Index (OREKIT 12.0.2 API)

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, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate: Build an instance from an instant in a 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(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) - 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: Base class for phase ambiguity modifier.
AbstractAmbiguityModifier(int, double) - Constructor for class org.orekit.estimation.measurements.modifiers.AbstractAmbiguityModifier: 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.
AbstractBatchLSModel - Class in org.orekit.estimation.leastsquares: Bridge between measurements and least squares problems.
AbstractBatchLSModel(PropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Constructor for class org.orekit.estimation.leastsquares.AbstractBatchLSModel: 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.
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: 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.
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.
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 C_i^j and the S_i^j 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 U_i^j and V_i^j 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 C_i^j and the S_i^j 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 U_i^j and V_i^j 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.
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.
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).
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.
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.
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.
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.
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.
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.
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.
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: 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.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.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: 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.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.SolarRadiationPressure: Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel: Compute acceleration.
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: Meta-data for Attitude Comprehensive Message.
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.
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.
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.
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.
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: 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: 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.
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 represents providers for additional state data beyond SpacecraftState.
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.
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 wich 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(EstimatedTroposphericModel, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel: Add a EstimatedTroposphericModel entry valid after a limit date.
Using addTroposphericModelValidAfter(entry, t) will make entry valid in [t, +∞[ (note the closed bracket).
addTroposphericModelValidBefore(EstimatedTroposphericModel, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel: 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.
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.
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: Builder class for AggregatedPVCoordinatesProvider.
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.
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: Name for ambiguity driver.
AMBIGUITY_NAME - Static variable in class org.orekit.estimation.measurements.gnss.OneWayGNSSPhase: Name for ambiguity driver.
AMBIGUITY_NAME - Static variable in class org.orekit.estimation.measurements.gnss.Phase: Name for ambiguity driver.
AmbiguityAcceptance - Interface in org.orekit.estimation.measurements.gnss: Interface defining ambiguity acceptance tests.
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.
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) - 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 ionospheric 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: Class modifying theoretical angular measurement with tropospheric delay.
AngularTroposphericDelayModifier(DiscreteTroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.AngularTroposphericDelayModifier: Constructor.
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.
ApsideDetector - Class in org.orekit.propagation.events: Finder for apside crossing events.
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: Protected 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.
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 H_f.
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: Keys for covariance history container entries.
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.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: Keys for attitude state history container entries.
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.DeSitterRelativity: Suffix for parameter name for attraction coefficient enabling Jacobian processing.
ATTRACTION_COEFFICIENT_SUFFIX - Static variable in class org.orekit.forces.gravity.SingleBodyAbsoluteAttraction: Suffix for parameter name for attraction coefficient enabling Jacobian processing.
ATTRACTION_COEFFICIENT_SUFFIX - Static variable in class org.orekit.forces.gravity.SingleBodyRelativeAttraction: Suffix for parameter name for attraction coefficient enabling Jacobian processing.
ATTRACTION_COEFFICIENT_SUFFIX - Static variable in class org.orekit.forces.gravity.ThirdBodyAttraction: 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.
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.
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: 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: 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: Bridge between measurements and least squares problems.
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.
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: 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: 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.
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.
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.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.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.
buildAcmParser() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder: Build a parser for Attitude Comprehensive Messages.
buildAcmWriter() - Method in class org.orekit.files.ccsds.ndm.WriterBuilder: Build a writer for Attitude Comprehensive Messages.
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.
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.
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.AbstractFieldIntegratorBuilder: Build a first order integrator.
buildIntegrator(Field<T>, Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.AbstractVariableStepFieldIntegratorBuilder: Build a first order integrator.
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.
buildLeastSquaresModel(PropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Method in class org.orekit.propagation.conversion.BrouwerLyddanePropagatorBuilder: 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.EcksteinHechlerPropagatorBuilder: 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.KeplerianPropagatorBuilder: 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.
buildLeastSquaresModel(PropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Method in class org.orekit.propagation.conversion.TLEPropagatorBuilder: 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(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.
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).
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: Caching wrapper for NormalizedSphericalHarmonicsProvider.
