensorSerialNumber(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
Set the humidity sensor serial number.
setI(double) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Set the orbit inclination.
setI0(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Setter for the Inclination Angle at Reference Time (rad).
setI0(double, double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouAlmanac
Sets the Inclination Angle at Reference Time (rad).
setId(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination
Set identification number.
setId(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set identification number.
setID(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver
Set maneuver identification number.
setIDot(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Setter for the Rate of Inclination Angle (rad/s).
setIgnoreCentralAttraction(boolean) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Set the flag to ignore or not the creation of a NewtonianAttraction.
setIgnoreCentralAttraction(boolean) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Set the flag to ignore or not the creation of a NewtonianAttraction.
setIlrsSatelliteId(String) - Method in class org.orekit.files.ilrs.ILRSHeader
Set the IRLS satellite ID (based on COSPAR ID).
setInclination(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Set the angle between the objects orbit plane and the orbit centers equatorial plane.
setIndexedRotationAngle(int, double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler
Set the Euler angle about axis.
setIndexedRotationRate(int, double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler
Set the rate of Euler angle about axis.
setInertiaMatrixEntry(int, int, double) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalProperties
Set an entry in the inertia matrix.
setInertiaMatrixEntry(int, int, double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Inertia
Set an entry in the inertia matrix.
setInertiaMatrixEntry(int, int, double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Set an entry in the inertia matrix.
setInertiaReferenceFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalProperties
Set reference frame for inertia.
setInitialJacobians(SpacecraftState) - Method in class org.orekit.propagation.numerical.EpochDerivativesEquations
Set the initial value of the Jacobian with respect to state and parameter.
setInitialJacobians(SpacecraftState, double[][], double[][]) - Method in class org.orekit.propagation.numerical.EpochDerivativesEquations
Set the initial value of the Jacobian with respect to state and parameter.
setInitialJacobians(SpacecraftState, double[][], double[][], double[]) - Method in class org.orekit.propagation.numerical.EpochDerivativesEquations
Set the Jacobian with respect to state into a one-dimensional additional state array.
setInitialPhi(SpacecraftState) - Method in class org.orekit.propagation.numerical.cr3bp.STMEquations
Method adding the standard initial values of the additional state to the initial spacecraft state.
setInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Set the initial state.
setInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Set the initial state with osculating orbital elements.
setInitialState(FieldSpacecraftState<T>, PropagationType) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Set the initial state.
setInitialState(SpacecraftState) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Set the initial state.
setInitialState(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Set the initial state with osculating orbital elements.
setInitialState(SpacecraftState, PropagationType) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Set the initial state.
setInitialWetMass(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Set the total mass at beginning of life.
setInRotationAngles(boolean) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler
Set flag for rotation angle parsing.
setIntegrationInterval(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the integrationInterval.
setIntegrationRef(IntegrationReference) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the integrationRef.
setIntegrityFlags(int) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage
Setter for B1C integrity flags.
setInternationalDes(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set the international designator used for object.
setInternationalDesignator(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata
Set the international designator for the object.
setInternationalDesignator(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the international designator for the object.
setInterpMethodEOP(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the interpolation method for Earth Orientation Parameters.
setInterpMethodSW(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set the interpolation method for Space Weather data.
setInterpolationDegree(int) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Set the interpolation degree.
setInterpolationDegree(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Set the interpolation degree.
setInterpolationDegree(int) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata
Set the interpolation degree.
setInterpolationDegree(int) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Set the interpolation degree.
setInterpolationDegree(int) - Method in class org.orekit.frames.LazyLoadedEop
Set the degree for interpolation degree.
setInterpolationGridToFixedNumberOfPoints(int) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Set the interpolation grid generator.
setInterpolationGridToFixedNumberOfPoints(int) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Set the interpolation grid generator.
setInterpolationGridToMaxTimeGap(double) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Set the interpolation grid generator.
setInterpolationGridToMaxTimeGap(T) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Set the interpolation grid generator.
setInterpolationMethod(String) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Set the interpolation method to be used.
setInterpolationMethod(String) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Set the interpolation method to be used.
setInterpolationMethod(InterpolationMethod) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Set the interpolation method to be used.
setInterpolationMethod(InterpolationMethod) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata
Set the interpolation method to be used.
setInterpolationSample(int) - Method in class org.orekit.files.ilrs.CPF
Set the interpolation sample.
setInterval(double) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Set the observation interval in seconds.
setIntrackThrust(YesNoUnknown) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set boolean that indicates if intrack thrust modeling was into account or not.
setIOD(int) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac
Sets the Issue of Data (IOD).
setIODC(int) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage
Setter for the Issue of Data Clock.
setIODC(int) - Method in class org.orekit.propagation.analytical.gnss.data.LegacyNavigationMessage
Setter for the Issue of Data Clock.
setIODE(double) - Method in class org.orekit.propagation.analytical.gnss.data.LegacyNavigationMessage
Setter for the Issue of Data Ephemeris.
setIODE(int) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage
Setter for the Issue of Data Ephemeris.
setIODEC(double) - Method in class org.orekit.propagation.analytical.gnss.data.IRNSSNavigationMessage
Setter for the Issue of Data, Ephemeris and Clock.
setIODN(double) - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage
Setter for the issue of data navigation.
setIODNav(int) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage
Setter for the Issue of Data of the navigation batch.
setIodSsr(int) - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionHeader
Set the IOD SSR.
setIodSsr(int) - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader
Set the IOD SSR.
setIonosphericCorrectionType(IonosphericCorrectionType) - Method in class org.orekit.files.rinex.navigation.RinexNavigationHeader
Setter for the ionospheric correction type.
setIscB1CD(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage
Setter for inter Signal Delay for B1 CD.
setIscB1CP(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage
Setter for inter Signal Delay for B1 CP.
setIscB2AD(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage
Setter for inter Signal Delay for B2 AD.
setIsCenterOfMassCorrectionApplied(boolean) - Method in class org.orekit.files.ilrs.CPFHeader
Set the flag telling if the center of mass correction is applied.
setIsCenterOfMassCorrectionApplied(boolean) - Method in class org.orekit.files.ilrs.CRDHeader
Set the center of mass correction applied indicator.
setIscL1CA(double) - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage
Setter for inter Signal Delay for L1 C/A.
setIscL1CD(double) - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage
Setter for inter Signal Delay for L1 CD.
setIscL1CP(double) - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage
Setter for inter Signal Delay for L1 CP.
setIscL2C(double) - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage
Setter for inter Signal Delay for L2 C.
setIscL5I5(double) - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage
Setter for inter Signal Delay for L5I.
setIscL5Q5(double) - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage
Setter for inter Signal Delay for L5Q.
setIsCompatibleWithTIVs(boolean) - Method in class org.orekit.files.ilrs.CPFHeader
Set the flag for compatibility with TIVs.
setIsConsistencyMaintained(boolean) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Header
Set the flag indicating if phase biases maintain consistency between non-dispersive and all original dispersive phase signals.
setIsFirst(boolean) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Set the flag for the placement of the quaternion QC in the attitude data.
setIsMelbourneWubbenaConsistencyMaintained(boolean) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Header
Set the flag indicating if consistency between code and phase biases is maintained for the MW combinations.
setIsReceiveAmplitudeCorrectionApplied(boolean) - Method in class org.orekit.files.ilrs.CRDHeader
Set the receive amplitude correction applied indicator.
setIsSpacecraftTimeSimplified(boolean) - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
Set the spacecraft time simplified flag.
setIsStationSystemDelayApplied(boolean) - Method in class org.orekit.files.ilrs.CRDHeader
Set the station system delay applied indicator.
setIsTransponderDelayApplied(boolean) - Method in class org.orekit.files.ilrs.CRDHeader
Set the spacecraft system delay applied (transponders) indicator.
setIsTroposphericRefractionApplied(boolean) - Method in class org.orekit.files.ilrs.CRDHeader
Set the tropospheric refraction correction applied indicator.
setIterationsCounter(Incrementor) - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel
Set the counter for iterations.
setITRFVersion(int) - Method in class org.orekit.files.sinex.SinexLoader
Set the ITRF version used in EOP entries processing.
setKlobucharAlpha(double[]) - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Set the "alpha" ionspheric parameters.
setKlobucharBeta(double[]) - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Set the "beta" ionospheric parameters.
setLabeledRotationAngle(char, double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler
Set the Euler angle about axis.
setLabeledRotationRate(char, double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler
Set the rate of Euler angle about axis.
setLaserId(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
Set the laser configuration ID.
setLaserType(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
Set the laser type.
setLeapSeconds(int) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Set the Number of leap seconds since 6-Jan-1980.
setLeapSecondsDayNum(int) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Set the respective leap second day number.
setLeapSecondsFuture(int) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Set the future or past leap seconds.
setLeapSecondsWeekNum(int) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Set the respective leap second week number.
setLicense(String) - Method in class org.orekit.files.rinex.section.RinexBaseHeader
Setter for the license of use.
setLNFifthString(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Set the GLONASS ln Word extracted from fifth string of the subframe.
setLNThirdString(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Set the GLONASS ln Word extracted from third string of the subframe.
setLocalTimingId(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration
Set the local timing system configuration ID.
setLod(double) - Method in class org.orekit.files.sinex.SinexEopEntry
Set the length of day.
setLowElevationThreshold(double) - Method in class org.orekit.models.earth.troposphere.CanonicalSaastamoinenModel
Set the low elevation threshold value for path delay computation.
setLowElevationThreshold(double) - Method in class org.orekit.models.earth.troposphere.ModifiedSaastamoinenModel
Set the low elevation threshold value for path delay computation.
setM(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Set the GLONASS M Word.
setM0(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Setter for the Mean Anomaly at Reference Time (rad).
setMahalanobisDistance(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the Mahalanobis Distance.
setMainFieldCoefficients(int, int, double, double) - Method in class org.orekit.models.earth.GeoMagneticField
Set the given main field coefficients.
setManBasis(ManBasis) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Set basis of this maneuver history data.
setManBasisID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Set identification number of the orbit determination or simulation upon which this maneuver is based.
setManComposition(List<ManeuverFieldType>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Set maneuver element of information.
setManDeviceID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Set identifier of the device used for this maneuver.
setManeuverable(Maneuvrable) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set the object maneuver ability.
setManeuversFrequency(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Set the average frequency of orbit or attitude maneuvers (in SI units, hence per second).
setManFrameEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Set epoch of the maneuver reference frame.
setManID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Set maneuver identification number.
setManNextEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Set start time of next maneuver.
setManNextID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Set identification number of next maneuver.
setManPredSource(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Set prediction source on which this maneuver is based.
setManPrevEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Set completion time of previous maneuver.
setManPrevID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Set identification number of previous maneuver.
setManPurpose(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver
Set purpose of maneuver.
setManPurpose(List<String>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Set the purposes of the maneuver.
setManReferenceFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Set reference frame of the maneuver.
setManufacturer(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Set manufacturer name.
setManUnits(List<Unit>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Set maneuver element of information units.
setMarkerName(String) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Set name of the antenna marker.
setMarkerNumber(String) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Set number of the antenna marker.
setMarkerType(String) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Set type of the antenna marker.
setMass(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Set the mass of the object.
setMass(double) - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters
Set the spacecraft mass.
setMass(double) - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Set the initial mass.
setMatrix(PolynomialFunction[][]) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix
Set values for all elements.
setMatrixLine(int, PolynomialFunction[]) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix
Set the value of a line of the matrix.
setMaxAreaForCollisionProbability(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Set the maximum cross-sectional area for collision probability estimation purposes.
setMaxCollisionProbability(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set max collision probability.
setMaxCollisionProbabilityMethod(PocMethodFacade) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set max collision probability method.
setMaxDate(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityDataLoader
Set the available data range maximum date.
setMaxEvaluations(int) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Set the maximum number of model evaluations.
setMaximumObsGap(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set maximum time between observations in the OD of the object.
setMaxIter(int) - Method in class org.orekit.utils.SecularAndHarmonic
Set maximum number of iterations.
setMaxIterations(int) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Set the maximum number of iterations.
setMaxIterations(int) - Method in class org.orekit.propagation.conversion.averaging.converters.FixedPointOsculatingToAveragedConverter
Setter for maximum number of iterations.
setMaxParseDegree(int) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Set the degree limit for the next file parsing.
setMaxParseDegree(int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Set the degree limit for the next file parsing.
setMaxParseOrder(int) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Set the order limit for the next file parsing.
setMaxParseOrder(int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Set the order limit for the next file parsing.
setMaxPredictedEigenMaj(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set maximum predicted major eigenvalue of 1σ positional error ellipsoid over entire time span of the OCM.
setMaxRcs(double) - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties
Set the maximum radar cross-section.
setMaxThrust(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Set the maximum composite thrust the spacecraft can accomplish.
setMaxValue(double) - Method in class org.orekit.utils.ParameterDriver
Set maximum parameter value.
setMeanElementTheory(String) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmMetadata
Set the description of the Mean Element Theory.
setMeanMotion(double) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Set the orbit mean motion.
setMeanMotionDot(double) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
Set the first time derivative of the mean motion.
setMeanMotionDotDot(double) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
Set the second time derivative of the mean motion.
setMergedFiles(int) - Method in class org.orekit.files.rinex.navigation.RinexNavigationHeader
Setter for the number of merged files.
setMessageFor(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmHeader
Set the spacecraft name for which the CDM is provided stored in MESSAGE_FOR key.
setMessageId(String) - Method in class org.orekit.files.ccsds.section.Header
Set the ID that uniquely identifies a message from a given originator.
setMetadata(M) - Method in class org.orekit.files.ccsds.section.Segment
Set the segment metadata.
setMeteorologicalId(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
Set the meteorological configuration ID.
setMethod(AdMethodType) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination
Set attitude determination method.
setMethod(OdMethodFacade) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set orbit determination method.
setMinAreaForCollisionProbability(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Set the minimum cross-sectional area for collision probability estimation purposes.
setMinDate(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityDataLoader
Set the available data range minimum date.
setMinPredictedEigenMin(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set minimum predicted minor eigenvalue of 1σ positional error ellipsoid over entire time span of the OCM.
setMinRcs(double) - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties
Set the minimum radar cross-section.
setMinValue(double) - Method in class org.orekit.utils.ParameterDriver
Set minimum parameter value.
setMissDistance(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the norm of relative position vector at TCA.
setMode(TrackingMode) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the mode.
setModifiedJulianDay(int) - Method in class org.orekit.files.sp3.SP3Header
Set the modified julian day for this SP3 file.
setMomentumAlpha(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
Set the right ascension of angular momentum vector (rad).
setMomentumDelta(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
Set the declination of the angular momentum vector (rad).
setMu(double) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Set the gravitational coefficient.
setMu(double) - Method in class org.orekit.files.ilrs.CPF
Set the gravitational coefficient.
setMu(double) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Set the central body attraction coefficient.
setMu(double) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Set the central attraction coefficient μ.
setMu(double) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Set the central attraction coefficient μ.
setMu(double) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Set the central attraction coefficient μ.
setMu(T) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Set the central attraction coefficient μ.
setMu(T) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Set the central attraction coefficient μ.
setMu(T) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Set the central attraction coefficient μ.
setMuCreated(double) - Method in class org.orekit.files.ccsds.ndm.odm.OdmParser
Set the gravitational coefficient created from the knowledge of the central body.
setMultipleMessageIndicator(int) - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionHeader
Set the Multiple Message Indicator.
setMuParsed(double) - Method in class org.orekit.files.ccsds.ndm.odm.OdmParser
Set the gravitational coefficient parsed in the ODM File.
setN4(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Set the four-year interval number starting from 1996.
setNA(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Set the GLONASS NA Word.
setName(int, SatelliteSystem) - Method in class org.orekit.estimation.measurements.gnss.AbstractCycleSlipDetector
Create the name of a satellite from its PRN number and satellite System it belongs to.
setName(String) - Method in class org.orekit.files.ilrs.ILRSHeader
Set the satellite target name.
setName(String) - Method in class org.orekit.utils.ParameterDriver
Change the general name of this parameter driver.
setNbObsPerSatellite(SatInSystem, ObservationType, int) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Set number of observations for a satellite.
setNBodyPerturbations(List<BodyFacade>) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set n-body perturbation bodies.
setNBodyPerturbations(List<BodyFacade>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set n-body perturbation bodies.
setNbSat(int) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Set number of satellites.
setNbSensorNoiseCovariance(int) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationSensor
Set number of noise elements for sensor.
setNbStates(int) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination
setNbStates(int) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata
Set the number of data states included (attitude components plus rates components).
setNeQuickAlpha(double[]) - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Set the "alpha" ionospheric parameters.
setNextLeapEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata
Set the epoch of next leap second.
setNextLeapEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the epoch of next leap second.
setNextLeapTaimutc(double) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata
Set the difference (TAI – UTC) in seconds incorporated at epoch AcmMetadata.getNextLeapEpoch().
setNextLeapTaimutc(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the difference (TAI – UTC) in seconds incorporated at epoch OcmMetadata.getNextLeapEpoch().
setNextMessageEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set Scheduled UTC epoch of the next CDM associated with the event identified by CONJUNCTION_ID.
setNextMessageEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the creation date of next message from a given originator.
setNextMessageID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the unique ID identifying next message from a given originator.
setNominalFireRate(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
Set the nominal fire rate.
setNoradId(String) - Method in class org.orekit.files.ilrs.ILRSHeader
Set the satellite NORAD ID.
setNoradID(int) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
Set the NORAD Catalog Number ("Satellite Number").
setNormalizedValue(double) - Method in class org.orekit.utils.ParameterDriver
Set normalized value at specific date.
setNormalizedValue(double, AbsoluteDate) - Method in class org.orekit.utils.ParameterDriver
Set normalized value at specific date.
setNt(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Set the current date.
setNumberOfBiasesProcessed(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm05Data
Set the number of biases processed for the current satellite.
setNumberOfBiasesProcessed(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data
Set the number of biases processed for the current satellite.
setNumberOfEpochs(int) - Method in class org.orekit.files.sp3.SP3Header
Set the number of epochs as contained in the SP3 file.
setNumberOfIonosphericLayers(int) - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Header
Set the number of ionospheric layers.
setNumberOfLeapSeconds(int) - Method in class org.orekit.files.rinex.clock.RinexClock
Setter for the number of leap seconds.
setNumberOfLeapSeconds(int) - Method in class org.orekit.files.rinex.navigation.RinexNavigationHeader
Setter for the current number of leap seconds.
setNumberOfLeapSecondsGNSS(int) - Method in class org.orekit.files.rinex.clock.RinexClock
Setter for the number of leap seconds for GNSS time scales.
setNumberOfSatellites(int) - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionHeader
Set the number of satellites for the current IGM message.
setNumberOfSatellites(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgmHeader
Set the number of satellites for the current IGM message.
setNutation(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
Set the nutation angle of spin axis (rad).
setNutationPeriod(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
Set the body nutation period of the spin axis (s).
setNutationPhase(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
Set the inertial nutation phase (rad).
setNutationVel(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
Set the angular velocity of spin vector around angular momentum vector.
setNutLn(double) - Method in class org.orekit.files.sinex.SinexEopEntry
Set the nutation correction in longitude.
setNutOb(double) - Method in class org.orekit.files.sinex.SinexEopEntry
Set the nutation correction in obliquity.
setNutX(double) - Method in class org.orekit.files.sinex.SinexEopEntry
Set the nutation correction X.
setNutY(double) - Method in class org.orekit.files.sinex.SinexEopEntry
Set the nutation correction Y.
setObject(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set the object name for which metadata are given.
setObjectDesignator(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata
Set the unique satellite identification designator for the object.
setObjectDesignator(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set the satellite designator for the object for which metadata are given.
setObjectDesignator(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the unique satellite identification designator for the object.
setObjectID(String) - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata
Set the spacecraft ID for which the attitude data are provided.
setObjectID(String) - Method in class org.orekit.files.ccsds.ndm.odm.OdmCommonMetadata
Set the spacecraft ID for which the orbit state is provided.
setObjectName(String) - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata
Set the spacecraft name for which the attitude data are provided.
setObjectName(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set the spacecraft name used for object.
setObjectName(String) - Method in class org.orekit.files.ccsds.ndm.odm.OdmMetadata
Set the spacecraft name for which the orbit state is provided.
setObjectType(ObjectType) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set the type of object.
setObjectType(ObjectType) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the type of object.
setOblateFlattening(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set central body oblate spheroid oblateness.
setObsAvailable(int) - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters
Set the number of observations available for the OD of the object.
setObsAvailable(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set number of observations available within the actual OD span.
setObsBeforeNextMessage(YesNoUnknown) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set the flag indicating whether new tracking observations are anticipated prior to the issue of the next CDM associated with the event specified by CONJUNCTION_ID.
setObservationCode(String) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Set the observation code of the average phasecenter position w/r to antenna reference point.
setObservations(List<Observation>) - Method in class org.orekit.files.ccsds.ndm.tdm.ObservationsBlock
Set the list of Observations Data Lines.
setObservationSampling(int) - Method in class org.orekit.files.sinex.DcbDescription
Set the observation sampling interval used for data analysis.
setObserver(BatchLSObserver) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Set an observer for iterations.
setObserver(KalmanObserver) - Method in class org.orekit.estimation.sequential.KalmanEstimator
Set the observer.
setObserver(KalmanObserver) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimator
Set the observer.
setObserver(KalmanObserver) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Set the observer.
setObserver(KalmanObserver) - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanEstimator
Set the observer.
setObserver(KalmanObserver) - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel
Set the observer.
setObserver(KalmanObserver) - Method in class org.orekit.estimation.sequential.UnscentedKalmanEstimator
Set the observer.
setObserverName(String) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Set name of the observer.
setObsUsed(int) - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters
Set the number of observations accepted for the OD of the object.
setObsUsed(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set number of observations accepted within the actual OD span.
setOceanTidesModel(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set ocean tides model.
setOcmDataElements(List<OcmElements>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the list of elements of information data blocks included in this message.
setOdEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters
Set the epoch of the orbit determination used for this message.
setOdmMessageLink(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata
Set the Unique identifier of Orbit Data Message linked to this Attitude Data Message.
setOdmMsgLink(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set the unique identifier of Orbit Data Message(s) that are linked (relevant) to this Conjunction Data Message.
setODParametersBlock(ODParameters) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmData
Set the OD parameters logical block.
setOebAreaAlongIntermediate(double) - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties
Set the cross-sectional area of Optimally Enclosing Box when viewed along the intermediate OEB direction.
setOebAreaAlongMax(double) - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties
Set the cross-sectional area of Optimally Enclosing Box when viewed along the maximum OEB direction.
setOebAreaAlongMin(double) - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties
Set the cross-sectional area of Optimally Enclosing Box when viewed along the minimum OEB direction.
setOebIntermediate(double) - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties
Set the intermediate physical dimension of the OEB.
setOebMax(double) - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties
Set the maximum physical dimension of the OEB.
setOebMin(double) - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties
Set the minimum physical dimension of the OEB.
setOebParentFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties
Set the Optimally Enclosing Box parent reference frame.
setOebParentFrameEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties
Set the Optimally Enclosing Box parent reference frame epoch.
setOebQ(int, double) - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties
set the component of quaternion defining Optimally Enclosing Box.
setOmega0(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Setter for the Longitude of Ascending Node of Orbit Plane at Weekly Epoch (rad).
setOmegaDot(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Setter for the rate of Rate of Right Ascension (rad/s).
setOperator(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the operator of the space object.
setOperatorContactPosition(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set the contact position for the object owner / operator.
setOperatorEmail(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set the object operator email.
setOperatorOrganization(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set the contact organisation of the object.
setOperatorPhone(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set the operator phone of the object.
setOpsStatus(OpsStatus) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the operational status.
setOrbAveraging(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Set type of averaging (Osculating, mean Brouwer, other.
setOrbitCategory(OrbitCategory) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the orbit category.
setOrbitCenter(BodyFacade) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set the central body name for object 1 and 2.
setOrbitCorrection(OrbitCorrection) - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCombinedCorrectionData
Set the orbit correction data.
setOrbitCorrection(OrbitCorrection) - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmOrbitCorrectionData
Set the orbit correction data.
setOrbitCorrection(OrbitCorrection) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01Data
Set the orbit correction data.
setOrbitCorrection(OrbitCorrection) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Data
Set the orbit correction data.
setOrbitType(OrbitType) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Set propagation orbit type.
setOrbitType(OrbitType) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Set propagation orbit type.
setOrbitType(OrbitType) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Set propagation orbit type.
setOrbitType(OrbitType) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Set propagation orbit type.
setOrbitTypeKey(String) - Method in class org.orekit.files.sp3.SP3Header
Set the orbit type key for this SP3 file.
setOrbRevNum(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Set the integer orbit revolution number.
setOrbRevNumBasis(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Set the basis for orbit revolution number.
setOriginator(String) - Method in class org.orekit.files.ccsds.section.Header
Set the message originator.
setOriginatorAddress(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata
Set the address of Programmatic Point Of Contact at originator.
setOriginatorAddress(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the address of Programmatic Point Of Contact at originator.
setOriginatorEmail(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata
Set the email address of Programmatic Point Of Contact at originator.
setOriginatorEmail(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the email address of Programmatic Point Of Contact at originator.
setOriginatorPhone(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata
Set the phone number of Programmatic Point Of Contact at originator.
setOriginatorPhone(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the phone number of Programmatic Point Of Contact at originator.
setOriginatorPOC(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata
Set the programmatic Point Of Contact at originator.
setOriginatorPOC(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the programmatic Point Of Contact at originator.
setOriginatorPosition(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata
Set the position of Programmatic Point Of Contact at originator.
setOriginatorPosition(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the position of Programmatic Point Of Contact at originator.
setOutputPulseType(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Set the output pulse type.
setOutputPulseWidth(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Set the output pulse width.
setOwner(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the owner of the space object.
setP(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Set the GLONASS P Word.
setP(int, double) - Method in class org.orekit.files.ccsds.ndm.odm.StateVector
Set position component.
setP1(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Set the GLONASS P1 Word.
setP2(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Set the GLONASS P2 Word.
setP3(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Set the the GLONASS P3 Word.
setP4(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Set the GLONASS P4 Word.
setPa(double) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Set the orbit argument of pericenter.
setPa(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Setter fir the Argument of Perigee (rad).
setParameterDerivatives(ParameterDriver, AbsoluteDate, double...) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Set the partial derivatives of the simulated measurement with respect to parameter.
setParameterDerivatives(ParameterDriver, TimeSpanMap<double[]>) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Set the partial derivatives of the simulated measurement with respect to parameter.
setParameters(double[]) - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Set the selected parameters.
setParametersConvergenceThreshold(double) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Set convergence threshold.
setParameterSpacing(int) - Method in class org.orekit.files.sinex.DcbDescription
Set the parameter spacing interval between the bias value.
setParticipants(Map<Integer, String>) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the participants.
setPatchPointComponentFreedom(int, int, boolean) - Method in class org.orekit.utils.AbstractMultipleShooting
Set a component of a patch point to free or not.
setPath(int[]) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the path.
setPath1(int[]) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the path1.
setPath2(int[]) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the path2.
setPeriapsisAltitude(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Set the distance of the closest point in the objects orbit above the equatorial radius of the central body.
setPhaseCenterSystem(SatelliteSystem) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Set satellite system for average phase center.
setPosition(Vector3D) - Method in class org.orekit.files.sinex.Station
Set the station position.
setPositionAngleType() - Method in class org.orekit.propagation.integration.FieldStateMapper
Set position angle type.
setPositionAngleType(PositionAngleType) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Set position angle type.
setPositionAngleType(PositionAngleType) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Set position angle type.
setPositionAngleType(PositionAngleType) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Set position angle type.
setPositionAngleType(PositionAngleType) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Set position angle type.
setPosVelBase(double) - Method in class org.orekit.files.sp3.SP3Header
Set the base for position/velocity accuracy.
setPredictionProvider(String) - Method in class org.orekit.files.ilrs.CRDHeader
Set the prediction provider.
setPredictionType(int) - Method in class org.orekit.files.ilrs.CRDHeader
Set the prediction type.
setPressSensorManufacturer(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
Set the pressure sensor manufacturer.
setPressSensorModel(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
Set the pressure sensor model.
setPressSensorSerialNumber(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
Set the pressure sensor serial number.
setPressure(double) - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction
Set the local pressure at the evaluation location
setPrevId(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination
Set identification of previous orbit determination.
setPrevId(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set identification of previous orbit determination.
setPrevID(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver
Set identification number of previous maneuver.
setPreviousMessageEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the UTC epoch of the previous CDM issued for the event identified by CONJUNCTION_ID.
setPreviousMessageEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the creation date of previous message from a given originator.
setPreviousMessageId(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the ID of previous CDM issued for event identified by CONJUNCTION_ID.
setPreviousMessageID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the unique ID identifying previous message from a given originator.
setPrf(double) - Method in class org.orekit.files.ilrs.CPFHeader
Set the Pulse Repetition Frequency (PRF).
setPrimaryWavelength(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
Set the primary wavelength.
setPrmMessageLink(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the Unique identifier of Pointing Request Message linked to this Orbit Data Message.
setPRN(int) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Setter for the PRN number of the satellite.
setPRN(int) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Setter for the PRN number of the satellite.
setProcessingSoftwareName(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.CalibrationTargetConfiguration
Set the processing software name.
setProcessingSoftwares(String[]) - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration
Set the processing softwares.
setProcessingSoftwareVersion(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.CalibrationTargetConfiguration
Set the processing software version.
setProcessingSoftwareVersions(String[]) - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration
Set the processing software versions.
setProductionEpoch(DateComponents) - Method in class org.orekit.files.ilrs.ILRSHeader
Set the date component of the ephemeris production.
setProductionHour(int) - Method in class org.orekit.files.ilrs.ILRSHeader
Set the hour of ephemeris production.
setProgramName(String) - Method in class org.orekit.files.rinex.clock.RinexClock
Setter for the program name.
setProgramName(String) - Method in class org.orekit.files.rinex.section.RinexBaseHeader
Setter for the program name.
setPropagator(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Set the orbit propagator used to generate this trajectory.
setProxy(Proxy.Type, String, int) - Method in class org.orekit.gnss.metric.ntrip.NtripClient
Set proxy parameters.
setPulseEnergy(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.CalibrationTargetConfiguration
Set the pulse energy.
setPulseEnergy(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
Set the pulse energy.
setPulseInOutgoingSemiTrain(int) - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
Set the number of pulses in outgoing semi-train.
setPulseWidth(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
Set the pulse width.
setQ(int, double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternion
Set quaternion component.
setQDot(int, double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternion
Set quaternion derivative component.
setQualityIndicator(int) - Method in class org.orekit.files.ilrs.CRDHeader
Set the data quality indicator.
setQuantumEfficiency(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Set the quantum efficiency at applicable wavelength.
setQzssCodeOnL2(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data
Set the QZSS code on L2.
setQzssFitInterval(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data
Set the QZSS fit interval.
setQzssNavigationMessage(QZSSLegacyNavigationMessage) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data
Set the QZSS navigation message.
setQzssToc(double) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data
Set the QZSS time of clock.
setRaan(double) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Set the orbit right ascension of ascending node.
setRangeMode(RangeMode) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the rangeMode.
setRangeType(int) - Method in class org.orekit.files.ilrs.CRDHeader
Set the range type indicator.
setRangeUnits(RangeUnits) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the rangeUnits.
setRateFrameIsA(boolean) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Set the frame in which rates are specified.
setRateFrameIsA(boolean) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler
Set the frame in which rates are specified.
setRateProcessNoiseStdDev(double) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination
Set process noise standard deviation if AttitudeDetermination.rateStates is RateElementsType.ANGVEL.
setRateStates(RateElementsType) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination
Set attitude rate states.
setRateType(RateElementsType) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata
Set attitude rate element set type.
setRawCoefficients(boolean, Flattener, double[], double[], String) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Set the tesseral-sectorial coefficients matrix.
setRawCorrectionRange(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the raw correction for range.
setRawRangeModulus(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the raw range modulus.
setRbar(double) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Set the critical distance from the center of the central body at which the atmosphere is considered to end, i.e.
setRcs(double) - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties
Set the typical (50th percentile) radar cross-section.
setRdmMessageLink(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the Unique identifier of Reentry Data Message linked to this Orbit Data Message.
setReadComplete(boolean) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Set the indicator for completed read.
setReceiveBand(String) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the receiveBand.
setReceiveDelays(Map<Integer, Double>) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the receiveDelays.
setReceiverClockModel(ClockModel) - Method in class org.orekit.files.rinex.observation.RinexObservationWriter
Set receiver clock model.
setReceiverNumber(String) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Set the number of the receiver.
setReceiverType(String) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Set the type of the receiver.
setReceiverVersion(String) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Set the version of the receiver.
setRecommendedOdSpan(double) - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters
Set the recommended OD time span calculated for the object.
setRecommendedOdSpan(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set time span of observation recommended for the OD of the object.
setReconnectParameters(double, double, int) - Method in class org.orekit.gnss.metric.ntrip.NtripClient
Set Reconnect parameters.
setReductionTheory(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set reduction theory used for precession and nutation modeling.
setReferenceDate(AbsoluteDate) - Method in class org.orekit.utils.ParameterDriver
Set reference date.
setReferenceEpoch(AbsoluteDate) - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage
Set the reference epoch.
setReferenceEpoch(AbsoluteDate) - Method in class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage
Set the reference epoch.
setReferenceFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.odm.CartesianCovariance
Set the reference frame in which data are given.
setReferenceFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.odm.OdmCommonMetadata
Set the reference frame in which data are given: used for state vector and Keplerian elements data (and for the covariance reference frame if none is given).
setReferenceFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver
Set Coordinate system for velocity increment vector.
setReferenceFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Set the reference frame in which data are given: used for RADEC tracking data.
setReferenceState(SpacecraftState) - Method in class org.orekit.propagation.AbstractMatricesHarvester
Set up reference state.
setReferenceState(SpacecraftState) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester
Set up reference state.
setReferenceState(SpacecraftState) - Method in interface org.orekit.propagation.MatricesHarvester
Set up reference state.
setReferenceState(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester
Set up reference state.
setReferenceTimeSystem(TimeSystem) - Method in class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage
Set the time system used as a reference to define a time system.
setReferenceTrajectories(Propagator[]) - Method in class org.orekit.estimation.sequential.KalmanModel
Setter for the reference trajectories.
setReferenceValue(double) - Method in class org.orekit.utils.ParameterDriver
Set reference parameter value.
setRefFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set the name of the reference frame in which the state vector data are given.
setRefFrame(Frame) - Method in class org.orekit.files.ilrs.CPFHeader
Set the reference frame.
setRefFrameId(int) - Method in class org.orekit.files.ilrs.CPFHeader
Set the reference frame identifier.
setReflectance(double) - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties
Set the typical (50th percentile) coefficient of reflectance.
setRegionCode(RegionCode) - Method in class org.orekit.files.rinex.navigation.IonosphereKlobucharMessage
Set the region code.
setRelativeMetadata(CdmRelativeMetadata) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set the relative metadata following header, they are the common metadata for the CDM.
setRelativePositionN(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the N component of Object2’s position relative to Object1’s in RTN frame.
setRelativePositionR(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the R component of Object2’s position relative to Object1’s in RTN frame.
setRelativePositionT(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the T component of Object2’s position relative to Object1’s in RTN frame.
setRelativeSpeed(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the norm of relative velocity vector at TCA.
setRelativeVelocityN(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the N component of Object2’s velocity relative to Object1’s in RTN frame.
setRelativeVelocityR(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the R component of Object2’s velocity relative to Object1’s in RTN frame.
setRelativeVelocityT(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the T component of Object2’s velocity relative to Object1’s in RTN frame.
setRemainingDv(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Set the total ΔV remaining for spacecraft.
setResetAtEnd(boolean) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Allow/disallow resetting the initial state at end of propagation.
setResetAtEnd(boolean) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Allow/disallow resetting the initial state at end of propagation.
setResidualsAccepted(double) - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters
Set the percentage of residuals accepted in the OD of the object (from 0 to 100).
setRevAtEpoch(int) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
Set the revolution rumber.
setRolloverReference(DateComponents) - Static method in class org.orekit.time.GNSSDate
Set a reference date for ensuring continuity across GNSS week rollover.
setRotationalAngleType(int) - Method in class org.orekit.files.ilrs.CPFHeader
Set the rotation angle type.
setRunByName(String) - Method in class org.orekit.files.rinex.section.RinexBaseHeader
Setter for the run/by name.
setSatConfiguration(int) - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac
Sets the satellite configuration.
setSatelliteID(int) - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionData
Set the satellite ID.
setSatelliteID(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.RtcmEphemerisData
Set the satellite ID.
setSatelliteID(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgmData
Set the satellite ID.
setSatelliteReferenceDatum(int) - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmOrbitCorrectionHeader
Set the satellite reference datum.
setSatelliteRevolution(int) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Override the default value of the parameter.
setSatelliteRevolution(int) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Override the default value of the parameter.
setSatelliteSystem(SatelliteSystem) - Method in class org.orekit.files.rinex.clock.RinexClock
Setter for the satellite system.
setSatelliteSystem(SatelliteSystem) - Method in class org.orekit.files.rinex.section.RinexBaseHeader
Setter for the satellite system.
setSatelliteType(BeidouSatelliteType) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage
Setter for satellite type.
setSbasId(SbasId) - Method in class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage
Set the SBAS Id.
setScale(double) - Method in class org.orekit.utils.ParameterDriver
Set scale.
setScaleLength(double) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPMultipleShooter
Set the scale length.
setScaleLength(double) - Method in class org.orekit.utils.AbstractMultipleShooting
Set the scale length.
setScalePositionDefects(double) - Method in class org.orekit.control.indirect.shooting.AbstractFixedBoundaryCartesianSingleShooting
Setter for scale of position defects.
setScaleTime(double) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPMultipleShooter
Set the scale time.
setScaleTime(double) - Method in class org.orekit.utils.AbstractMultipleShooting
Set the scale time.
setScaleVelocityDefects(double) - Method in class org.orekit.control.indirect.shooting.AbstractFixedBoundaryCartesianSingleShooting
Setter for scale of velocity defects.
setSclkOffsetAtEpoch(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the spacecraft clock count at OcmMetadata.getEpochT0().
setSclkSecPerSISec(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the number of spacecraft clock seconds occurring during one SI second.
setScreenEntryTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the time in UTC when Object2 enters the screening volume.
setScreenExitTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the time in UTC when Object2 exits the screening volume.
setScreeningDataSource(String) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadata
Set the source (or origin) of the specific orbital data for this object.
setScreenPcThreshold(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the collision probability screening threshold used to identify this conjunction.
setScreenType(ScreenType) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the type of screening to be used.
setScreenVolumeFrame(ScreenVolumeFrame) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the name of the Object1 centered reference frame in which the screening volume data are given.
setScreenVolumeRadius(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
set the screen volume radius.
setScreenVolumeShape(ScreenVolumeShape) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the shape of the screening volume.
setScreenVolumeX(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the R or T (depending on if RTN or TVN is selected) component size of the screening volume in the corresponding frame.
setScreenVolumeY(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the T or V (depending on if RTN or TVN is selected) component size of the screening volume in the corresponding frame.
setScreenVolumeZ(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the N component size of the screening volume in the corresponding frame.
setSecondsOfWeek(double) - Method in class org.orekit.files.sp3.SP3Header
Set the seconds of the GPS week for this SP3 file.
setSecularVariationCoefficients(int, int, double, double) - Method in class org.orekit.models.earth.GeoMagneticField
Set the given secular variation coefficients.
setSedr(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Set the amount of energy being removed from the object’s orbit by atmospheric drag.
setSedr(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set Specific Energy Dissipation Rate.
setSefiCollisionProbability(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the Space Environment Fragmentation Impact probability.
setSefiCollisionProbabilityMethod(PocMethodFacade) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the Space Environment Fragmentation Impact probability method.
setSefiFragmentationModel(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the Space Environment Fragmentation Impact fragmentation model.
setSegments(List<S>) - Method in class org.orekit.files.ccsds.ndm.NdmConstituent
Set the segments.
setSelected(boolean) - Method in class org.orekit.utils.ParameterDriver
Configure a parameter selection status.
setSelectedCoefficients(Set<String>) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Set the selected short periodic coefficients that must be stored as additional states.
setSelectedCoefficients(Set<String>) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Set the selected short periodic coefficients that must be stored as additional states.
setSensorFrequency(double) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationSensor
Set frequency of sensor data for sensor.
setSensorNoiseCovariance(double[]) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationSensor
Set standard deviation of sensor noise for sensor.
setSensorNumber(int) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationSensor
Set number of the sensor.
setSensors(List<String>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set description of sensors used.
setSensorsN(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set number of sensors used.
setSensorUsed(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationSensor
Set sensor used.
setSequenceNumber(int) - Method in class org.orekit.files.ilrs.ILRSHeader
Set the ephemeris sequence number.
setShadowBodies(List<BodyFacade>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set celestial bodies casting shadows.
setShadowModel(ShadowModel) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set shadow model used for solar radiation pressure.
setShortPeriodTerms(List<ShortPeriodTerms>) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Override the default value short periodic terms.
setSic(String) - Method in class org.orekit.files.ilrs.ILRSHeader
Set the SIC ID.
setSigma(double[]) - Method in class org.orekit.estimation.measurements.modifiers.DynamicOutlierFilter
Set the current value of sigma.
setSigmaU(double) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination
Set rate random walk if AttitudeDetermination.rateStates is RateElementsType.GYRO_BIAS.
setSigmaV(double) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination
Set angle random walk if AttitudeDetermination.rateStates is RateElementsType.GYRO_BIAS.
setSignalStrengthUnit(String) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Set the unit of the carrier to noise ratio observables.
setSisa(double) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage
Setter for the signal in space accuracy.
setSisaiOc1(int) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage
Setter for Signal In Space Accuracy Index (clock drift accuracy).
setSisaiOc2(int) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage
Setter for Signal In Space Accuracy Index (clock drift rate accuracy).
setSisaiOcb(int) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage
Setter for Signal In Space Accuracy Index (radial and clock).
setSisaiOe(int) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage
Setter for Signal In Space Accuracy Index (along track and across track).
setSismai(int) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage
Setter for Signal In Space Monitoring Accuracy Index.
setSiteCode(String) - Method in class org.orekit.files.sinex.Station
Set the site code (station identifier).
setSma(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Setter for the semi-major axis.
setSnm(double[][]) - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data
Set the sine parameters of spherical harmonics expansion of degree N and order M.
setSoftwareId(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration
Set the software configuration ID.
setSolarRadArea(double) - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters
Set the solar radiation pressure area.
setSolarRadCoeff(double) - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters
Get the solar radiation pressure coefficient.
setSolarRadiationPressure(YesNoUnknown) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set Enum that indicates if Solar Radiation Pressure is taken into account or not.
setSolidTidesModel(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set solid tides model.
setSolveN(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set number of solved-for states.
setSolveStates(List<String>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set description of state elements solved-for.
setSource(String) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination
Set source of attitude estimate.
setSource(String) - Method in class org.orekit.files.ilrs.CPFHeader
Set the ephemeris source.
setSource(String) - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac
Sets the source of this GPS almanac.
setSource(String) - Method in class org.orekit.propagation.analytical.gnss.data.QZSSAlmanac
Sets the source of this GPS almanac.
setSpacecraftClockAndDriftApplied(int) - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
Set the spacecraft clock offset and drift applied indicator.
setSpacecraftEpochTimeScale(int) - Method in class org.orekit.files.ilrs.CRDHeader
Set the spacecraft epoch time scale.
setSpaceWeatherEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set epoch of the Space Weather data.
setSpaceWeatherSource(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set Space Weather data source.
setSpatialFilter(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Set the spatial filter.
setSpectralFilter(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Set the spectral filter.
setSphericalHarmonicsDegree(int) - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data
Set the degree of spherical harmonic expansion.
setSphericalHarmonicsOrder(int) - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data
Set the order of spherical harmonic expansion.
setSpinAlpha(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
Set the right ascension of spin axis vector (rad).
setSpinAngle(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
Set the phase of the satellite about the spin axis (rad).
setSpinAngleVel(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
Set the angular velocity of satellite around spin axis (rad/s).
setSpinDelta(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
Set the declination of the spin axis vector (rad).
setSqrtA(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Setter for the Square Root of Semi-Major Axis (√m).
setSqrtA(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouAlmanac
Sets the Square Root of Semi-Major Axis (m^1/2).
setSqrtA(double) - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac
Setter for the Square Root of Semi-Major Axis (m^1/2).
setSqrtA(double) - Method in class org.orekit.propagation.analytical.gnss.data.IRNSSAlmanac
Setter for the Square Root of Semi-Major Axis (m^1/2).
setSqrtA(double) - Method in class org.orekit.propagation.analytical.gnss.data.QZSSAlmanac
Setter for the Square Root of Semi-Major Axis (m^1/2).
setSrpCoefficient(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Set the nominal SRP coefficient.
setSrpConstantArea(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Set the attitude-independent SRP area, not already into attitude-dependent area along OEB.
setSrpModel(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set Solar Radiation Pressure model.
setSrpUncertainty(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Set the SRP coefficient 1σ uncertainty.
setSsrEpoch1s(double) - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader
Set the SSR Epoch Time 1s.
setSsrMultipleMessageIndicator(int) - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader
Set the SSR Multiple Message Indicator.
setSsrProviderId(int) - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionHeader
Set the SSR Provider ID.
setSsrProviderId(int) - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader
Set the SSR Provider ID.
setSsrSolutionId(int) - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionHeader
Set the SSR Solution ID.
setSsrSolutionId(int) - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader
Set the SSR Solution ID.
setSsrUpdateInterval(int) - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader
Set the SSR Update Interval.
setSsrUpdateInterval(SsrUpdateInterval) - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionHeader
Set the SSR Update Interval.
setSsrUra(double) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm07Data
Set the SSR User Range Accuracy (URA).
setStartDate(AbsoluteDate) - Method in class org.orekit.propagation.AbstractPropagator
Set a start date.
setStartDate(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator
Set a start date.
setStartEpoch(AbsoluteDate) - Method in class org.orekit.files.ilrs.ILRSHeader
Set the staring epoch (UTC).
setStartScreenPeriod(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the start time in UTC of the screening period for the conjunction assessment.
setStartTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata
Set the time of the earliest data contained in the OCM.
setStartTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Set start of total time span covered by attitude data.
setStartTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the time of the earliest data contained in the OCM.
setStartTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata
Set start of total time span covered by ephemerides data and covariance data.
setStartTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the startTime.
setStateDerivatives(int, double[]...) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Set the partial derivatives of the simulated measurement with respect to state Cartesian coordinates.
setStationClockAndDriftApplied(int) - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
Set the station clock offset and drift applied indicator.
setStationIdentifier(String) - Method in class org.orekit.files.rinex.clock.RinexClock
Setter for the station identifier.
setStationInformation(String) - Method in class org.orekit.files.rinex.section.RinexBaseHeader
Setter for the station information.
setStationName(String) - Method in class org.orekit.files.ilrs.CRDHeader
Set the station name from official list.
setStationName(String) - Method in class org.orekit.files.rinex.clock.RinexClock
Setter for the station name.
setStationNetword(String) - Method in class org.orekit.files.ilrs.CRDHeader
Set the station network.
setStationOscDrift(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
Set the estimated station oscillator drift in parts in 10¹⁵.
setStationUTCOffset(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
Set the estimated station UTC offset.
setStatus(EstimatedMeasurementBase.Status) - Method in class org.orekit.estimation.measurements.EstimatedMeasurementBase
Set the status.
setStatusFlags(double) - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage
Set status flag.
setStep(int) - Method in class org.orekit.files.ilrs.CPFHeader
Set the time between table entries.
setStepHandler(double, OrekitFixedStepHandler) - Method in interface org.orekit.propagation.Propagator
Set a single handler for fixed stepsizes.
setStepHandler(FieldOrekitStepHandler<T>) - Method in interface org.orekit.propagation.FieldPropagator
Set a single handler for variable stepsizes.
setStepHandler(OrekitStepHandler) - Method in interface org.orekit.propagation.Propagator
Set a single handler for variable stepsizes.
setStepHandler(T, FieldOrekitFixedStepHandler<T>) - Method in interface org.orekit.propagation.FieldPropagator
Set a single handler for fixed stepsizes.
setStopScreenPeriod(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the stop time in UTC of the screening period for the conjunction assessment.
setStopTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata
Set the time of the latest data contained in the OCM.
setStopTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Set end of total time span covered by attitude data.
setStopTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the time of the latest data contained in the OCM.
setStopTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata
Set end of total time span covered by ephemerides data and covariance data.
setStopTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the stopTime.
setSubDailySequenceNumber(int) - Method in class org.orekit.files.ilrs.CPFHeader
Set the sub-daily ephemeris sequence number.
setSumOfAllConstantDelays(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.CalibrationTargetConfiguration
Set the sum of all constant delays (electronic, geometric, optical) that are not included in the time of flight measurements or time- variant or point angle-variant delays in the “42” record below (m, one way).
setSupportedNames(String) - Method in class org.orekit.data.AbstractSelfFeedingLoader
Set the supported names regular expression.
setSurveyedTargetDistance(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.CalibrationTargetConfiguration
Set the surveyed target distance.
setSurveyError(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.CalibrationTargetConfiguration
Set the survey error.
setSvAccuracy(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouLegacyNavigationMessage
Setter for the user SV accuracy.
setSvAccuracy(double) - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage
Setter for the user SV accuracy.
setSvAccuracy(double) - Method in class org.orekit.propagation.analytical.gnss.data.LegacyNavigationMessage
Setter for the user SV accuracy.
setSvHealth(double) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1042Data
Set the satellite health status.
setSvHealth(double) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage
Setter for the SV health status.
setSvHealth(double) - Method in class org.orekit.propagation.analytical.gnss.data.IRNSSNavigationMessage
Setter for the satellite health status.
setSvHealth(int) - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage
Setter for the satellite health status.
setSvHealth(int) - Method in class org.orekit.propagation.analytical.gnss.data.LegacyNavigationMessage
Setter for the satellite health status.