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.
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.
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.
cartesianBuilder(OneAxisEllipsoid) - Static method in class org.orekit.utils.WaypointPVBuilder: Construct a waypoint builder interpolating points using a linear cartesian interpolation.
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: Keys for OPM/OMM/OCM Cartesian covariance entries.
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: ProcessingState for CDM header.
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.
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_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.
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.
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.
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.
CircularOrbit(double, double, double, double, double, double, 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 S_j(k, h) and the C_j(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: C_j(k, h) and S_j(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.
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.
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_ACCURACY_UNIT - Static variable in class org.orekit.files.sp3.SP3Utils: Clock accuracy unit.
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.
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 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.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(CombinationType, MeasurementType, double, double, List<ObservationData>) - Constructor for class org.orekit.estimation.measurements.gnss.CombinedObservationData: Constructor.
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.
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, StaticTransform, StaticTransform) - Static method in interface org.orekit.frames.StaticTransform: 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.
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.
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.AbstractShortTermEncounter2DPOCMethod: 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.AbstractShortTermEncounter2DPOCMethod: 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.
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.
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.
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.
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(SpacecraftState) - Method in class org.orekit.propagation.events.ExtremumApproachDetector: Compute the relative PV between primary and secondary objects.
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.
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 G_s and H_s 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 G_s and H_s 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.
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 Q_n,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 Q_n,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.
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 V_n,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: 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: 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: 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: 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.
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.
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.
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.
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(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.
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.
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.
convertToFieldOrbit(Field<T>, Orbit) - Method in enum org.orekit.orbits.OrbitType: Convert an orbit to the "Fielded" instance type.
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: Create a new instance identical to this one.
copy() - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder: Create a copy of a DSSTPropagatorBuilder object.
copy() - Method in class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder: Create a new instance identical to this one.
copy() - Method in class org.orekit.propagation.conversion.EphemerisPropagatorBuilder: Create a new instance identical to this one.
copy() - Method in class org.orekit.propagation.conversion.KeplerianPropagatorBuilder: Create a new instance identical to this one.
copy() - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder: Create a copy of a NumericalPropagatorBuilder object.
copy() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder: Create a new instance identical to this one.
copy() - Method in class org.orekit.propagation.conversion.TLEPropagatorBuilder: Create a new instance identical to this one.
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: Epoch of the covariance reference frame.
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: Build a new instance.
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.BooleanDetector
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.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.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(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: Build a new instance.
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.FieldBooleanDetector
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.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.FieldLongitudeCrossingDetector: 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(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.
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.
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, T, 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.
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.
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.
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: 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.TimeSpanEstimatedTroposphericModel: Prefix for dates after in the tropospheric parameter drivers' name.
DATE_BEFORE - Static variable in class org.orekit.forces.drag.TimeSpanDragForce: 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.TimeSpanEstimatedTroposphericModel: 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: 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.
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_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_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.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.FieldAbstractDetector: Default cmaximum 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_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.FieldAbstractDetector: 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: 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.FieldAbstractDetector: Default convergence threshold (s).
DEFAULT_THRESHOLD - Static variable in class org.orekit.propagation.events.FieldDateDetector: Default value for convergence threshold.
DEFAULT_TIMEOUT - Static variable in class org.orekit.gnss.metric.ntrip.NtripClient: Default timeout for connections and reads (ms).
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.
dependsOnPositionOnly() - Method in class org.orekit.forces.drag.AbstractDragForceModel: Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.empirical.ParametricAcceleration: Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration: Check if force models depends on position only.
dependsOnPositionOnly() - Method in interface org.orekit.forces.ForceModel: Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.DeSitterRelativity: Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel: Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.LenseThirringRelativity: Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.NewtonianAttraction: Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.OceanTides: Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.Relativity: Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.SingleBodyAbsoluteAttraction: Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.SingleBodyRelativeAttraction: Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.SolidTides: Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.ThirdBodyAttraction: Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.inertia.InertialForces: Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.maneuvers.Maneuver: Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel: Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel: Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel: Check if force models depends on position only.
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 a_f2.
DF083 - org.orekit.gnss.metric.parser.RtcmDataField: GPS a_f1.