setSVN(int) - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac
Sets the "SVN" reference number.
setSystemId(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.SystemConfiguration
Set the system configuration ID.
setSystemIdentifier(int) - Method in class org.orekit.files.ilrs.CRDHeader
Set the system identifier.
setSystemNumber(int) - Method in class org.orekit.files.ilrs.CRDHeader
Set the system number.
setSystemOccupancy(int) - Method in class org.orekit.files.ilrs.CRDHeader
Set the system occupancy.
setTaimutcT0(double) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata
Set the difference (TAI – UTC) in seconds at epoch AcmMetadata.getEpochT0().
setTaimutcT0(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the difference (TAI – UTC) in seconds at epoch OcmMetadata.getEpochT0().
setTargetAttitude(Rotation) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver
Set target attitude (if purpose is attitude adjustment).
setTargetClass(int) - Method in class org.orekit.files.ilrs.ILRSHeader
Set the target class.
setTargetLocation(int) - Method in class org.orekit.files.ilrs.ILRSHeader
Set the target location.
setTargetMomentum(Vector3D) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver
Set target momentum (if purpose is momentum desaturation).
setTargetMomFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver
Set reference frame for AttitudeManeuver.getTargetMomentum().
setTargetName(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.CalibrationTargetConfiguration
Set the target name or ID.
setTargetSpinRate(double) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver
Set target spin rate (if purpose is spin rate adjustment).
setTauC(double) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Set the GLONASS time scale correction to UTC time.
setTauGps(double) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Set the correction to GPS time relative to GLONASS time.
setTauN(double) - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage
Setter for the SV clock bias.
setTca(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the date and time in UTC of the closest approach.
setTdmMessageLink(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the Unique identifier of Tracking Data Message linked to this Orbit Data Message.
setTechAddress(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the address of Technical Point Of Contact at originator.
setTechEmail(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the email address of Technical Point Of Contact at originator.
setTechOrg(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the creating agency or operator.
setTechPhone(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the phone number of Technical Point Of Contact at originator.
setTechPOC(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the Technical Point Of Contact at originator.
setTechPosition(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the position of Technical Point Of Contact at originator.
setTemperature(double) - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction
Set the local temperature at the evaluation location
setTempSensorManufacturer(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
Set the temperature sensor manufacturer.
setTempSensorModel(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
Set the temperature sensor model.
setTempSensorSerialNumber(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
Set the temperature sensor serial number.
setTFirstObs(AbsoluteDate) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Set the time of First observation record.
setTGD(double) - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage
Setter for the Group Delay Differential (s).
setTGD(double) - Method in class org.orekit.propagation.analytical.gnss.data.IRNSSNavigationMessage
Setter for the Group Delay Differential (s).
setTGD(double) - Method in class org.orekit.propagation.analytical.gnss.data.LegacyNavigationMessage
Setter for the Group Delay Differential (s).
setTGD1(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouLegacyNavigationMessage
Setter for the B1/B3 Group Delay Differential (s).
setTGD2(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouLegacyNavigationMessage
Setter for the B2/B3 Group Delay Differential (s).
setTgdB1Cp(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage
Setter for B1/B3 Group Delay Differential (s).
setTgdB2ap(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage
Setter for B2 AP Group Delay Differential (s).
setTgdB2bI(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage
Setter for B2B_i / B3I Group Delay Differential (s).
setThrust(int, double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Set thrust component.
setThrustAcceleration(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Set the object’s acceleration due to in-track thrust used to propagate the state vector and covariance to TCA.
setThrustDirectionSigma(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Set one σ angular off-nominal thrust direction.
setThrustEfficiency(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Set thrust efficiency η.
setThrustInterpolation(OnOff) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Set interpolation mode between current and next thrust line.
setThrustIsp(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Set thrust specific impulse.
setThrustMagnitudeSigma(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver
Set one σ percent error on thrust magnitude.
setTideSystem(TideSystem) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Set the TideSystem used in the gravity field.
setTime(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Setter for the reference time of the orbit as a duration from week start.
setTime(double) - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage
Setter for the message frame time.
setTime(double) - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage
Setter for the reference time of the SBAS orbit in GPS seconds of the week.
setTimeLastObsEnd(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters
Set the start of a time interval (UTC) that contains the time of the last accepted observation.
setTimeLastObsStart(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters
Set the start of a time interval (UTC) that contains the time of the last accepted observation.
setTimeout(int) - Method in class org.orekit.data.NetworkCrawler
Set the timeout for connection.
setTimeout(int) - Method in class org.orekit.gnss.metric.ntrip.NtripClient
Set timeout for connections and reads.
setTimer(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration
Set the timer name.
setTimerSerialNumber(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration
Set the timer serial number.
setTimeScale(TimeScale) - Method in class org.orekit.files.ilrs.CPF
Set the time scale.
setTimeScale(TimeScale) - Method in class org.orekit.files.rinex.clock.RinexClock
Setter for the data time scale.
setTimeSinceFirstObservation(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set time elapsed between first accepted observation on epoch.
setTimeSinceLastObservation(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set time elapsed between last accepted observation on epoch.
setTimeSource(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration
Set the time source.
setTimeSpan(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the span of time in seconds that the OCM covers.
setTimeSystem(TimeSystem) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the Time System that: for CDM, is used for relative metadata, metadata, OD parameters, state vector.
setTimeSystem(TimeSystem) - Method in class org.orekit.files.ccsds.section.Metadata
Set the Time System that: for OPM, is used for metadata, state vector, maneuver and covariance data, for OMM, is used for metadata, orbit state and covariance data, for OEM, is used for metadata, ephemeris and covariance data.
setTimeSystem(TimeSystem) - Method in class org.orekit.files.rinex.clock.RinexClock
Setter for the file time system.
setTimeSystem(TimeSystem) - Method in class org.orekit.files.sinex.DcbDescription
Set the time system used for DCB data.
setTimeSystem(TimeSystem) - Method in class org.orekit.files.sp3.SP3Header
Set the time system used in this SP3 file.
setTimetagRef(TimetagReference) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the timetagRef.
setTk(double) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Set the time referenced to the beginning of the frame within the current day.
setTLastObs(AbsoluteDate) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Set the time of last observation record.
setToleranceMassAdjoint(double) - Method in class org.orekit.control.indirect.shooting.AbstractFixedBoundaryCartesianSingleShooting
Setter for mass adjoint tolerance.
setTorque(int, double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver
Set the torque vector (N.m).
setTrackId(String) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the tracking data identifier.
setTrackingSoftwares(String[]) - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration
Set the tracking softwares.
setTrackingSoftwareVersions(String[]) - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration
Set the tracking software versions.
setTracksAvailable(int) - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters
Set the number of sensor tracks available for the OD of the object.
setTracksAvailable(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set number of sensors tracks available for the OD within the actual OD span.
setTracksUsed(int) - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters
Set the number of sensor tracks used for the OD of the object.
setTracksUsed(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set number of sensors tracks accepted for the OD within the actual OD span.
setTrajBasis(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Set basis of this trajectory state time history data.
setTrajBasisID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Set identification number of the orbit determination or simulation upon which this trajectory is based.
setTrajFrameEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Set epoch of the trajectory reference frame.
setTrajID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Set trajectory identification number.
setTrajNextID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Set identification number of next trajectory.
setTrajPrevID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Set identification number of previous trajectory.
setTrajReferenceFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Set reference frame of the trajectory.
setTrajType(OrbitElementsType) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Set trajectory element set type.
setTrajUnits(List<Unit>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Set trajectory element set units.
setTransmissionOfSpectralFilter(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Set the percentage of transmission of spectral filter.
setTransmissionTime(double) - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage
Set the message transmission time.
setTransmissionTime(double) - Method in class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage
Set the message transmission time.
setTransmissionTime(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Setter for transmission time.
setTransmitBand(String) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the transmitBand.
setTransmitDelays(Map<Integer, Double>) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the transmitDelays.
setTransmitTime(AbsoluteDate) - Method in class org.orekit.files.rinex.navigation.IonosphereBaseMessage
Set the transmit time.
setTranspClkRef(double) - Method in class org.orekit.files.ilrs.CPFHeader
Set the transponder Clock Reference Time.
setTranspClkRefTime(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
Set the transponder clock reference time.
setTransponderId(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
Set the transponder configuration ID.
setTranspOscDrift(double) - Method in class org.orekit.files.ilrs.CPFHeader
Set the transponder Oscillator Drift in parts.
setTranspOscDrift(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
Set the estimated transponder oscillator drift in parts in 10¹⁵.
setTranspTransmitDelay(double) - Method in class org.orekit.files.ilrs.CPFHeader
Set the transponder transmit delay.
setTranspUtcOffset(double) - Method in class org.orekit.files.ilrs.CPFHeader
Set the transponder UTC offset.
setTranspUTCOffset(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
Set the estimated transponder UTC offset.
setTurnaroundDenominator(int) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the turnaroundDenominator.
setTurnaroundNumerator(int) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the turnaroundNumerator.
setTypAreaForCollisionProbability(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Get the typical (50th percentile) cross-sectional area for collision probability estimation purposes.
setType(SP3FileType) - Method in class org.orekit.files.sp3.SP3Header
Set the file type for this SP3 file.
setTypeObs(SatelliteSystem, List<ObservationType>) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Set number of observations for a satellite.
setUpEventDetector(FieldODEIntegrator<T>, FieldEventDetector<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Wrap an Orekit event detector and register it to the integrator.
setUpEventDetector(ODEIntegrator, EventDetector) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Wrap an Orekit event detector and register it to the integrator.
setupMatricesComputation(String, RealMatrix, DoubleArrayDictionary) - Method in class org.orekit.propagation.AbstractPropagator
Set up computation of State Transition Matrix and Jacobians matrix with respect to parameters.
setupMatricesComputation(String, RealMatrix, DoubleArrayDictionary) - Method in interface org.orekit.propagation.Propagator
Set up computation of State Transition Matrix and Jacobians matrix with respect to parameters.
setupMatricesComputation(String, RealMatrix, DoubleArrayDictionary) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Set up computation of State Transition Matrix and Jacobians matrix with respect to parameters.
setUpStmAndJacobianGenerators() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Set up State Transition Matrix and Jacobian matrix handling.
setUpStmAndJacobianGenerators() - Method in class org.orekit.propagation.numerical.NumericalPropagator
Set up State Transition Matrix and Jacobian matrix handling.
setUpStmAndJacobianGenerators() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Set up State Transition Matrix and Jacobian matrix handling.
setUpUserEventDetectors() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Set up all user defined event detectors.
setUpUserEventDetectors() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Set up all user defined event detectors.
setURA(double) - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage
Setter for the user range accuracy.
setURA(double) - Method in class org.orekit.propagation.analytical.gnss.data.IRNSSNavigationMessage
Setter for the user range accuracy.
setURA(double) - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage
Setter for the user range accuracy.
setURA(int) - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac
Sets the average URA number.
setUraiEd(int) - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage
Setter for Elevation-Dependent User Range Accuracy.
setUraiNed0(int) - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage
Setter for term 0 of Non-Elevation-Dependent User Range Accuracy.
setUraiNed1(int) - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage
Setter for term 1 of Non-Elevation-Dependent User Range Accuracy.
setUraiNed2(int) - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage
Setter for term 2 of Non-Elevation-Dependent User Range Accuracy.
setUseableStartTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Set start of useable time span covered by attitude data.
setUseableStartTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Set start of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.
setUseableStartTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata
Set start of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.
setUseableStopTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Set end of useable time span covered by ephemerides data.
setUseableStopTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Set end of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.
setUseableStopTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata
Set end of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.
setUserDefinedBlock(UserDefined) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmData
Set the user defined logical block.
setUt1MinusUtc(double) - Method in class org.orekit.files.sinex.SinexEopEntry
Set the UT1-UTC offset.
setUt1mutcT0(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the difference (UT1 – UTC) in seconds at epoch OcmMetadata.getEpochT0().
setUtcId(UtcId) - Method in class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage
Set the UTC Id.
setV(int, double) - Method in class org.orekit.files.ccsds.ndm.odm.StateVector
Set velocity component.
setValidFrom(AbsoluteDate) - Method in class org.orekit.files.sinex.Station
Set the start of validity.
setValidUntil(AbsoluteDate) - Method in class org.orekit.files.sinex.Station
Set the end of validity.
setValue(double) - Method in class org.orekit.utils.ParameterDriver
Set parameter value.
setValue(double, AbsoluteDate) - Method in class org.orekit.utils.ParameterDriver
Set parameter value at specific date.
setValueSpanMap(ParameterDriver) - Method in class org.orekit.utils.ParameterDriver
Set current parameter value span map to match another driver.
setVelocity(Vector3D) - Method in class org.orekit.files.sinex.Station
Set the station velocity.
setVersion(char) - Method in class org.orekit.files.sp3.SP3Header
Set the file version.
setVersion(int) - Method in class org.orekit.files.ilrs.ILRSHeader
Set the format version.
setVmAbsolute(double) - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties
Set the typical (50th percentile) visual magnitude.
setVmApparent(double) - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties
Set the typical (50th percentile) apparent visual magnitude.
setVmApparentMax(double) - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties
Set the maximum apparent visual magnitude.
setVmApparentMin(double) - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties
Set the minimum apparent visual magnitude.
setVtecQualityIndicator(double) - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Header
Set the VTEC quality indicator.
setWavelength(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.SystemConfiguration
Set the transmit wavelength.
setWeek(int) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Setter for the reference week of the orbit.
setWeightedRms(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set weighted RMS residual ratio.
setWeightedRMS(double) - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters
Set the weighted Root Mean Square (RMS) of the residuals from a batch least squares OD.
setWetMass(double) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalProperties
Set the total mass at T₀.
setWetMass(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties
Set the total mass at T₀.
setX(double) - Method in class org.orekit.files.ccsds.ndm.cdm.StateVector
Set object Position Vector X component.
setX(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Setter for the satellite X position.
setXdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.StateVector
Set object Velocity Vector X component.
setXDot(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Setter for the satellite X velocity.
setXDotDot(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Setter for the satellite X acceleration.
setXp(double) - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage
Set the X component of the pole.
setXpDot(double) - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage
Set the X component of the pole first derivative.
setXpDotDot(double) - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage
Set the X component of the pole second derivative.
setxPo(double) - Method in class org.orekit.files.sinex.SinexEopEntry
Set the X polar motion.
setY(double) - Method in class org.orekit.files.ccsds.ndm.cdm.StateVector
Set object Position Vector Y component.
setY(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Setter for the satellite Y position.
setYawAngle(double) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data
Set the yaw angle used for computation of phase wind-up correction.
setYawRate(double) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data
Set the yaw rate.
setYdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.StateVector
Set object Velocity Vector Y component.
setYDot(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Setter for the satellite Y velocity.
setYDotDot(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Setter for the satellite Y acceleration.
setYearOfCentury(int) - Method in class org.orekit.files.ilrs.CRDHeader
Set the year of century from CPF or TLE.
setYp(double) - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage
Set the Y component of the pole.
setYpDot(double) - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage
Set the Y component of the pole first derivative.
setYpDotDot(double) - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage
Set the Y component of the pole second derivative.
setyPo(double) - Method in class org.orekit.files.sinex.SinexEopEntry
Set the Y polar motion.
setZ(double) - Method in class org.orekit.files.ccsds.ndm.cdm.StateVector
Set object Position Vector Z component.
setZ(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Setter for the satellite Z position.
setZdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.StateVector
Set object Velocity Vector Z component.
setZDot(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Setter for the satellite Z velocity.
setZDotDot(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Setter for the satellite Z acceleration.
SEVERAL_REFERENCE_DATES_IN_GRAVITY_FIELD - org.orekit.errors.OrekitMessages
SEVERAL_REFERENCE_DATES_IN_GRAVITY_FIELD.
SEZ_INERTIAL - org.orekit.files.ccsds.definitions.OrbitRelativeFrame
South, East, Zenith coordinate system.
SEZ_ROTATING - org.orekit.files.ccsds.definitions.OrbitRelativeFrame
South, East, Zenith coordinate system.
SF - org.orekit.files.ccsds.definitions.OdMethodType
Sequential Filter.
SFU - Static variable in class org.orekit.files.rinex.navigation.IonosphereNequickGMessage
Converter for Nequick-G aᵢ₀ parameter.
SFU_PER_DEG - Static variable in class org.orekit.files.rinex.navigation.IonosphereNequickGMessage
Converter for Nequick-G aᵢ₁ parameter.
SFU_PER_DEG2 - Static variable in class org.orekit.files.rinex.navigation.IonosphereNequickGMessage
Converter for Nequick-G aᵢ₂ parameter.
SGP - Static variable in class org.orekit.propagation.analytical.tle.FieldTLE
Identifier for SGP type of ephemeris.
SGP - Static variable in class org.orekit.propagation.analytical.tle.TLE
Identifier for SGP type of ephemeris.
SGP_SGP4_THEORY - Static variable in class org.orekit.files.ccsds.ndm.odm.omm.OmmMetadata
Constant for SGP/SGP4 mean elements theory.
SGP4 - Class in org.orekit.propagation.analytical.tle
This class contains methods to compute propagated coordinates with the SGP4 model.
SGP4 - Static variable in class org.orekit.propagation.analytical.tle.FieldTLE
Identifier for SGP4 type of ephemeris.
SGP4 - Static variable in class org.orekit.propagation.analytical.tle.TLE
Identifier for SGP4 type of ephemeris.
SGP4(TLE, AttitudeProvider, double) - Constructor for class org.orekit.propagation.analytical.tle.SGP4
Constructor for a unique initial TLE.
SGP4(TLE, AttitudeProvider, double, Frame) - Constructor for class org.orekit.propagation.analytical.tle.SGP4
Constructor for a unique initial TLE.
SGP4_XP_THEORY - Static variable in class org.orekit.files.ccsds.ndm.odm.omm.OmmMetadata
Constant for SGP4-XP mean elements theory.
SGP4OrbitalState - Class in org.orekit.propagation.conversion.averaging
Class representing an averaged orbital state as in the TLE-related theory.
SGP4OrbitalState(AbsoluteDate, AveragedKeplerianWithMeanAngle) - Constructor for class org.orekit.propagation.conversion.averaging.SGP4OrbitalState
Constructor with default data context.
SGP4OrbitalState(AbsoluteDate, AveragedKeplerianWithMeanAngle, DataContext) - Constructor for class org.orekit.propagation.conversion.averaging.SGP4OrbitalState
Constructor.
SGP8 - Static variable in class org.orekit.propagation.analytical.tle.FieldTLE
Identifier for SGP8 type of ephemeris.
SGP8 - Static variable in class org.orekit.propagation.analytical.tle.TLE
Identifier for SGP8 type of ephemeris.
SHA_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory
Default regular expression for SHA files.
SHADOW_BODIES - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey
Names of shadow bodies.
SHADOW_MODEL - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey
Shadow model used for solar radiation pressure.
ShadowModel - Enum in org.orekit.files.ccsds.ndm.odm.ocm
Shadow model for solar radiation pressure.
SHAFormatReader - Class in org.orekit.forces.gravity.potential
Reader for the SHA gravity field format.
SHAFormatReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.SHAFormatReader
Simple constructor.
SHAPE - org.orekit.files.ccsds.ndm.cdm.ScreenType
Shape type.
shapiroCorrection(TimeStampedPVCoordinates, TimeStampedPVCoordinates) - Method in class org.orekit.estimation.measurements.modifiers.AbstractShapiroBaseModifier
Compute Shapiro path dilation between two points in a gravity field.
ShapiroInterSatellitePhaseModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical inter-satellites phase measurement with Shapiro time delay.
ShapiroInterSatellitePhaseModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.ShapiroInterSatellitePhaseModifier
Simple constructor.
ShapiroInterSatelliteRangeModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical range measurement with Shapiro time delay.
ShapiroInterSatelliteRangeModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.ShapiroInterSatelliteRangeModifier
Simple constructor.
ShapiroOneWayGNSSPhaseModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical one-way GNSS phase measurement with Shapiro time delay.
ShapiroOneWayGNSSPhaseModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.ShapiroOneWayGNSSPhaseModifier
Simple constructor.
ShapiroOneWayGNSSRangeModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical range measurement with Shapiro time delay.
ShapiroOneWayGNSSRangeModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.ShapiroOneWayGNSSRangeModifier
Simple constructor.
ShapiroPhaseModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical phase measurement with Shapiro time delay.
ShapiroPhaseModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.ShapiroPhaseModifier
Simple constructor.
ShapiroRangeModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical range measurement with Shapiro time delay.
ShapiroRangeModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.ShapiroRangeModifier
Simple constructor.
shiftedBy(double) - Method in class org.orekit.attitudes.Attitude
Get a time-shifted attitude.
shiftedBy(double) - Method in class org.orekit.attitudes.FieldAttitude
Get a time-shifted attitude.
shiftedBy(double) - Method in class org.orekit.frames.FieldTransform
Get a time-shifted instance.
shiftedBy(double) - Method in class org.orekit.frames.Transform
Get a time-shifted instance.
shiftedBy(double) - Method in class org.orekit.orbits.CartesianOrbit
Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.orbits.CircularOrbit
Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.orbits.EquinoctialOrbit
Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.orbits.FieldCartesianOrbit
Get a time-shifted instance.
shiftedBy(double) - Method in class org.orekit.orbits.FieldCircularOrbit
Get a time-shifted instance.
shiftedBy(double) - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get a time-shifted instance.
shiftedBy(double) - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get a time-shifted instance.
shiftedBy(double) - Method in class org.orekit.orbits.KeplerianOrbit
Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.orbits.Orbit
Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.propagation.FieldSpacecraftState
Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.propagation.SpacecraftState
Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.time.AbsoluteDate
Get a time-shifted date.
shiftedBy(double) - Method in class org.orekit.time.FieldAbsoluteDate
Get a time-shifted date.
shiftedBy(double) - Method in interface org.orekit.time.TimeShiftable
Get a time-shifted instance.
shiftedBy(double) - Method in class org.orekit.utils.AbsolutePVCoordinates
Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.AngularCoordinates
Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.FieldAbsolutePVCoordinates
Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.FieldAngularCoordinates
Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.FieldPVCoordinates
Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.PVCoordinates
Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.TimeStampedAngularCoordinates
Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates
Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.TimeStampedFieldPVCoordinates
Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.TimeStampedPVCoordinates
Get a time-shifted state.
shiftedBy(long, TimeUnit) - Method in class org.orekit.time.AbsoluteDate
Get a time-shifted date.
shiftedBy(long, TimeUnit) - Method in class org.orekit.time.FieldAbsoluteDate
Get a time-shifted date.
shiftedBy(KK) - Method in interface org.orekit.time.FieldTimeShiftable
Get a time-shifted instance.
shiftedBy(Field<T>, FieldOrbit<T>, T) - Method in class org.orekit.propagation.FieldStateCovariance
Get a time-shifted covariance matrix.
shiftedBy(Orbit, double) - Method in class org.orekit.propagation.StateCovariance
Get a time-shifted covariance matrix.
shiftedBy(T) - Method in class org.orekit.attitudes.FieldAttitude
Get a time-shifted attitude.
shiftedBy(T) - Method in class org.orekit.frames.FieldTransform
Get a time-shifted instance.
shiftedBy(T) - Method in class org.orekit.orbits.FieldCartesianOrbit
Get a time-shifted orbit.
shiftedBy(T) - Method in class org.orekit.orbits.FieldCircularOrbit
Get a time-shifted orbit.
shiftedBy(T) - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get a time-shifted orbit.
shiftedBy(T) - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get a time-shifted orbit.
shiftedBy(T) - Method in class org.orekit.orbits.FieldOrbit
Get a time-shifted orbit.
shiftedBy(T) - Method in class org.orekit.propagation.FieldSpacecraftState
Get a time-shifted state.
shiftedBy(T) - Method in class org.orekit.time.FieldAbsoluteDate
Get a time-shifted date.
shiftedBy(T) - Method in class org.orekit.utils.FieldAbsolutePVCoordinates
Get a time-shifted state.
shiftedBy(T) - Method in class org.orekit.utils.FieldAngularCoordinates
Get a time-shifted state.
shiftedBy(T) - Method in class org.orekit.utils.FieldPVCoordinates
Get a time-shifted state.
shiftedBy(T) - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates
Get a time-shifted state.
shiftedBy(T) - Method in class org.orekit.utils.TimeStampedFieldPVCoordinates
Get a time-shifted state.
ShiftingPVCoordinatesProvider - Class in org.orekit.utils
Provider using simple PVCoordinates.shiftedBy(double) shiftedBy} and frame transforms for evolution.
ShiftingPVCoordinatesProvider(TimeStampedPVCoordinates, Frame) - Constructor for class org.orekit.utils.ShiftingPVCoordinatesProvider
Simple constructor.
ShiftingTransformProvider - Class in org.orekit.frames
Transform provider using thread-safe shifts on transforms sample.
ShiftingTransformProvider(TransformProvider, CartesianDerivativesFilter, AngularDerivativesFilter, int, double, int, double, double) - Constructor for class org.orekit.frames.ShiftingTransformProvider
Simple constructor.
SHM_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory
Default regular expression for SHM files.
SHMFormatReader - Class in org.orekit.forces.gravity.potential
Reader for the SHM gravity field format.
SHMFormatReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.SHMFormatReader
Simple constructor.
SHMFormatReader(String, boolean, TimeScale) - Constructor for class org.orekit.forces.gravity.potential.SHMFormatReader
Simple constructor.
ShootingBoundaryOutput - Class in org.orekit.control.indirect.shooting
Data container for two-point boundary output of indirect shooting methods.
ShootingBoundaryOutput(boolean, int, SpacecraftState, ShootingPropagationSettings, SpacecraftState) - Constructor for class org.orekit.control.indirect.shooting.ShootingBoundaryOutput
Constructor.
ShootingIntegrationSettings - Interface in org.orekit.control.indirect.shooting.propagation
Defines integration settings for indirect shooting methods.
ShootingPropagationSettings - Class in org.orekit.control.indirect.shooting.propagation
Defines propagation settings for indirect shooting methods.
ShootingPropagationSettings(List<ForceModel>, AdjointDynamicsProvider, ShootingIntegrationSettings) - Constructor for class org.orekit.control.indirect.shooting.propagation.ShootingPropagationSettings
Simple constructor with default frame and attitude provider.
ShootingPropagationSettings(List<ForceModel>, AdjointDynamicsProvider, Frame, ShootingIntegrationSettings, AttitudeProvider) - Constructor for class org.orekit.control.indirect.shooting.propagation.ShootingPropagationSettings
Constructor.
SHORT_PERIOD_PREFIX - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Name of the prefix for short period coefficients keys.
SHORT_PERIOD_PREFIX - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Name of the prefix for short period coefficients keys.
SHORT_PERIOD_PREFIX - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Name of the prefix for short period coefficients keys.
ShortPeriodicsInterpolatedCoefficient - Class in org.orekit.propagation.semianalytical.dsst.utilities
Interpolated short periodics coefficients.
ShortPeriodicsInterpolatedCoefficient(int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.ShortPeriodicsInterpolatedCoefficient
Simple constructor.
ShortPeriodTerms - Interface in org.orekit.propagation.semianalytical.dsst.forces
Additive short period terms contributing to the mean to osculating orbit mapping.
ShortTermEncounter2DDefinition - Class in org.orekit.ssa.collision.shorttermencounter.probability.twod
Defines the encounter between two collision object at time of closest approach assuming a short-term encounter model .
ShortTermEncounter2DDefinition(Orbit, StateCovariance, double, Orbit, StateCovariance, double) - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition
Constructor.
ShortTermEncounter2DDefinition(Orbit, StateCovariance, double, Orbit, StateCovariance, double, EncounterLOFType, double) - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition
Constructor.
ShortTermEncounter2DDefinition(Orbit, StateCovariance, Orbit, StateCovariance, double) - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition
Constructor.
ShortTermEncounter2DDefinition(Orbit, StateCovariance, Orbit, StateCovariance, double, EncounterLOFType, double) - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition
Constructor.
ShortTermEncounter2DPOCMethod - Interface in org.orekit.ssa.collision.shorttermencounter.probability.twod
Interface common to all short-term encounter probability of collision computing methods.
ShortTermEncounter2DPOCMethodType - Enum in org.orekit.ssa.collision.shorttermencounter.probability.twod
This enum stores every probability of collision computing method using the short-term encounter model available in Orekit.
siAccuracy(Unit, double, int) - Static method in class org.orekit.files.sp3.SP3Utils
Convert an accuracy to SI units.
SIGMA_U - org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationKey
SIGMA_V - org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationKey
SigmaEigenvectorsCovariance - Class in org.orekit.files.ccsds.ndm.cdm
Container for Sigma/Eigenvectors Covariance data.
SigmaEigenvectorsCovariance(boolean) - Constructor for class org.orekit.files.ccsds.ndm.cdm.SigmaEigenvectorsCovariance
Simple constructor.
SigmaEigenvectorsCovarianceKey - Enum in org.orekit.files.ccsds.ndm.cdm
Keys for covariance format entries.
sign(double) - Method in class org.orekit.estimation.measurements.gnss.ModifiedLambdaMethod
Return the symbol of parameter a.
SIGNAL_STRENGTH - org.orekit.gnss.MeasurementType
Signal-strength measurement.
SIGNAL_STRENGTH_UNIT - org.orekit.files.rinex.section.RinexLabels
Unit of signal strength.
SignalCode - Enum in org.orekit.gnss
Enumerate for satellite signal code.
SignalInSpaceAccuracy - Class in org.orekit.gnss.metric.messages.common
Signal-In-Space Accuracy (SISA).
SignalInSpaceAccuracy(int) - Constructor for class org.orekit.gnss.metric.messages.common.SignalInSpaceAccuracy
Simple constructor.
signalTimeOfFlight(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, FieldVector3D<T>, FieldAbsoluteDate<T>, Frame) - Static method in class org.orekit.estimation.measurements.AbstractMeasurement
Compute propagation delay on a link leg (typically downlink or uplink).
signalTimeOfFlight(PVCoordinatesProvider, AbsoluteDate, Vector3D, AbsoluteDate, Frame) - Static method in class org.orekit.estimation.measurements.AbstractMeasurement
Compute propagation delay on a link leg (typically downlink or uplink).
signalTimeOfFlight(TimeStampedFieldPVCoordinates<T>, FieldVector3D<T>, FieldAbsoluteDate<T>) - Static method in class org.orekit.estimation.measurements.AbstractMeasurement
signalTimeOfFlight(TimeStampedFieldPVCoordinates<T>, FieldVector3D<T>, FieldAbsoluteDate<T>, Frame) - Static method in class org.orekit.estimation.measurements.AbstractMeasurement
Compute propagation delay on a link leg (typically downlink or uplink).
signalTimeOfFlight(TimeStampedPVCoordinates, Vector3D, AbsoluteDate) - Static method in class org.orekit.estimation.measurements.AbstractMeasurement
signalTimeOfFlight(TimeStampedPVCoordinates, Vector3D, AbsoluteDate, Frame) - Static method in class org.orekit.estimation.measurements.AbstractMeasurement
Compute propagation delay on a link leg (typically downlink or uplink).
signedAmplitude(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.forces.empirical.AccelerationModel
Compute the signed amplitude of the acceleration.
signedAmplitude(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.empirical.HarmonicAccelerationModel
Compute the signed amplitude of the acceleration.
signedAmplitude(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.empirical.PolynomialAccelerationModel
Compute the signed amplitude of the acceleration.
signedAmplitude(SpacecraftState, double[]) - Method in interface org.orekit.forces.empirical.AccelerationModel
Compute the signed amplitude of the acceleration.
signedAmplitude(SpacecraftState, double[]) - Method in class org.orekit.forces.empirical.HarmonicAccelerationModel
Compute the signed amplitude of the acceleration.
signedAmplitude(SpacecraftState, double[]) - Method in class org.orekit.forces.empirical.PolynomialAccelerationModel
Compute the signed amplitude of the acceleration.
SignSemantic - Enum in org.orekit.estimation.measurements.generation
Enumerate for the semantic of the g function sign during measurements generation.
SimpleExponentialAtmosphere - Class in org.orekit.models.earth.atmosphere
Simple exponential atmospheric model.
SimpleExponentialAtmosphere(BodyShape, double, double, double) - Constructor for class org.orekit.models.earth.atmosphere.SimpleExponentialAtmosphere
Create an exponential atmosphere.
SimpleRatioAmbiguityAcceptance - Class in org.orekit.estimation.measurements.gnss
Ambiguity acceptance test based on a ratio of the two best candidates.
SimpleRatioAmbiguityAcceptance(double) - Constructor for class org.orekit.estimation.measurements.gnss.SimpleRatioAmbiguityAcceptance
Simple constructor.
SimpleTimeStampedTableParser<T extends TimeStamped> - Class in org.orekit.data
Parser for simple tables containing time stamped data.
SimpleTimeStampedTableParser(int, SimpleTimeStampedTableParser.RowConverter<T>) - Constructor for class org.orekit.data.SimpleTimeStampedTableParser
Simple constructor.
SimpleTimeStampedTableParser.RowConverter<S extends TimeStamped> - Interface in org.orekit.data
Interface for converting a table row into time-stamped data.
SIMULATED - org.orekit.files.ccsds.ndm.odm.ocm.ManBasis
Generic maneuver simulation.
SinexEopEntry - Class in org.orekit.files.sinex
Container for EOP entry read in a Sinex file.
SinexEopEntry(AbsoluteDate) - Constructor for class org.orekit.files.sinex.SinexEopEntry
Constructor.
SinexLoader - Class in org.orekit.files.sinex
Loader for Solution INdependent EXchange (SINEX) files.
SinexLoader(String) - Constructor for class org.orekit.files.sinex.SinexLoader
Simple constructor.
SinexLoader(String, DataProvidersManager, TimeScales) - Constructor for class org.orekit.files.sinex.SinexLoader
Construct a loader by specifying the source of SINEX auxiliary data files.
SinexLoader(DataSource) - Constructor for class org.orekit.files.sinex.SinexLoader
Simple constructor.
SinexLoader(DataSource, TimeScales) - Constructor for class org.orekit.files.sinex.SinexLoader
Loads SINEX from the given input stream using the specified auxiliary data.
SINGLE_DIFF - org.orekit.files.ccsds.ndm.tdm.TrackingMode
Single diff mode, applies to differenced data.
SingleBodyAbsoluteAttraction - Class in org.orekit.forces.gravity
Body attraction force model computed as absolute acceleration towards a body.
SingleBodyAbsoluteAttraction(CelestialBody) - Constructor for class org.orekit.forces.gravity.SingleBodyAbsoluteAttraction
Simple constructor.
SingleBodyRelativeAttraction - Class in org.orekit.forces.gravity
Body attraction force model computed as relative acceleration towards frame center.
SingleBodyRelativeAttraction(CelestialBody) - Constructor for class org.orekit.forces.gravity.SingleBodyRelativeAttraction
Simple constructor.
SingleFrequencyHatchFilter - Class in org.orekit.estimation.measurements.filtering
Single frequency Hatch filter.
SingleFrequencyHatchFilter(ObservationData, ObservationData, MeasurementType, double, double, int, double) - Constructor for class org.orekit.estimation.measurements.filtering.SingleFrequencyHatchFilter
Constructor for the Single Frequency Hatch Filter.
SingleFrequencySmoother - Class in org.orekit.estimation.measurements.filtering
Handler to perform pseudo-range smoothing using single frequency measurements.
SingleFrequencySmoother(MeasurementType, double, int, double) - Constructor for class org.orekit.estimation.measurements.filtering.SingleFrequencySmoother
Simple constructor.
SingleLayerModelMappingFunction - Class in org.orekit.models.earth.ionosphere
Single Layer Model (SLM) ionospheric mapping function.
SingleLayerModelMappingFunction() - Constructor for class org.orekit.models.earth.ionosphere.SingleLayerModelMappingFunction
Constructor with default value.
SingleLayerModelMappingFunction(double) - Constructor for class org.orekit.models.earth.ionosphere.SingleLayerModelMappingFunction
Constructor.
SingleParameterFitter - Class in org.orekit.frames
Fitter for one Earth Orientation Parameter.
SingleParameterFitter(double, double, double, int, double...) - Constructor for class org.orekit.frames.SingleParameterFitter
SingleParameterFitter(double, double, int, double...) - Constructor for class org.orekit.frames.SingleParameterFitter
Simple constructor.
SINGULAR_JACOBIAN_FOR_ORBIT_TYPE - org.orekit.errors.OrekitMessages
SINGULAR_JACOBIAN_FOR_ORBIT_TYPE.
sini0 - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
sinus original inclination.
sini0 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
sinus original inclination.
siToCcsdsName(String) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Convert a SI unit name to a CCSDS name.
siToCcsdsName(String) - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Convert a SI unit name to a CCSDS name.
siToRaw(RangeUnitsConverter, TdmMetadata, AbsoluteDate, double) - Method in enum org.orekit.files.ccsds.ndm.tdm.ObservationType
Convert a measurement from SI units.
size() - Method in class org.orekit.utils.DoubleArrayDictionary.Entry
Get the size of the value array.
size() - Method in class org.orekit.utils.DoubleArrayDictionary
Get the number of dictionary entries.
size() - Method in class org.orekit.utils.FieldArrayDictionary.Entry
Get the size of the value array.
size() - Method in class org.orekit.utils.FieldArrayDictionary
Get the number of dictionary entries.
SlewingPanel - Class in org.orekit.forces
Class representing one panel of a satellite, slewing about an axis at constant rate.
SlewingPanel(Vector3D, double, AbsoluteDate, Vector3D, double, double, double, double, double) - Constructor for class org.orekit.forces.SlewingPanel
Simple constructor.
SM_COEFFICIENTS - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Identifier for sMm coefficients.
SMALL_TRUNCATION_TOLERANCE - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Truncation tolerance for small orbits.
SmallManeuverAnalyticalModel - Class in org.orekit.forces.maneuvers
Analytical model for small maneuvers.
SmallManeuverAnalyticalModel(SpacecraftState, Vector3D, double) - Constructor for class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
Build a maneuver defined in spacecraft frame with default orbit type.
SmallManeuverAnalyticalModel(SpacecraftState, Frame, Vector3D, double) - Constructor for class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
Build a maneuver defined in user-specified frame.
SmallManeuverAnalyticalModel(SpacecraftState, OrbitType, Vector3D, double) - Constructor for class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
Build a maneuver defined in spacecraft frame.
SmallManeuverAnalyticalModel(SpacecraftState, OrbitType, Frame, Vector3D, double) - Constructor for class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
Build a maneuver defined in user-specified frame.
SmoothedObservationDataSet - Class in org.orekit.estimation.measurements.filtering
Container used to store smoothed observation data along with the original data set it originates from.
SmoothedObservationDataSet(ObservationData, ObservationDataSet) - Constructor for class org.orekit.estimation.measurements.filtering.SmoothedObservationDataSet
Simple constructor.
SmoothFieldOfView - Class in org.orekit.geometry.fov
Class representing a spacecraft sensor Field Of View with shape defined by a smooth single loop.
SmoothFieldOfView(Vector3D, Vector3D, double) - Constructor for class org.orekit.geometry.fov.SmoothFieldOfView
Build a new instance.
SoftwareConfiguration() - Constructor for class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration
Empty constructor.
SOLAR_FLUX_UNIT - Static variable in class org.orekit.utils.units.Unit
Solar Flux Unit.
SOLAR_RAD_AREA - org.orekit.files.ccsds.ndm.odm.SpacecraftParametersKey
Solar radiation pressure area.
SOLAR_RAD_COEFF - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Nominal SRP coefficient.
SOLAR_RAD_COEFF - org.orekit.files.ccsds.ndm.odm.SpacecraftParametersKey
Solar radiation pressure coefficient.
SOLAR_RAD_PRESSURE - org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey
Is solar radiation pressure used for the OD of the object ?
SOLAR_RAD_UNCERTAINTY - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
SRP coefficient 1σ uncertainty.
SOLAR_SYSTEM_BARYCENTER - org.orekit.bodies.JPLEphemeridesLoader.EphemerisType
Constant for solar system barycenter.
SOLAR_SYSTEM_BARYCENTER - org.orekit.files.ccsds.definitions.CenterName
Solar system barycenter aggregated body.
SOLAR_SYSTEM_BARYCENTER - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for solar system barycenter.
SolarActivityGenerator(Collection<L>) - Constructor for class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData.SolarActivityGenerator
Constructor.
SolarRadiationPressure - Class in org.orekit.forces.radiation
Solar radiation pressure force model.
SolarRadiationPressure(double, double, ExtendedPVCoordinatesProvider, OneAxisEllipsoid, RadiationSensitive) - Constructor for class org.orekit.forces.radiation.SolarRadiationPressure
Complete constructor.
SolarRadiationPressure(ExtendedPVCoordinatesProvider, OneAxisEllipsoid, RadiationSensitive) - Constructor for class org.orekit.forces.radiation.SolarRadiationPressure
Simple constructor with default reference values.
SOLFSMYDataLoader - Class in org.orekit.models.earth.atmosphere.data
This class reads solar activity data from SOLFSMY files for the class JB2008SpaceEnvironmentData.
SOLFSMYDataLoader(TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader
Constructor.
SOLFSMYDataLoader.LineParameters - Class in org.orekit.models.earth.atmosphere.data
Container class for Solar activity indexes.
SOLID_TIDES_MODEL - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey
Solid tides model.
SolidTides - Class in org.orekit.forces.gravity
Solid tides force model.
SolidTides(Frame, double, double, TideSystem, boolean, double, int, IERSConventions, UT1Scale, CelestialBody...) - Constructor for class org.orekit.forces.gravity.SolidTides
Simple constructor.
SolidTides(Frame, double, double, TideSystem, IERSConventions, UT1Scale, CelestialBody...) - Constructor for class org.orekit.forces.gravity.SolidTides
Simple constructor.
solve(double, double[]) - Method in class org.orekit.control.indirect.shooting.AbstractFixedBoundaryCartesianSingleShooting
Solve for the boundary conditions, given an initial mass and an initial guess for the adjoint variables.
solve(double, double[]) - Method in class org.orekit.control.indirect.shooting.AbstractIndirectShooting
Solve for the boundary conditions, given an initial mass and an initial guess for the adjoint variables.
SOLVE_N - org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey
Number of solved-for states.
SOLVE_STATES - org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey
Description of state elements solved-for.
solveILS(int, double[], int[], RealMatrix) - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Find the best solutions to an Integer Least Square problem.
solveILS(int, double[], int[], RealMatrix) - Method in interface org.orekit.estimation.measurements.gnss.IntegerLeastSquareSolver
Find the best solutions to an Integer Least Square problem.
sort() - Method in class org.orekit.utils.ParameterDriversList
Sort the parameters lexicographically.
SortedListTrimmer - Class in org.orekit.utils
A trimmer for externally stored chronologically sorted lists.
SortedListTrimmer(int) - Constructor for class org.orekit.utils.SortedListTrimmer
Create a new trimmer with the given neighbors size.
SourceTable - Class in org.orekit.gnss.metric.ntrip
Source table for ntrip streams retrieval.
SOURCETABLE_PARSE_ERROR - org.orekit.errors.OrekitMessages
SOURCETABLE_PARSE_ERROR.
SOUTH_POLE - Static variable in class org.orekit.bodies.GeodeticPoint
South pole.
SOUTHERN - org.orekit.orbits.LibrationOrbitFamily
Southern.
SP3 - Class in org.orekit.files.sp3
Represents a parsed SP3 orbit file.
SP3 - org.orekit.gnss.metric.ntrip.DataFormat
SP3.
SP3(double, int, Frame) - Constructor for class org.orekit.files.sp3.SP3
Create a new SP3 file object.
SP3(SP3Header, double, int, Frame) - Constructor for class org.orekit.files.sp3.SP3
Create a new SP3 file object.
SP3_FRAME_CENTER_STRING - Static variable in class org.orekit.files.sp3.SP3Header
String representation of the center of ephemeris coordinate system.
SP3_FRAME_CENTER_STRING - Static variable in class org.orekit.files.sp3.SP3Parser
Deprecated.
as of 12.1 not used anymore
SP3_INCOMPATIBLE_FILE_METADATA - org.orekit.errors.OrekitMessages
SP3_INCOMPATIBLE_FILE_METADATA.
SP3_INCOMPATIBLE_SATELLITE_MEDATADA - org.orekit.errors.OrekitMessages
SP3_INCOMPATIBLE_SATELLITE_MEDATADA.
SP3_INVALID_HEADER_ENTRY - org.orekit.errors.OrekitMessages
SP3_INVALID_HEADER_ENTRY.
SP3_NUMBER_OF_EPOCH_MISMATCH - org.orekit.errors.OrekitMessages
SP3_NUMBER_OF_EPOCH_MISMATCH.
SP3_TOO_MANY_SATELLITES_FOR_VERSION - org.orekit.errors.OrekitMessages
SP3_TOO_MANY_SATELLITES_FOR_VERSION.
SP3_UNSUPPORTED_VERSION - org.orekit.errors.OrekitMessages
SP3_UNSUPPORTED_VERSION.
SP3Coordinate - Class in org.orekit.files.sp3
A single record of position clock and possibly derivatives in an SP3 file.
SP3Coordinate(AbsoluteDate, Vector3D, Vector3D, Vector3D, Vector3D, double, double, double, double, boolean, boolean, boolean, boolean) - Constructor for class org.orekit.files.sp3.SP3Coordinate
Create a coordinate with position and velocity.
SP3CoordinateHermiteInterpolator - Class in org.orekit.files.sp3
Interpolator for SP3 coordinates.
SP3CoordinateHermiteInterpolator(int, double, boolean) - Constructor for class org.orekit.files.sp3.SP3CoordinateHermiteInterpolator
Constructor.
SP3Ephemeris - Class in org.orekit.files.sp3
Single satellite ephemeris from an SP3 file.
SP3Ephemeris(String, double, Frame, int, CartesianDerivativesFilter) - Constructor for class org.orekit.files.sp3.SP3Ephemeris
Create an ephemeris for a single satellite.
SP3FileType - Enum in org.orekit.files.sp3
File type indicator.
SP3Header - Class in org.orekit.files.sp3
Header for SP3 files.
SP3Header() - Constructor for class org.orekit.files.sp3.SP3Header
Create a new SP3 header.
SP3OrbitType - Enum in org.orekit.files.sp3
Orbit type indicator.
SP3Parser - Class in org.orekit.files.sp3
A parser for the SP3 orbit file format.
SP3Parser() - Constructor for class org.orekit.files.sp3.SP3Parser
Create an SP3 parser using default values.
SP3Parser(double, int, Function<? super String, ? extends Frame>) - Constructor for class org.orekit.files.sp3.SP3Parser
Create an SP3 parser and specify the extra information needed to create a Propagator from the ephemeris data.
SP3Parser(double, int, Function<? super String, ? extends Frame>, TimeScales) - Constructor for class org.orekit.files.sp3.SP3Parser
Create an SP3 parser and specify the extra information needed to create a Propagator from the ephemeris data.
SP3Segment - Class in org.orekit.files.sp3
One segment of an SP3Ephemeris.
SP3Segment(double, Frame, int, CartesianDerivativesFilter) - Constructor for class org.orekit.files.sp3.SP3Segment
Simple constructor.
SP3Utils - Class in org.orekit.files.sp3
Constants for SP3 files.
SP3Writer - Class in org.orekit.files.sp3
Writer for SP3 file.
SP3Writer(Appendable, String, TimeScales) - Constructor for class org.orekit.files.sp3.SP3Writer
Simple constructor.
SpacecraftBodyFrame - Class in org.orekit.files.ccsds.definitions
Frames used in CCSDS Attitude Data Messages for the spacecraft body.
SpacecraftBodyFrame(SpacecraftBodyFrame.BaseEquipment, String) - Constructor for class org.orekit.files.ccsds.definitions.SpacecraftBodyFrame
Simple constructor.
SpacecraftBodyFrame.BaseEquipment - Enum in org.orekit.files.ccsds.definitions
Equipment on which the frame is located.
SpacecraftParameters - Class in org.orekit.files.ccsds.ndm.odm
Container for spacecraft parameters.
SpacecraftParameters() - Constructor for class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters
Create an empty state data set.
SpacecraftParametersKey - Enum in org.orekit.files.ccsds.ndm.odm
Keys for ODM spacecraft parameters entries.
SpacecraftParametersWriter - Class in org.orekit.files.ccsds.ndm.odm
Writer for spacecraft parameters data.
SpacecraftParametersWriter(String, String, SpacecraftParameters) - Constructor for class org.orekit.files.ccsds.ndm.odm.SpacecraftParametersWriter
Create a writer.
SpacecraftState - Class in org.orekit.propagation
This class is the representation of a complete state holding orbit, attitude and mass information at a given date, meant primarily for propagation.
SpacecraftState(Orbit) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from orbit only.
SpacecraftState(Orbit, double) - Constructor for class org.orekit.propagation.SpacecraftState
Create a new instance from orbit and mass.
SpacecraftState(Orbit, double, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState
Create a new instance from orbit, mass and additional states.
SpacecraftState(Orbit, Attitude) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from orbit and attitude.
SpacecraftState(Orbit, Attitude, double) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from orbit, attitude and mass.
SpacecraftState(Orbit, Attitude, double, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from orbit, attitude, mass and additional states.
SpacecraftState(Orbit, Attitude, double, DoubleArrayDictionary, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from orbit, attitude, mass, additional states and derivatives.
SpacecraftState(Orbit, Attitude, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from orbit, attitude and additional states.
SpacecraftState(Orbit, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from orbit and additional states.
SpacecraftState(AbsolutePVCoordinates) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from position-velocity-acceleration only.
SpacecraftState(AbsolutePVCoordinates, double) - Constructor for class org.orekit.propagation.SpacecraftState
Create a new instance from position-velocity-acceleration and mass.
SpacecraftState(AbsolutePVCoordinates, double, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState
Create a new instance from position-velocity-acceleration, mass and additional states.
SpacecraftState(AbsolutePVCoordinates, Attitude) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from position-velocity-acceleration and attitude.
SpacecraftState(AbsolutePVCoordinates, Attitude, double) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from position-velocity-acceleration, attitude and mass.
SpacecraftState(AbsolutePVCoordinates, Attitude, double, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from position-velocity-acceleration, attitude, mass and additional states.
SpacecraftState(AbsolutePVCoordinates, Attitude, double, DoubleArrayDictionary, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from position-velocity-acceleration, attitude, mass and additional states and derivatives.
SpacecraftState(AbsolutePVCoordinates, Attitude, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from position-velocity-acceleration, attitude and additional states.
SpacecraftState(AbsolutePVCoordinates, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from position-velocity-acceleration and additional states.
SpacecraftStateInterpolator - Class in org.orekit.propagation
Generic class for spacecraft state interpolator.
SpacecraftStateInterpolator(int, double, Frame) - Constructor for class org.orekit.propagation.SpacecraftStateInterpolator
Constructor to create a customizable Hermite interpolator for every spacecraft state field.
SpacecraftStateInterpolator(int, double, Frame, Frame) - Constructor for class org.orekit.propagation.SpacecraftStateInterpolator
Constructor to create a customizable Hermite interpolator for every spacecraft state field.
SpacecraftStateInterpolator(int, double, Frame, Frame, CartesianDerivativesFilter, AngularDerivativesFilter) - Constructor for class org.orekit.propagation.SpacecraftStateInterpolator
Constructor to create a customizable Hermite interpolator for every spacecraft state field.
SpacecraftStateInterpolator(int, double, Frame, TimeInterpolator<Orbit>, TimeInterpolator<AbsolutePVCoordinates>, TimeInterpolator<TimeStampedDouble>, TimeInterpolator<Attitude>, TimeInterpolator<TimeStampedDouble>) - Constructor for class org.orekit.propagation.SpacecraftStateInterpolator
Constructor.
SpacecraftStateInterpolator(int, Frame) - Constructor for class org.orekit.propagation.SpacecraftStateInterpolator
Constructor to create a customizable Hermite interpolator for every spacecraft state field.
SpacecraftStateInterpolator(int, Frame, Frame) - Constructor for class org.orekit.propagation.SpacecraftStateInterpolator
Constructor to create a customizable Hermite interpolator for every spacecraft state field.
SpacecraftStateInterpolator(Frame) - Constructor for class org.orekit.propagation.SpacecraftStateInterpolator
Simplest constructor to create a default Hermite interpolator for every spacecraft state field.
SpacecraftStateInterpolator(Frame, TimeInterpolator<Orbit>, TimeInterpolator<AbsolutePVCoordinates>, TimeInterpolator<TimeStampedDouble>, TimeInterpolator<Attitude>, TimeInterpolator<TimeStampedDouble>) - Constructor for class org.orekit.propagation.SpacecraftStateInterpolator
SPAN - org.orekit.files.rinex.navigation.SbasId
Southern Positioning Augmentation System.
SPAN - Static variable in class org.orekit.utils.ParameterDriver
Name of the parameter.
SPEED_OF_LIGHT - Static variable in interface org.orekit.utils.Constants
Speed of light: 299792458.0 m/s.
SPHERE - org.orekit.files.ccsds.ndm.cdm.ScreenVolumeShape
Sphere.
SphericalHarmonicsProvider - Interface in org.orekit.forces.gravity.potential
Interface used to provide spherical harmonics coefficients.
spin - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Spin sub-section.
SPIN - org.orekit.files.ccsds.ndm.adm.AttitudeType
Spin.
SPIN_ALPHA - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Right ascension of spin axis vector.
SPIN_ALPHA - org.orekit.files.ccsds.ndm.adm.apm.SpinStabilizedKey
Spin right ascension entry.
SPIN_ANGLE - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Phase of satellite about spin axis.
SPIN_ANGLE - org.orekit.files.ccsds.ndm.adm.apm.SpinStabilizedKey
Spin phase entry.
SPIN_ANGLE_VEL - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
angular velocity of satellite around spin axis.
SPIN_ANGLE_VEL - org.orekit.files.ccsds.ndm.adm.apm.SpinStabilizedKey
Spin angular velocity entry.
SPIN_DELTA - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Declination of spin axis vector.
SPIN_DELTA - org.orekit.files.ccsds.ndm.adm.apm.SpinStabilizedKey
Spin declination entry.
SPIN_DIR - org.orekit.files.ccsds.ndm.adm.apm.SpinStabilizedKey
Rotation direction entry (only for ADM V1).
SPIN_FRAME_A - org.orekit.files.ccsds.ndm.adm.apm.SpinStabilizedKey
First reference frame entry (only for ADM V1).
SPIN_FRAME_B - org.orekit.files.ccsds.ndm.adm.apm.SpinStabilizedKey
Second reference frame entry (only for ADM V1).
SPIN_NUTATION - org.orekit.files.ccsds.ndm.adm.AttitudeType
Spin and nutation.
SPIN_NUTATION_MOMENTUM - org.orekit.files.ccsds.ndm.adm.AttitudeType
Spin and momentum.
spinNutation - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Spin/nutation sub-section.
spinNutationMom - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Spin/nutation/momentum sub-section.
SpinStabilized - Class in org.orekit.attitudes
This class handles a spin stabilized attitude provider.
SpinStabilized - Class in org.orekit.files.ccsds.ndm.adm.apm
Container for Attitude Parameter Message data lines.
SpinStabilized() - Constructor for class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
Simple constructor.
SpinStabilized(AttitudeProvider, AbsoluteDate, Vector3D, double) - Constructor for class org.orekit.attitudes.SpinStabilized
Creates a new instance.
SpinStabilizedKey - Enum in org.orekit.files.ccsds.ndm.adm.apm
Keys for APM spin-stabilized entries.
splice(Collection<RinexClock>, double) - Static method in class org.orekit.files.rinex.clock.RinexClock
Splice several Rinex clock files together.
splice(Collection<SP3>) - Static method in class org.orekit.files.sp3.SP3
Splice several SP3 files together.
sqrt(String) - Method in class org.orekit.utils.units.Unit
Create root of unit.
SRIF - org.orekit.files.ccsds.definitions.OdMethodType
Square Root Information Filter.
SRP_CONST_AREA - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Attitude-independent SRP area, not already into attitude-dependent area along OEB.
SRP_MODEL - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey
Solar Radiation Pressure model.
SSA - Static variable in class org.orekit.models.earth.displacement.Tide
Ssa tide.
SSEM - org.orekit.files.ccsds.definitions.OdMethodType
Sequential Simultaneous Estimation Method.
SsrData - Class in org.orekit.gnss.metric.messages.ssr
Container for common data in SSR message data.
SsrData() - Constructor for class org.orekit.gnss.metric.messages.ssr.SsrData
Empty constructor.
SsrHeader - Class in org.orekit.gnss.metric.messages.ssr
Container for common data in SSR messages header.
SsrHeader() - Constructor for class org.orekit.gnss.metric.messages.ssr.SsrHeader
Empty constructor.
SsrIgm01 - Class in org.orekit.gnss.metric.messages.ssr.igm
GNSS SSR Orbit Correction Message.
SsrIgm01(int, SatelliteSystem, SsrIgm01Header, List<SsrIgm01Data>) - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01
Constructor.
SsrIgm01Data - Class in org.orekit.gnss.metric.messages.ssr.igm
Container for SSR IGM01 data.
SsrIgm01Data() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01Data
Constructor.
SsrIgm01Header - Class in org.orekit.gnss.metric.messages.ssr.igm
Container for SSR IGM01 header.
SsrIgm01Header() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01Header
Constructor.
SsrIgm02 - Class in org.orekit.gnss.metric.messages.ssr.igm
GNSS SSR Clock Correction Message.
SsrIgm02(int, SatelliteSystem, SsrIgm02Header, List<SsrIgm02Data>) - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm02
Constructor.
SsrIgm02Data - Class in org.orekit.gnss.metric.messages.ssr.igm
Container for SSR IGM02 data.
SsrIgm02Data() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm02Data
Constructor.
SsrIgm02Header - Class in org.orekit.gnss.metric.messages.ssr.igm
Container for SSR IGM02 header.
SsrIgm02Header() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm02Header
Constructor.
SsrIgm03 - Class in org.orekit.gnss.metric.messages.ssr.igm
GNSS SSR Combined Orbit and Clock Correction Message.
SsrIgm03(int, SatelliteSystem, SsrIgm03Header, List<SsrIgm03Data>) - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03
Constructor.
SsrIgm03Data - Class in org.orekit.gnss.metric.messages.ssr.igm
Container for SSR IGM03 data.
SsrIgm03Data() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Data
Constructor.
SsrIgm03Header - Class in org.orekit.gnss.metric.messages.ssr.igm
Container for SSR IGM03 header.
SsrIgm03Header() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Header
Constructor.
SsrIgm04 - Class in org.orekit.gnss.metric.messages.ssr.igm
GNSS SSR High Rate Clock Correction Message.
SsrIgm04(int, SatelliteSystem, SsrIgm04Header, List<SsrIgm04Data>) - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm04
Constructor.
SsrIgm04Data - Class in org.orekit.gnss.metric.messages.ssr.igm
Container for SSR IGM04 data.
SsrIgm04Data() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm04Data
Constructor.
SsrIgm04Header - Class in org.orekit.gnss.metric.messages.ssr.igm
Container for SSR IGM04 header.
SsrIgm04Header() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm04Header
Constructor.
SsrIgm05 - Class in org.orekit.gnss.metric.messages.ssr.igm
GNSS SSR Code Bias Message.
SsrIgm05(int, SatelliteSystem, SsrIgm05Header, List<SsrIgm05Data>) - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm05
Constructor.
SsrIgm05Data - Class in org.orekit.gnss.metric.messages.ssr.igm
Container for SSR IGM05 data.
SsrIgm05Data() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm05Data
Constructor.
SsrIgm05Header - Class in org.orekit.gnss.metric.messages.ssr.igm
Container for SSR IGM05 header.
SsrIgm05Header() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm05Header
Constructor.
SsrIgm06 - Class in org.orekit.gnss.metric.messages.ssr.igm
GNSS SSR Phase Bias Message.
SsrIgm06(int, SatelliteSystem, SsrIgm06Header, List<SsrIgm06Data>) - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06
Constructor.
SsrIgm06Data - Class in org.orekit.gnss.metric.messages.ssr.igm
Container for SSR IGM06 data.
SsrIgm06Data() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data
Constructor.
SsrIgm06Header - Class in org.orekit.gnss.metric.messages.ssr.igm
Container for SSR IGM06 header.
SsrIgm06Header() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Header
Constructor.
SsrIgm07 - Class in org.orekit.gnss.metric.messages.ssr.igm
GNSS SSR SSR URA Message.
SsrIgm07(int, SatelliteSystem, SsrIgm07Header, List<SsrIgm07Data>) - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm07
Constructor.
SsrIgm07Data - Class in org.orekit.gnss.metric.messages.ssr.igm
Container for SSR IGM07 data.
SsrIgm07Data() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm07Data
Constructor.
SsrIgm07Header - Class in org.orekit.gnss.metric.messages.ssr.igm
Container for SSR IGM07 header.
SsrIgm07Header() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm07Header
Constructor.
SsrIgmData - Class in org.orekit.gnss.metric.messages.ssr.igm
Container for common data in IGS Generic SSR Message type.
SsrIgmData() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgmData
Constructor.
SsrIgmHeader - Class in org.orekit.gnss.metric.messages.ssr.igm
Container for common data in IGS Generic SSR Message type header.
SsrIgmHeader() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgmHeader
Constructor.
SsrIgmMessage<H extends SsrIgmHeader,​D extends SsrIgmData> - Class in org.orekit.gnss.metric.messages.ssr.igm
The IGS Generic SSR Message types provide elements to calculate GNSS satellite corrections.
SsrIgmMessage(int, SatelliteSystem, H, List<D>) - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgmMessage
Constructor.
SsrIm201 - Class in org.orekit.gnss.metric.messages.ssr.subtype
SSR Ionosphere VTEC Spherical Harmonics Message.
SsrIm201(int, SsrIm201Header, List<SsrIm201Data>) - Constructor for class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201
Constructor.
SsrIm201Data - Class in org.orekit.gnss.metric.messages.ssr.subtype
Container for SSR IM201 data.
SsrIm201Data() - Constructor for class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data
Constructor.
SsrIm201Header - Class in org.orekit.gnss.metric.messages.ssr.subtype
Container for SSR IM201 header.
SsrIm201Header() - Constructor for class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Header
Constructor.
SsrMessage<H extends SsrHeader,​D extends SsrData> - Class in org.orekit.gnss.metric.messages.ssr
Base class for SSR messages.
SsrMessage(int, H, List<D>) - Constructor for class org.orekit.gnss.metric.messages.ssr.SsrMessage
Constructor.
SsrUpdateInterval - Class in org.orekit.gnss.metric.messages.common
SSR Update interval.
SsrUpdateInterval(int) - Constructor for class org.orekit.gnss.metric.messages.common.SsrUpdateInterval
Constructor.
SsrVtecIonosphericModel - Class in org.orekit.models.earth.ionosphere
Ionospheric model based on SSR IM201 message.
SsrVtecIonosphericModel(SsrIm201) - Constructor for class org.orekit.models.earth.ionosphere.SsrVtecIonosphericModel
Constructor.
STANBY - org.orekit.files.ccsds.ndm.odm.ocm.OpsStatus
Object in stand-by.
STANDARD_ATM_PRESSURE - Static variable in class org.orekit.models.earth.EarthStandardAtmosphereRefraction
NIST standard atmospheric pressure (Pa).
STANDARD_ATM_TEMPERATURE - Static variable in class org.orekit.models.earth.EarthStandardAtmosphereRefraction
NIST standard atmospheric temperature (K).
STANDARD_ATMOSPHERE - Static variable in class org.orekit.models.earth.troposphere.TroposphericModelUtils
Standard atmosphere.
STANDARD_ATMOSPHERE_PROVIDER - Static variable in class org.orekit.models.earth.troposphere.TroposphericModelUtils
Provider for standard atmosphere.
STANDARDIZED_LOCALE - Static variable in class org.orekit.utils.AccurateFormatter
Standardized locale to use, to ensure files can be exchanged without internationalization issues.
start() - Method in class org.orekit.gnss.metric.parser.AbstractEncodedMessage
Start message extraction.
start() - Method in class org.orekit.gnss.metric.parser.ByteArrayEncodedMessage
Start message extraction.
start() - Method in interface org.orekit.gnss.metric.parser.EncodedMessage
Start message extraction.
start() - Method in class org.orekit.gnss.metric.parser.HexadecimalSequenceEncodedMessage
Start message extraction.
START - org.orekit.files.ccsds.ndm.tdm.IntegrationReference
Time tag at integration interval start.
START - org.orekit.files.ccsds.utils.lexical.TokenType
Block or entry start token.
START_SCREEN_PERIOD - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
The start time in UTC of the screening period for the conjunction assessment.
START_SUFFIX - Static variable in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector
Default suffix for start driver.
START_SUFFIX - Static variable in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector
Default suffix for start driver.
START_TIME - org.orekit.files.ccsds.ndm.adm.acm.AcmMetadataKey
Start time entry.
START_TIME - org.orekit.files.ccsds.ndm.adm.aem.AemMetadataKey
Start time entry.
START_TIME - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Start time entry.
START_TIME - org.orekit.files.ccsds.ndm.odm.oem.OemMetadataKey
Start time entry.
START_TIME - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Start time entry.
started(TaskEvent) - Method in class org.orekit.compiler.plugin.DefaultDataContextPlugin
 