DF084 - org.orekit.gnss.metric.parser.RtcmDataField: GPS a_f0.
DF085 - org.orekit.gnss.metric.parser.RtcmDataField: GPS IODC (Issue Of Data, Clock).
DF086 - org.orekit.gnss.metric.parser.RtcmDataField: GPS C_rs.
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 C_uc.
DF090 - org.orekit.gnss.metric.parser.RtcmDataField: GPS Eccentricity (e).
DF091 - org.orekit.gnss.metric.parser.RtcmDataField: GPS C_us.
DF092 - org.orekit.gnss.metric.parser.RtcmDataField: GPS A^1/2.
DF093 - org.orekit.gnss.metric.parser.RtcmDataField: GPS t_oe.
DF094 - org.orekit.gnss.metric.parser.RtcmDataField: GPS C_ic.
DF095 - org.orekit.gnss.metric.parser.RtcmDataField: GPS Ω₀ (OMEGA)₀.
DF096 - org.orekit.gnss.metric.parser.RtcmDataField: GPS C_is.
DF097 - org.orekit.gnss.metric.parser.RtcmDataField: GPS i₀.
DF098 - org.orekit.gnss.metric.parser.RtcmDataField: GPS C_rc.
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 t_GD.
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 (C_n 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 t_k (s).
DF108 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS MSB of B_n word.
DF109 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS P2 Flag.
DF110 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS t_b.
DF111 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS x_n (t_b), first derivative.
DF112 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS x_n (t_b).
DF113 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS x_n (t_b), second derivative.
DF114 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS y_n (t_b), first derivative.
DF115 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS y_n (t_b).
DF116 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS y_n (t_b), second derivative.
DF117 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS z_n (t_b), first derivative.
DF118 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS z_n (t_b).
DF119 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS z_n (t_b), second derivative.
DF120 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS P3 Flag.
DF121 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS γ_n (t_b).
DF122 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS-M P.
DF123 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS-M l_n (third string).
DF124 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS τ_n (t_b).
DF125 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS Δτ_n.
DF126 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS E_n.
DF127 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS-M P4.
DF128 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS-M F_T.
DF129 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS-M N_T.
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 N^A.
DF133 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS τ_c.
DF134 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS-M N₄.
DF135 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS τ_GPS.
DF136 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS-M l_n (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 t_oc.
DF294 - org.orekit.gnss.metric.parser.RtcmDataField: Galileo a_f2.
DF295 - org.orekit.gnss.metric.parser.RtcmDataField: Galileo a_f1.
DF296 - org.orekit.gnss.metric.parser.RtcmDataField: Galileo a_f0.
DF297 - org.orekit.gnss.metric.parser.RtcmDataField: Galileo C_rs.
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 C_uc.
DF301 - org.orekit.gnss.metric.parser.RtcmDataField: Galileo e.
DF302 - org.orekit.gnss.metric.parser.RtcmDataField: Galileo C_us.
DF303 - org.orekit.gnss.metric.parser.RtcmDataField: Galileo A^1/2.
DF304 - org.orekit.gnss.metric.parser.RtcmDataField: Galileo t_oe.
DF305 - org.orekit.gnss.metric.parser.RtcmDataField: Galileo C_ic.
DF306 - org.orekit.gnss.metric.parser.RtcmDataField: Galileo Ω₀.
DF307 - org.orekit.gnss.metric.parser.RtcmDataField: Galileo C_is.
DF308 - org.orekit.gnss.metric.parser.RtcmDataField: Galileo i₀.
DF309 - org.orekit.gnss.metric.parser.RtcmDataField: Galileo C_rc.
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 t_oc.
DF431 - org.orekit.gnss.metric.parser.RtcmDataField: QZSS a_f2.
DF432 - org.orekit.gnss.metric.parser.RtcmDataField: QZSS a_f1.
DF433 - org.orekit.gnss.metric.parser.RtcmDataField: QZSS a_f0.
DF434 - org.orekit.gnss.metric.parser.RtcmDataField: QZSS IODE.