startMessage(String, String, double) - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Start CCSDS message.
startMessage(String, String, double) - Method in class org.orekit.files.ccsds.utils.generation.KvnGenerator
Start CCSDS message.
startMessage(String, String, double) - Method in class org.orekit.files.ccsds.utils.generation.XmlGenerator
Start CCSDS message.
startParse(String) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Start parsing.
STARTRACKER - org.orekit.files.ccsds.definitions.SpacecraftBodyFrame.BaseEquipment
Star Tracker.
StartStopEventsTrigger<A extends AbstractDetector<A>,​O extends AbstractDetector<O>> - Class in org.orekit.forces.maneuvers.trigger
Maneuver triggers based on a pair of event detectors that defines firing start and stop.
StartStopEventsTrigger(A, O) - Constructor for class org.orekit.forces.maneuvers.trigger.StartStopEventsTrigger
Simple constructor.
startStreaming(String, Type, boolean, boolean) - Method in class org.orekit.gnss.metric.ntrip.NtripClient
Connect to a mount point and start streaming data from it.
STATE_AND_COVARIANCE_DATES_MISMATCH - org.orekit.errors.OrekitMessages
STATE_AND_COVARIANCE_DATES_MISMATCH.
STATE_AND_PARAMETERS_JACOBIANS_ROWS_MISMATCH - org.orekit.errors.OrekitMessages
STATE_AND_PARAMETERS_JACOBIANS_ROWS_MISMATCH.
STATE_DIMENSION - Static variable in class org.orekit.propagation.AbstractMatricesHarvester
State dimension, fixed to 6.
STATE_DIMENSION - Static variable in class org.orekit.propagation.numerical.EpochDerivativesEquations
State dimension, fixed to 6.
STATE_DIMENSION - Static variable in class org.orekit.propagation.StateCovariance
State dimension.
STATE_JACOBIAN_NOT_6X6 - org.orekit.errors.OrekitMessages
STATE_JACOBIAN_NOT_6X6.
STATE_JACOBIAN_NOT_INITIALIZED - org.orekit.errors.OrekitMessages
STATE_JACOBIAN_NOT_INITIALIZED.
stateChanged(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator
Notify about a state change.
stateChanged(SpacecraftState) - Method in class org.orekit.propagation.AbstractPropagator
Notify about a state change.
StateCovariance - Class in org.orekit.propagation
This class is the representation of a covariance matrix at a given date.
StateCovariance(RealMatrix, AbsoluteDate, Frame, OrbitType, PositionAngleType) - Constructor for class org.orekit.propagation.StateCovariance
Constructor.
StateCovariance(RealMatrix, AbsoluteDate, LOF) - Constructor for class org.orekit.propagation.StateCovariance
Constructor.
StateCovarianceBlender - Class in org.orekit.propagation
State covariance blender.
StateCovarianceBlender(SmoothStepFactory.SmoothStepFunction, TimeInterpolator<Orbit>, Frame, OrbitType, PositionAngleType) - Constructor for class org.orekit.propagation.StateCovarianceBlender
Constructor.
StateCovarianceBlender(SmoothStepFactory.SmoothStepFunction, TimeInterpolator<Orbit>, LOFType) - Constructor for class org.orekit.propagation.StateCovarianceBlender
Constructor.
StateCovarianceKeplerianHermiteInterpolator - Class in org.orekit.propagation
State covariance Keplerian quintic interpolator.
StateCovarianceKeplerianHermiteInterpolator(int, double, TimeInterpolator<Orbit>, CartesianDerivativesFilter, Frame, OrbitType, PositionAngleType) - Constructor for class org.orekit.propagation.StateCovarianceKeplerianHermiteInterpolator
Constructor using an output frame.
StateCovarianceKeplerianHermiteInterpolator(int, double, TimeInterpolator<Orbit>, CartesianDerivativesFilter, LOFType) - Constructor for class org.orekit.propagation.StateCovarianceKeplerianHermiteInterpolator
Constructor using an output local orbital frame.
StateCovarianceKeplerianHermiteInterpolator(int, TimeInterpolator<Orbit>, Frame, OrbitType, PositionAngleType) - Constructor for class org.orekit.propagation.StateCovarianceKeplerianHermiteInterpolator
Constructor using an output frame and : Default number of interpolation points of DEFAULT_INTERPOLATION_POINTS Use of position and two time derivatives during interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).
StateCovarianceKeplerianHermiteInterpolator(int, TimeInterpolator<Orbit>, LOFType) - Constructor for class org.orekit.propagation.StateCovarianceKeplerianHermiteInterpolator
Constructor using an output local orbital frame and : Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of position and two time derivatives during interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).
StateCovarianceKeplerianHermiteInterpolator(int, TimeInterpolator<Orbit>, CartesianDerivativesFilter, Frame, OrbitType, PositionAngleType) - Constructor for class org.orekit.propagation.StateCovarianceKeplerianHermiteInterpolator
Constructor using an output frame and : Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).
StateCovarianceKeplerianHermiteInterpolator(int, TimeInterpolator<Orbit>, CartesianDerivativesFilter, LOFType) - Constructor for class org.orekit.propagation.StateCovarianceKeplerianHermiteInterpolator
Constructor using an output local orbital frame and : Use of position and two time derivatives during interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).
StateCovarianceKeplerianHermiteInterpolator(TimeInterpolator<Orbit>, Frame, OrbitType, PositionAngleType) - Constructor for class org.orekit.propagation.StateCovarianceKeplerianHermiteInterpolator
Constructor using an output frame and : Default number of interpolation points of DEFAULT_INTERPOLATION_POINTS Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of position and two time derivatives during interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).
StateCovarianceKeplerianHermiteInterpolator(TimeInterpolator<Orbit>, LOFType) - Constructor for class org.orekit.propagation.StateCovarianceKeplerianHermiteInterpolator
Constructor using an output local orbital frame and : Default number of interpolation points of DEFAULT_INTERPOLATION_POINTS Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of position and two time derivatives during interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).
StateCovarianceMatrixProvider - Class in org.orekit.propagation
Additional state provider for state covariance matrix.
StateCovarianceMatrixProvider(String, String, MatricesHarvester, StateCovariance) - Constructor for class org.orekit.propagation.StateCovarianceMatrixProvider
Constructor.
StateFunction - Interface in org.orekit.utils
Interface representing a vector function depending on SpacecraftState.
StateJacobian - Interface in org.orekit.utils
Interface representing the Jacobian of a vector function depending on SpacecraftState.
StateMapper - Class in org.orekit.propagation.integration
This class maps between raw double elements and SpacecraftState instances.
StateMapper(AbsoluteDate, double, OrbitType, PositionAngleType, AttitudeProvider, Frame) - Constructor for class org.orekit.propagation.integration.StateMapper
Simple constructor.
stateToTLE(FieldSpacecraftState<T>, FieldTLE<T>, TleGenerationAlgorithm) - Static method in class org.orekit.propagation.analytical.tle.FieldTLE
Convert Spacecraft State into TLE.
stateToTLE(SpacecraftState, TLE, TleGenerationAlgorithm) - Static method in class org.orekit.propagation.analytical.tle.TLE
Convert Spacecraft State into TLE.
stateVector - org.orekit.files.ccsds.ndm.cdm.XmlSubStructureKey
State Vector section.
StateVector - Class in org.orekit.files.ccsds.ndm.cdm
Container for state vector data.
StateVector - Class in org.orekit.files.ccsds.ndm.odm
Container for state vector data.
StateVector() - Constructor for class org.orekit.files.ccsds.ndm.cdm.StateVector
Simple constructor.
StateVector() - Constructor for class org.orekit.files.ccsds.ndm.odm.StateVector
Create an empty data set.
StateVectorKey - Enum in org.orekit.files.ccsds.ndm.cdm
Keys for CDM state vector entries.
StateVectorKey - Enum in org.orekit.files.ccsds.ndm.odm
Keys for ODM state vector container entries.
StateVectorWriter - Class in org.orekit.files.ccsds.ndm.cdm
Writer for state vector data for CCSDS Conjunction Data Messages.
StateVectorWriter - Class in org.orekit.files.ccsds.ndm.odm
Writer for state vector data.
StateVectorWriter(String, String, StateVector, TimeConverter) - Constructor for class org.orekit.files.ccsds.ndm.odm.StateVectorWriter
Create a writer.
staticShiftedBy(double) - Method in class org.orekit.frames.Transform
Shift the transform in time considering all rates, then return only the translation and rotation portion of the transform.
staticShiftedBy(T) - Method in class org.orekit.frames.FieldTransform
Shift the transform in time considering all rates, then return only the translation and rotation portion of the transform.
StaticTransform - Interface in org.orekit.frames
A transform that only includes translation and rotation.
Station - Class in org.orekit.files.sinex
Station model.
Station() - Constructor for class org.orekit.files.sinex.Station
Constructor.
STATION_INFORMATION - org.orekit.files.rinex.section.RinexLabels
Station information.
STATION_NOT_FOUND - org.orekit.errors.OrekitMessages
STATION_NOT_FOUND.
Station.ReferenceSystem - Enum in org.orekit.files.sinex
Eccentricity reference system.
StationDisplacement - Interface in org.orekit.models.earth.displacement
Interface for computing reference points displacement.
stec(AbsoluteDate, GeodeticPoint, GeodeticPoint) - Method in class org.orekit.models.earth.ionosphere.NeQuickModel
This method allows the computation of the Stant Total Electron Content (STEC).
stec(FieldAbsoluteDate<T>, FieldGeodeticPoint<T>, FieldGeodeticPoint<T>) - Method in class org.orekit.models.earth.ionosphere.NeQuickModel
This method allows the computation of the Stant Total Electron Content (STEC).
STEC - org.orekit.files.ccsds.ndm.tdm.ObservationType
Data: STEC - Slant Total Electron Count [TECU].
STEC_INTEGRATION_DID_NOT_CONVERGE - org.orekit.errors.OrekitMessages
STEC_INTEGRATION_DID_NOT_CONVERGE.
StepHandlerMultiplexer - Class in org.orekit.propagation.sampling
This class gathers several OrekitStepHandler instances into one.
StepHandlerMultiplexer() - Constructor for class org.orekit.propagation.sampling.StepHandlerMultiplexer
Simple constructor.
stillAcceptsData() - Method in interface org.orekit.data.DataLoader
Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader
Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.gnss.SEMParser
 