DF435 - org.orekit.gnss.metric.parser.RtcmDataField: QZSS C_rs.
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 C_uc.
DF439 - org.orekit.gnss.metric.parser.RtcmDataField: QZSS e.
DF440 - org.orekit.gnss.metric.parser.RtcmDataField: QZSS C_us.
DF441 - org.orekit.gnss.metric.parser.RtcmDataField: QZSS A^1/2.
DF442 - org.orekit.gnss.metric.parser.RtcmDataField: QZSS t_oe.
DF443 - org.orekit.gnss.metric.parser.RtcmDataField: QZSS C_ic.
DF444 - org.orekit.gnss.metric.parser.RtcmDataField: QZSS Ω₀.
DF445 - org.orekit.gnss.metric.parser.RtcmDataField: QZSS C_is.
DF446 - org.orekit.gnss.metric.parser.RtcmDataField: QZSS i₀.
DF447 - org.orekit.gnss.metric.parser.RtcmDataField: QZSS C_rc.
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 t_GD.
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 t_oc.
DF494 - org.orekit.gnss.metric.parser.RtcmDataField: BDS a_f2.
DF495 - org.orekit.gnss.metric.parser.RtcmDataField: BDS a_f1.
DF496 - org.orekit.gnss.metric.parser.RtcmDataField: BDS a_f0.
DF497 - org.orekit.gnss.metric.parser.RtcmDataField: BDS AODC.
DF498 - org.orekit.gnss.metric.parser.RtcmDataField: BDS C_rs.
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 C_uc.
DF502 - org.orekit.gnss.metric.parser.RtcmDataField: BDS e.
DF503 - org.orekit.gnss.metric.parser.RtcmDataField: BDS C_us.
DF504 - org.orekit.gnss.metric.parser.RtcmDataField: BDS a^1/2.
DF505 - org.orekit.gnss.metric.parser.RtcmDataField: BDS t_oe.
DF506 - org.orekit.gnss.metric.parser.RtcmDataField: BDS C_ic.
DF507 - org.orekit.gnss.metric.parser.RtcmDataField: BDS Ω₀.
DF508 - org.orekit.gnss.metric.parser.RtcmDataField: BDS C_is.
DF509 - org.orekit.gnss.metric.parser.RtcmDataField: BDS i₀.
DF510 - org.orekit.gnss.metric.parser.RtcmDataField: BDS C_rc.
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 t_GD1.
DF514 - org.orekit.gnss.metric.parser.RtcmDataField: BDS t_GD2.
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.
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: Defines a tropospheric model, used to calculate the path delay imposed to electro-magnetic signals between an orbital satellite and a ground station.
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 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.
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(EstimatedMeasurement<?>) - Method in class org.orekit.estimation.measurements.modifiers.AbstractAmbiguityModifier: Modify measurement.
doModify(EstimatedMeasurementBase<?>) - Method in class org.orekit.estimation.measurements.modifiers.AbstractShapiroBaseModifier: Modify measurement.
doModifyWithoutDerivatives(EstimatedMeasurementBase<?>) - Method in class org.orekit.estimation.measurements.modifiers.AbstractAmbiguityModifier: 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.
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.
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.
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.
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).
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: Simple constructor.
DragSensitive - Interface in org.orekit.forces.drag: Interface for spacecraft that are sensitive to atmospheric drag forces.
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.
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: Bridge between measurements and least squares problems.
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.
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 default reference values.
DSSTZonal(UnnormalizedSphericalHarmonicsProvider, int, int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal: Simple 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.
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(FieldAbsoluteDate<T>) - 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_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.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.