stillAcceptsData() - Method in class org.orekit.gnss.YUMAParser
 
stillAcceptsData() - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityDataLoader
Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.models.earth.atmosphere.data.DtcDataLoader
Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader
Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.models.earth.GeoMagneticModelLoader
Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader
Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader
 
stillAcceptsData() - Method in class org.orekit.utils.InterpolationTableLoader
Check if the loader still accepts new data.
STK_INVALID_OR_UNSUPPORTED_COORDINATE_SYSTEM - org.orekit.errors.OrekitMessages
STK_INVALID_OR_UNSUPPORTED_COORDINATE_SYSTEM.
STK_UNEXPECTED_END_OF_FILE - org.orekit.errors.OrekitMessages
STK_UNEXPECTED_END_OF_FILE.
STK_UNMAPPED_COORDINATE_SYSTEM - org.orekit.errors.OrekitMessages
STK_UNMAPPED_COORDINATE_SYSTEM.
STKEphemeris(String, double, List<STKEphemerisFile.STKEphemerisSegment>) - Constructor for class org.orekit.files.stk.STKEphemerisFile.STKEphemeris
Constructs a STKEphemerisFile.STKEphemeris instance.
STKEphemerisFile - Class in org.orekit.files.stk
STK ephemeris file.
STKEphemerisFile(String, String, STKEphemerisFile.STKEphemeris) - Constructor for class org.orekit.files.stk.STKEphemerisFile
Constructs a STKEphemerisFile instance.
STKEphemerisFile.STKCoordinateSystem - Enum in org.orekit.files.stk
STK coordinate system.
STKEphemerisFile.STKEphemeris - Class in org.orekit.files.stk
Ephemeris from an STK ephemeris file.
STKEphemerisFile.STKEphemerisSegment - Class in org.orekit.files.stk
Ephemeris segment from an STK ephemeris file.
STKEphemerisFileParser - Class in org.orekit.files.stk
Parser of STKEphemerisFiles.
STKEphemerisFileParser(String, double, UTCScale, Map<STKEphemerisFile.STKCoordinateSystem, Frame>) - Constructor for class org.orekit.files.stk.STKEphemerisFileParser
Constructs a STKEphemerisFileParser instance.
STKEphemerisSegment(double, Frame, int, CartesianDerivativesFilter, List<TimeStampedPVCoordinates>) - Constructor for class org.orekit.files.stk.STKEphemerisFile.STKEphemerisSegment
STMEquations - Class in org.orekit.propagation.numerical.cr3bp
Class calculating the state transition matrix coefficient for CR3BP Computation.
STMEquations(CR3BPSystem) - Constructor for class org.orekit.propagation.numerical.cr3bp.STMEquations
Simple constructor.
STOP - org.orekit.files.ccsds.utils.lexical.TokenType
Block or entry stop token.
STOP_SCREEN_PERIOD - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
The stop time in UTC of the screening period for the conjunction assessment.
STOP_SUFFIX - Static variable in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector
Default suffix for stop driver.
STOP_SUFFIX - Static variable in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector
Default suffix for stop driver.
STOP_TIME - org.orekit.files.ccsds.ndm.adm.acm.AcmMetadataKey
Stop time entry.
STOP_TIME - org.orekit.files.ccsds.ndm.adm.aem.AemMetadataKey
Stop time entry.
STOP_TIME - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Stop time entry.
STOP_TIME - org.orekit.files.ccsds.ndm.odm.oem.OemMetadataKey
Stop time entry.
STOP_TIME - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Stop time entry.
stopMonitoring() - Method in class org.orekit.gnss.metric.ntrip.StreamMonitor
Stop monitoring.
StopOnDecreasing - Class in org.orekit.propagation.events.handlers
Handle a detection event and choose what to do next.
StopOnDecreasing() - Constructor for class org.orekit.propagation.events.handlers.StopOnDecreasing
Empty constructor.
StopOnEvent - Class in org.orekit.propagation.events.handlers
Event handler which will always return stop as a state.
StopOnEvent() - Constructor for class org.orekit.propagation.events.handlers.StopOnEvent
Empty constructor.
StopOnIncreasing - Class in org.orekit.propagation.events.handlers
Handle a detection event and choose what to do next.
StopOnIncreasing() - Constructor for class org.orekit.propagation.events.handlers.StopOnIncreasing
Empty constructor.
stopStreaming(int) - Method in class org.orekit.gnss.metric.ntrip.NtripClient
Stop streaming data from all connected mount points.
STR - org.orekit.gnss.metric.ntrip.RecordType
Data streams.
STR_NAN - Static variable in class org.orekit.files.ilrs.CRD
String of "NaN".
STR_VALUE_NOT_AVAILABLE - Static variable in class org.orekit.files.ilrs.CRD
Value of 'not available' or 'not applicable' or 'no information'.
STREAM_REQUIRES_NMEA_FIX - org.orekit.errors.OrekitMessages
STREAM_REQUIRES_NMEA_FIX.
StreamedMessage - Class in org.orekit.gnss.metric.ntrip
Container for streamed messages meta-data.
StreamingAemWriter - Class in org.orekit.files.ccsds.ndm.adm.aem
A writer for AEM files.
StreamingAemWriter(Generator, AemWriter, AdmHeader, AemMetadata) - Constructor for class org.orekit.files.ccsds.ndm.adm.aem.StreamingAemWriter
Simple constructor.
StreamingAemWriter.SegmentWriter - Class in org.orekit.files.ccsds.ndm.adm.aem
A writer for a segment of an AEM.
StreamingCpfWriter - Class in org.orekit.files.ilrs
A writer for CPF files.
StreamingCpfWriter(Appendable, TimeScale, CPFHeader) - Constructor for class org.orekit.files.ilrs.StreamingCpfWriter
Create a CPF writer than streams data to the given output stream.
StreamingCpfWriter(Appendable, TimeScale, CPFHeader, boolean) - Constructor for class org.orekit.files.ilrs.StreamingCpfWriter
Create a CPF writer than streams data to the given output stream.
StreamingCpfWriter.HeaderLineWriter - Enum in org.orekit.files.ilrs
Writer for specific header lines.
StreamingCpfWriter.Segment - Class in org.orekit.files.ilrs
A writer for a segment of a CPF.
StreamingOcmWriter - Class in org.orekit.files.ccsds.ndm.odm.ocm
A writer for OCM files.
StreamingOcmWriter(Generator, OcmWriter, OdmHeader, OcmMetadata, TrajectoryStateHistoryMetadata) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.StreamingOcmWriter
Construct a writer that for each segment uses the reference frame of the first state's attitude.
StreamingOcmWriter(Generator, OcmWriter, OdmHeader, OcmMetadata, TrajectoryStateHistoryMetadata, boolean) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.StreamingOcmWriter
Simple constructor.
StreamingOcmWriter.BlockWriter - Class in org.orekit.files.ccsds.ndm.odm.ocm
A writer for a trajectory state history block of an OCM.
StreamingOemWriter - Class in org.orekit.files.ccsds.ndm.odm.oem
A writer for OEM files.
StreamingOemWriter(Generator, OemWriter, OdmHeader, OemMetadata) - Constructor for class org.orekit.files.ccsds.ndm.odm.oem.StreamingOemWriter
Construct a writer that for each segment uses the reference frame of the first state's attitude.
StreamingOemWriter(Generator, OemWriter, OdmHeader, OemMetadata, boolean) - Constructor for class org.orekit.files.ccsds.ndm.odm.oem.StreamingOemWriter
Construct a writer that writes position, velocity, and acceleration at each time step.
StreamingOemWriter(Generator, OemWriter, OdmHeader, OemMetadata, boolean, boolean) - Constructor for class org.orekit.files.ccsds.ndm.odm.oem.StreamingOemWriter
Simple constructor.
StreamingOemWriter.SegmentWriter - Class in org.orekit.files.ccsds.ndm.odm.oem
A writer for a segment of an OEM.
StreamMonitor - Class in org.orekit.gnss.metric.ntrip
Monitor for retrieving streamed data from one mount point.
StreamMonitor(NtripClient, String, Type, boolean, boolean, double, double, int) - Constructor for class org.orekit.gnss.metric.ntrip.StreamMonitor
Build a monitor for streaming data from a mount point.
STRICT_COMPLIANCE - org.orekit.files.ccsds.ndm.ParsedUnitsBehavior
Enforce strict compliance with CCSDS standard.
stringValue(EncodedMessage, int) - Method in interface org.orekit.gnss.metric.parser.DataField
Get the value of the field as a String.
STRONG - org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation.StrengthLevel
Strong level of activity.
SU - org.orekit.files.rinex.navigation.UtcId
UTC(SU).
SubFrame - Class in org.orekit.gnss.rflink.gps
Container for sub-frames in a GPS navigation message.
SubFrame(int[], int) - Constructor for class org.orekit.gnss.rflink.gps.SubFrame
Simple constructor.
SubFrame1 - Class in org.orekit.gnss.rflink.gps
Container for sub-frames 1.
SubFrame2 - Class in org.orekit.gnss.rflink.gps
Container for sub-frames 2.
SubFrame3 - Class in org.orekit.gnss.rflink.gps
Container for sub-frames 3.
SubFrame45 - Class in org.orekit.gnss.rflink.gps
Base container for sub-frames 4 and 5.
SubFrame4A - Class in org.orekit.gnss.rflink.gps
Container for sub-frames 4, pages 1, 6, 11, 16 and 21, but also for sub-frames 4, pages 2, 3, 4, 5, 7, 8, and 9 which have a similar structure.
SubFrame4A0 - Class in org.orekit.gnss.rflink.gps
Container for sub-frames 4, pages 1, 6, 11, 16 and 21.
SubFrame4A1 - Class in org.orekit.gnss.rflink.gps
Container for sub-frames 4, pages 2, 3, 4, 5, 7, 8, and 9.
SubFrame4B - Class in org.orekit.gnss.rflink.gps
Container for sub-frames 4, pages 10, 14, 15, 17.
SubFrame4C - Class in org.orekit.gnss.rflink.gps
Container for sub-frames 4, page 13.
SubFrame4D - Class in org.orekit.gnss.rflink.gps
Container for sub-frames 4, page 18.
SubFrame4E - Class in org.orekit.gnss.rflink.gps
Container for sub-frames 4, page 25.
SubFrame5B - Class in org.orekit.gnss.rflink.gps
Container for sub-frames 5, page 25.
SubFrameAlmanac - Class in org.orekit.gnss.rflink.gps
Container for sub-frames 5, page 1-24.
SubFrameDummyAlmanac - Class in org.orekit.gnss.rflink.gps
Almanac for dummy SV.
subtractOffset(AngularCoordinates) - Method in class org.orekit.utils.AngularCoordinates
Subtract an offset from the instance.
subtractOffset(AngularCoordinates) - Method in class org.orekit.utils.TimeStampedAngularCoordinates
Subtract an offset from the instance.
subtractOffset(FieldAngularCoordinates<T>) - Method in class org.orekit.utils.FieldAngularCoordinates
Subtract an offset from the instance.
subtractOffset(FieldAngularCoordinates<T>) - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates
Subtract an offset from the instance.
SUN - org.orekit.attitudes.PredefinedTarget
Sun direction.
SUN - org.orekit.bodies.JPLEphemeridesLoader.EphemerisType
Constant for the Sun.
SUN - org.orekit.files.ccsds.definitions.CenterName
Sun body.
SUN - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Sun.
SUN_PULSATION - Static variable in class org.orekit.frames.SingleParameterFitter
Sun pulsation, one year period.
SUN_RADIUS - Static variable in interface org.orekit.utils.Constants
Sun radius: 695700000 m (source: resolution B3 from IAU 2015).
SUPPORTED_NAMES - Static variable in class org.orekit.frames.ITRFVersionLoader
Regular expression for supported files names.
supportsTimeTransform() - Method in class org.orekit.models.earth.GeoMagneticField
Indicates whether this model supports time transformation or not.
SW_DATA_EPOCH - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey
Epoch of the Space Weather data.
SW_DATA_SOURCE - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey
Space Weather data source.
SW_INTERP_METHOD - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey
Interpolation method for Space Weather data.
swap12() - Method in class org.orekit.attitudes.FieldInertia
Swap axes 1 and 2.
swap12() - Method in class org.orekit.attitudes.Inertia
Swap axes 1 and 2.
swap13() - Method in class org.orekit.attitudes.FieldInertia
Swap axes 1 and 3.
swap13() - Method in class org.orekit.attitudes.Inertia
Swap axes 1 and 3.
swap23() - Method in class org.orekit.attitudes.FieldInertia
Swap axes 2 and 3.
swap23() - Method in class org.orekit.attitudes.Inertia
Swap axes 2 and 3.
switchOccurred(AttitudeProvider, AttitudeProvider, SpacecraftState) - Method in interface org.orekit.attitudes.AttitudesSequence.SwitchHandler
Method called when attitude is switched from one law to another law.
sxpInitialize() - Method in class org.orekit.propagation.analytical.tle.SGP4
Initialization proper to each propagator (SGP or SDP).
sxpInitialize() - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
Initialization proper to each propagator (SGP or SDP).
sxpInitialize(T[]) - Method in class org.orekit.propagation.analytical.tle.FieldSGP4
Initialization proper to each propagator (SGP or SDP).
sxpInitialize(T[]) - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
Initialization proper to each propagator (SGP or SDP).
sxpPropagate(double) - Method in class org.orekit.propagation.analytical.tle.SGP4
Propagation proper to each propagator (SGP or SDP).
sxpPropagate(double) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
Propagation proper to each propagator (SGP or SDP).
sxpPropagate(T, T[]) - Method in class org.orekit.propagation.analytical.tle.FieldSGP4
Propagation proper to each propagator (SGP or SDP).
sxpPropagate(T, T[]) - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
Propagation proper to each propagator (SGP or SDP).
SYNCHRONOUS_RADIUS_KM - Static variable in class org.orekit.propagation.analytical.intelsat.IntelsatElevenElements
Sun synchronous radius in kilometers.
SYS_DCBS_APPLIED - org.orekit.files.rinex.section.RinexLabels
Differential code bias corrections.
SYS_NB_TYPES_OF_OBSERV - org.orekit.files.rinex.section.RinexLabels
Number and types of observations.
SYS_PCVS_APPLIED - org.orekit.files.rinex.section.RinexLabels
Phase center variations corrections.
SYS_PHASE_SHIFT - org.orekit.files.rinex.section.RinexLabels
Phase shift.
SYS_SCALE_FACTOR - org.orekit.files.rinex.section.RinexLabels
Scale factor.
SystemConfiguration() - Constructor for class org.orekit.files.ilrs.CRDConfiguration.SystemConfiguration
Constructor.
SystemTimeOffsetMessage - Class in org.orekit.files.rinex.navigation
Container for data contained in a System Time Offset navigation message.
SystemTimeOffsetMessage(SatelliteSystem, int, String) - Constructor for class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage
Simple constructor.

T

t2cof - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
3/2 * C1.
t2cof - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
3/2 * C1.
TabulatedLofOffset - Class in org.orekit.attitudes
This class handles an attitude provider interpolating from a predefined table containing offsets from a Local Orbital Frame.
TabulatedLofOffset(Frame, LOF, List<? extends TimeStampedAngularCoordinates>, int, AngularDerivativesFilter) - Constructor for class org.orekit.attitudes.TabulatedLofOffset
Creates new instance.
TabulatedLofOffset(Frame, LOF, List<? extends TimeStampedAngularCoordinates>, int, AngularDerivativesFilter, AbsoluteDate, AbsoluteDate) - Constructor for class org.orekit.attitudes.TabulatedLofOffset
Creates new instance.
TabulatedProvider - Class in org.orekit.attitudes
This class handles an attitude provider interpolating from a predefined table.
TabulatedProvider(List<? extends TimeStampedAngularCoordinates>, int, AngularDerivativesFilter, AbsoluteDate, AbsoluteDate, AttitudeBuilder) - Constructor for class org.orekit.attitudes.TabulatedProvider
Creates new instance.
TabulatedProvider(Frame, List<? extends TimeStampedAngularCoordinates>, int, AngularDerivativesFilter) - Constructor for class org.orekit.attitudes.TabulatedProvider
Creates new instance.
TAI - org.orekit.files.ccsds.definitions.TimeSystem
International Atomic Time.
TAI - org.orekit.gnss.TimeSystem
International Atomic Time.
TAIMUTC_AT_TZERO - org.orekit.files.ccsds.ndm.adm.acm.AcmMetadataKey
Difference (TAI – UTC) in seconds at epoch AcmMetadataKey.EPOCH_TZERO.
TAIMUTC_AT_TZERO - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Difference (TAI – UTC) in seconds at epoch OcmMetadataKey.EPOCH_TZERO.
TAIScale - Class in org.orekit.time
International Atomic Time.
TAIUTCDatFilesLoader - Class in org.orekit.time
Loader for UTC-TAI extracted from tai-utc.dat file from USNO.
TAIUTCDatFilesLoader(String) - Constructor for class org.orekit.time.TAIUTCDatFilesLoader
Build a loader for tai-utc.dat file from USNO.
TAIUTCDatFilesLoader(String, DataProvidersManager) - Constructor for class org.orekit.time.TAIUTCDatFilesLoader
Build a loader for tai-utc.dat file from USNO.
TAIUTCDatFilesLoader.Parser - Class in org.orekit.time
Internal class performing the parsing.
TAM - org.orekit.files.ccsds.definitions.SpacecraftBodyFrame.BaseEquipment
Three Axis Magnetometer.
TARGET_ATTITUDE - org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuverKey
Target attitude.
TARGET_MOM_FRAME - org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuverKey
Target momentum frame.
TARGET_MOMENTUM - org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuverKey
Target momentum.
TARGET_SPINRATE - org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuverKey
Target spin rate.
TargetPointing - Class in org.orekit.attitudes
This class handles target pointing attitude provider.
TargetPointing(Frame, GeodeticPoint, BodyShape) - Constructor for class org.orekit.attitudes.TargetPointing
Creates a new instance from body shape and target expressed in geodetic coordinates.
TargetPointing(Frame, Frame, Vector3D) - Constructor for class org.orekit.attitudes.TargetPointing
Creates a new instance from body frame and target expressed in Cartesian coordinates.
TargetProvider - Interface in org.orekit.attitudes
Provider for target vector.
TCA - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
Date and time in UTC of the closest approach.
TCB - org.orekit.files.ccsds.definitions.TimeSystem
Barycentric Coordinate Time.
TCBScale - Class in org.orekit.time
Barycentric Coordinate Time.
TCG - org.orekit.files.ccsds.definitions.TimeSystem
Geocentric Coordinate Time.
TCGScale - Class in org.orekit.time
Geocentric Coordinate Time.
TDB - org.orekit.files.ccsds.definitions.TimeSystem
Barycentric Dynamical Time.
TDBScale - Class in org.orekit.time
Barycentric Dynamic Time.
Tdm - Class in org.orekit.files.ccsds.ndm.tdm
This class stores all the information of the CCSDS Tracking Data Message parsed by TDMParser or TDMXMLParser.
Tdm(TdmHeader, List<Segment<TdmMetadata, ObservationsBlock>>, IERSConventions, DataContext) - Constructor for class org.orekit.files.ccsds.ndm.tdm.Tdm
Simple constructor.
TDM_MSG_LINK - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Unique identifier of Tracking Data Message linked to this Orbit Data Message.
TdmDataKey - Enum in org.orekit.files.ccsds.ndm.tdm
Keys for TDM observations entries, except the measurements themselves.
TdmHeader - Class in org.orekit.files.ccsds.ndm.tdm
Header of a CCSDS Tracking Data Message.
TdmHeader() - Constructor for class org.orekit.files.ccsds.ndm.tdm.TdmHeader
Constructor.
TdmMetadata - Class in org.orekit.files.ccsds.ndm.tdm
The TDMMetadata class gathers the meta-data present in the Tracking Data Message (TDM).
TdmMetadata() - Constructor for class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Create a new TDM meta-data.
TdmMetadataKey - Enum in org.orekit.files.ccsds.ndm.tdm
Keys for TDM container entries.
TdmParser - Class in org.orekit.files.ccsds.ndm.tdm
Class for CCSDS Tracking Data Message parsers.
TdmParser(IERSConventions, boolean, DataContext, ParsedUnitsBehavior, RangeUnitsConverter, Function<ParseToken, List<ParseToken>>[]) - Constructor for class org.orekit.files.ccsds.ndm.tdm.TdmParser
Complete constructor.
TdmWriter - Class in org.orekit.files.ccsds.ndm.tdm
Writer for CCSDS Tracking Data Message.
TdmWriter(IERSConventions, DataContext, RangeUnitsConverter) - Constructor for class org.orekit.files.ccsds.ndm.tdm.TdmWriter
Complete constructor.
TDOA - Class in org.orekit.estimation.measurements
Class modeling a Time Difference of Arrival measurement with a satellite as emitter and two ground stations as receivers.
TDOA(GroundStation, GroundStation, AbsoluteDate, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.TDOA
Simple constructor.
TDOABuilder - Class in org.orekit.estimation.measurements.generation
Builder for TDOA measurements.
TDOABuilder(CorrelatedRandomVectorGenerator, GroundStation, GroundStation, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.TDOABuilder
Simple constructor.
TDOAIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical TDOA measurements with ionospheric delay.
TDOAIonosphericDelayModifier(IonosphericModel, double) - Constructor for class org.orekit.estimation.measurements.modifiers.TDOAIonosphericDelayModifier
Constructor.
TDOATroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical TDOA measurements with tropospheric delay.
TDOATroposphericDelayModifier(DiscreteTroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.TDOATroposphericDelayModifier
Deprecated.
TDOATroposphericDelayModifier(TroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.TDOATroposphericDelayModifier
Constructor.
TDR - org.orekit.files.ccsds.definitions.CelestialBodyFrame
True of Date, Rotating.
TECH_ADDRESS - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Address of Technical Point Of Contact at originator.
TECH_EMAIL - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Email address of Technical Point Of Contact at originator.
TECH_ORG - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Creating agency or operator.
TECH_PHONE - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Phone number of Technical Point Of Contact at originator.
TECH_POC - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Technical Point Of Contact at originator.
TECH_POSITION - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Position of Technical Point Of Contact at originator.
TectonicsDisplacement - Class in org.orekit.models.earth.displacement
Modeling of displacement of reference points due to plate tectonics.
TectonicsDisplacement(AbsoluteDate, Vector3D) - Constructor for class org.orekit.models.earth.displacement.TectonicsDisplacement
Simple constructor.
TEME - org.orekit.files.ccsds.definitions.CelestialBodyFrame
True Equator Mean Equinox.
TEME - org.orekit.frames.Predefined
TEME frame.
TEME_OF_DATE - org.orekit.files.stk.STKEphemerisFile.STKCoordinateSystem
True equator and mean equinox of date.
TEMPERATURE - org.orekit.files.ccsds.ndm.tdm.ObservationType
Data: Temperature [K].
TESLA - Static variable in class org.orekit.utils.units.Unit
tesla unit.
tessellate(SphericalPolygonsSet, double, double, double, double, boolean, boolean) - Method in class org.orekit.models.earth.tessellation.EllipsoidTessellator
Tessellate a zone of interest into tiles.
THDT - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
THDT.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.AngularAzEl
Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.AngularRaDec
Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.BistaticRange
Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.BistaticRangeRate
Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.FDOA
Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.gnss.InterSatellitesOneWayRangeRate
Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.gnss.InterSatellitesPhase
Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.gnss.OneWayGNSSPhase
Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.gnss.OneWayGNSSRange
Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.gnss.OneWayGNSSRangeRate
Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.gnss.Phase
Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.InterSatellitesRange
Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.MultiplexedMeasurement
Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.Position
Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.PV
Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.Range
Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.RangeRate
Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.TDOA
Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.TurnAroundRange
Estimate the theoretical value.
theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Estimate the theoretical value without derivatives.
theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.AngularAzEl
Estimate the theoretical value without derivatives.
theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.AngularRaDec
Estimate the theoretical value without derivatives.
theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.BistaticRange
Estimate the theoretical value without derivatives.
theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.BistaticRangeRate
Estimate the theoretical value without derivatives.
theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.FDOA
Estimate the theoretical value without derivatives.
theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.gnss.InterSatellitesOneWayRangeRate
Estimate the theoretical value without derivatives.
theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.gnss.InterSatellitesPhase
Estimate the theoretical value without derivatives.
theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.gnss.OneWayGNSSPhase
Estimate the theoretical value without derivatives.
theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.gnss.OneWayGNSSRange
Estimate the theoretical value without derivatives.
theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.gnss.OneWayGNSSRangeRate
Estimate the theoretical value without derivatives.
theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.gnss.Phase
Estimate the theoretical value without derivatives.
theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.InterSatellitesRange
Estimate the theoretical value without derivatives.
theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.MultiplexedMeasurement
Estimate the theoretical value without derivatives.
theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.Position
Estimate the theoretical value without derivatives.
theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.PV
Estimate the theoretical value without derivatives.
theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.Range
Estimate the theoretical value without derivatives.
theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.RangeRate
Estimate the theoretical value without derivatives.
theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.TDOA
Estimate the theoretical value without derivatives.
theoreticalEvaluationWithoutDerivatives(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.TurnAroundRange
Estimate the theoretical value without derivatives.
theoryIsSgpSdp() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmMetadata
Check if mean element theory in SGP or SDP.
theta2 - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
cos io squared.
theta2 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
cos io squared.
ThirdBodyAttraction - Class in org.orekit.forces.gravity
Third body attraction force model.
ThirdBodyAttraction(CelestialBody) - Constructor for class org.orekit.forces.gravity.ThirdBodyAttraction
Simple constructor.
ThirdBodyAttractionEpoch - Class in org.orekit.forces.gravity
Third body attraction force model.
ThirdBodyAttractionEpoch(CelestialBody) - Constructor for class org.orekit.forces.gravity.ThirdBodyAttractionEpoch
Simple constructor.
THR_DIR_SIGMA - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
One σ angular off-nominal thrust direction.
THR_EFFIC - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
Thrust efficiency η typically between 0.0 and 1.0.
THR_INTERP - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
Interpolation mode between current and next acceleration line.
THR_ISP - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
Thrust specific impulse.
THR_MAG_SIGMA - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
One σ percent error on thrust magnitude.
THR_X - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
Thrust component along X axis.
THR_Y - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
Thrust component along Y axis.
THR_Z - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
Thrust component along Z axis.
ThreeEighthesFieldIntegratorBuilder<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.conversion
Builder for ThreeEighthesFieldIntegrator.
ThreeEighthesFieldIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.ThreeEighthesFieldIntegratorBuilder
Constructor.
ThreeEighthesFieldIntegratorBuilder(T) - Constructor for class org.orekit.propagation.conversion.ThreeEighthesFieldIntegratorBuilder
Constructor using a "fielded" step.
ThreeEighthesIntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for ThreeEighthesIntegrator.
ThreeEighthesIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.ThreeEighthesIntegratorBuilder
Build a new instance.
THRUST - Static variable in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
Parameter name for thrust.
THRUST_ACCELERATION - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
The object’s acceleration due to in-track thrust used to propagate the state vector and covariance to TCA.
THRUST_SCALE - Static variable in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
Thrust scaling factor.
ThrustDirectionAndAttitudeProvider - Class in org.orekit.forces.maneuvers.propulsion
This class is used in to both manage the attitude of the satellite and the direction of thrust.
ThrustDirectionProvider - Interface in org.orekit.forces.maneuvers.propulsion
Interface to compute the thrust direction of a maneuver.
ThrustPropulsionModel - Interface in org.orekit.forces.maneuvers.propulsion
Interface for a thrust-based propulsion model.
THRUSTX_SCALE_FACTOR - Static variable in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel
Parameter name for the scale factor on the X component of the thrust in S/C frame.
THRUSTY_SCALE_FACTOR - Static variable in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel
Parameter name for the scale factor on the Y component of the thrust in S/C frame.
THRUSTZ_SCALE_FACTOR - Static variable in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel
Parameter name for the scale factor on the Z component of the thrust in S/C frame.
TidalDisplacement - Class in org.orekit.models.earth.displacement
Modeling of displacement of reference points due to tidal effects.
TidalDisplacement(double, double, double, PVCoordinatesProvider, PVCoordinatesProvider, IERSConventions, boolean) - Constructor for class org.orekit.models.earth.displacement.TidalDisplacement
Simple constructor.
Tide - Class in org.orekit.models.earth.displacement
Class representing a tide.
Tide(int) - Constructor for class org.orekit.models.earth.displacement.Tide
Simple constructor.
Tide(int, int, int, int, int, int) - Constructor for class org.orekit.models.earth.displacement.Tide
Simple constructor.
TIDE_FREE - org.orekit.forces.gravity.potential.TideSystem
Constant for tide-free gravity fields.
TideSystem - Enum in org.orekit.forces.gravity.potential
Enumerate for tie systems.
TideSystemProvider - Interface in org.orekit.forces.gravity.potential
Interface used to provide tide systems.
Tile - Class in org.orekit.models.earth.tessellation
Simple data structure for a quadrilateral tile shape on a body surface.
Tile(GeodeticPoint, GeodeticPoint, GeodeticPoint, GeodeticPoint) - Constructor for class org.orekit.models.earth.tessellation.Tile
Create a tile.
TileAiming - Interface in org.orekit.models.earth.tessellation
Interface defining the aiming direction of tiles.
TIME - org.orekit.files.ccsds.definitions.DutyCycleType
Time-based duty cycle.
TIME_ABSOLUTE - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
Absolute epoch time.
TIME_AND_ANGLE - org.orekit.files.ccsds.definitions.DutyCycleType
Duty cycle based on phasing/clocking of space object body past a reference direction.
TIME_LASTOB_END - org.orekit.files.ccsds.ndm.cdm.ODParametersKey
The start of a time interval (UTC) that contains the time of the last accepted observation.
TIME_LASTOB_START - org.orekit.files.ccsds.ndm.cdm.ODParametersKey
The start of a time interval (UTC) that contains the time of the last accepted observation.
TIME_OF_FIRST_OBS - org.orekit.files.rinex.section.RinexLabels
Time of first observation.
TIME_OF_LAST_OBS - org.orekit.files.rinex.section.RinexLabels
Time of last observation.
TIME_RELATIVE - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
Relative epoch time.
TIME_SPAN - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Span of time that the OCM covers.
TIME_SYSTEM - org.orekit.files.ccsds.section.MetadataKey
Time system entry.
TimeComponents - Class in org.orekit.time
Class representing a time within the day broken up as hour, minute and second components.
TimeComponents(double) - Constructor for class org.orekit.time.TimeComponents
Build a time from the second number within the day.
TimeComponents(int, double) - Constructor for class org.orekit.time.TimeComponents
Build a time from the second number within the day.
TimeComponents(int, int, double) - Constructor for class org.orekit.time.TimeComponents
Build a time from its clock elements.
TimeComponents(int, int, double, int) - Constructor for class org.orekit.time.TimeComponents
Build a time from its clock elements.
TimeConverter - Class in org.orekit.files.ccsds.definitions
Dates reader/writer.
TimeConverter(TimeScale, AbsoluteDate) - Constructor for class org.orekit.files.ccsds.definitions.TimeConverter
Build a time system.
TimeDerivativesEquations - Interface in org.orekit.propagation.numerical
Interface summing up the contribution of several forces into orbit and mass derivatives.
timeFactor(double) - Method in enum org.orekit.models.earth.displacement.PsdCorrection.TimeEvolution
Evaluate correction time factor.
TimeInterpolator<T extends TimeStamped> - Interface in org.orekit.time
This interface represents objects that can interpolate a time stamped value with respect to time.
TimeScalarFunction - Interface in org.orekit.time
This interface represents a scalar function of time.
TimeScale - Interface in org.orekit.time
Interface for time scales.
TimeScales - Interface in org.orekit.time
A collection of TimeScales.
TimeScalesFactory - Class in org.orekit.time
Factory for predefined time scales.
timeScalesOffset(TimeScale, TimeScale) - Method in class org.orekit.time.AbsoluteDate
Compute the offset between two time scales at the current instant.
timeScalesOffset(TimeScale, TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate
Compute the offset between two time scales at the current instant.
TimeShiftable<T extends TimeShiftable<T>> - Interface in org.orekit.time
This interface represents objects that can be shifted in time.
TimeSpanDragForce - Class in org.orekit.forces.drag
Deprecated.
as of 12.1
TimeSpanDragForce(Atmosphere, DragSensitive) - Constructor for class org.orekit.forces.drag.TimeSpanDragForce
Deprecated.
Constructor with default UTC time scale for the default names of the drag parameter drivers.
TimeSpanDragForce(Atmosphere, DragSensitive, TimeScale) - Constructor for class org.orekit.forces.drag.TimeSpanDragForce
Deprecated.
Constructor.
TimeSpanEstimatedModel - Class in org.orekit.models.earth.troposphere
Time span estimated tropospheric model.
TimeSpanEstimatedModel(EstimatedModel) - Constructor for class org.orekit.models.earth.troposphere.TimeSpanEstimatedModel
Constructor with default UTC time scale.
TimeSpanEstimatedModel(EstimatedModel, TimeScale) - Constructor for class org.orekit.models.earth.troposphere.TimeSpanEstimatedModel
Constructor with default UTC time scale.
TimeSpanEstimatedTroposphericModel - Class in org.orekit.models.earth.troposphere
Deprecated.
as of 12.1, replaced by TimeSpanEstimatedModel
TimeSpanEstimatedTroposphericModel(EstimatedTroposphericModel) - Constructor for class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
Deprecated.
Constructor with default UTC time scale.
TimeSpanEstimatedTroposphericModel(EstimatedTroposphericModel, TimeScale) - Constructor for class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
Deprecated.
Constructor with default UTC time scale.
TimeSpanMap<T> - Class in org.orekit.utils
Container for objects that apply to spans of time.
TimeSpanMap(T) - Constructor for class org.orekit.utils.TimeSpanMap
Create a map containing a single object, initially valid throughout the timeline.
TimeSpanMap.Span<S> - Class in org.orekit.utils
Holder for one time span.
TimeSpanMap.Transition<S> - Class in org.orekit.utils
Class holding transition times.
TimeSpanParametricAcceleration - Class in org.orekit.forces.empirical
Time span parametric acceleration model.
TimeSpanParametricAcceleration(Vector3D, boolean, AccelerationModel) - Constructor for class org.orekit.forces.empirical.TimeSpanParametricAcceleration
Simple constructor.
TimeSpanParametricAcceleration(Vector3D, AttitudeProvider, AccelerationModel) - Constructor for class org.orekit.forces.empirical.TimeSpanParametricAcceleration
Simple constructor.
TimeStamped - Interface in org.orekit.time
This interface represents objects that have a AbsoluteDate date attached to them.
TimeStampedAngularCoordinates - Class in org.orekit.utils
TimeStampedAngularCoordinates(AbsoluteDate, FieldRotation<U>) - Constructor for class org.orekit.utils.TimeStampedAngularCoordinates
Builds a TimeStampedAngularCoordinates from a FieldRotation<Derivative>.
TimeStampedAngularCoordinates(AbsoluteDate, Rotation, Vector3D, Vector3D) - Constructor for class org.orekit.utils.TimeStampedAngularCoordinates
Builds a rotation/rotation rate pair.
TimeStampedAngularCoordinates(AbsoluteDate, PVCoordinates, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedAngularCoordinates
Build one of the rotations that transform one pv coordinates into another one.
TimeStampedAngularCoordinates(AbsoluteDate, PVCoordinates, PVCoordinates, PVCoordinates, PVCoordinates, double) - Constructor for class org.orekit.utils.TimeStampedAngularCoordinates
Build the rotation that transforms a pair of pv coordinates into another pair.
TimeStampedAngularCoordinatesHermiteInterpolator - Class in org.orekit.utils
Class using Hermite interpolator to interpolate time stamped angular coordinates.
TimeStampedAngularCoordinatesHermiteInterpolator() - Constructor for class org.orekit.utils.TimeStampedAngularCoordinatesHermiteInterpolator
Constructor with : Default number of interpolation points of DEFAULT_INTERPOLATION_POINTS Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of angular and first time derivative for attitude interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).
TimeStampedAngularCoordinatesHermiteInterpolator(int) - Constructor for class org.orekit.utils.TimeStampedAngularCoordinatesHermiteInterpolator
/** Constructor with : Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of angular and first time derivative for attitude interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).
TimeStampedAngularCoordinatesHermiteInterpolator(int, double, AngularDerivativesFilter) - Constructor for class org.orekit.utils.TimeStampedAngularCoordinatesHermiteInterpolator
Constructor.
TimeStampedAngularCoordinatesHermiteInterpolator(int, AngularDerivativesFilter) - Constructor for class org.orekit.utils.TimeStampedAngularCoordinatesHermiteInterpolator
Constructor with : Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).
TimeStampedCache<T extends TimeStamped> - Interface in org.orekit.utils
Interface for a data structure that can provide concurrent access to TimeStamped data surrounding a given date.
TimeStampedCacheException - Exception in org.orekit.errors
This class is the base class for all specific exceptions thrown by during the GenericTimeStampedCache.
TimeStampedCacheException(Throwable, Localizable, Object...) - Constructor for exception org.orekit.errors.TimeStampedCacheException
Simple constructor.
TimeStampedCacheException(Localizable, Object...) - Constructor for exception org.orekit.errors.TimeStampedCacheException
Simple constructor.
TimeStampedCacheException(MathRuntimeException) - Constructor for exception org.orekit.errors.TimeStampedCacheException
Simple constructor.
TimeStampedCacheException(OrekitException) - Constructor for exception org.orekit.errors.TimeStampedCacheException
Simple constructor.
TimeStampedDouble - Class in org.orekit.time
Class that associates a double with a date.
TimeStampedDouble(double, AbsoluteDate) - Constructor for class org.orekit.time.TimeStampedDouble
Constructor.
TimeStampedDoubleAndDerivative - Class in org.orekit.time
Class that associates a double, its time derivative with a date.
TimeStampedDoubleAndDerivative(double, double, AbsoluteDate) - Constructor for class org.orekit.time.TimeStampedDoubleAndDerivative
Constructor.
TimeStampedDoubleAndDerivativeHermiteInterpolator - Class in org.orekit.time
Hermite interpolator of time stamped double value.
TimeStampedDoubleAndDerivativeHermiteInterpolator() - Constructor for class org.orekit.time.TimeStampedDoubleAndDerivativeHermiteInterpolator
Constructor with : Default number of interpolation points of DEFAULT_INTERPOLATION_POINTS Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).
TimeStampedDoubleAndDerivativeHermiteInterpolator(int) - Constructor for class org.orekit.time.TimeStampedDoubleAndDerivativeHermiteInterpolator
Constructor with default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s).
TimeStampedDoubleAndDerivativeHermiteInterpolator(int, double) - Constructor for class org.orekit.time.TimeStampedDoubleAndDerivativeHermiteInterpolator
Constructor.
TimeStampedDoubleHermiteInterpolator - Class in org.orekit.time
Hermite interpolator of time stamped double value.
TimeStampedDoubleHermiteInterpolator() - Constructor for class org.orekit.time.TimeStampedDoubleHermiteInterpolator
Constructor with : Default number of interpolation points of DEFAULT_INTERPOLATION_POINTS Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).
TimeStampedDoubleHermiteInterpolator(int) - Constructor for class org.orekit.time.TimeStampedDoubleHermiteInterpolator
Constructor with default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s).
TimeStampedDoubleHermiteInterpolator(int, double) - Constructor for class org.orekit.time.TimeStampedDoubleHermiteInterpolator
Constructor.
TimeStampedField<KK extends CalculusFieldElement<KK>> - Class in org.orekit.time
Class that associates a field with a date.
TimeStampedField(KK, AbsoluteDate) - Constructor for class org.orekit.time.TimeStampedField
Constructor with normal date.
TimeStampedField(KK, FieldAbsoluteDate<KK>) - Constructor for class org.orekit.time.TimeStampedField
Constructor.
TimeStampedFieldAngularCoordinates<T extends CalculusFieldElement<T>> - Class in org.orekit.utils
TimeStampedFieldAngularCoordinates(Field<T>, TimeStampedAngularCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinates
Builds an instance for a regular TimeStampedAngularCoordinates.
TimeStampedFieldAngularCoordinates(AbsoluteDate, FieldRotation<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinates
Builds a rotation/rotation rate pair.
TimeStampedFieldAngularCoordinates(AbsoluteDate, FieldPVCoordinates<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>, double) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinates
Build the rotation that transforms a pair of pv coordinates into another pair.
TimeStampedFieldAngularCoordinates(FieldAbsoluteDate<T>, FieldRotation<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinates
Builds a rotation/rotation rate pair.
TimeStampedFieldAngularCoordinates(FieldAbsoluteDate<T>, FieldRotation<U>) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinates
Builds a TimeStampedFieldAngularCoordinates from a FieldRotation<FieldDerivativeStructure>.
TimeStampedFieldAngularCoordinates(FieldAbsoluteDate<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>, double) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinates
Build the rotation that transforms a pair of pv coordinates into another pair.
TimeStampedFieldAngularCoordinatesHermiteInterpolator<KK extends CalculusFieldElement<KK>> - Class in org.orekit.utils
Class using Hermite interpolator to interpolate time stamped angular coordinates.
TimeStampedFieldAngularCoordinatesHermiteInterpolator() - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinatesHermiteInterpolator
Constructor with : Default number of interpolation points of DEFAULT_INTERPOLATION_POINTS Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of angular and first time derivative for attitude interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).
TimeStampedFieldAngularCoordinatesHermiteInterpolator(int) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinatesHermiteInterpolator
/** Constructor with : Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of angular and first time derivative for attitude interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).
TimeStampedFieldAngularCoordinatesHermiteInterpolator(int, double, AngularDerivativesFilter) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinatesHermiteInterpolator
Constructor.
TimeStampedFieldAngularCoordinatesHermiteInterpolator(int, AngularDerivativesFilter) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinatesHermiteInterpolator
Constructor with : Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).
TimeStampedFieldHermiteInterpolator<KK extends CalculusFieldElement<KK>> - Class in org.orekit.time
Hermite interpolator of time stamped field value.
TimeStampedFieldHermiteInterpolator() - Constructor for class org.orekit.time.TimeStampedFieldHermiteInterpolator
Constructor with : Default number of interpolation points of DEFAULT_INTERPOLATION_POINTS Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).
TimeStampedFieldHermiteInterpolator(int) - Constructor for class org.orekit.time.TimeStampedFieldHermiteInterpolator
Constructor with : Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).
TimeStampedFieldHermiteInterpolator(int, double) - Constructor for class org.orekit.time.TimeStampedFieldHermiteInterpolator
Constructor.
TimeStampedFieldPVCoordinates<T extends CalculusFieldElement<T>> - Class in org.orekit.utils
TimeStampedFieldPVCoordinates(Field<T>, TimeStampedPVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Constructor from Field and TimeStampedPVCoordinates.
TimeStampedFieldPVCoordinates(AbsoluteDate, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Multiplicative constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, FieldVector3D<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Builds a PVCoordinates pair.
TimeStampedFieldPVCoordinates(AbsoluteDate, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Basic constructor.
TimeStampedFieldPVCoordinates(AbsoluteDate, FieldPVCoordinates<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Subtractive constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Multiplicative constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Multiplicative constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Multiplicative constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, FieldVector3D<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Builds a PVCoordinates pair.
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, FieldVector3D<U>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Builds a TimeStampedFieldPVCoordinates triplet from a FieldVector3D<FieldDerivativeStructure>.
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Basic constructor.
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Subtractive constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Multiplicative constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Multiplicative constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinatesHermiteInterpolator<KK extends CalculusFieldElement<KK>> - Class in org.orekit.utils
Class using a Hermite interpolator to interpolate time stamped position-velocity-acceleration coordinates.
TimeStampedFieldPVCoordinatesHermiteInterpolator() - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinatesHermiteInterpolator
Constructor with : Default number of interpolation points of DEFAULT_INTERPOLATION_POINTS Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of angular and first time derivative for attitude interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).
TimeStampedFieldPVCoordinatesHermiteInterpolator(int) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinatesHermiteInterpolator
Constructor with : Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of position and both time derivatives for attitude interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).
TimeStampedFieldPVCoordinatesHermiteInterpolator(int, double, CartesianDerivativesFilter) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinatesHermiteInterpolator
Constructor.
TimeStampedFieldPVCoordinatesHermiteInterpolator(int, CartesianDerivativesFilter) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinatesHermiteInterpolator
Constructor with : Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).
TimeStampedGenerator<T extends TimeStamped> - Interface in org.orekit.utils
Generator to use for creating entries in time stamped caches.
TimeStampedPair<K extends TimeStamped,​V extends TimeStamped> - Class in org.orekit.time
Pair of time stamped values being defined at the same date.
TimeStampedPair(K, V) - Constructor for class org.orekit.time.TimeStampedPair
Constructor.
TimeStampedPair(K, V, double) - Constructor for class org.orekit.time.TimeStampedPair
Constructor.
TimeStampedPVCoordinates - Class in org.orekit.utils
TimeStampedPVCoordinates(AbsoluteDate, double, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates
Multiplicative constructor
TimeStampedPVCoordinates(AbsoluteDate, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates
Linear constructor
TimeStampedPVCoordinates(AbsoluteDate, double, PVCoordinates, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates
Linear constructor
TimeStampedPVCoordinates(AbsoluteDate, double, PVCoordinates, double, PVCoordinates, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates
Linear constructor
TimeStampedPVCoordinates(AbsoluteDate, FieldVector3D<U>) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates
Builds a TimeStampedPVCoordinates triplet from a FieldVector3D<Derivative>.
TimeStampedPVCoordinates(AbsoluteDate, Vector3D, Vector3D) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates
Build from position and velocity.
TimeStampedPVCoordinates(AbsoluteDate, Vector3D, Vector3D, Vector3D) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates
Builds a TimeStampedPVCoordinates pair.
TimeStampedPVCoordinates(AbsoluteDate, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates
Build from position velocity acceleration coordinates.
TimeStampedPVCoordinates(AbsoluteDate, PVCoordinates, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates
Subtractive constructor
TimeStampedPVCoordinatesHermiteInterpolator - Class in org.orekit.utils
Class using a Hermite interpolator to interpolate time stamped position-velocity-acceleration coordinates.
TimeStampedPVCoordinatesHermiteInterpolator() - Constructor for class org.orekit.utils.TimeStampedPVCoordinatesHermiteInterpolator
Constructor with : Default number of interpolation points of DEFAULT_INTERPOLATION_POINTS Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of position and both time derivatives for attitude interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).
TimeStampedPVCoordinatesHermiteInterpolator(int) - Constructor for class org.orekit.utils.TimeStampedPVCoordinatesHermiteInterpolator
Constructor with : Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of position and both time derivatives for attitude interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).
TimeStampedPVCoordinatesHermiteInterpolator(int, double, CartesianDerivativesFilter) - Constructor for class org.orekit.utils.TimeStampedPVCoordinatesHermiteInterpolator
Constructor.
TimeStampedPVCoordinatesHermiteInterpolator(int, CartesianDerivativesFilter) - Constructor for class org.orekit.utils.TimeStampedPVCoordinatesHermiteInterpolator
Constructor with : Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).
TimeSystem - Enum in org.orekit.files.ccsds.definitions
The set of time systems defined in CCSDS standards (ADM, ODM, NDM).
TimeSystem - Enum in org.orekit.gnss
Enumerate for the time systems used in navigation files.
TimeSystemCorrection - Class in org.orekit.files.rinex.navigation
Container for time system corrections.
TimeSystemCorrection(String, AbsoluteDate, double, double) - Constructor for class org.orekit.files.rinex.navigation.TimeSystemCorrection
Constructor.
TIMETAG_REF - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Timetag reference entry.
TimetagReference - Enum in org.orekit.files.ccsds.ndm.tdm
Reference for time tag.
TimeVectorFunction - Interface in org.orekit.time
This interface represents a multi-valued function of time.
TimingSystemConfiguration() - Constructor for class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration
Empty constructor.
TIRF_CONVENTIONS_1996_ACCURATE_EOP - org.orekit.frames.Predefined
TIRF, IERS 996 conventions, with accurate EOP interpolation.
TIRF_CONVENTIONS_1996_SIMPLE_EOP - org.orekit.frames.Predefined
TIRF, IERS 1996 conventions, with simple EOP interpolation.
TIRF_CONVENTIONS_2003_ACCURATE_EOP - org.orekit.frames.Predefined
TIRF, IERS 2003 conventions, with accurate EOP interpolation.
TIRF_CONVENTIONS_2003_SIMPLE_EOP - org.orekit.frames.Predefined
TIRF, IERS 2003 conventions, with simple EOP interpolation.
TIRF_CONVENTIONS_2010_ACCURATE_EOP - org.orekit.frames.Predefined
TIRF, IERS 2010 conventions, with accurate EOP interpolation.
TIRF_CONVENTIONS_2010_SIMPLE_EOP - org.orekit.frames.Predefined
TIRF, IERS 2010 conventions, with simple EOP interpolation.
tle - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
Initial state.
tle - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
Initial state.
TLE - Class in org.orekit.propagation.analytical.tle
This class is a container for a single set of TLE data.
TLE(int, char, int, int, String, int, int, AbsoluteDate, double, double, double, double, double, double, double, double, int, double) - Constructor for class org.orekit.propagation.analytical.tle.TLE
Simple constructor from already parsed elements.
TLE(int, char, int, int, String, int, int, AbsoluteDate, double, double, double, double, double, double, double, double, int, double, TimeScale) - Constructor for class org.orekit.propagation.analytical.tle.TLE
Simple constructor from already parsed elements using the given time scale as UTC.
TLE(String, String) - Constructor for class org.orekit.propagation.analytical.tle.TLE
Simple constructor from unparsed two lines.
TLE(String, String, TimeScale) - Constructor for class org.orekit.propagation.analytical.tle.TLE
Simple constructor from unparsed two lines using the given time scale as UTC.
TLE_CHECKSUM_ERROR - org.orekit.errors.OrekitMessages
TLE_CHECKSUM_ERROR.
TLE_INVALID_PARAMETER - org.orekit.errors.OrekitMessages
TLE_INVALID_PARAMETER.
TLE_LINES_DO_NOT_REFER_TO_SAME_OBJECT - org.orekit.errors.OrekitMessages
TLE_LINES_DO_NOT_REFER_TO_SAME_OBJECT.
TLEConstants - Class in org.orekit.propagation.analytical.tle
Constants necessary to TLE propagation.
TleGenerationAlgorithm - Interface in org.orekit.propagation.analytical.tle.generation
This interface provides a way to generate a TLE from a spacecraft state.
TleGenerationUtil - Class in org.orekit.propagation.analytical.tle.generation
Utility class for TLE generation algorithm.
TLEPropagator - Class in org.orekit.propagation.analytical.tle
This class provides elements to propagate TLE's.
TLEPropagator(TLE, AttitudeProvider, double) - Constructor for class org.orekit.propagation.analytical.tle.TLEPropagator
Protected constructor for derived classes.
TLEPropagator(TLE, AttitudeProvider, double, Frame) - Constructor for class org.orekit.propagation.analytical.tle.TLEPropagator
Protected constructor for derived classes.
TLEPropagatorBuilder - Class in org.orekit.propagation.conversion
Builder for TLEPropagator.
TLEPropagatorBuilder(TLE, PositionAngleType, double, DataContext, TleGenerationAlgorithm) - Constructor for class org.orekit.propagation.conversion.TLEPropagatorBuilder
Build a new instance.
TLEPropagatorBuilder(TLE, PositionAngleType, double, DataContext, TleGenerationAlgorithm, AttitudeProvider) - Constructor for class org.orekit.propagation.conversion.TLEPropagatorBuilder
Build a new instance.
TLEPropagatorBuilder(TLE, PositionAngleType, double, TleGenerationAlgorithm) - Constructor for class org.orekit.propagation.conversion.TLEPropagatorBuilder
Build a new instance.
TNW - org.orekit.files.ccsds.definitions.OrbitRelativeFrame
TNW : x-axis along the velocity vector, W along the orbital angular momentum vector and N completes the right-handed system.
TNW - org.orekit.frames.LOFType
Constant for TNW frame (X axis aligned with velocity, Z axis aligned with orbital momentum).
TNW_INERTIAL - org.orekit.files.ccsds.definitions.OrbitRelativeFrame
Tangential, Normal, Cross-track coordinate system (X towards velocity, Z towards momentum).
TNW_INERTIAL - org.orekit.frames.LOFType
Constant for TNW frame considered inertial (X axis aligned with velocity, Z axis aligned with orbital momentum).
TNW_ROTATING - org.orekit.files.ccsds.definitions.OrbitRelativeFrame
Tangential, Normal, Cross-track coordinate system (X towards velocity, Z towards momentum).
toAbsoluteDate() - Method in class org.orekit.time.FieldAbsoluteDate
Transform the FieldAbsoluteDate in an AbsoluteDate.
toAbsolutePVCoordinates() - Method in class org.orekit.utils.FieldAbsolutePVCoordinates
Converts to an AbsolutePVCoordinates instance.
toAngular(RotationOrder) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeState
Convert to angular coordinates.
toAngular(AbsoluteDate, RotationOrder, Rotation, int, double[]) - Method in enum org.orekit.files.ccsds.ndm.adm.acm.RateElementsType
Convert to angyla coordinates.
toAngularCoordinates() - Method in class org.orekit.utils.FieldAngularCoordinates
Convert to a regular angular coordinates.
toArray() - Method in class org.orekit.propagation.conversion.averaging.elements.AveragedCircularWithMeanAngle
Write values from instance into an array of doubles.
toArray() - Method in class org.orekit.propagation.conversion.averaging.elements.AveragedEquinoctialWithMeanAngle
Write values from instance into an array of doubles.
toArray() - Method in class org.orekit.propagation.conversion.averaging.elements.AveragedKeplerianWithMeanAngle
Write values from instance into an array of doubles.
toArray() - Method in interface org.orekit.propagation.conversion.averaging.elements.AveragedOrbitalElements
Write values from instance into an array of doubles.
toAttitude() - Method in class org.orekit.attitudes.FieldAttitude
Converts to an Attitude instance.
toAuxiliaryElements() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Transforms the FieldAuxiliaryElements instance into an AuxiliaryElements instance.
toCartesian(OneAxisEllipsoid, double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryState
Convert to Cartesian coordinates.
toCartesian(AbsoluteDate, double[], OneAxisEllipsoid, double) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitElementsType
Convert to Cartesian coordinates.
toCrdString() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement
Get a string representation of the instance in the CRD format.
toCrdString() - Method in class org.orekit.files.ilrs.CRD.Calibration
Get a string representation of the instance in the CRD format.
toCrdString() - Method in class org.orekit.files.ilrs.CRD.CalibrationDetail
Get a string representation of the instance in the CRD format.
toCrdString() - Method in class org.orekit.files.ilrs.CRD.FrRangeMeasurement
Get a string representation of the instance in the CRD format.
toCrdString() - Method in class org.orekit.files.ilrs.CRD.MeteorologicalMeasurement
Get a string representation of the instance in the CRD format.
toCrdString() - Method in class org.orekit.files.ilrs.CRD.NptRangeMeasurement
Get a string representation of the instance in the CRD format.
toCrdString() - Method in class org.orekit.files.ilrs.CRD.RangeMeasurement
Get a string representation of the instance in the CRD format.
toCrdString() - Method in class org.orekit.files.ilrs.CRD.RangeSupplement
Get a string representation of the instance in the CRD format.
toCrdString() - Method in class org.orekit.files.ilrs.CRD.SessionStatistics
Get a string representation of the instance in the CRD format.
toCrdString() - Method in class org.orekit.files.ilrs.CRDConfiguration.BaseConfiguration
Get a string representation of the instance in the CRD format.
toCrdString() - Method in class org.orekit.files.ilrs.CRDConfiguration.CalibrationTargetConfiguration
Get a string representation of the instance in the CRD format.
toCrdString() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Get a string representation of the instance in the CRD format.
toCrdString() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
Get a string representation of the instance in the CRD format.
toCrdString() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
Get a string representation of the instance in the CRD format.
toCrdString() - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration
Get a string representation of the instance in the CRD format.
toCrdString() - Method in class org.orekit.files.ilrs.CRDConfiguration.SystemConfiguration
Get a string representation of the instance in the CRD format.
toCrdString() - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration
Get a string representation of the instance in the CRD format.
toCrdString() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
Get a string representation of the instance in the CRD format.
TOD - org.orekit.files.ccsds.definitions.CelestialBodyFrame
True of Date.
TOD_CONVENTIONS_1996_ACCURATE_EOP - org.orekit.frames.Predefined
TOD, IERS 1996 conventions, with accurate EOP interpolation.
TOD_CONVENTIONS_1996_SIMPLE_EOP - org.orekit.frames.Predefined
TOD, IERS 1996 conventions, with simple EOP interpolation.
TOD_CONVENTIONS_2003_ACCURATE_EOP - org.orekit.frames.Predefined
TOD, IERS 2003 conventions, with accurate EOP interpolation.
TOD_CONVENTIONS_2003_SIMPLE_EOP - org.orekit.frames.Predefined
TOD, IERS 2003 conventions, with simple EOP interpolation.
TOD_CONVENTIONS_2010_ACCURATE_EOP - org.orekit.frames.Predefined
TOD, IERS 2010 conventions, with accurate EOP interpolation.
TOD_CONVENTIONS_2010_SIMPLE_EOP - org.orekit.frames.Predefined
TOD, IERS 2010 conventions, with simple EOP interpolation.
TOD_WITHOUT_EOP_CORRECTIONS - org.orekit.frames.Predefined
TOD, IERS 1996 conventions without EOP corrections.
toDate(DateComponents) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Create a date from components.
toDate(DateComponents, TimeComponents) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Create a date from components.
toDate(TimeScale) - Method in class org.orekit.time.AbsoluteDate
Convert the instance to a Java Date.
toDate(TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate
Convert the instance to a Java Date.
toDerivativeStructurePV(int) - Method in class org.orekit.utils.FieldPVCoordinates
Transform the instance to a FieldPVCoordinates<FieldDerivativeStructure>.
toDerivativeStructurePV(int) - Method in class org.orekit.utils.PVCoordinates
Transform the instance to a FieldPVCoordinates<DerivativeStructure>.
toDerivativeStructureRotation(int) - Method in class org.orekit.utils.AngularCoordinates
Transform the instance to a FieldRotation<DerivativeStructure>.
toDerivativeStructureRotation(int) - Method in class org.orekit.utils.FieldAngularCoordinates
Transform the instance to a FieldRotation<FieldDerivativeStructure>.
toDerivativeStructureVector(int) - Method in class org.orekit.utils.FieldPVCoordinates
Transform the instance to a FieldVector3D<FieldDerivativeStructure>.
toDerivativeStructureVector(int) - Method in class org.orekit.utils.PVCoordinates
Transform the instance to a FieldVector3D<DerivativeStructure>.
toEncounter() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Get new encounter instance.
toEopEntry(IERSConventions.NutationCorrectionConverter, ITRFVersion, TimeScale) - Method in class org.orekit.files.sinex.SinexEopEntry
Converts to an EOPEntry.
toEquinox(AbsoluteDate, double, double) - Method in interface org.orekit.utils.IERSConventions.NutationCorrectionConverter
Convert nutation corrections.
toEventDetectionSettings() - Method in class org.orekit.propagation.events.FieldEventDetectionSettings
Create a non-Field equivalent object.
toFieldPVCoordinatesProvider(Field<T>) - Method in interface org.orekit.utils.ExtendedPositionProvider
Convert to a FieldPVCoordinatesProvider with a specific type.
toFUD2Field() - Method in class org.orekit.time.FieldAbsoluteDate
Creates Field date with offset as univariate derivative of second order, with a unit linear coefficient in time.
toGeodetic(S2Point) - Method in class org.orekit.models.earth.tessellation.EllipsoidTessellator
Convert a point on the unit 2-sphere to geodetic coordinates.
toGeodeticPoint() - Method in class org.orekit.bodies.FieldGeodeticPoint
Get non-Field equivalent.
toGradientModel(int, Map<String, Integer>, AbsoluteDate) - Method in class org.orekit.estimation.measurements.QuadraticClockModel
Convert to gradient model.
toInstant() - Method in class org.orekit.time.AbsoluteDate
Convert the instance to a Java Instant.
toInstant() - Method in class org.orekit.time.FieldAbsoluteDate
Convert the instance to a Java Instant.
toInstant(TimeScales) - Method in class org.orekit.time.AbsoluteDate
Convert the instance to a Java Instant.
toInstant(TimeScales) - Method in class org.orekit.time.FieldAbsoluteDate
Convert the instance to a Java Instant.
TokenType - Enum in org.orekit.files.ccsds.utils.lexical
Enumerate for tokens occurring during CCSDS file parsing.
tolerances(double, double, Orbit) - Static method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Estimate tolerance vectors for an AdaptativeStepsizeIntegrator.
tolerances(double, double, Orbit, OrbitType) - Static method in class org.orekit.propagation.numerical.NumericalPropagator
Estimate tolerance vectors for integrators when propagating in orbits.
tolerances(double, Orbit) - Static method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Estimate tolerance vectors for an AdaptativeStepsizeIntegrator.
tolerances(double, Orbit, OrbitType) - Static method in class org.orekit.propagation.numerical.NumericalPropagator
Estimate tolerance vectors for integrators when propagating in orbits.
tolerances(double, AbsolutePVCoordinates) - Static method in class org.orekit.propagation.numerical.NumericalPropagator
Estimate tolerance vectors for integrators when propagating in absolute position-velocity-acceleration.
tolerances(T, FieldOrbit<T>) - Static method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Estimate tolerance vectors for an AdaptativeStepsizeIntegrator.
tolerances(T, FieldOrbit<T>, OrbitType) - Static method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Estimate tolerance vectors for integrators.
tolerances(T, T, FieldOrbit<T>) - Static method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Estimate tolerance vectors for an AdaptativeStepsizeIntegrator.
tolerances(T, T, FieldOrbit<T>, OrbitType) - Static method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Estimate tolerance vectors for integrators when propagating in orbits.
toMap() - Method in class org.orekit.utils.DoubleArrayDictionary
Create a map from the instance.
toMap() - Method in class org.orekit.utils.FieldArrayDictionary
Create a map from the instance.
ton2a - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext
2 / (n² * a) .
ton2a - Variable in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext
2 / (n² * a) .
toNonRotating(AbsoluteDate, double, double) - Method in interface org.orekit.utils.IERSConventions.NutationCorrectionConverter
Convert nutation corrections.
TOO_LARGE_DATA_TYPE - org.orekit.errors.OrekitMessages
TOO_LARGE_DATA_TYPE.
TOO_LARGE_DEGREE_FOR_GRAVITY_FIELD - org.orekit.errors.OrekitMessages
TOO_LARGE_DEGREE_FOR_GRAVITY_FIELD.
TOO_LARGE_ECCENTRICITY_FOR_PROPAGATION_MODEL - org.orekit.errors.OrekitMessages
TOO_LARGE_ECCENTRICITY_FOR_PROPAGATION_MODEL.
TOO_LARGE_ORDER_FOR_GRAVITY_FIELD - org.orekit.errors.OrekitMessages
TOO_LARGE_ORDER_FOR_GRAVITY_FIELD.
TOO_LONG_TIME_GAP_BETWEEN_DATA_POINTS - org.orekit.errors.OrekitMessages
TOO_LONG_TIME_GAP_BETWEEN_DATA_POINTS.
TOO_SHORT_TRANSITION_TIME_FOR_ATTITUDES_SWITCH - org.orekit.errors.OrekitMessages
TOO_SHORT_TRANSITION_TIME_FOR_ATTITUDES_SWITCH.
TOO_SMALL_SCALE_FOR_PARAMETER - org.orekit.errors.OrekitMessages
TOO_SMALL_SCALE_FOR_PARAMETER.
toOrbit() - Method in class org.orekit.orbits.FieldCartesianOrbit
 
toOrbit() - Method in class org.orekit.orbits.FieldCircularOrbit
Transforms the FieldOrbit instance into an Orbit instance.
toOrbit() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Transforms the FieldOrbit instance into an Orbit instance.
toOrbit() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Transforms the FieldOrbit instance into an Orbit instance.
toOrbit() - Method in class org.orekit.orbits.FieldOrbit
Transforms the FieldOrbit instance into an Orbit instance.
toOrbitRelativeFrame() - Method in enum org.orekit.frames.LOFType
Convert current local orbital frame to CCSDS equivalent orbit relative frame when possible, null otherwise.
toOsculatingOrbit() - Method in interface org.orekit.propagation.conversion.averaging.AveragedOrbitalState
Convert instance to an osculating orbit.
toOsculatingOrbit() - Method in class org.orekit.propagation.conversion.averaging.BrouwerLyddaneOrbitalState
Convert instance to an osculating orbit.
toOsculatingOrbit() - Method in class org.orekit.propagation.conversion.averaging.DSST6X0OrbitalState
Convert instance to an osculating orbit.
toOsculatingOrbit() - Method in class org.orekit.propagation.conversion.averaging.EcksteinHechlerOrbitalState
Convert instance to an osculating orbit.
toOsculatingOrbit() - Method in class org.orekit.propagation.conversion.averaging.SGP4OrbitalState
Convert instance to an osculating orbit.
toPlane(FieldVector3D<T>) - Method in class org.orekit.bodies.FieldEllipse
Project a point to the ellipse plane.
toPlane(Vector3D) - Method in class org.orekit.bodies.Ellipse
Project a point to the ellipse plane.
TopocentricFrame - Class in org.orekit.frames
Topocentric frame.
TopocentricFrame(BodyShape, GeodeticPoint, String) - Constructor for class org.orekit.frames.TopocentricFrame
Simple constructor.
toPVCoordinates() - Method in class org.orekit.utils.FieldPVCoordinates
Convert to a constant position-velocity.
toRawElements(TimeStampedPVCoordinates, Frame, OneAxisEllipsoid, double) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitElementsType
Convert to raw elements array.
toRotation(RotationOrder, double[]) - Method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeElementsType
Convert to rotation.
TorqueFree - Class in org.orekit.attitudes
This class handles torque-free motion of a general (non-symmetrical) body.
TorqueFree(Attitude, Inertia) - Constructor for class org.orekit.attitudes.TorqueFree
Simple constructor.
toSI(double) - Method in enum org.orekit.data.PolynomialParser.Unit
Convert value from instance unit to corresponding SI unit.
toSI(double) - Method in class org.orekit.utils.units.Unit
Convert a value to SI units.
toSI(Double) - Method in class org.orekit.utils.units.Unit
Convert a value to SI units.
toSI(T) - Method in class org.orekit.utils.units.Unit
Convert a value to SI units.
toSpace(FieldVector2D<T>) - Method in class org.orekit.bodies.FieldEllipse
Create a point from its ellipse-relative coordinates.
toSpace(Vector2D) - Method in class org.orekit.bodies.Ellipse
Create a point from its ellipse-relative coordinates.
toSpacecraftState() - Method in class org.orekit.propagation.FieldSpacecraftState
To convert a FieldSpacecraftState instance into a SpacecraftState instance.
toStateCovariance() - Method in class org.orekit.propagation.FieldStateCovariance
Get new state covariance instance.
toStaticTransform() - Method in class org.orekit.frames.FieldTransform
Create a so-called static transform from the instance.
toStaticTransform() - Method in class org.orekit.frames.Transform
Create a so-called static transform from the instance.
toStaticTransform() - Method in class org.orekit.propagation.FieldSpacecraftState
Compute the static transform from state defining frame to spacecraft frame.
toStaticTransform() - Method in class org.orekit.propagation.SpacecraftState
Compute the static transform from state defining frame to spacecraft frame.
toString() - Method in class org.orekit.bodies.FieldGeodeticPoint
 
toString() - Method in class org.orekit.bodies.GeodeticPoint
 
toString() - Method in class org.orekit.files.ccsds.definitions.SpacecraftBodyFrame
toString() - Method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeElementsType
toString() - Method in enum org.orekit.files.ccsds.ndm.adm.acm.RateElementsType
toString() - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints
toString() - Method in enum org.orekit.files.ccsds.ndm.adm.AttitudeType
toString() - Method in enum org.orekit.files.ccsds.ndm.cdm.Maneuvrable
.
toString() - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.OpsStatus
toString() - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitCategory
toString() - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitElementsType
toString() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement
 
toString() - Method in class org.orekit.files.ilrs.CRD.Calibration
 
toString() - Method in class org.orekit.files.ilrs.CRD.FrRangeMeasurement
 
toString() - Method in class org.orekit.files.ilrs.CRD.MeteorologicalMeasurement
 
toString() - Method in class org.orekit.files.ilrs.CRD.NptRangeMeasurement
 
toString() - Method in class org.orekit.files.ilrs.CRD.RangeSupplement
 
toString() - Method in class org.orekit.files.ilrs.CRD.SessionStatistics
 
toString() - Method in class org.orekit.files.ilrs.CRDConfiguration.CalibrationTargetConfiguration
 
toString() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
 
toString() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
 
toString() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
 
toString() - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration
 
toString() - Method in class org.orekit.files.ilrs.CRDConfiguration.SystemConfiguration
 
toString() - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration
 
toString() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
 
toString() - Method in class org.orekit.frames.Frame
New definition of the java.util toString() method.
toString() - Method in class org.orekit.frames.OrphanFrame
toString() - Method in class org.orekit.gnss.metric.ntrip.GnssData
 
toString() - Method in enum org.orekit.gnss.metric.ntrip.NavigationSystem
toString() - Method in class org.orekit.models.earth.GeoMagneticElements
 
toString() - Method in class org.orekit.orbits.CartesianOrbit
Returns a string representation of this Orbit object.
toString() - Method in class org.orekit.orbits.CircularOrbit
Returns a string representation of this Orbit object.
toString() - Method in class org.orekit.orbits.EquinoctialOrbit
Returns a string representation of this equinoctial parameters object.
toString() - Method in class org.orekit.orbits.FieldCartesianOrbit
Returns a string representation of this Orbit object.
toString() - Method in class org.orekit.orbits.FieldCircularOrbit
Returns a string representation of this Orbit object.
toString() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Returns a string representation of this equinoctial parameters object.
toString() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Returns a string representation of this Keplerian parameters object.
toString() - Method in class org.orekit.orbits.KeplerianOrbit
Returns a string representation of this Keplerian parameters object.
toString() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get a string representation of this TLE set.
toString() - Method in class org.orekit.propagation.analytical.tle.TLE
Get a string representation of this TLE set.
toString() - Method in class org.orekit.propagation.events.handlers.FieldRecordAndContinue.Event
 
toString() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue.Event
 
toString() - Method in class org.orekit.propagation.FieldSpacecraftState
 
toString() - Method in class org.orekit.propagation.SpacecraftState
 
toString() - Method in class org.orekit.time.AbsoluteDate
Get a String representation of the instant location with up to 16 digits of precision for the seconds value.
toString() - Method in class org.orekit.time.ConstantOffsetTimeScale
toString() - Method in class org.orekit.time.DateComponents
Get a string representation (ISO-8601) of the date.
toString() - Method in class org.orekit.time.DateTimeComponents
Return a string representation of this pair.
toString() - Method in class org.orekit.time.FieldAbsoluteDate
Get a String representation of the instant location with up to 16 digits of precision for the seconds value.
toString() - Method in class org.orekit.time.GLONASSScale
toString() - Method in class org.orekit.time.GMSTScale
toString() - Method in class org.orekit.time.SatelliteClockScale
toString() - Method in class org.orekit.time.TCBScale
toString() - Method in class org.orekit.time.TCGScale
toString() - Method in class org.orekit.time.TDBScale
toString() - Method in class org.orekit.time.TimeComponents
Get a string representation of the time including the offset from UTC.
toString() - Method in class org.orekit.time.UT1Scale
toString() - Method in class org.orekit.time.UTCScale
toString() - Method in class org.orekit.utils.DoubleArrayDictionary
Get a string representation of the dictionary.
toString() - Method in class org.orekit.utils.FieldArrayDictionary
Get a string representation of the dictionary.
toString() - Method in class org.orekit.utils.FieldPVCoordinates
Return a string representation of this position/velocity pair.
toString() - Method in class org.orekit.utils.ImmutableFieldTimeStampedCache
toString() - Method in class org.orekit.utils.ImmutableTimeStampedCache
toString() - Method in class org.orekit.utils.ParameterDriver
Get a text representation of the parameter.
toString() - Method in class org.orekit.utils.PVCoordinates
Return a string representation of this position/velocity pair.
toString() - Method in class org.orekit.utils.TimeStampedFieldPVCoordinates
Return a string representation of this date, position, velocity, and acceleration.
toString() - Method in class org.orekit.utils.TimeStampedPVCoordinates
Return a string representation of this date, position, velocity, and acceleration.
toString() - Method in class org.orekit.utils.units.Unit
toString() - Method in class org.orekit.utils.units.UnitsConverter
toString(int) - Method in class org.orekit.time.AbsoluteDate
Get a String representation of the instant location for a local time.
toString(int) - Method in class org.orekit.time.DateTimeComponents
Return a string representation of this date-time, rounded to millisecond precision.
toString(int) - Method in class org.orekit.time.FieldAbsoluteDate
Get a String representation of the instant location for a local time.
toString(int, int) - Method in class org.orekit.time.DateTimeComponents
Return a string representation of this date-time, rounded to the given precision.
toString(int, TimeScale) - Method in class org.orekit.time.AbsoluteDate
Get a String representation of the instant location for a local time.
toString(int, TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate
Get a String representation of the instant location for a local time.
toString(TimeZone) - Method in class org.orekit.time.AbsoluteDate
Get a String representation of the instant location for a time zone.
toString(TimeZone) - Method in class org.orekit.time.FieldAbsoluteDate
Get a String representation of the instant location for a time zone.
toString(TimeZone, TimeScale) - Method in class org.orekit.time.AbsoluteDate
Get a String representation of the instant location for a time zone.
toString(TimeZone, TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate
Get a String representation of the instant location for a time zone.
toString(TimeScale) - Method in class org.orekit.time.AbsoluteDate
Get a String representation of the instant location in ISO-8601 format without the UTC offset and with up to 16 digits of precision for the seconds value.
toString(TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate
Get a String representation of the instant location in ISO-8601 format without the UTC offset and with up to 16 digits of precision for the seconds value.
toString(TimeScale) - Method in class org.orekit.utils.TimeStampedFieldPVCoordinates
Return a string representation of this date, position, velocity, and acceleration.
toString(TimeScale) - Method in class org.orekit.utils.TimeStampedPVCoordinates
Return a string representation of this date, position, velocity, and acceleration.
toStringRfc3339() - Method in class org.orekit.time.DateTimeComponents
Represent the given date and time as a string according to the format in RFC 3339.
toStringRfc3339(TimeScale) - Method in class org.orekit.time.AbsoluteDate
Represent the given date as a string according to the format in RFC 3339.
toStringWithoutUtcOffset() - Method in class org.orekit.time.DateTimeComponents
Get a string representation of the date-time without the offset from UTC.
toStringWithoutUtcOffset() - Method in class org.orekit.time.TimeComponents
Get a string representation of the time without the offset from UTC.
toStringWithoutUtcOffset(int, int) - Method in class org.orekit.time.DateTimeComponents
Return a string representation of this date-time, rounded to the given precision.
toStringWithoutUtcOffset(TimeScale, int) - Method in class org.orekit.time.AbsoluteDate
Return a string representation of this date-time, rounded to the given precision.
toStringWithoutUtcOffset(TimeScale, int) - Method in class org.orekit.time.FieldAbsoluteDate
Return a string representation of this date-time, rounded to the given precision.
TOTAL_ELECTRON_CONTENT_UNIT - Static variable in class org.orekit.utils.units.Unit
Total Electron Content Unit.
TOTAL_ZENITH_DELAY - Static variable in class org.orekit.models.earth.troposphere.EstimatedModel
Name of the parameter of this model: the total zenith delay.
TOTAL_ZENITH_DELAY - Static variable in class org.orekit.models.earth.troposphere.EstimatedTroposphericModel
Deprecated.
Name of the parameter of this model: the total zenith delay.
toTaylorProvider() - Method in class org.orekit.utils.AbsolutePVCoordinates
Create a local provider using simply Taylor expansion through AbsolutePVCoordinates.shiftedBy(double).
toTaylorProvider() - Method in class org.orekit.utils.FieldAbsolutePVCoordinates
Create a local provider using simply Taylor expansion through FieldAbsolutePVCoordinates.shiftedBy(double).
toTaylorProvider(Frame) - Method in class org.orekit.utils.TimeStampedPVCoordinates
Create a local provider using simply Taylor expansion through TimeStampedPVCoordinates.shiftedBy(double).
toTimeStampedPVCoordinates() - Method in class org.orekit.files.ccsds.ndm.odm.StateVector
toTimeStampedPVCoordinates() - Method in class org.orekit.utils.TimeStampedFieldPVCoordinates
Convert to a constant position-velocity.
toTLE() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Convert FieldTLE into TLE.
toTransform() - Method in class org.orekit.propagation.FieldSpacecraftState
Compute the transform from state defining frame to spacecraft frame.
toTransform() - Method in class org.orekit.propagation.SpacecraftState
Compute the transform from state defining frame to spacecraft frame.
toUnivariateDerivative1PV() - Method in class org.orekit.utils.FieldPVCoordinates
Transform the instance to a FieldPVCoordinates<FieldUnivariateDerivative1>.
toUnivariateDerivative1PV() - Method in class org.orekit.utils.PVCoordinates
Transform the instance to a FieldPVCoordinates<UnivariateDerivative1>.
toUnivariateDerivative1Rotation() - Method in class org.orekit.utils.AngularCoordinates
Transform the instance to a FieldRotation<UnivariateDerivative1>.
toUnivariateDerivative1Rotation() - Method in class org.orekit.utils.FieldAngularCoordinates
Transform the instance to a FieldRotation<UnivariateDerivative1>.
toUnivariateDerivative1Vector() - Method in class org.orekit.utils.FieldPVCoordinates
Transform the instance to a FieldVector3D<FieldUnivariateDerivative1>.
toUnivariateDerivative1Vector() - Method in class org.orekit.utils.PVCoordinates
Transform the instance to a FieldVector3D<UnivariateDerivative1>.
toUnivariateDerivative2PV() - Method in class org.orekit.utils.FieldPVCoordinates
Transform the instance to a FieldPVCoordinates<FieldUnivariateDerivative2>.
toUnivariateDerivative2PV() - Method in class org.orekit.utils.PVCoordinates
Transform the instance to a FieldPVCoordinates<UnivariateDerivative2>.
toUnivariateDerivative2Rotation() - Method in class org.orekit.utils.AngularCoordinates
Transform the instance to a FieldRotation<UnivariateDerivative2>.
toUnivariateDerivative2Rotation() - Method in class org.orekit.utils.FieldAngularCoordinates
Transform the instance to a FieldRotation<UnivariateDerivative2>.
toUnivariateDerivative2Vector() - Method in class org.orekit.utils.FieldPVCoordinates
Transform the instance to a FieldVector3D<FieldUnivariateDerivative2>.
toUnivariateDerivative2Vector() - Method in class org.orekit.utils.PVCoordinates
Transform the instance to a FieldVector3D<UnivariateDerivative2>.
TRACK_ID - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Identifier for the tracking data.
TrackingCoordinates - Class in org.orekit.utils
Container for azimut/elevation/range coordinates as seen from a ground point.
TrackingCoordinates(double, double, double) - Constructor for class org.orekit.utils.TrackingCoordinates
Simple constructor.
TrackingMode - Enum in org.orekit.files.ccsds.ndm.tdm
Tracking mode.
TRACKS_AVAILABLE - org.orekit.files.ccsds.ndm.cdm.ODParametersKey
The number of sensor tracks available for the OD of the object.
TRACKS_AVAILABLE - org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey
Number of sensors tracks available for the OD within the actual OD span.
TRACKS_USED - org.orekit.files.ccsds.ndm.cdm.ODParametersKey
The number of sensor tracks accepted for the OD of the object.
TRACKS_USED - org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey
Number of sensors tracks accepted for the OD within the actual OD span.
traj - org.orekit.files.ccsds.ndm.odm.ocm.OcmDataSubStructureKey
Trajectory state time history section.
TRAJ - org.orekit.files.ccsds.ndm.odm.ocm.OcmDataSubStructureKey
Trajectory state time history section.
TRAJ_BASIS - org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadataKey
Basis of this trajectory state time history data.
TRAJ_BASIS_ID - org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadataKey
Identification number of the orbit determination or simulation upon which this trajectory is based.
TRAJ_FRAME_EPOCH - org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadataKey
TRAJ_ID - org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadataKey
Trajectory identification number.
TRAJ_LINE - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.Ocm
Trajectory line element for XML messages.
TRAJ_NEXT_ID - org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadataKey
Identification number of next trajectory.
TRAJ_PREV_ID - org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadataKey
Identification number of previous trajectory.
TRAJ_REF_FRAME - org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadataKey
Reference frame of the trajectory.
TRAJ_TYPE - org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadataKey
Trajectory element set type.
TRAJ_UNITS - org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadataKey
SI units for each elements of the trajectory state.
TRAJECTORY_INSIDE_BRILLOUIN_SPHERE - org.orekit.errors.OrekitMessages
TRAJECTORY_INSIDE_BRILLOUIN_SPHERE.
TRAJECTORY_NOT_CROSSING_XZPLANE - org.orekit.errors.OrekitMessages
TRAJECTORY_NOT_CROSSING_XZPLANE.
TrajectoryState - Class in org.orekit.files.ccsds.ndm.odm.ocm
Trajectory state entry.
TrajectoryState(OrbitElementsType, AbsoluteDate, double[]) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryState
Simple constructor.
TrajectoryState(OrbitElementsType, AbsoluteDate, String[], int, List<Unit>) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryState
Simple constructor.
TrajectoryStateHistory - Class in org.orekit.files.ccsds.ndm.odm.ocm
Trajectory state history.
TrajectoryStateHistory(TrajectoryStateHistoryMetadata, List<TrajectoryState>, OneAxisEllipsoid, double) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory
Simple constructor.
TrajectoryStateHistoryMetadata - Class in org.orekit.files.ccsds.ndm.odm.ocm
Metadata for trajectory state history.
TrajectoryStateHistoryMetadata(AbsoluteDate, DataContext) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Simple constructor.
TrajectoryStateHistoryMetadataKey - Enum in org.orekit.files.ccsds.ndm.odm.ocm
transform(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.BodyShape
Transform a Cartesian point to a surface-relative point.
transform(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.bodies.OneAxisEllipsoid
Transform a Cartesian point to a surface-relative point.
transform(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.Geoid
Transform a Cartesian point to a surface-relative point.
transform(Vector3D, Frame, AbsoluteDate) - Method in interface org.orekit.bodies.BodyShape
Transform a Cartesian point to a surface-relative point.
transform(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.bodies.OneAxisEllipsoid
Transform a Cartesian point to a surface-relative point.
transform(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.models.earth.Geoid
Transform a Cartesian point to a surface-relative point.
transform(FieldGeodeticPoint<T>) - Method in interface org.orekit.bodies.BodyShape
Transform a surface-relative point to a Cartesian point.
transform(FieldGeodeticPoint<T>) - Method in class org.orekit.bodies.OneAxisEllipsoid
Transform a surface-relative point to a Cartesian point.
transform(FieldGeodeticPoint<T>) - Method in class org.orekit.models.earth.Geoid
Transform a surface-relative point to a Cartesian point.
transform(GeodeticPoint) - Method in interface org.orekit.bodies.BodyShape
Transform a surface-relative point to a Cartesian point.
transform(GeodeticPoint) - Method in class org.orekit.bodies.OneAxisEllipsoid
Transform a surface-relative point to a Cartesian point.
transform(GeodeticPoint) - Method in class org.orekit.models.earth.Geoid
Transform a surface-relative point to a Cartesian point.
transform(PVCoordinates, Frame, AbsoluteDate) - Method in class org.orekit.bodies.OneAxisEllipsoid
Transform a Cartesian point to a surface-relative point.
Transform - Class in org.orekit.frames
Transformation class in three dimensional space.
Transform(AbsoluteDate, Rotation) - Constructor for class org.orekit.frames.Transform
Build a rotation transform.
Transform(AbsoluteDate, Rotation, Vector3D) - Constructor for class org.orekit.frames.Transform
Build a rotation transform.
Transform(AbsoluteDate, Rotation, Vector3D, Vector3D) - Constructor for class org.orekit.frames.Transform
Build a rotation transform.
Transform(AbsoluteDate, Vector3D) - Constructor for class org.orekit.frames.Transform
Build a translation transform.
Transform(AbsoluteDate, Vector3D, Rotation) - Constructor for class org.orekit.frames.Transform
Build a combined translation and rotation transform.
Transform(AbsoluteDate, Vector3D, Vector3D) - Constructor for class org.orekit.frames.Transform
Build a translation transform, with its first time derivative.
Transform(AbsoluteDate, Vector3D, Vector3D, Vector3D) - Constructor for class org.orekit.frames.Transform
Build a translation transform, with its first and second time derivatives.
Transform(AbsoluteDate, Transform, Transform) - Constructor for class org.orekit.frames.Transform
Build a transform by combining two existing ones.
Transform(AbsoluteDate, AngularCoordinates) - Constructor for class org.orekit.frames.Transform
Build a rotation transform.
Transform(AbsoluteDate, PVCoordinates) - Constructor for class org.orekit.frames.Transform
Build a translation transform, with its first time derivative.
Transform(AbsoluteDate, PVCoordinates, AngularCoordinates) - Constructor for class org.orekit.frames.Transform
Build a transform from its primitive operations.
transformFromInertial(AbsoluteDate, PVCoordinates) - Method in interface org.orekit.frames.LOF
Get the transform from an inertial frame defining position-velocity and the local orbital frame.
transformFromInertial(FieldAbsoluteDate<T>, FieldPVCoordinates<T>) - Method in interface org.orekit.frames.LOF
Get the transform from an inertial frame defining position-velocity and the local orbital frame.
transformFromLOF(LOF, AbsoluteDate, PVCoordinates) - Method in interface org.orekit.frames.LOF
Get the rotation from input local orbital frame to the instance.
transformFromLOF(LOF, FieldAbsoluteDate<T>, FieldPVCoordinates<T>) - Method in interface org.orekit.frames.LOF
Get the rotation from input commonly used local orbital frame to the instance.
transformFromLOFInToLOFOut(LOF, LOF, AbsoluteDate, PVCoordinates) - Static method in interface org.orekit.frames.LOF
Get the transform from input to output local orbital frame.
transformFromLOFInToLOFOut(LOF, LOF, FieldAbsoluteDate<T>, FieldPVCoordinates<T>) - Static method in interface org.orekit.frames.LOF
Get the transform from input to output local orbital frame.
TransformGenerator - Class in org.orekit.frames
Generator to use transforms in GenericTimeStampedCache.
TransformGenerator(int, TransformProvider, double) - Constructor for class org.orekit.frames.TransformGenerator
simple constructor.
transformLine(FieldLine<T>) - Method in interface org.orekit.frames.FieldStaticTransform
Transform a line.
transformLine(Line) - Method in interface org.orekit.frames.FieldStaticTransform
Transform a line.
transformLine(Line) - Method in interface org.orekit.frames.StaticTransform
Transform a line.
transformModel(double) - Method in class org.orekit.models.earth.GeoMagneticField
Time transform the model coefficients from the base year of the model using secular variation coefficients.
transformModel(GeoMagneticField, double) - Method in class org.orekit.models.earth.GeoMagneticField
Time transform the model coefficients from the base year of the model using a linear interpolation with a second model.
transformOnlyPV(FieldPVCoordinates<T>) - Method in interface org.orekit.frames.FieldKinematicTransform
Transform PVCoordinates, without the acceleration vector.
transformOnlyPV(PVCoordinates) - Method in interface org.orekit.frames.KinematicTransform
Transform PVCoordinates, without the acceleration vector.
transformOnlyPV(TimeStampedFieldPVCoordinates<T>) - Method in interface org.orekit.frames.FieldKinematicTransform
Transform TimeStampedPVCoordinates, without the acceleration vector.
transformOnlyPV(TimeStampedPVCoordinates) - Method in interface org.orekit.frames.KinematicTransform
Transform TimeStampedPVCoordinates, without the acceleration vector.
transformPosition(FieldVector3D<T>) - Method in interface org.orekit.frames.FieldStaticTransform
Transform a position vector (including translation effects).
transformPosition(FieldVector3D<T>) - Method in interface org.orekit.frames.StaticTransform
Transform a position vector (including translation effects).
transformPosition(Vector3D) - Method in interface org.orekit.frames.FieldStaticTransform
Transform a position vector (including translation effects).
transformPosition(Vector3D) - Method in interface org.orekit.frames.StaticTransform
Transform a position vector (including translation effects).
TransformProvider - Interface in org.orekit.frames
Interface for Transform providers.
TransformProviderUtils - Class in org.orekit.frames
Utility for Transform providers.
transformPVCoordinates(FieldPVCoordinates<T>) - Method in class org.orekit.frames.FieldTransform
Transform TimeStampedFieldPVCoordinates including kinematic effects.
transformPVCoordinates(FieldPVCoordinates<T>) - Method in class org.orekit.frames.Transform
Transform FieldPVCoordinates including kinematic effects.
transformPVCoordinates(PVCoordinates) - Method in class org.orekit.frames.FieldTransform
Transform TimeStampedPVCoordinates including kinematic effects.
transformPVCoordinates(PVCoordinates) - Method in class org.orekit.frames.Transform
Transform PVCoordinates including kinematic effects.
transformPVCoordinates(TimeStampedFieldPVCoordinates<T>) - Method in class org.orekit.frames.FieldTransform
Transform TimeStampedFieldPVCoordinates including kinematic effects.
transformPVCoordinates(TimeStampedFieldPVCoordinates<T>) - Method in class org.orekit.frames.Transform
Transform TimeStampedFieldPVCoordinates including kinematic effects.
transformPVCoordinates(TimeStampedPVCoordinates) - Method in class org.orekit.frames.FieldTransform
Transform TimeStampedPVCoordinates including kinematic effects.
transformPVCoordinates(TimeStampedPVCoordinates) - Method in class org.orekit.frames.Transform
Transform TimeStampedPVCoordinates including kinematic effects.
transformVector(FieldVector3D<T>) - Method in interface org.orekit.frames.FieldStaticTransform
Transform a vector (ignoring translation effects).
transformVector(FieldVector3D<T>) - Method in interface org.orekit.frames.StaticTransform
Transform a vector (ignoring translation effects).
transformVector(Vector3D) - Method in interface org.orekit.frames.FieldStaticTransform
Transform a vector (ignoring translation effects).
transformVector(Vector3D) - Method in interface org.orekit.frames.StaticTransform
Transform a vector (ignoring translation effects).
TRANSMIT - org.orekit.files.ccsds.ndm.tdm.TimetagReference
Reference at transmit time.
TRANSMIT_BAND - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Transmit band entry.
TRANSMIT_DELAY_1 - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
First transmit delay entry.
TRANSMIT_DELAY_2 - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Second transmit delay entry.
TRANSMIT_DELAY_3 - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Third transmit delay entry.
TRANSMIT_DELAY_4 - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Fourth transmit delay entry.
TRANSMIT_DELAY_5 - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Fifth transmit delay entry.
TRANSMIT_FREQ_1 - org.orekit.files.ccsds.ndm.tdm.ObservationType
Data: Transmitted frequencies [Hz].
TRANSMIT_FREQ_2 - org.orekit.files.ccsds.ndm.tdm.ObservationType
Transmitted frequency 2.
TRANSMIT_FREQ_3 - org.orekit.files.ccsds.ndm.tdm.ObservationType
Transmitted frequency 3.
TRANSMIT_FREQ_4 - org.orekit.files.ccsds.ndm.tdm.ObservationType
Transmitted frequency 4.
TRANSMIT_FREQ_5 - org.orekit.files.ccsds.ndm.tdm.ObservationType
Transmitted frequency 5.
TRANSMIT_FREQ_RATE_1 - org.orekit.files.ccsds.ndm.tdm.ObservationType
Data: Transmitted frequencies rates [Hz/s].
TRANSMIT_FREQ_RATE_2 - org.orekit.files.ccsds.ndm.tdm.ObservationType
Transmitted frequency rate 2.
TRANSMIT_FREQ_RATE_3 - org.orekit.files.ccsds.ndm.tdm.ObservationType
Transmitted frequency rate 3.
TRANSMIT_FREQ_RATE_4 - org.orekit.files.ccsds.ndm.tdm.ObservationType
Transmitted frequency rate 4.
TRANSMIT_FREQ_RATE_5 - org.orekit.files.ccsds.ndm.tdm.ObservationType
Transmitted frequency rate 5.
TRANSMIT_PHASE_CT_1 - org.orekit.files.ccsds.ndm.tdm.ObservationType
Data: phase cycle count at transmitter.
TRANSMIT_PHASE_CT_2 - org.orekit.files.ccsds.ndm.tdm.ObservationType
Data: phase cycle count at transmitter.
TRANSMIT_PHASE_CT_3 - org.orekit.files.ccsds.ndm.tdm.ObservationType
Data: phase cycle count at transmitter.
TRANSMIT_PHASE_CT_4 - org.orekit.files.ccsds.ndm.tdm.ObservationType
Data: phase cycle count at transmitter.
TRANSMIT_PHASE_CT_5 - org.orekit.files.ccsds.ndm.tdm.ObservationType
Data: phase cycle count at transmitter.
TransponderConfiguration() - Constructor for class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
Empty constructor.
TRIAD - org.orekit.files.ccsds.definitions.AdMethodType
TRIaxial Attitude Determination.
TRIGGER_ONLY_DECREASING_EVENTS - org.orekit.propagation.events.FilterType
Constant for triggering only decreasing events.
TRIGGER_ONLY_INCREASING_EVENTS - org.orekit.propagation.events.FilterType
Constant for triggering only increasing events.
TriggerDate - Class in org.orekit.forces.maneuvers.jacobians
Generator for one column of a Jacobian matrix for special case of trigger dates.
TriggerDate(String, String, boolean, Maneuver, double) - Constructor for class org.orekit.forces.maneuvers.jacobians.TriggerDate
Simple constructor.
TROPO_DRY - org.orekit.files.ccsds.ndm.tdm.ObservationType
Data: TROPO DRY [m].
TROPO_WET - org.orekit.files.ccsds.ndm.tdm.ObservationType
Data: TROPO WET [m].
TroposphereMappingFunction - Interface in org.orekit.models.earth.troposphere
Interface for mapping functions used in the tropospheric delay computation.
TroposphereMappingFunctionAdapter - Class in org.orekit.models.earth.troposphere
Deprecated.
temporary adapter to be removed when MappingFunction is removed
TroposphereMappingFunctionAdapter(MappingFunction) - Constructor for class org.orekit.models.earth.troposphere.TroposphereMappingFunctionAdapter
Deprecated.
Simple constructor.
TroposphericDelay - Class in org.orekit.models.earth.troposphere
Container for tropospheric delay.
TroposphericDelay(double, double, double, double) - Constructor for class org.orekit.models.earth.troposphere.TroposphericDelay
Simple constructor.
TroposphericModel - Interface in org.orekit.models.earth.troposphere
Defines a tropospheric model, used to calculate the path delay imposed to electro-magnetic signals between an orbital satellite and a ground station.
TroposphericModelAdapter - Class in org.orekit.models.earth.troposphere
Deprecated.
temporary adapter to be removed when DiscreteTroposphericModel is removed
TroposphericModelAdapter(DiscreteTroposphericModel) - Constructor for class org.orekit.models.earth.troposphere.TroposphericModelAdapter
Deprecated.
Simple constructor.
TroposphericModelUtils - Class in org.orekit.models.earth.troposphere
Utility class for tropospheric models.
TRUE - org.orekit.orbits.PositionAngleType
True angle.
TRUE_ANOM - Static variable in enum org.orekit.orbits.OrbitType
Name for mean anomaly.
TRUE_ANOMALY - org.orekit.files.ccsds.ndm.odm.KeplerianElementsKey
Orbit true anomaly.
TRUE_LAT_ARG - Static variable in enum org.orekit.orbits.OrbitType
Name for mean argument of latitude.
TRUE_LON_ARG - Static variable in enum org.orekit.orbits.OrbitType
Name for mean argument of longitude.
TRUE_OF_DATE - org.orekit.files.stk.STKEphemerisFile.STKCoordinateSystem
True equator and true equinox of date.
trueToEccentric(double, double, double) - Static method in class org.orekit.orbits.CircularLatitudeArgumentUtility
Computes the eccentric latitude argument from the true latitude argument.
trueToEccentric(double, double, double) - Static method in class org.orekit.orbits.CircularOrbit
Deprecated.
trueToEccentric(double, double, double) - Static method in class org.orekit.orbits.EquinoctialLongitudeArgumentUtility
Computes the eccentric longitude argument from the true longitude argument.
trueToEccentric(double, double, double) - Static method in class org.orekit.orbits.EquinoctialOrbit
Deprecated.
trueToEccentric(T, T, T) - Static method in class org.orekit.orbits.FieldCircularLatitudeArgumentUtility
Computes the eccentric latitude argument from the true latitude argument.
trueToEccentric(T, T, T) - Static method in class org.orekit.orbits.FieldCircularOrbit
Deprecated.
trueToEccentric(T, T, T) - Static method in class org.orekit.orbits.FieldEquinoctialLongitudeArgumentUtility
Computes the eccentric longitude argument from the true longitude argument.
trueToEccentric(T, T, T) - Static method in class org.orekit.orbits.FieldEquinoctialOrbit
Deprecated.
trueToMean(double, double, double) - Static method in class org.orekit.orbits.CircularLatitudeArgumentUtility
Computes the mean latitude argument from the eccentric latitude argument.
trueToMean(double, double, double) - Static method in class org.orekit.orbits.EquinoctialLongitudeArgumentUtility
Computes the mean longitude argument from the eccentric longitude argument.
trueToMean(T, T, T) - Static method in class org.orekit.orbits.FieldCircularLatitudeArgumentUtility
Computes the mean latitude argument from the eccentric latitude argument.
trueToMean(T, T, T) - Static method in class org.orekit.orbits.FieldEquinoctialLongitudeArgumentUtility
Computes the mean longitude argument from the eccentric longitude argument.
TruncatingFilter - Class in org.orekit.data
Filter for truncating line-oriented files.
TruncatingFilter(int) - Constructor for class org.orekit.data.TruncatingFilter
Simple constructor.
tryAdvance(FieldSpacecraftState<T>, FieldOrekitStepInterpolator<T>) - Method in class org.orekit.propagation.events.FieldEventState
Try to accept the current history up to the given time.
tryAdvance(SpacecraftState, OrekitStepInterpolator) - Method in class org.orekit.propagation.events.EventState
Try to accept the current history up to the given time.
tsi - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
tsi from SPTRCK #3.
tsi - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
tsi from SPTRCK #3.
TT - org.orekit.files.ccsds.definitions.TimeSystem
Terrestrial Time.
TTScale - Class in org.orekit.time
Terrestrial Time as defined by IAU(1991) recommendation IV.
TURNAROUND_DENOMINATOR - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
turnaround denominator entry.
TURNAROUND_NUMERATOR - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Turnaround numerator entry.
TurnAroundRange - Class in org.orekit.estimation.measurements
Class modeling a turn-around range measurement using a primary ground station and a secondary ground station.
TurnAroundRange(GroundStation, GroundStation, AbsoluteDate, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.TurnAroundRange
Simple constructor.
TurnAroundRangeBuilder - Class in org.orekit.estimation.measurements.generation
Builder for TurnAroundRange measurements.
TurnAroundRangeBuilder(CorrelatedRandomVectorGenerator, GroundStation, GroundStation, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.TurnAroundRangeBuilder
Simple constructor.
TurnAroundRangeIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical TurnAroundRange measurement with ionospheric delay.
TurnAroundRangeIonosphericDelayModifier(IonosphericModel, double) - Constructor for class org.orekit.estimation.measurements.modifiers.TurnAroundRangeIonosphericDelayModifier
Constructor.
TurnAroundRangeTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical turn-around TurnAroundRange measurement with tropospheric delay.
TurnAroundRangeTroposphericDelayModifier(DiscreteTroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.TurnAroundRangeTroposphericDelayModifier
TurnAroundRangeTroposphericDelayModifier(TroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.TurnAroundRangeTroposphericDelayModifier
Constructor.
TVN - org.orekit.files.ccsds.ndm.cdm.ScreenVolumeFrame
Transverse Velocity Normal frame.
TWO_NORM - org.orekit.forces.maneuvers.Control3DVectorCostType
2-norm also known as Euclidean.
TWO_RECEIVER_ONE_SATELLITE_CARRIER_PHASE - org.orekit.files.sp3.DataUsed
2-receiver/1-satellite carrier phase.
TWO_RECEIVER_ONE_SATELLITE_CODE_PHASE - org.orekit.files.sp3.DataUsed
2-receiver/1-satellite code phase.
TWO_RECEIVER_TWO_SATELLITE_CARRIER_PHASE - org.orekit.files.sp3.DataUsed
2-receiver/2-satellite carrier phase.
TWO_RECEIVER_TWO_SATELLITE_CODE_PHASE - org.orekit.files.sp3.DataUsed
2-receiver/2-satellite code phase.
TWO_THIRD - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
Constant 2.0 / 3.0.
TWO_WAY - org.orekit.files.ilrs.CRDHeader.RangeType
Two-way ranging.
TwoBodiesBaryFrame - Class in org.orekit.frames
Class creating the inertial barycenter frame from two bodies.
TwoBodiesBaryFrame(CelestialBody, CelestialBody) - Constructor for class org.orekit.frames.TwoBodiesBaryFrame
Simple constructor.
TwoDVariation - Class in org.orekit.gnss.antenna
Interpolator for 2D phase center variation data.
TwoDVariation(double, double, double, double[][]) - Constructor for class org.orekit.gnss.antenna.TwoDVariation
Simple constructor.
twoWayDistanceModification(EstimatedMeasurementBase<InterSatellitesRange>) - Method in class org.orekit.estimation.measurements.modifiers.PhaseCentersInterSatellitesBaseModifier
Compute distance modification for two way measurement.
twoWayDistanceModification(EstimatedMeasurementBase<T>) - Method in class org.orekit.estimation.measurements.modifiers.PhaseCentersGroundReceiverBaseModifier
Apply a modifier to a two-way range measurement.
Type - Enum in org.orekit.gnss.metric.ntrip
Enumerate for messages type.
TypeSvMessage - Class in org.orekit.files.rinex.navigation
Container for data shared by several navigation messages.
TypeSvMessage(SatelliteSystem, int, String) - Constructor for class org.orekit.files.rinex.navigation.TypeSvMessage
Simple constructor.

U

U_INT_10 - org.orekit.gnss.metric.parser.DataType
10 bits unsigned integer.
U_INT_11 - org.orekit.gnss.metric.parser.DataType
11 bits unsigned integer.
U_INT_12 - org.orekit.gnss.metric.parser.DataType
12 bits unsigned integer.
U_INT_13 - org.orekit.gnss.metric.parser.DataType
13 bits unsigned integer.
U_INT_14 - org.orekit.gnss.metric.parser.DataType
14 bits unsigned integer.
U_INT_16 - org.orekit.gnss.metric.parser.DataType
16 bits unsigned integer.
U_INT_17 - org.orekit.gnss.metric.parser.DataType
17 bits unsigned integer.
U_INT_18 - org.orekit.gnss.metric.parser.DataType
18 bits unsigned integer.
U_INT_2 - org.orekit.gnss.metric.parser.DataType
2 bits unsigned integer.
U_INT_20 - org.orekit.gnss.metric.parser.DataType
20 bits unsigned integer.
U_INT_23 - org.orekit.gnss.metric.parser.DataType
23 bits unsigned integer.
U_INT_24 - org.orekit.gnss.metric.parser.DataType
24 bits unsigned integer.
U_INT_25 - org.orekit.gnss.metric.parser.DataType
25 bits unsigned integer.
U_INT_26 - org.orekit.gnss.metric.parser.DataType
26 bits unsigned integer.
U_INT_27 - org.orekit.gnss.metric.parser.DataType
27 bits unsigned integer.
U_INT_3 - org.orekit.gnss.metric.parser.DataType
3 bits unsigned integer.
U_INT_30 - org.orekit.gnss.metric.parser.DataType
30 bits unsigned integer.
U_INT_32 - org.orekit.gnss.metric.parser.DataType
32 bits unsigned integer.
U_INT_35 - org.orekit.gnss.metric.parser.DataType
35 bits unsigned integer.
U_INT_36 - org.orekit.gnss.metric.parser.DataType
36 bits unsigned integer.
U_INT_4 - org.orekit.gnss.metric.parser.DataType
4 bits unsigned integer.
U_INT_5 - org.orekit.gnss.metric.parser.DataType
5 bits unsigned integer.
U_INT_6 - org.orekit.gnss.metric.parser.DataType
6 bits unsigned integer.
U_INT_7 - org.orekit.gnss.metric.parser.DataType
7 bits unsigned integer.
U_INT_8 - org.orekit.gnss.metric.parser.DataType
8 bits unsigned integer.
U_INT_9 - org.orekit.gnss.metric.parser.DataType
9 bits unsigned integer.
UFO - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCategory
UFO: Undefined Orbit.
UNABLE_TO_COMPUTE_BROUWER_LYDDANE_MEAN_PARAMETERS - org.orekit.errors.OrekitMessages
UNABLE_TO_COMPUTE_BROUWER_LYDDANE_MEAN_PARAMETERS.
UNABLE_TO_COMPUTE_DSST_MEAN_PARAMETERS - org.orekit.errors.OrekitMessages
UNABLE_TO_COMPUTE_DSST_MEAN_PARAMETERS.
UNABLE_TO_COMPUTE_ECCENTRIC_LATITUDE_ARGUMENT - org.orekit.errors.OrekitMessages
UNABLE_TO_COMPUTE_ECCENTRIC_LATITUDE_ARGUMENT.
UNABLE_TO_COMPUTE_ECCENTRIC_LONGITUDE_ARGUMENT - org.orekit.errors.OrekitMessages
UNABLE_TO_COMPUTE_ECCENTRIC_LONGITUDE_ARGUMENT.
UNABLE_TO_COMPUTE_ECKSTEIN_HECHLER_MEAN_PARAMETERS - org.orekit.errors.OrekitMessages
UNABLE_TO_COMPUTE_ECKSTEIN_HECHLER_MEAN_PARAMETERS.
UNABLE_TO_COMPUTE_HYPERBOLIC_ECCENTRIC_ANOMALY - org.orekit.errors.OrekitMessages
UNABLE_TO_COMPUTE_HYPERBOLIC_ECCENTRIC_ANOMALY.
UNABLE_TO_COMPUTE_TLE - org.orekit.errors.OrekitMessages
UNABLE_TO_COMPUTE_TLE.
UNABLE_TO_FIND_FILE - org.orekit.errors.OrekitMessages
UNABLE_TO_FIND_FILE.
UNABLE_TO_FIND_RESOURCE - org.orekit.errors.OrekitMessages
UNABLE_TO_FIND_RESOURCE.
UNABLE_TO_GENERATE_NEW_DATA_AFTER - org.orekit.errors.OrekitMessages
UNABLE_TO_GENERATE_NEW_DATA_AFTER.
UNABLE_TO_GENERATE_NEW_DATA_BEFORE - org.orekit.errors.OrekitMessages
UNABLE_TO_GENERATE_NEW_DATA_BEFORE.
UNABLE_TO_PARSE_ELEMENT_IN_FILE - org.orekit.errors.OrekitMessages
UNABLE_TO_PARSE_ELEMENT_IN_FILE.
UNABLE_TO_PARSE_LINE_IN_FILE - org.orekit.errors.OrekitMessages
UNABLE_TO_PARSE_LINE_IN_FILE.
UNABLE_TO_READ_JPL_HEADER - org.orekit.errors.OrekitMessages
UNABLE_TO_READ_JPL_HEADER.
UnboundedCartesianEnergy - Class in org.orekit.control.indirect.adjoint.cost
Class for unbounded energy cost with Cartesian coordinates.
UnboundedCartesianEnergy(String, double) - Constructor for class org.orekit.control.indirect.adjoint.cost.UnboundedCartesianEnergy
Constructor.
UnboundedCartesianEnergy(String, double, EventDetectionSettings) - Constructor for class org.orekit.control.indirect.adjoint.cost.UnboundedCartesianEnergy
Constructor.
UnboundedCartesianEnergyNeglectingMass - Class in org.orekit.control.indirect.adjoint.cost
Class for unbounded energy cost with Cartesian coordinates neglecting the mass consumption.
UnboundedCartesianEnergyNeglectingMass(String) - Constructor for class org.orekit.control.indirect.adjoint.cost.UnboundedCartesianEnergyNeglectingMass
Constructor.
UNDEFINED - org.orekit.files.sp3.SP3FileType
undefined file format.
UNDEFINED_ABSOLUTE_PVCOORDINATES - org.orekit.errors.OrekitMessages
UNDEFINED_ABSOLUTE_PVCOORDINATES.
UNDEFINED_ORBIT - org.orekit.errors.OrekitMessages
UNDEFINED_ORBIT.
UNDIFFERENTIATED_CARRIER_PHASE - org.orekit.files.sp3.DataUsed
Undifferenciated carrier phase.
UNDIFFERENTIATED_CODE_PHASE - org.orekit.files.sp3.DataUsed
Undifferenciated code phase.
UNE - org.orekit.files.sinex.Station.ReferenceSystem
Local reference system Up, North, East.
UNEXPECTED_CONTENT_TYPE - org.orekit.errors.OrekitMessages
UNEXPECTED_CONTENT_TYPE.
UNEXPECTED_DATA_AFTER_LINE_IN_FILE - org.orekit.errors.OrekitMessages
UNEXPECTED_DATA_AFTER_LINE_IN_FILE.
UNEXPECTED_DATA_AT_LINE_IN_FILE - org.orekit.errors.OrekitMessages
UNEXPECTED_DATA_AT_LINE_IN_FILE.
UNEXPECTED_END_OF_FILE - org.orekit.errors.OrekitMessages
UNEXPECTED_END_OF_FILE.
UNEXPECTED_END_OF_FILE_AFTER_LINE - org.orekit.errors.OrekitMessages
UNEXPECTED_END_OF_FILE_AFTER_LINE.
UNEXPECTED_FILE_FORMAT_ERROR_FOR_LOADER - org.orekit.errors.OrekitMessages
UNEXPECTED_FILE_FORMAT_ERROR_FOR_LOADER.
UNEXPECTED_FORMAT_FOR_ILRS_FILE - org.orekit.errors.OrekitMessages
UNEXPECTED_FORMAT_FOR_ILRS_FILE.
UNEXPECTED_TWO_ELEVATION_VALUES_FOR_ONE_AZIMUTH - org.orekit.errors.OrekitMessages
UNEXPECTED_TWO_ELEVATION_VALUES_FOR_ONE_AZIMUTH.
unFixAmbiguity(ParameterDriver) - Method in class org.orekit.estimation.measurements.gnss.AmbiguitySolver
Un-fix an integer ambiguity (typically after a phase cycle slip).
UNINITIALIZED_VALUE_FOR_KEY - org.orekit.errors.OrekitMessages
UNINITIALIZED_VALUE_FOR_KEY.
Unit - Class in org.orekit.utils.units
Basic handling of multiplicative units.
Unit(String, double, Fraction, Fraction, Fraction, Fraction, Fraction) - Constructor for class org.orekit.utils.units.Unit
Simple constructor.
Units - Class in org.orekit.files.ccsds.definitions
Units used in CCSDS messages.
Units - Class in org.orekit.gnss.metric.parser
Units used in RTCM and IGS SSR messages.
UNITS - Static variable in class org.orekit.files.ccsds.utils.generation.XmlGenerator
Name of the units attribute.
UnitsCache - Class in org.orekit.utils.units
Cache for parsed units.
UnitsCache() - Constructor for class org.orekit.utils.units.UnitsCache
Simple constructor.
UnitsConverter - Class in org.orekit.utils.units
Converter between units.
UnitsConverter(Unit, Unit) - Constructor for class org.orekit.utils.units.UnitsConverter
Simple constructor.
unitsListToString(List<Unit>) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Convert a list of units to a bracketed string.
unitsListToString(List<Unit>) - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Convert a list of units to a bracketed string.
UnivariateProcessNoise - Class in org.orekit.estimation.sequential
Provider for a temporal evolution of the process noise matrix.
UnivariateProcessNoise(RealMatrix, LOFType, PositionAngleType, UnivariateFunction[], UnivariateFunction[]) - Constructor for class org.orekit.estimation.sequential.UnivariateProcessNoise
Simple constructor.
UnivariateProcessNoise(RealMatrix, LOFType, PositionAngleType, UnivariateFunction[], UnivariateFunction[], UnivariateFunction[]) - Constructor for class org.orekit.estimation.sequential.UnivariateProcessNoise
Simple constructor.
UnixCompressFilter - Class in org.orekit.data
Filter for Unix compressed data.
UnixCompressFilter() - Constructor for class org.orekit.data.UnixCompressFilter
Empty constructor.
UNKNOWN - org.orekit.files.ccsds.ndm.odm.ocm.ObjectType
Unknown.
UNKNOWN - org.orekit.files.ccsds.ndm.odm.ocm.OpsStatus
Unknown status.
UNKNOWN - org.orekit.forces.gravity.potential.TideSystem
Constant for unknown tide system.
UNKNOWN - org.orekit.gnss.TimeSystem
Unknown (should only be used in RUN BY / DATE entries).
UNKNOWN_ADDITIONAL_STATE - org.orekit.errors.OrekitMessages
UNKNOWN_ADDITIONAL_STATE.
UNKNOWN_AUTHENTICATION_METHOD - org.orekit.errors.OrekitMessages
UNKNOWN_AUTHENTICATION_METHOD.
UNKNOWN_CARRIER_PHASE_CODE - org.orekit.errors.OrekitMessages
UNKNOWN_CARRIER_PHASE_CODE.
UNKNOWN_CLOCK_DATA_TYPE - org.orekit.errors.OrekitMessages
UNKNOWN_CLOCK_DATA_TYPE.
UNKNOWN_DATA_FORMAT - org.orekit.errors.OrekitMessages
UNKNOWN_DATA_FORMAT.
UNKNOWN_ENCODED_MESSAGE_NUMBER - org.orekit.errors.OrekitMessages
UNKNOWN_ENCODED_MESSAGE_NUMBER.
UNKNOWN_HOST - org.orekit.errors.OrekitMessages
UNKNOWN_HOST.
UNKNOWN_MONTH - org.orekit.errors.OrekitMessages
UNKNOWN_MONTH.
UNKNOWN_NAVIGATION_SYSTEM - org.orekit.errors.OrekitMessages
UNKNOWN_NAVIGATION_SYSTEM.
UNKNOWN_OBJECT - Static variable in class org.orekit.files.ccsds.ndm.adm.acm.Acm
Default name for unknown object.
UNKNOWN_OBJECT - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.Ocm
Default name for unknown object.
UNKNOWN_RINEX_FREQUENCY - org.orekit.errors.OrekitMessages
UNKNOWN_RINEX_FREQUENCY.
UNKNOWN_SATELLITE_ANTENNA_CODE - org.orekit.errors.OrekitMessages
UNKNOWN_SATELLITE_ANTENNA_CODE.
UNKNOWN_SATELLITE_SYSTEM - org.orekit.errors.OrekitMessages
UNKNOWN_SATELLITE_SYSTEM.
UNKNOWN_TIME_SYSTEM - org.orekit.errors.OrekitMessages
UNKNOWN_TIME_SYSTEM.
UNKNOWN_UNIT - org.orekit.errors.OrekitMessages
UNKNOWN_UNIT.
UNKNOWN_UTC_ID - org.orekit.errors.OrekitMessages
UNKNOWN_UTC_ID.
UNKOWN - org.orekit.files.ccsds.definitions.YesNoUnknown
UNKOWN value.
unmodifiableView() - Method in class org.orekit.utils.DoubleArrayDictionary
Get an unmodifiable view of the dictionary.
unmodifiableView() - Method in class org.orekit.utils.FieldArrayDictionary
Get an unmodifiable view of the dictionary.
unnormalizeCovarianceMatrix(RealMatrix, double[]) - Static method in class org.orekit.estimation.sequential.KalmanEstimatorUtil
Un-nomalized the covariance matrix.
UnnormalizedSphericalHarmonicsProvider - Interface in org.orekit.forces.gravity.potential
Interface used to provide un-normalized spherical harmonics coefficients.
UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics - Interface in org.orekit.forces.gravity.potential
Un-normalized spherical harmonics coefficients evaluated at a specific instant.
unnormalizeInnovationCovarianceMatrix(RealMatrix, double[]) - Static method in class org.orekit.estimation.sequential.KalmanEstimatorUtil
Un-normalize the innovation covariance matrix.
unnormalizeKalmanGainMatrix(RealMatrix, double[], double[]) - Static method in class org.orekit.estimation.sequential.KalmanEstimatorUtil
Un-normalize the Kalman gain matrix.
unnormalizeMeasurementJacobian(RealMatrix, double[], double[]) - Static method in class org.orekit.estimation.sequential.KalmanEstimatorUtil
Un-normalize the measurement matrix.
unnormalizeStateTransitionMatrix(RealMatrix, double[]) - Static method in class org.orekit.estimation.sequential.KalmanEstimatorUtil
Un-nomalized the state transition matrix.
UnscentedKalmanEstimator - Class in org.orekit.estimation.sequential
Implementation of an Unscented Kalman filter to perform orbit determination.
UnscentedKalmanEstimatorBuilder - Class in org.orekit.estimation.sequential
Builder for an Unscented Kalman filter estimator.
UnscentedKalmanEstimatorBuilder() - Constructor for class org.orekit.estimation.sequential.UnscentedKalmanEstimatorBuilder
Default constructor.
UnscentedKalmanModel - Class in org.orekit.estimation.sequential
Class defining the process model dynamics to use with a UnscentedKalmanEstimator.
UnscentedKalmanModel(List<PropagatorBuilder>, List<CovarianceMatrixProvider>, ParameterDriversList, CovarianceMatrixProvider) - Constructor for class org.orekit.estimation.sequential.UnscentedKalmanModel
Unscented Kalman process model constructor (package private).
unscentedTransformProvider(UnscentedTransformProvider) - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanEstimatorBuilder
Configure the unscented transform provider.
unscentedTransformProvider(UnscentedTransformProvider) - Method in class org.orekit.estimation.sequential.UnscentedKalmanEstimatorBuilder
Configure the unscented transform provider.
UNSUPPORTED_FILE_FORMAT - org.orekit.errors.OrekitMessages
UNSUPPORTED_FILE_FORMAT.
UNSUPPORTED_FILE_FORMAT_VERSION - org.orekit.errors.OrekitMessages
UNSUPPORTED_FILE_FORMAT_VERSION.
UNSUPPORTED_FREQUENCY_FOR_ANTENNA - org.orekit.errors.OrekitMessages
UNSUPPORTED_FREQUENCY_FOR_ANTENNA.
UNSUPPORTED_LOCAL_ORBITAL_FRAME - org.orekit.errors.OrekitMessages
UNSUPPORTED_LOCAL_ORBITAL_FRAME.
UNSUPPORTED_PARAMETER_NAME - org.orekit.errors.OrekitMessages
UNSUPPORTED_PARAMETER_NAME.
UNSUPPORTED_TIME_TRANSFORM - org.orekit.errors.OrekitMessages
UNSUPPORTED_TIME_TRANSFORM.
UNSUPPORTED_TRANSFORM - org.orekit.errors.OrekitMessages
UNSUPPORTED_TRANSFORM.
UnsupportedParameterException - Exception in org.orekit.errors
Exception for unsupported ParameterDriver in a model implementing ParameterDriversProvider.
UnsupportedParameterException(String, List<ParameterDriver>) - Constructor for exception org.orekit.errors.UnsupportedParameterException
Constructor.
unwrap(MathRuntimeException) - Static method in exception org.orekit.errors.OrekitException
Recover a OrekitException, possibly embedded in a MathRuntimeException.
unwrap(MathRuntimeException) - Static method in exception org.orekit.errors.TimeStampedCacheException
Recover a TimeStampedCacheException, possibly embedded in a MathRuntimeException.
unwrap(OrekitException) - Static method in exception org.orekit.errors.TimeStampedCacheException
Recover a TimeStampedCacheException, possibly embedded in a OrekitException.
UP - org.orekit.models.earth.displacement.PsdCorrection.Axis
Up axis.
UpdatableFrame - Class in org.orekit.frames
Frame whose transform from its parent can be updated.
UpdatableFrame(Frame, Transform, String) - Constructor for class org.orekit.frames.UpdatableFrame
Build a non-inertial frame from its transform with respect to its parent.
UpdatableFrame(Frame, Transform, String, boolean) - Constructor for class org.orekit.frames.UpdatableFrame
Build a frame from its transform with respect to its parent.
update(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.FieldAbstractStateModifier
Update a state.
update(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.FieldAdditionalStateProvider
Update a state.
update(SpacecraftState) - Method in class org.orekit.propagation.AbstractStateModifier
Update a state.
update(SpacecraftState) - Method in interface org.orekit.propagation.AdditionalStateProvider
Update a state.
updateAdditionalConstraints(int, double[]) - Method in class org.orekit.utils.AbstractMultipleShooting
Update the array of additional constraints.
updateAdditionalStates(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator
Update state by adding all additional states.
updateAdditionalStates(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
Update state by adding all additional states.
updateAdditionalStates(SpacecraftState) - Method in class org.orekit.propagation.AbstractPropagator
Update state by adding all additional states.
updateAdditionalStates(SpacecraftState) - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Update state by adding all additional states.
updateAdjoint(double[], FieldSpacecraftState<Gradient>) - Method in class org.orekit.control.indirect.shooting.AbstractFixedBoundaryCartesianSingleShooting
Update initial adjoint vector.
updateAdjoint(double[], FieldSpacecraftState<Gradient>) - Method in class org.orekit.control.indirect.shooting.NewtonFixedBoundaryCartesianSingleShooting
Update initial adjoint vector.
updateAdjointDerivatives(double[], double, double[]) - Method in interface org.orekit.control.indirect.adjoint.cost.CartesianCost
Update the adjoint derivatives if necessary.
updateAdjointDerivatives(double[], double, double[]) - Method in class org.orekit.control.indirect.adjoint.cost.UnboundedCartesianEnergyNeglectingMass
 
updateFieldAdjointDerivatives(T[], T, T[]) - Method in interface org.orekit.control.indirect.adjoint.cost.CartesianCost
Update the adjoint derivatives if necessary.
updateFieldAdjointDerivatives(T[], T, T[]) - Method in class org.orekit.control.indirect.adjoint.cost.UnboundedCartesianEnergyNeglectingMass
 
updateFieldShortPeriodTerms(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester
Update the short periodic terms for the "field" elements.
updateMass(double) - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
Update a spacecraft mass due to maneuver.
updateNominalSpacecraftState(SpacecraftState) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Update the nominal spacecraft state.
updateNominalSpacecraftState(SpacecraftState) - Method in interface org.orekit.estimation.sequential.SemiAnalyticalProcess
Update the nominal spacecraft state.
updateNominalSpacecraftState(SpacecraftState) - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel
Update the nominal spacecraft state.
updateReferenceTrajectories(Propagator[]) - Method in class org.orekit.estimation.sequential.KalmanModel
Update the reference trajectories using the propagators as input.
updateReferenceTrajectory(DSSTPropagator) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Update the reference trajectories using the propagator as input.
updateShortPeriods(SpacecraftState) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Update the DSST short periodic terms.
updateShortPeriods(SpacecraftState) - Method in interface org.orekit.estimation.sequential.SemiAnalyticalProcess
Update the DSST short periodic terms.
updateShortPeriods(SpacecraftState) - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel
Update the DSST short periodic terms.
updateShortPeriodTerms(double[], SpacecraftState...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Update the short period terms.
updateShortPeriodTerms(double[], SpacecraftState...) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Update the short period terms.
updateShortPeriodTerms(double[], SpacecraftState...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTJ2SquaredClosedForm
Update the short period terms.
updateShortPeriodTerms(double[], SpacecraftState...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction
Update the short period terms.
updateShortPeriodTerms(double[], SpacecraftState...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Update the short period terms.
updateShortPeriodTerms(double[], SpacecraftState...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Update the short period terms.
updateShortPeriodTerms(double[], SpacecraftState...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Update the short period terms.
updateShortPeriodTerms(double[], SpacecraftState...) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.J2SquaredModel
Update the J2-squared short period terms.
updateShortPeriodTerms(T[], FieldSpacecraftState<T>...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Update the short period terms.
updateShortPeriodTerms(T[], FieldSpacecraftState<T>...) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Update the short period terms.
updateShortPeriodTerms(T[], FieldSpacecraftState<T>...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTJ2SquaredClosedForm
Update the short period terms.
updateShortPeriodTerms(T[], FieldSpacecraftState<T>...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction
Update the short period terms.
updateShortPeriodTerms(T[], FieldSpacecraftState<T>...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Update the short period terms.
updateShortPeriodTerms(T[], FieldSpacecraftState<T>...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Update the short period terms.
updateShortPeriodTerms(T[], FieldSpacecraftState<T>...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Update the short period terms.
updateShortPeriodTerms(T[], FieldSpacecraftState<T>...) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.J2SquaredModel
Update the J2-squared short period terms.
updateTransform(Frame, Frame, Transform, AbsoluteDate) - Method in class org.orekit.frames.UpdatableFrame
Update the transform from parent frame implicitly according to two other frames.
updateUnmanagedStates(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator
Update state by adding unmanaged states.
updateUnmanagedStates(SpacecraftState) - Method in class org.orekit.propagation.AbstractPropagator
Update state by adding unmanaged states.
UpperBounds - Class in org.orekit.propagation.semianalytical.dsst.utilities
Utility class to compute upper bounds for truncation algorithms.
URANUS - org.orekit.bodies.JPLEphemeridesLoader.EphemerisType
Constant for Uranus.
URANUS - org.orekit.files.ccsds.definitions.CenterName
Uranus body.
URANUS - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Uranus.
USE_P - org.orekit.utils.CartesianDerivativesFilter
Use only positions, ignoring velocities.
USE_PV - org.orekit.utils.CartesianDerivativesFilter
Use positions and velocities.
USE_PVA - org.orekit.utils.CartesianDerivativesFilter
Use positions, velocities and accelerations.
USE_R - org.orekit.utils.AngularDerivativesFilter
Use only rotations, ignoring rotation rates.
USE_RR - org.orekit.utils.AngularDerivativesFilter
Use rotations and rotation rates.
USE_RRA - org.orekit.utils.AngularDerivativesFilter
Use rotations, rotation rates and acceleration.
USEABLE_START_TIME - org.orekit.files.ccsds.ndm.adm.aem.AemMetadataKey
Useable start time entry.
USEABLE_START_TIME - org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadataKey
Useable start time entry.
USEABLE_START_TIME - org.orekit.files.ccsds.ndm.odm.oem.OemMetadataKey
Useable start time entry.
USEABLE_STOP_TIME - org.orekit.files.ccsds.ndm.adm.aem.AemMetadataKey
Useable stop time entry.
USEABLE_STOP_TIME - org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadataKey
Useable stop time entry.
USEABLE_STOP_TIME - org.orekit.files.ccsds.ndm.odm.oem.OemMetadataKey
Useable stop time entry.
user - org.orekit.files.ccsds.ndm.adm.acm.AcmDataSubStructureKey
User-defined parameters section.
user - org.orekit.files.ccsds.ndm.odm.ocm.OcmDataSubStructureKey
User-defined parameters section.
USER - org.orekit.files.ccsds.ndm.adm.acm.AcmDataSubStructureKey
User-defined parameters section.
USER - org.orekit.files.ccsds.ndm.adm.acm.AcmElements
User defined.
USER - org.orekit.files.ccsds.ndm.odm.ocm.OcmDataSubStructureKey
User-defined parameters section.
USER - org.orekit.files.ccsds.ndm.odm.ocm.OcmElements
User defined.
USER_DEFINED_A - org.orekit.gnss.SatelliteSystem
User-defined system A.
USER_DEFINED_B - org.orekit.gnss.SatelliteSystem
User-defined system B.
USER_DEFINED_D - org.orekit.gnss.SatelliteSystem
User-defined system D.
USER_DEFINED_F - org.orekit.gnss.SatelliteSystem
User-defined system F.
USER_DEFINED_H - org.orekit.gnss.SatelliteSystem
User-defined system H.
USER_DEFINED_K - org.orekit.gnss.SatelliteSystem
User-defined system K.
USER_DEFINED_L - org.orekit.gnss.SatelliteSystem
User-defined system L.
USER_DEFINED_N - org.orekit.gnss.SatelliteSystem
User-defined system N.
USER_DEFINED_O - org.orekit.gnss.SatelliteSystem
User-defined system O.
USER_DEFINED_P - org.orekit.gnss.SatelliteSystem
User-defined system P.
USER_DEFINED_PREFIX - Static variable in class org.orekit.files.ccsds.ndm.odm.UserDefined
Prefix for user defined parameters keys.
USER_DEFINED_Q - org.orekit.gnss.SatelliteSystem
User-defined system Q.
USER_DEFINED_T - org.orekit.gnss.SatelliteSystem
User-defined system T.
USER_DEFINED_U - org.orekit.gnss.SatelliteSystem
User-defined system U.
USER_DEFINED_V - org.orekit.gnss.SatelliteSystem
User-defined system V.
USER_DEFINED_W - org.orekit.gnss.SatelliteSystem
User-defined system W.
USER_DEFINED_X - org.orekit.gnss.SatelliteSystem
User-defined system X.
USER_DEFINED_XML_ATTRIBUTE - Static variable in class org.orekit.files.ccsds.ndm.odm.UserDefined
Attribute name for user defined parameters keys.
USER_DEFINED_XML_TAG - Static variable in class org.orekit.files.ccsds.ndm.odm.UserDefined
Tag name for user defined parameters keys.
USER_DEFINED_Y - org.orekit.gnss.SatelliteSystem
User-defined system Y.
USER_DEFINED_Z - org.orekit.gnss.SatelliteSystem
User-defined system Z.
UserDefined - Class in org.orekit.files.ccsds.ndm.odm
Container for user defined data.
UserDefined() - Constructor for class org.orekit.files.ccsds.ndm.odm.UserDefined
Create an empty data set.
userDefinedParameters - org.orekit.files.ccsds.ndm.cdm.XmlSubStructureKey
User-defined parameters section.
UserDefinedWriter - Class in org.orekit.files.ccsds.ndm.odm
Writer for user defined parameters data.
UserDefinedWriter(String, String, UserDefined) - Constructor for class org.orekit.files.ccsds.ndm.odm.UserDefinedWriter
Create a writer.
UserDefinedXmlTokenBuilder - Class in org.orekit.files.ccsds.utils.lexical
Builder for user-defined parameters.
UserDefinedXmlTokenBuilder() - Constructor for class org.orekit.files.ccsds.utils.lexical.UserDefinedXmlTokenBuilder
Empty constructor.
UserRangeAccuracy - Class in org.orekit.gnss.metric.messages.common
User Range Accuracy.
UserRangeAccuracy(int) - Constructor for class org.orekit.gnss.metric.messages.common.UserRangeAccuracy
Simple constructor.
USNO - org.orekit.files.rinex.navigation.UtcId
UTC(USNO).
UT1 - org.orekit.files.ccsds.definitions.TimeSystem
Universal Time.
UT1MUTC_AT_TZERO - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Difference (UT1 – UTC) in seconds at epoch OcmMetadataKey.EPOCH_TZERO.
UT1Scale - Class in org.orekit.time
Universal Time 1.
UT1Scale(EOPHistory, UTCScale) - Constructor for class org.orekit.time.UT1Scale
Simple constructor.
utc - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
UTC time scale.
utc - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
UTC time scale.
UTC - org.orekit.files.ccsds.definitions.TimeSystem
Universal Coordinated Time.
UTC - org.orekit.gnss.TimeSystem
Coordinated Universal Time.
UtcId - Enum in org.orekit.files.rinex.navigation
Enumerate for the UTC ids.
UTCScale - Class in org.orekit.time
Coordinated Universal Time.
UTCTAIBulletinAFilesLoader - Class in org.orekit.time
Loader for UTC-TAI extracted from bulletin A files.
UTCTAIBulletinAFilesLoader(String) - Constructor for class org.orekit.time.UTCTAIBulletinAFilesLoader
Build a loader for IERS bulletins A files.
UTCTAIBulletinAFilesLoader(String, DataProvidersManager) - Constructor for class org.orekit.time.UTCTAIBulletinAFilesLoader
Build a loader for IERS bulletins A files.
UTCTAIHistoryFilesLoader - Class in org.orekit.time
Loader for UTC versus TAI history files.
UTCTAIHistoryFilesLoader() - Constructor for class org.orekit.time.UTCTAIHistoryFilesLoader
Build a loader for UTC-TAI history file.
UTCTAIHistoryFilesLoader(DataProvidersManager) - Constructor for class org.orekit.time.UTCTAIHistoryFilesLoader
Build a loader for UTC-TAI history file.
UTCTAIHistoryFilesLoader.Parser - Class in org.orekit.time
Internal class performing the parsing.
UTCTAIOffset - Class in org.orekit.time
Offset between UTC and TAI time scales.
UTCTAIOffsetsLoader - Interface in org.orekit.time
Interface for loading UTC-TAI offsets data files.
UTCTAIOffsetsLoader.Parser - Interface in org.orekit.time
Interface for parsing UTC-TAI offsets from a stream.
UTM - org.orekit.files.ccsds.ndm.odm.ocm.Ordering
Upper Triangular Matrix.
UTMWCC - org.orekit.files.ccsds.ndm.odm.ocm.Ordering
Upper Triangular Matrix conflated with cross-correlation terms.

V

validate() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Check is all mandatory entries have been initialized.
validate() - Method in class org.orekit.files.ccsds.ndm.NdmConstituent
Validate the file message for required and forbidden entries.
validate(boolean, String) - Method in class org.orekit.files.sp3.SP3
Check file is valid.
validate(double) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmData
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadata
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationSensor
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalProperties
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.AngularVelocity
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternion
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Inertia
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadata
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmData
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmHeader
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.cdm.SigmaEigenvectorsCovariance
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.cdm.StateVector
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.CartesianCovariance
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmData
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.OdmCommonMetadata
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmData
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.StateVector
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.section.CommentsContainer
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.section.Header
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.section.Metadata
Check is all mandatory entries have been initialized.
validate(double) - Method in interface org.orekit.files.ccsds.section.Section
Check is all mandatory entries have been initialized.
VALIDATED - org.orekit.files.ccsds.ndm.tdm.DataQuality
Sata passed quality check.
validFrom() - Method in class org.orekit.models.earth.GeoMagneticField
Returns the start of the validity period for this model.
validityEnd() - Method in interface org.orekit.gnss.attitude.GNSSAttitudeProvider
Get end of validity for this provider.
validityStart() - Method in interface org.orekit.gnss.attitude.GNSSAttitudeProvider
Get start of validity for this provider.
validTo() - Method in class org.orekit.models.earth.GeoMagneticField
Returns the end of the validity period for this model.
VALSECCHI - org.orekit.frames.encounter.EncounterLOFType
Valsecchi encounter local orbital frame based on Valsecchi formulation from : "Valsecchi, G.
ValsecchiEncounterFrame - Class in org.orekit.frames.encounter
Valsecchi encounter local orbital frame based on Valsecchi formulation from : "Valsecchi, G.
ValsecchiEncounterFrame(FieldPVCoordinates<T>) - Constructor for class org.orekit.frames.encounter.ValsecchiEncounterFrame
Constructor.
ValsecchiEncounterFrame(PVCoordinates) - Constructor for class org.orekit.frames.encounter.ValsecchiEncounterFrame
Constructor.
value(double) - Method in class org.orekit.data.PolynomialNutation
Evaluate the value of the polynomial.
value(double) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.IntegrableFunction
value(double, double) - Method in class org.orekit.gnss.antenna.OneDVariation
Evaluate phase center variation in one signal direction.
value(double, double) - Method in interface org.orekit.gnss.antenna.PhaseCenterVariationFunction
Evaluate phase center variation in one signal direction.
value(double, double) - Method in class org.orekit.gnss.antenna.TwoDVariation
Evaluate phase center variation in one signal direction.
value(RealVector) - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel
value(BodiesElements) - Method in interface org.orekit.data.PoissonSeries.CompiledSeries
Evaluate a set of Poisson series.
value(BodiesElements) - Method in class org.orekit.data.PoissonSeries
Evaluate the value of the series.
value(FieldBodiesElements<S>) - Method in interface org.orekit.data.PoissonSeries.CompiledSeries
Evaluate a set of Poisson series.
value(FieldBodiesElements<T>) - Method in class org.orekit.data.PoissonSeries
Evaluate the value of the series.
value(FieldOrbit<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldGaussianShortPeriodicCoefficients
Evaluate the contributions of the short period terms.
value(FieldOrbit<T>) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.FieldShortPeriodTerms
Evaluate the contributions of the short period terms.
value(Orbit) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.GaussianShortPeriodicCoefficients
Evaluate the contributions of the short period terms.
value(Orbit) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.ShortPeriodTerms
Evaluate the contributions of the short period terms.
value(SpacecraftState) - Method in interface org.orekit.utils.StateFunction
Evaluate the function.
value(SpacecraftState) - Method in interface org.orekit.utils.StateJacobian
Evaluate the Jacobian of the function.
value(AbsoluteDate) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.ShortPeriodicsInterpolatedCoefficient
Compute the value of the coefficient.
value(AbsoluteDate) - Method in interface org.orekit.time.TimeScalarFunction
Compute a function of time.
value(AbsoluteDate) - Method in interface org.orekit.time.TimeVectorFunction
Compute a function of time.
value(AbsoluteDate, Vector3D, double) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Compute the value of the gravity field.
value(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldShortPeriodicsInterpolatedCoefficient
Compute the value of the coefficient.
value(FieldAbsoluteDate<T>) - Method in interface org.orekit.time.TimeScalarFunction
Compute a function of time.
value(FieldAbsoluteDate<T>) - Method in interface org.orekit.time.TimeVectorFunction
Compute a function of time.
value(ParameterDriver, AbsoluteDate) - Method in interface org.orekit.utils.ParameterFunction
Evaluate the function.
value(T) - Method in class org.orekit.data.PolynomialNutation
Evaluate the value of the polynomial.
value(T) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldIntegrableFunction
VALUE_NOT_FOUND - org.orekit.errors.OrekitMessages
VALUE_NOT_FOUND.
valueChanged(double, ParameterDriver, AbsoluteDate) - Method in interface org.orekit.utils.ParameterObserver
Notify that a parameter value has been changed.
valueOf(String) - Static method in enum org.orekit.attitudes.PredefinedTarget
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.bodies.JPLEphemeridesLoader.EphemerisType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.data.PolynomialParser.Unit
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.errors.OrekitMessages
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.estimation.measurements.EstimatedMeasurementBase.Status
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.estimation.measurements.generation.SignSemantic
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.estimation.measurements.gnss.CombinationType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.definitions.AdMethodType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.definitions.CelestialBodyFrame
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.definitions.CenterName
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.definitions.DutyCycleType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.definitions.OdMethodType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.definitions.OnOff
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.definitions.OrbitRelativeFrame
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.definitions.PocMethodType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.definitions.SpacecraftBodyFrame.BaseEquipment
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.definitions.TimeSystem
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.definitions.YesNoUnknown
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.AcmDataSubStructureKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.AcmElements
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.AcmMetadataKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadataKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationSensorKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeElementsType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuverKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalPropertiesKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadataKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.RateElementsType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.AdmCommonMetadataKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.AdmMetadataKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.aem.AemMetadataKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.apm.AngularVelocityKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternionKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.apm.EulerKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.apm.InertiaKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.apm.ManeuverKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.apm.SpinStabilizedKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.AttitudeType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadataKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.AltCovarianceType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.CdmHeaderKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.CovarianceMethod
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.Maneuvrable
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.ODParametersKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.ScreenType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.ScreenVolumeFrame
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.ScreenVolumeShape
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.SigmaEigenvectorsCovarianceKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.StateVectorKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.XmlSubStructureKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.CommonMetadataKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.KeplerianElementsKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.ManBasis
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.ObjectType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OcmDataSubStructureKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OcmElements
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OpsStatus
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitCategory
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadataKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitElementsType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.Ordering
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.ShadowModel
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadataKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.OdmMetadataKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.oem.InterpolationMethod
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.oem.OemMetadataKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.omm.OmmMetadataKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.omm.OmmTleKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.opm.ManeuverKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.SpacecraftParametersKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.StateVectorKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.ParsedUnitsBehavior
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.tdm.AngleType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.tdm.CorrectionApplied
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.tdm.DataQuality
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.tdm.IntegrationReference
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.tdm.ObservationType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.tdm.RangeMode
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.tdm.RangeUnits
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.tdm.TdmDataKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.tdm.TimetagReference
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.tdm.TrackingMode
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.section.HeaderKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.section.KvnStructureKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.section.MetadataKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.section.XmlStructureKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.utils.FileFormat
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.utils.lexical.TokenType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ilrs.CRDHeader.DataType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ilrs.CRDHeader.RangeType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ilrs.StreamingCpfWriter.HeaderLineWriter
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.rinex.clock.RinexClock.ClockDataType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.rinex.navigation.IonosphericCorrectionType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.rinex.navigation.RegionCode
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.rinex.navigation.SbasId
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.rinex.navigation.UtcId
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.rinex.section.RinexLabels
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.rinex.utils.RinexFileType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.sinex.Station.ReferenceSystem
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.sp3.DataUsed
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.sp3.SP3FileType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.sp3.SP3OrbitType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.stk.STKEphemerisFile.STKCoordinateSystem
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.forces.gravity.potential.OceanLoadDeformationCoefficients
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.forces.gravity.potential.TideSystem
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.forces.maneuvers.Control3DVectorCostType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.frames.encounter.EncounterLOFType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.frames.HelmertTransformation.Predefined
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.frames.ITRFVersion
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.frames.LocalMagneticFieldFrame.LOFBuilderVector
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.frames.LOFType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.frames.Predefined
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.geometry.fov.PolygonalFieldOfView.DefiningConeType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.gnss.antenna.SatelliteType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.gnss.Frequency
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.gnss.MeasurementType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.gnss.metric.ntrip.Authentication
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.gnss.metric.ntrip.CarrierPhase
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.gnss.metric.ntrip.DataFormat
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.gnss.metric.ntrip.NavigationSystem
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.gnss.metric.ntrip.RecordType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.gnss.metric.ntrip.Type
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.gnss.metric.parser.DataType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.gnss.metric.parser.IgsSsrDataField
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.gnss.metric.parser.IgsSsrMessageType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.gnss.metric.parser.RtcmDataField
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.gnss.metric.parser.RtcmMessageType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.gnss.ObservationTimeScale
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.gnss.ObservationType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.gnss.SatelliteSystem
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.gnss.SignalCode
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.gnss.TimeSystem
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation.StrengthLevel
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.models.earth.displacement.PsdCorrection.Axis
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.models.earth.displacement.PsdCorrection.TimeEvolution
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.models.earth.GeoMagneticFieldFactory.FieldModel
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.models.earth.troposphere.ViennaModelType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.orbits.LibrationOrbitFamily
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.orbits.LibrationOrbitType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.orbits.OrbitType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.orbits.PositionAngleType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.propagation.analytical.gnss.data.BeidouSatelliteType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.propagation.events.FilterType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.propagation.events.VisibilityTrigger
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.propagation.PropagationType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethodType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.time.Month
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.utils.AngularDerivativesFilter
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.utils.CartesianDerivativesFilter
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.utils.IERSConventions
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.utils.LagrangianPoints
Returns the enum constant of this type with the specified name.
values() - Static method in enum org.orekit.attitudes.PredefinedTarget
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.bodies.JPLEphemeridesLoader.EphemerisType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.data.PolynomialParser.Unit
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.errors.OrekitMessages
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.estimation.measurements.EstimatedMeasurementBase.Status
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.estimation.measurements.generation.SignSemantic
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.estimation.measurements.gnss.CombinationType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.definitions.AdMethodType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.definitions.CelestialBodyFrame
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.definitions.CenterName
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.definitions.DutyCycleType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.definitions.OdMethodType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.definitions.OnOff
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.definitions.OrbitRelativeFrame
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.definitions.PocMethodType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.definitions.SpacecraftBodyFrame.BaseEquipment
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.definitions.TimeSystem
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.definitions.YesNoUnknown
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.AcmDataSubStructureKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.AcmElements
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.AcmMetadataKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadataKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationSensorKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeElementsType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuverKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalPropertiesKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadataKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.adm.acm.RateElementsType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.adm.AdmCommonMetadataKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.adm.AdmMetadataKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.adm.aem.AemMetadataKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.adm.apm.AngularVelocityKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternionKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.adm.apm.EulerKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.adm.apm.InertiaKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.adm.apm.ManeuverKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.adm.apm.SpinStabilizedKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.adm.AttitudeType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadataKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.AltCovarianceType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.CdmHeaderKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.CovarianceMethod
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.Maneuvrable
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.ODParametersKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.ScreenType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.ScreenVolumeFrame
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.ScreenVolumeShape
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.SigmaEigenvectorsCovarianceKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.StateVectorKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.XmlSubStructureKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.CommonMetadataKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.KeplerianElementsKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.ManBasis
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.ObjectType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OcmDataSubStructureKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OcmElements
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OpsStatus
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitCategory
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadataKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitElementsType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.Ordering
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.ShadowModel
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadataKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.OdmMetadataKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.oem.InterpolationMethod
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.oem.OemMetadataKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.omm.OmmMetadataKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.omm.OmmTleKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.opm.ManeuverKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.SpacecraftParametersKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.StateVectorKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.ParsedUnitsBehavior
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.tdm.AngleType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.tdm.CorrectionApplied
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.tdm.DataQuality
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.tdm.IntegrationReference
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.tdm.ObservationType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.tdm.RangeMode
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.tdm.RangeUnits
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.tdm.TdmDataKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.tdm.TimetagReference
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.tdm.TrackingMode
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.section.HeaderKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.section.KvnStructureKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.section.MetadataKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.section.XmlStructureKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.utils.FileFormat
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.utils.lexical.TokenType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ilrs.CRDHeader.DataType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ilrs.CRDHeader.RangeType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ilrs.StreamingCpfWriter.HeaderLineWriter
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.rinex.clock.RinexClock.ClockDataType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.rinex.navigation.IonosphericCorrectionType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.rinex.navigation.RegionCode
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.rinex.navigation.SbasId
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.rinex.navigation.UtcId
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.rinex.section.RinexLabels
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.rinex.utils.RinexFileType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.sinex.Station.ReferenceSystem
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.sp3.DataUsed
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.sp3.SP3FileType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.sp3.SP3OrbitType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.stk.STKEphemerisFile.STKCoordinateSystem
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.forces.gravity.potential.OceanLoadDeformationCoefficients
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.forces.gravity.potential.TideSystem
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.forces.maneuvers.Control3DVectorCostType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.frames.encounter.EncounterLOFType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.frames.HelmertTransformation.Predefined
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.frames.ITRFVersion
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.frames.LocalMagneticFieldFrame.LOFBuilderVector
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.frames.LOFType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.frames.Predefined
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.geometry.fov.PolygonalFieldOfView.DefiningConeType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.gnss.antenna.SatelliteType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.gnss.Frequency
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.gnss.MeasurementType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.gnss.metric.ntrip.Authentication
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.gnss.metric.ntrip.CarrierPhase
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.gnss.metric.ntrip.DataFormat
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.gnss.metric.ntrip.NavigationSystem
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.gnss.metric.ntrip.RecordType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.gnss.metric.ntrip.Type
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.gnss.metric.parser.DataType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.gnss.metric.parser.IgsSsrDataField
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.gnss.metric.parser.IgsSsrMessageType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.gnss.metric.parser.RtcmDataField
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.gnss.metric.parser.RtcmMessageType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.gnss.ObservationTimeScale
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.gnss.ObservationType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.gnss.SatelliteSystem
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.gnss.SignalCode
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.gnss.TimeSystem
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation.StrengthLevel
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.models.earth.displacement.PsdCorrection.Axis
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.models.earth.displacement.PsdCorrection.TimeEvolution
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.models.earth.GeoMagneticFieldFactory.FieldModel
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.models.earth.troposphere.ViennaModelType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.orbits.LibrationOrbitFamily
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.orbits.LibrationOrbitType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.orbits.OrbitType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.orbits.PositionAngleType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.propagation.analytical.gnss.data.BeidouSatelliteType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.propagation.events.FilterType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.propagation.events.VisibilityTrigger
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.propagation.PropagationType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethodType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.time.Month
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.utils.AngularDerivativesFilter
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.utils.CartesianDerivativesFilter
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.utils.IERSConventions
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.utils.LagrangianPoints
Returns an array containing the constants of this enum type, in the order they are declared.
valueSpanMapChanged(TimeSpanMap<Double>, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver
Notify that a parameter value span map has been changed.
vector(GeodeticPoint) - Method in enum org.orekit.models.earth.displacement.PsdCorrection.Axis
Get axis unit vector.
VEIS_1950 - org.orekit.frames.Predefined
Veis 1950.
VEL_X - Static variable in enum org.orekit.orbits.OrbitType
Name for velocity along X.
VEL_Y - Static variable in enum org.orekit.orbits.OrbitType
Name for velocity along Y.
VEL_Z - Static variable in enum org.orekit.orbits.OrbitType
Name for velocity along Z.
VELOCITY - org.orekit.attitudes.PredefinedTarget
Satellite velocity.
VELOCITY_ACCURACY_UNIT - Static variable in class org.orekit.files.sp3.SP3Utils
Velocity accuracy unit.
VELOCITY_UNIT - Static variable in class org.orekit.files.sp3.SP3Utils
Velocity unit.
VENUS - org.orekit.bodies.JPLEphemeridesLoader.EphemerisType
Constant for Venus.
VENUS - org.orekit.files.ccsds.definitions.CenterName
Venus body.
VENUS - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Venus.
VERSION - org.orekit.files.rinex.section.RinexLabels
Version, file type and satellite system.
VersionedITRF - Class in org.orekit.frames
Specific version of International Terrestrial Reference Frame.
VERTICAL_TOTAL_ELECTRON_CONTENT - Static variable in class org.orekit.models.earth.ionosphere.EstimatedIonosphericModel
Name of the parameter of this model: the Vertical Total Electron Content.
verticesRadius(double, int) - Method in enum org.orekit.geometry.fov.PolygonalFieldOfView.DefiningConeType
Compute radius of cone going through vertices.
VIENNA_ACOEF_OR_ZENITH_DELAY_NOT_AVAILABLE_FOR_DATE - org.orekit.errors.OrekitMessages
VIENNA_ACOEF_OR_ZENITH_DELAY_NOT_AVAILABLE_FOR_DATE.
VIENNA_ACOEF_OR_ZENITH_DELAY_NOT_LOADED - org.orekit.errors.OrekitMessages
VIENNA_ACOEF_OR_ZENITH_DELAY_NOT_LOADED.
VIENNA_ONE - org.orekit.models.earth.troposphere.ViennaModelType
Vienna one tropospheric model.
VIENNA_THREE - org.orekit.models.earth.troposphere.ViennaModelType
Vienna three tropospheric model.
ViennaACoefficients - Class in org.orekit.models.earth.troposphere
Container for the ViennaOne and ViennaThree coefficients ah and aw.
ViennaACoefficients(double, double) - Constructor for class org.orekit.models.earth.troposphere.ViennaACoefficients
Simple constructor.
ViennaAProvider - Interface in org.orekit.models.earth.troposphere
Provider for ViennaOne and ViennaThree coefficients ah and aw.
ViennaModelCoefficientsLoader - Class in org.orekit.models.earth.troposphere
Loads Vienna tropospheric coefficients a given input stream.
ViennaModelCoefficientsLoader(double, double, ViennaModelType) - Constructor for class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader
Constructor with default supported names.
ViennaModelCoefficientsLoader(String, double, double, ViennaModelType) - Constructor for class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader
Constructor with supported names given by user.
ViennaModelCoefficientsLoader(String, double, double, ViennaModelType, DataProvidersManager) - Constructor for class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader
Constructor with supported names and source of mapping function files given by the user.
ViennaModelType - Enum in org.orekit.models.earth.troposphere
Enumerate for Vienna tropospheric model 1 and 3.
ViennaOne - Class in org.orekit.models.earth.troposphere
The Vienna 1 tropospheric delay model for radio techniques.
ViennaOne(ViennaAProvider, AzimuthalGradientProvider, TroposphericModel, TimeScale) - Constructor for class org.orekit.models.earth.troposphere.ViennaOne
Build a new instance.
ViennaOneModel - Class in org.orekit.models.earth.troposphere
Deprecated.
as of 12.1, replaced by ViennaOne
ViennaOneModel(double[], double[]) - Constructor for class org.orekit.models.earth.troposphere.ViennaOneModel
Deprecated.
Build a new instance.
ViennaOneModel(double[], double[], TimeScale) - Constructor for class org.orekit.models.earth.troposphere.ViennaOneModel
Deprecated.
Build a new instance.
ViennaThree - Class in org.orekit.models.earth.troposphere
The Vienna 3 tropospheric delay model for radio techniques.
ViennaThree(ViennaAProvider, AzimuthalGradientProvider, TroposphericModel, TimeScale) - Constructor for class org.orekit.models.earth.troposphere.ViennaThree
Build a new instance.
ViennaThreeModel - Class in org.orekit.models.earth.troposphere
Deprecated.
as of 12.1, replaced by ViennaThree
ViennaThreeModel(double[], double[]) - Constructor for class org.orekit.models.earth.troposphere.ViennaThreeModel
Deprecated.
Build a new instance.
ViennaThreeModel(double[], double[], TimeScale) - Constructor for class org.orekit.models.earth.troposphere.ViennaThreeModel
Deprecated.
Build a new instance.
VisibilityTrigger - Enum in org.orekit.propagation.events
Enumerate for triggering visibility of spherical bodies.
VISIBLE_AS_SOON_AS_PARTIALLY_IN_FOV - org.orekit.propagation.events.VisibilityTrigger
Trigger for bodies that are considered visible as soon as a part touches Field Of View.
VISIBLE_ONLY_WHEN_FULLY_IN_FOV - org.orekit.propagation.events.VisibilityTrigger
Trigger for bodies that are considered visible only when fully inside Field Of View.
VLBI_DELAY - org.orekit.files.ccsds.ndm.tdm.ObservationType
Data: VLBI delay [s].
VM_ABSOLUTE - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
Typical (50th percentile) absolute visual magnitude.
VM_ABSOLUTE - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Typical (50th percentile) visual magnitude.
VM_APPARENT - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
Typical (50th percentile) apparent visual magnitude.
VM_APPARENT - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Typical (50th percentile) apparent visual magnitude.
VM_APPARENT_MAX - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
Maximum apparent visual magnitude.
VM_APPARENT_MAX - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Maximum apparent visual magnitude.
VM_APPARENT_MIN - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
Minimum apparent visual magnitude.
VM_APPARENT_MIN - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Minimum apparent visual magnitude.
VNC - org.orekit.frames.LOFType
Constant for Velocity - Normal - Co-normal frame (X axis aligned with velocity, Y axis aligned with orbital momentum).
VNC_INERTIAL - org.orekit.files.ccsds.definitions.OrbitRelativeFrame
Velocity, Normal, Co-normal coordinate system (X towards velocity, Y towards momentum).
VNC_INERTIAL - org.orekit.frames.LOFType
Constant for Velocity - Normal - Co-normal frame considered inertial (X axis aligned with velocity, Y axis aligned with orbital momentum).
VNC_ROTATING - org.orekit.files.ccsds.definitions.OrbitRelativeFrame
Velocity, Normal, Co-normal coordinate system (X towards velocity, Y towards momentum).
VOLT - Static variable in class org.orekit.utils.units.Unit
Volt unit.
VVLH - org.orekit.frames.LOFType
Constant for Vehicle Velocity, Local Horizontal frame (Z axis aligned with opposite of position, Y axis aligned with opposite of orbital momentum).
VVLH_INERTIAL - org.orekit.frames.LOFType
Constant for Vehicle Velocity, Local Horizontal frame considered inertial (Z axis aligned with opposite of position, Y axis aligned with opposite of orbital momentum).

W

W - org.orekit.gnss.SignalCode
GPS Z - tracking and similar (AS off) / code.
W_PER_KG - Static variable in class org.orekit.files.ccsds.definitions.Units
Watt per kilograms units.
WAAS - org.orekit.files.rinex.navigation.SbasId
Wide Area Augmentation System.
WALKER_INCONSISTENT_PLANES - org.orekit.errors.OrekitMessages
WALKER_INCONSISTENT_PLANES.
WalkerConstellation - Class in org.orekit.orbits
Builder for orbits of satellites forming a Walker constellation.
WalkerConstellation(int, int, int) - Constructor for class org.orekit.orbits.WalkerConstellation
Simple constructor.
WalkerConstellationSlot<O extends Orbit> - Class in org.orekit.orbits
Container for one satellite slot in a Walker constellation.
Wang1988 - Class in org.orekit.models.earth.weather.water
Conversion polynomial from "The Principle of the GPS Precise Positioning System", Wang et al, 1988.
Wang1988() - Constructor for class org.orekit.models.earth.weather.water.Wang1988
 
wasEndTagSeen() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser
Check if XML end tag has been seen.
WATER - Static variable in class org.orekit.models.earth.troposphere.ModifiedSaastamoinenModel
Provider for water pressure.
waterVaporPressure(double, double, double) - Method in class org.orekit.models.earth.weather.water.CIPM2007
Compute water vapor pressure.
waterVaporPressure(double, double, double) - Method in class org.orekit.models.earth.weather.water.NbsNrcSteamTable
Compute water vapor pressure.
waterVaporPressure(double, double, double) - Method in class org.orekit.models.earth.weather.water.Wang1988
Compute water vapor pressure.
waterVaporPressure(double, double, double) - Method in interface org.orekit.models.earth.weather.water.WaterVaporPressureProvider
Compute water vapor pressure.
waterVaporPressure(T, T, T) - Method in class org.orekit.models.earth.weather.water.CIPM2007
Compute water vapor pressure.
waterVaporPressure(T, T, T) - Method in class org.orekit.models.earth.weather.water.NbsNrcSteamTable
Compute water vapor pressure.
waterVaporPressure(T, T, T) - Method in class org.orekit.models.earth.weather.water.Wang1988
Compute water vapor pressure.
waterVaporPressure(T, T, T) - Method in interface org.orekit.models.earth.weather.water.WaterVaporPressureProvider
Compute water vapor pressure.
WaterVaporPressureProvider - Interface in org.orekit.models.earth.weather.water
Interface for converting between relative humidity and water vapor pressure.
WATT - Static variable in class org.orekit.utils.units.Unit
Watt unit.
WAVELENGTH_FACT_L1_2 - org.orekit.files.rinex.section.RinexLabels
Wavelength factors.
WaypointPVBuilder - Class in org.orekit.utils
Builder class, enabling incremental building of an PVCoordinatesProvider instance using waypoints defined on an ellipsoid.
WaypointPVBuilder(WaypointPVBuilder.InterpolationFactory, OneAxisEllipsoid) - Constructor for class org.orekit.utils.WaypointPVBuilder
Create a new instance.
WaypointPVBuilder.InterpolationFactory - Interface in org.orekit.utils
Factory interface, creating the PVCoordinatesProvider instances between the provided waypoints.
WEAK - org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation.StrengthLevel
Weak level of activity.
WeatherModel - Interface in org.orekit.models.earth.weather
Deprecated.
as of 12.1, replaced by PressureTemperatureHumidityProvider
weatherParameters(double, AbsoluteDate) - Method in class org.orekit.models.earth.weather.GlobalPressureTemperature2Model
Deprecated.
 
weatherParameters(double, AbsoluteDate) - Method in class org.orekit.models.earth.weather.GlobalPressureTemperatureModel
Deprecated.
 
weatherParameters(double, AbsoluteDate) - Method in interface org.orekit.models.earth.weather.WeatherModel
Deprecated.
Calculates the weather parameters of the model.
WEIGHTED_RMS - org.orekit.files.ccsds.ndm.cdm.ODParametersKey
The weighted Root Mean Square (RMS) of the residuals from a batch least squares OD.
WEIGHTED_RMS - org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey
Weighted RMS residual ratio.
WET_MASS - org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalPropertiesKey
Total mass at T₀.
WET_MASS - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Total mass at T₀.
WGS84_EARTH_ANGULAR_VELOCITY - Static variable in interface org.orekit.utils.Constants
Earth angular velocity from WGS84 model: 7.292115e-5 rad/s.
WGS84_EARTH_C20 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized second zonal coefficient from WGS84 model: .
WGS84_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Earth equatorial radius from WGS84 model: 6378137.0 m.
WGS84_EARTH_FLATTENING - Static variable in interface org.orekit.utils.Constants
Earth flattening from WGS84 model: 1.0 / 298.257223563.
WGS84_EARTH_MU - Static variable in interface org.orekit.utils.Constants
Earth gravitational constant from WGS84 model: 3.986004418e14 m³/s².
WIDE_AREA - org.orekit.files.rinex.navigation.RegionCode
Wide Area.
WIDE_LANE - org.orekit.estimation.measurements.gnss.CombinationType
Wide-lane combination.
WideLaneCombination - Class in org.orekit.estimation.measurements.gnss
Wide-Lane combination.
WindUp - Class in org.orekit.estimation.measurements.gnss
Modifier for wind-up effect in GNSS phase measurements.
WindUpFactory - Class in org.orekit.estimation.measurements.gnss
Factory for wind-up modifiers.
WindUpFactory() - Constructor for class org.orekit.estimation.measurements.gnss.WindUpFactory
Simple constructor.
withBetaThreshold(double) - Method in class org.orekit.propagation.events.BetaAngleDetector
Create a new instance with the provided beta angle threshold.
withBetaThreshold(T) - Method in class org.orekit.propagation.events.FieldBetaAngleDetector
Create a new instance with the provided beta angle threshold.
withCelestialProvider(FieldPVCoordinatesProvider<T>) - Method in class org.orekit.propagation.events.FieldBetaAngleDetector
Create a new instance with the provided coordinate provider.
withCelestialProvider(PVCoordinatesProvider) - Method in class org.orekit.propagation.events.BetaAngleDetector
Create a new instance with the provided coordinate provider.
withConstantElevation(double) - Method in class org.orekit.propagation.events.ElevationDetector
Setup the minimum elevation for detection.
withConstantElevation(double) - Method in class org.orekit.propagation.events.FieldElevationDetector
Setup the minimum elevation for detection.
withConventions(IERSConventions) - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder
Set up IERS conventions.
withDataContext(DataContext) - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder
Set up data context used to retrieve frames, time scales, etc..
withDefaultInterpolationDegree(int) - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Set up the default interpolation degree.
withDefaultMass(double) - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Set up the default mass.
withDetectionSettings(EventDetectionSettings) - Method in class org.orekit.propagation.events.AbstractDetector
Set up the event detection settings.
withDetectionSettings(FieldEventDetectionSettings<T>) - Method in class org.orekit.propagation.events.FieldAbstractDetector
Set up the event detection settings.
withDoodson(int, int) - Method in class org.orekit.data.PoissonSeriesParser
Set up columns for Doodson multipliers and Doodson number.
withElevationMask(ElevationMask) - Method in class org.orekit.gnss.DOPComputer
Set the elevation mask.
withElevationMask(ElevationMask) - Method in class org.orekit.propagation.events.ElevationDetector
Setup the elevation mask for detection using the passed in mask object.
withElevationMask(ElevationMask) - Method in class org.orekit.propagation.events.FieldElevationDetector
Setup the elevation mask for detection using the passed in mask object.
withEquatorialRadius(double) - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder
Set up the central body equatorial radius.
withFilter(Function<ParseToken, List<ParseToken>>) - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Add a filter for parsed tokens.
withFirstDelaunay(int) - Method in class org.orekit.data.PoissonSeriesParser
Set up first column of Delaunay multiplier.
withFirstPlanetary(int) - Method in class org.orekit.data.PoissonSeriesParser
Set up first column of planetary multiplier.
withFlattening(double) - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder
Set up the central body flattening.
withFunction(Function<FieldSpacecraftState<T>, T>) - Method in class org.orekit.propagation.events.FieldFunctionalDetector
Create a new event detector with a new g function, keeping all other attributes the same.
withFunction(ToDoubleFunction<SpacecraftState>) - Method in class org.orekit.propagation.events.FunctionalDetector
Create a new event detector with a new g function, keeping all other attributes the same.
withGamma(int) - Method in class org.orekit.data.PoissonSeriesParser
Set up column of GMST tide multiplier.
withHandler(EventHandler) - Method in class org.orekit.propagation.events.AbstractDetector
Set up the event handler to call at event occurrences.
withHandler(FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldAbstractDetector
Set up the event handler to call at event occurrences.
withInertialFrame(Frame) - Method in class org.orekit.propagation.events.BetaAngleDetector
Create a new instance with the provided inertial frame.
withInertialFrame(Frame) - Method in class org.orekit.propagation.events.FieldBetaAngleDetector
Create a new instance with the provided inertial frame.
withMargin(double) - Method in class org.orekit.propagation.events.EclipseDetector
Setup a margin to angle detection.
withMargin(double) - Method in class org.orekit.propagation.events.GeographicZoneDetector
Setup the detector margin.
withMargin(T) - Method in class org.orekit.propagation.events.FieldEclipseDetector
Setup a margin to angle detection.
withMaxCheck(double) - Method in class org.orekit.propagation.events.AbstractDetector
Set up the maximum checking interval.
withMaxCheck(double) - Method in class org.orekit.propagation.events.FieldAbstractDetector
Set up the maximum checking interval.
withMaxCheck(AdaptableInterval) - Method in class org.orekit.propagation.events.AbstractDetector
Set up the maximum checking interval.
withMaxCheck(FieldAdaptableInterval<T>) - Method in class org.orekit.propagation.events.FieldAbstractDetector
Set up the maximum checking interval.
withMaxIter(int) - Method in class org.orekit.propagation.events.AbstractDetector
Set up the maximum number of iterations in the event time search.
withMaxIter(int) - Method in class org.orekit.propagation.events.FieldAbstractDetector
Set up the maximum number of iterations in the event time search.
withMinElevation(double) - Method in class org.orekit.gnss.DOPComputer
Set the minimum elevation.
withMinGap(double) - Method in class org.orekit.propagation.events.DateDetector
Setup minimum gap between added dates.
withMinGap(double) - Method in class org.orekit.propagation.events.FieldDateDetector
Setup minimum gap between added dates.
withMissionReferenceDate(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder
Set up mission reference date or Mission Elapsed Time or Mission Relative Time time systems.
withMu(double) - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Set up the gravitational coefficient.
withOptionalColumn(int) - Method in class org.orekit.data.PoissonSeriesParser
Set up optional column.
withParsedUnitsBehavior(ParsedUnitsBehavior) - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Set up the behavior to adopt for handling parsed units.
withPenumbra() - Method in class org.orekit.propagation.events.EclipseDetector
Setup the detector to penumbra detection.
withPenumbra() - Method in class org.orekit.propagation.events.FieldEclipseDetector
Setup the detector to penumbra detection.
withPolynomialPart(char, PolynomialParser.Unit) - Method in class org.orekit.data.PoissonSeriesParser
Set up polynomial part parsing.
withRangeUnitsConverter(RangeUnitsConverter) - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder
Set up the converter for Range Units.
withReferenceFrame(Frame) - Method in class org.orekit.attitudes.Attitude
Get a similar attitude with a specific reference frame.
withReferenceFrame(Frame) - Method in class org.orekit.attitudes.FieldAttitude
Get a similar attitude with a specific reference frame.
withRefraction(AtmosphericRefractionModel) - Method in class org.orekit.propagation.events.ElevationDetector
Setup the elevation detector to use an atmospheric refraction model in its calculations.
withRefraction(AtmosphericRefractionModel) - Method in class org.orekit.propagation.events.FieldElevationDetector
Setup the elevation detector to use an atmospheric refraction model in its calculations.
withSimpleEOP(boolean) - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Set up flag for ignoring tidal effects when interpolating EOP.
withSinCos(int, int, double, int, double) - Method in class org.orekit.data.PoissonSeriesParser
Set up columns of the sine and cosine coefficients.
withSkimmingAltitude(double) - Method in class org.orekit.propagation.events.InterSatDirectViewDetector
Setup the skimming altitude.
withSwitch(int, int) - Method in class org.orekit.models.earth.atmosphere.NRLMSISE00
Change a switch.
withThreshold(double) - Method in class org.orekit.propagation.events.AbstractDetector
Set up the convergence threshold.
withThreshold(T) - Method in class org.orekit.propagation.events.FieldAbstractDetector
Set up the convergence threshold.
withUmbra() - Method in class org.orekit.propagation.events.EclipseDetector
Setup the detector to full umbra detection.
withUmbra() - Method in class org.orekit.propagation.events.FieldEclipseDetector
Setup the detector to full umbra detection.
WMM - org.orekit.models.earth.GeoMagneticFieldFactory.FieldModel
World Magnetic Model.
WORD_SIZE - Static variable in class org.orekit.gnss.rflink.gps.SubFrame
Words size.
write(Appendable, AttitudeEphemerisFile<C, S>) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AttitudeWriter
Write the passed in AttitudeEphemerisFile using the passed in Appendable.
write(Appendable, AttitudeEphemerisFile<C, S>) - Method in interface org.orekit.files.general.AttitudeEphemerisFileWriter
Write the passed in AttitudeEphemerisFile using the passed in Appendable.
write(Appendable, EphemerisFile<C, S>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.EphemerisOcmWriter
Write the passed in EphemerisFile using the passed in Appendable.
write(Appendable, EphemerisFile<C, S>) - Method in class org.orekit.files.ccsds.ndm.odm.oem.EphemerisOemWriter
Write the passed in EphemerisFile using the passed in Appendable.
write(Appendable, EphemerisFile<C, S>) - Method in interface org.orekit.files.general.EphemerisFileWriter
Write the passed in EphemerisFile using the passed in Appendable.
write(Appendable, EphemerisFile<C, S>) - Method in class org.orekit.files.ilrs.CPFWriter
Write the passed in EphemerisFile using the passed in Appendable.
write(String, AttitudeEphemerisFile<C, S>) - Method in interface org.orekit.files.general.AttitudeEphemerisFileWriter
Write the passed in AttitudeEphemerisFile to a file at the output path specified.
write(String, EphemerisFile<C, S>) - Method in interface org.orekit.files.general.EphemerisFileWriter
Write the passed in EphemerisFile to a file at the output path specified.
write(Generator) - Method in class org.orekit.files.ccsds.section.AbstractWriter
Write the section, including surrounding tags.
write(CPFHeader, Appendable, TimeScale) - Method in enum org.orekit.files.ilrs.StreamingCpfWriter.HeaderLineWriter
Write a line.
write(SP3) - Method in class org.orekit.files.sp3.SP3Writer
Write a SP3 file.
writeComment(Generator, String) - Method in class org.orekit.files.ccsds.ndm.NdmWriter
Write a comment line.
writeComments(List<String>) - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Write comment lines.
writeComments(List<String>) - Method in class org.orekit.files.ccsds.utils.generation.KvnGenerator
Write comment lines.
writeComments(List<String>) - Method in class org.orekit.files.ccsds.utils.generation.XmlGenerator
Write comment lines.
writeCompleteFile(RinexObservation) - Method in class org.orekit.files.rinex.observation.RinexObservationWriter
Write a complete observation file.
writeConstituent(Generator, F) - Method in class org.orekit.files.ccsds.ndm.NdmWriter
Write a constituent.
writeContent(Generator) - Method in class org.orekit.files.ccsds.ndm.adm.AdmCommonMetadataWriter
Write the content of the section, excluding surrounding tags.
writeContent(Generator) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParametersWriter
Write the content of the section, excluding surrounding tags.
writeContent(Generator) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadataWriter
Write the content of the section, excluding surrounding tags.
writeContent(Generator) - Method in class org.orekit.files.ccsds.ndm.cdm.ODParametersWriter
Write the content of the section, excluding surrounding tags.
writeContent(Generator) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovarianceWriter
Write the content of the section, excluding surrounding tags.
writeContent(Generator) - Method in class org.orekit.files.ccsds.ndm.cdm.StateVectorWriter
Write the content of the section, excluding surrounding tags.
writeContent(Generator) - Method in class org.orekit.files.ccsds.ndm.odm.CartesianCovarianceWriter
Write the content of the section, excluding surrounding tags.
writeContent(Generator) - Method in class org.orekit.files.ccsds.ndm.odm.CommonMetadataWriter
Write the content of the section, excluding surrounding tags.
writeContent(Generator) - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParametersWriter
Write the content of the section, excluding surrounding tags.
writeContent(Generator) - Method in class org.orekit.files.ccsds.ndm.odm.StateVectorWriter
Write the content of the section, excluding surrounding tags.
writeContent(Generator) - Method in class org.orekit.files.ccsds.ndm.odm.UserDefinedWriter
Write the content of the section, excluding surrounding tags.
writeContent(Generator) - Method in class org.orekit.files.ccsds.section.AbstractWriter
Write the content of the section, excluding surrounding tags.
writeEndOfFile() - Method in class org.orekit.files.ilrs.StreamingCpfWriter
Write end of file.
writeEntry(String, char, boolean) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Write a single key/value entry.
writeEntry(String, char, boolean) - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Write a single key/value entry.
writeEntry(String, double, Unit, boolean) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Write a single key/value entry.
writeEntry(String, double, Unit, boolean) - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Write a single key/value entry.
writeEntry(String, int, boolean) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Write a single key/value entry.
writeEntry(String, int, boolean) - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Write a single key/value entry.
writeEntry(String, Double, Unit, boolean) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Write a single key/value entry.
writeEntry(String, Double, Unit, boolean) - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Write a single key/value entry.
writeEntry(String, Enum<?>, boolean) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Write a single key/value entry.
writeEntry(String, Enum<?>, boolean) - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Write a single key/value entry.
writeEntry(String, String, Unit, boolean) - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Write a single key/value entry.
writeEntry(String, String, Unit, boolean) - Method in class org.orekit.files.ccsds.utils.generation.KvnGenerator
Write a single key/value entry.
writeEntry(String, String, Unit, boolean) - Method in class org.orekit.files.ccsds.utils.generation.XmlGenerator
Write a single key/value entry.
writeEntry(String, List<String>, boolean) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Write a single key/value entry.
writeEntry(String, List<String>, boolean) - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Write a single key/value entry.
writeEntry(String, TimeConverter, AbsoluteDate, boolean, boolean) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Write a single key/value entry.
writeEntry(String, TimeConverter, AbsoluteDate, boolean, boolean) - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Write a single key/value entry.
writeEphemerisLine(TimeStampedPVCoordinates) - Method in class org.orekit.files.ilrs.StreamingCpfWriter.Segment
Write ephemeris lines.
writeFooter(Generator) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter
Write footer for the file.
writeFooter(Generator) - Method in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter
Write footer for the file.
writeFooter(Generator) - Method in interface org.orekit.files.ccsds.utils.generation.MessageWriter
Write footer for the file.
writeHeader() - Method in class org.orekit.files.ilrs.StreamingCpfWriter
Writes the CPF header for the file.
writeHeader(Generator, H) - Method in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter
Write header for the file.
writeHeader(Generator, H) - Method in interface org.orekit.files.ccsds.utils.generation.MessageWriter
Write header for the file.
writeHeader(Generator, CdmHeader) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter
Write header for the file.
writeHeader(RinexObservationHeader) - Method in class org.orekit.files.rinex.observation.RinexObservationWriter
Write header.
writeMessage(Generator, F) - Method in interface org.orekit.files.ccsds.utils.generation.MessageWriter
Write one complete message.
writeMessage(Generator, Ndm) - Method in class org.orekit.files.ccsds.ndm.NdmWriter
Write one complete message.
writeObservationDataSet(ObservationDataSet) - Method in class org.orekit.files.rinex.observation.RinexObservationWriter
Write one observation data set.
writeOneAttributeElement(String, String, String, String) - Method in class org.orekit.files.ccsds.utils.generation.XmlGenerator
Write an element with one attribute.
writePendingRinex2Observations() - Method in class org.orekit.files.rinex.observation.RinexObservationWriter
Write one observation data set in RINEX 2 format.
writePendingRinex34Observations() - Method in class org.orekit.files.rinex.observation.RinexObservationWriter
Write one observation data set in RINEX 3/4 format.
writeRawData(char) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Write raw data.
writeRawData(char) - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Write raw data.
writeRawData(CharSequence) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Write raw data.
writeRawData(CharSequence) - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Write raw data.
WriterBuilder - Class in org.orekit.files.ccsds.ndm
Builder for all CCSDS Message files writers.
WriterBuilder() - Constructor for class org.orekit.files.ccsds.ndm.WriterBuilder
Simple constructor.
WriterBuilder(DataContext) - Constructor for class org.orekit.files.ccsds.ndm.WriterBuilder
Simple constructor.
writeRelativeMetadataContent(Generator, double, CdmRelativeMetadata) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter
Write RelativeMetadata part only once after header.
writeRelativeMetadataContent(Generator, double, CdmRelativeMetadata) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmWriter
 
writeSegment(Generator, CdmSegment) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter
Write one segment.
writeSegment(Generator, S) - Method in class org.orekit.files.ccsds.ndm.odm.oem.EphemerisOemWriter
Write one segment.
writeSegment(Generator, S) - Method in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter
Write one segment.
writeSegment(Generator, S) - Method in interface org.orekit.files.ccsds.utils.generation.MessageWriter
Write one segment.
writeSegmentContent(Generator, double, AemSegment) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemWriter
Write one segment content (without XML wrapping).
writeSegmentContent(Generator, double, OemSegment) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemWriter
Write one segment content (without XML wrapping).
writeSegmentContent(Generator, double, Segment<AcmMetadata, AcmData>) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmWriter
Write one segment content (without XML wrapping).
writeSegmentContent(Generator, double, Segment<AdmMetadata, ApmData>) - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmWriter
Write one segment content (without XML wrapping).
writeSegmentContent(Generator, double, Segment<CdmMetadata, CdmData>) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter
Write one segment content (without XML wrapping).
writeSegmentContent(Generator, double, Segment<CdmMetadata, CdmData>) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmWriter
Write one segment content (without XML wrapping).
writeSegmentContent(Generator, double, Segment<OcmMetadata, OcmData>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmWriter
Write one segment content (without XML wrapping).
writeSegmentContent(Generator, double, Segment<OdmCommonMetadata, OpmData>) - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmWriter
Write one segment content (without XML wrapping).
writeSegmentContent(Generator, double, Segment<OmmMetadata, OmmData>) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmWriter
Write one segment content (without XML wrapping).
writeSegmentContent(Generator, double, Segment<TdmMetadata, ObservationsBlock>) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmWriter
Write one segment content (without XML wrapping).
writeSegmentContent(Generator, double, S) - Method in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter
Write one segment content (without XML wrapping).
writeTwoAttributesElement(String, String, String, String, String, String) - Method in class org.orekit.files.ccsds.utils.generation.XmlGenerator
Write an element with two attributes.
writeUnits(Unit) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Check if unit must be written.
WRONG_COLUMNS_NUMBER - org.orekit.errors.OrekitMessages
WRONG_COLUMNS_NUMBER.
WRONG_COORDINATES_FOR_ADJOINT_EQUATION - org.orekit.errors.OrekitMessages
WRONG_COORDINATES_FOR_ADJOINT_EQUATION.
WRONG_DEGREE_OR_ORDER - org.orekit.errors.OrekitMessages
WRONG_DEGREE_OR_ORDER.
WRONG_ELEMENTS_FOR_AVERAGING_THEORY - org.orekit.errors.OrekitMessages
WRONG ELEMENTS FOR AVERAGING THEORY.
WRONG_EOP_INTERPOLATION_DEGREE - org.orekit.errors.OrekitMessages
WRONG_EOP_INTERPOLATION_DEGREE.
WRONG_INTERPOLATOR_DEFINED_FOR_STATE_INTERPOLATION - org.orekit.errors.OrekitMessages
WRONG_INTERPOLATOR_DEFINED_FOR_STATE_INTERPOLATION.
WRONG_NB_COMPONENTS - org.orekit.errors.OrekitMessages
WRONG_NB_COMPONENTS.
WRONG_ORBIT_PARAMETERS_TYPE - org.orekit.errors.OrekitMessages
WRONG_ORBIT_PARAMETERS_TYPE.
WRONG_PARSING_TYPE - org.orekit.errors.OrekitMessages
WRONG_PARSING_TYPE.

X

X - org.orekit.files.ccsds.ndm.cdm.StateVectorKey
Object Position Vector X component.
X - org.orekit.files.ccsds.ndm.odm.StateVectorKey
Position vector X-component.
X - org.orekit.gnss.SignalCode
GPS L1C (D+P), L2C (M+L) and I+Q / GLONASS I+Q, L1OCd+L1OCp and L2CSI+LO2Cp / Galileo B+C and I+Q / SBAS I+Q / QZSS L1C (D+P), L2C (M+L), I+Q and S+L / Beidou B1 (I+Q), B2b I+Q, B2a Data+Pilot, B3 (I+Q) / IRNSS B+C codes.
X_ANGLE - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Rotation about X axis (only for ADM V1).
X_ANGLE - org.orekit.files.ccsds.ndm.adm.apm.EulerKey
X body rotation angle entry (ADM V1 only).
X_DDOT - org.orekit.files.ccsds.ndm.odm.StateVectorKey
Acceleration vector X-component.
X_DOT - org.orekit.files.ccsds.ndm.cdm.StateVectorKey
Object Velocity Vector X component.
X_DOT - org.orekit.files.ccsds.ndm.odm.StateVectorKey
Velocity vector X-component.
X_RATE - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Rotation about X axis (only for ADM V1).
X_RATE - org.orekit.files.ccsds.ndm.adm.apm.EulerKey
X body rotation rate entry (ADM V1 only).
XEYN - org.orekit.files.ccsds.ndm.tdm.AngleType
X-East, Y-North.
XJ2 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
XJ2.
XJ3 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
XJ3.
XJ4 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
XJ4.
XKE - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
XKE.
xl - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
L from SPTRCK #3.
xl - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
L from SPTRCK #3.
xmdot - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
common parameter for mean anomaly (M) computation.
xmdot - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
common parameter for mean anomaly (M) computation.
XML - org.orekit.files.ccsds.utils.FileFormat
XML format.
XML_1980_FILENAME - Static variable in class org.orekit.frames.FramesFactory
Default regular expression for the EOP XML files (IAU1980 compatibles).
XML_2000_FILENAME - Static variable in class org.orekit.frames.FramesFactory
Default regular expression for the EOP XML files (IAU2000 compatibles).
XmlGenerator - Class in org.orekit.files.ccsds.utils.generation
Generator for eXtended Markup Language CCSDS messages.
XmlGenerator(Appendable, int, String, double, boolean, String) - Constructor for class org.orekit.files.ccsds.utils.generation.XmlGenerator
Simple constructor.
XmlLexicalAnalyzer - Class in org.orekit.files.ccsds.utils.lexical
Lexical analyzer for XML CCSDS messages.
XmlLexicalAnalyzer(DataSource) - Constructor for class org.orekit.files.ccsds.utils.lexical.XmlLexicalAnalyzer
Simple constructor.
XmlStructureKey - Enum in org.orekit.files.ccsds.section
Keys for FileFormat.XML format structure.
XmlStructureProcessingState - Class in org.orekit.files.ccsds.section
ProcessingState for structure of FileFormat.XML CCSDS Messages.
XmlStructureProcessingState(String, AbstractConstituentParser<?, ?, ?>) - Constructor for class org.orekit.files.ccsds.section.XmlStructureProcessingState
Simple constructor.
XmlSubStructureKey - Enum in org.orekit.files.ccsds.ndm.cdm
Keywords for CDM data sub-structure in XML files.
XmlTokenBuilder - Interface in org.orekit.files.ccsds.utils.lexical
Builder for building ParseToken from XML elements.
xn0dp - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
original recovered mean motion.
xn0dp - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
original recovered mean motion.
xnodcf - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
common parameter for raan (OMEGA) computation.
xnodcf - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
common parameter for raan (OMEGA) computation.
xnode - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
final RAAN.
xnode - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
final RAAN.
xnodot - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
common parameter for raan (OMEGA) computation.
xnodot - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
common parameter for raan (OMEGA) computation.
XSYE - org.orekit.files.ccsds.ndm.tdm.AngleType
X-South, Y-East.
XYZ - org.orekit.files.ccsds.ndm.cdm.AltCovarianceType
Lower Triangular Format, specified in XYZ frame.
XYZ - org.orekit.files.sinex.Station.ReferenceSystem
Cartesian reference system X, Y, Z.
XYZCovariance - Class in org.orekit.files.ccsds.ndm.cdm
Container for XYZ covariance matrix data.
XYZCovariance(boolean) - Constructor for class org.orekit.files.ccsds.ndm.cdm.XYZCovariance
Simple constructor.
XYZCovarianceKey - Enum in org.orekit.files.ccsds.ndm.cdm
Keys for CDM covariance matrix entries.

Y

Y - org.orekit.files.ccsds.ndm.cdm.StateVectorKey
Object Position Vector Y component.
Y - org.orekit.files.ccsds.ndm.odm.StateVectorKey
Position vector Y-component.
Y - org.orekit.gnss.SignalCode
GPS Y code.
Y_ANGLE - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Rotation about Y axis (only for ADM V1).
Y_ANGLE - org.orekit.files.ccsds.ndm.adm.apm.EulerKey
Y body rotation angle entry (ADM V1 only).
Y_DDOT - org.orekit.files.ccsds.ndm.odm.StateVectorKey
Acceleration vector Y-component.
Y_DOT - org.orekit.files.ccsds.ndm.cdm.StateVectorKey
Object Velocity Vector Y component.
Y_DOT - org.orekit.files.ccsds.ndm.odm.StateVectorKey
Velocity vector Y-component.
Y_RATE - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Rotation about Y axis (only for ADM V1).
Y_RATE - org.orekit.files.ccsds.ndm.adm.apm.EulerKey
Y body rotation rate entry (ADM V1 only).
YawCompensation - Class in org.orekit.attitudes
This class handles yaw compensation attitude provider.
YawCompensation(Frame, GroundPointing) - Constructor for class org.orekit.attitudes.YawCompensation
Creates a new instance.
YawSteering - Class in org.orekit.attitudes
This class handles yaw steering law.
YawSteering(Frame, GroundPointing, PVCoordinatesProvider, Vector3D) - Constructor for class org.orekit.attitudes.YawSteering
Creates a new instance.
YEAR - Static variable in class org.orekit.utils.units.Unit
Julian year unit.
YES - org.orekit.files.ccsds.definitions.YesNoUnknown
YES value.
YES - org.orekit.files.ccsds.ndm.cdm.Maneuvrable
Maneuvrable.
YES - org.orekit.files.ccsds.ndm.tdm.CorrectionApplied
Corrections have already been applied to the tracking data.
YesNoUnknown - Enum in org.orekit.files.ccsds.definitions
Yes, No, Unknown values for various elements.
yields(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.FieldAdditionalStateProvider
Check if this provider should yield so another provider has an opportunity to add missing parts.
yields(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.integration.FieldAdditionalDerivativesProvider
Check if this provider should yield so another provider has an opportunity to add missing parts.
yields(SpacecraftState) - Method in class org.orekit.forces.maneuvers.jacobians.Duration
Check if this provider should yield so another provider has an opportunity to add missing parts.
yields(SpacecraftState) - Method in class org.orekit.forces.maneuvers.jacobians.MedianDate
Check if this provider should yield so another provider has an opportunity to add missing parts.
yields(SpacecraftState) - Method in class org.orekit.forces.maneuvers.jacobians.TriggerDate
Check if this provider should yield so another provider has an opportunity to add missing parts.
yields(SpacecraftState) - Method in interface org.orekit.propagation.AdditionalStateProvider
Check if this provider should yield so another provider has an opportunity to add missing parts.
yields(SpacecraftState) - Method in interface org.orekit.propagation.integration.AdditionalDerivativesProvider
Check if this provider should yield so another provider has an opportunity to add missing parts.
yields(SpacecraftState) - Method in class org.orekit.propagation.StateCovarianceMatrixProvider
Check if this provider should yield so another provider has an opportunity to add missing parts.
YUMAParser - Class in org.orekit.gnss
This class reads Yuma almanac files and provides GPS almanacs.
YUMAParser(String) - Constructor for class org.orekit.gnss.YUMAParser
Simple constructor.
YUMAParser(String, DataProvidersManager, TimeScales) - Constructor for class org.orekit.gnss.YUMAParser
Create a YUMA loader/parser with the given source for YUMA auxiliary data files.

Z

Z - org.orekit.files.ccsds.ndm.cdm.StateVectorKey
Object Position Vector Z component.
Z - org.orekit.files.ccsds.ndm.odm.StateVectorKey
Position vector Z-component.
Z - org.orekit.gnss.SignalCode
Galileo A+B+C / QZSS L1-SAIF, L5(D+P) and L6(D+E) / Beidou B2b Data+Pilot codes.
Z_ANGLE - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Rotation about Z axis (only for ADM V1).
Z_ANGLE - org.orekit.files.ccsds.ndm.adm.apm.EulerKey
Z body rotation angle entry (ADM V1 only).
Z_DDOT - org.orekit.files.ccsds.ndm.odm.StateVectorKey
Acceleration vector Z-component.
Z_DOT - org.orekit.files.ccsds.ndm.cdm.StateVectorKey
Object Velocity Vector Z component.
Z_DOT - org.orekit.files.ccsds.ndm.odm.StateVectorKey
Velocity vector Z-component.
Z_RATE - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Rotation about Z axis (only for ADM V1).
Z_RATE - org.orekit.files.ccsds.ndm.adm.apm.EulerKey
Z body rotation rate entry (ADM V1 only).
ZeisModel - Class in org.orekit.propagation.semianalytical.dsst.forces
Zeis model for J2-squared second-order terms.
ZeisModel() - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.ZeisModel
Constructor.
ZEL - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
ZEL.
zero() - Method in class org.orekit.utils.DoubleArrayDictionary.Entry
Reset the value to zero.
zero() - Method in class org.orekit.utils.FieldArrayDictionary.Entry
Reset the value to zero.
ZERO - Static variable in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities
0 represented as a polynomial.
ZERO - Static variable in class org.orekit.utils.PVCoordinates
Fixed position/velocity at origin (both p, v and a are zero vectors).
ZERO_CORRECTION - Static variable in class org.orekit.gnss.antenna.FrequencyPattern
Pattern with zero correction (i.e.
ZERO_TIDE - org.orekit.forces.gravity.potential.TideSystem
Constant for zero-tide gravity fields.
ZES - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
ZES.
zIndex(int, int) - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Get the index of an entry in the Z transformation matrix.
ZIP_ARCHIVE_PATTERN - Static variable in interface org.orekit.data.DataProvider
Pattern for name of zip/jar archives.
ZipJarCrawler - Class in org.orekit.data
Helper class for loading data files from a zip/jar archive.
ZipJarCrawler(File) - Constructor for class org.orekit.data.ZipJarCrawler
Build a zip crawler for an archive file on filesystem.
ZipJarCrawler(ClassLoader, String) - Constructor for class org.orekit.data.ZipJarCrawler
Build a zip crawler for an archive file in classpath.
ZipJarCrawler(String) - Constructor for class org.orekit.data.ZipJarCrawler
Build a zip crawler for an archive file in classpath.
ZipJarCrawler(URL) - Constructor for class org.orekit.data.ZipJarCrawler
Build a zip crawler for an archive file on network.
ZNL - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
ZNL.
ZNS - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
ZNS.
A B C D E F G H I J K L M N O P Q R S T U V W X Y Z 
All Classes All Packages