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.CircularOrbit: Computes the mean latitude argument from the eccentric latitude argument.
eccentricToMean(double, double, double) - Static method in class org.orekit.orbits.EquinoctialOrbit: Computes the mean longitude argument from the eccentric longitude argument.
eccentricToMean(T, T, T) - Static method in class org.orekit.orbits.FieldCircularOrbit: Computes the mean latitude argument from the eccentric latitude argument.
eccentricToMean(T, T, T) - Static method in class org.orekit.orbits.FieldEquinoctialOrbit: Computes the mean longitude argument from the eccentric longitude argument.
eccentricToTrue(double, double, double) - Static method in class org.orekit.orbits.CircularOrbit: Computes the true latitude argument from the eccentric latitude argument.
eccentricToTrue(double, double, double) - Static method in class org.orekit.orbits.EquinoctialOrbit: Computes the true longitude argument from the eccentric longitude argument.
eccentricToTrue(T, T, T) - Static method in class org.orekit.orbits.FieldCircularOrbit: Computes the true latitude argument from the eccentric latitude argument.
eccentricToTrue(T, T, T) - Static method in class org.orekit.orbits.FieldEquinoctialOrbit: Computes the true longitude argument from the eccentric longitude argument.
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.
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: 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.
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.
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.ImmutableTimeStampedCache: Get an empty immutable cache, cast to the correct type.
emptyCache(Field<CFE>) - Static method in class org.orekit.utils.ImmutableFieldTimeStampedCache: Get an empty immutable cache, cast to the correct type.
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>, 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.
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.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.
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.
EquinoctialOrbit(double, double, double, double, double, double, 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(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.
EstimatedTroposphericModel - Class in org.orekit.models.earth.troposphere: An estimated tropospheric model.
EstimatedTroposphericModel(double, double, MappingFunction, double) - Constructor for class org.orekit.models.earth.troposphere.EstimatedTroposphericModel: Build a new instance using the given environmental conditions.
EstimatedTroposphericModel(MappingFunction, double) - Constructor for class org.orekit.models.earth.troposphere.EstimatedTroposphericModel: 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.
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.
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).
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.
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: Wrap an event detector.
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.FieldRecordAndContinue
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.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.RecordAndContinue
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: Wrap an event detector.
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.
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.
ExtendedPVCoordinatesProvider - Interface in org.orekit.utils: Interface for PV coordinates providers that also support fields.
ExtendedPVCoordinatesProviderAdapter - Class in org.orekit.utils: Adapter from ExtendedPVCoordinatesProvider to TransformProvider.
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.
extractDragSensitiveRange(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.forces.drag.TimeSpanDragForce: Extract a range of the DragSensitive map.
extractParameters(double[], AbsoluteDate) - Method in class org.orekit.forces.drag.TimeSpanDragForce: 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.TimeSpanEstimatedTroposphericModel: 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: 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.TimeSpanEstimatedTroposphericModel: 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(PVCoordinatesProvider) - Constructor for class org.orekit.propagation.events.ExtremumApproachDetector: Constructor with default values.

F

F0 - Static variable in enum org.orekit.gnss.Frequency: Common frequency F0 in MHz (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: Feed the given loader with AbstractSelfFeedingLoader.getDataProvidersManager() and AbstractSelfFeedingLoader.getSupportedNames().
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.
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, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate: Build an instance from an instant in a 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, 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>, 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(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) - 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: 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.
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 represents providers for additional state data beyond SpacecraftState.
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) - 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, 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.
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.
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.
FieldChronologicalComparator<KK extends CalculusFieldElement<KK>> - Class in org.orekit.time: Comparator for FieldTimeStamped instance.
FieldChronologicalComparator() - Constructor for class org.orekit.time.FieldChronologicalComparator: Simple constructor.
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.
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.
FieldCjSjCoefficient<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities: Compute the S_j(k, h) and the C_j(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: C_j(k, h) and S_j(k, h) 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.
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.
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: 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.
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, T, T, T, T, T, T, PositionAngleType, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit: Creates a new instance.
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: Wrap an event detector.
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: Wrap an event detector.
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.
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 Γ^m_n,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(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 G_js, H_js, I_js and J_js 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 G_js, H_js, I_js and J_js polynomials.
FieldGHmsjPolynomials<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities: Compute the G_ms^j and the H_ms^j 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 G_ms^j and H_ms^j 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: Fieldify given orbit with given field.
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.
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, T, T, T, T, T, T, 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.
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.
FieldLegendrePolynomials<T extends CalculusFieldElement<T>> - Class in org.orekit.utils: Computes the P_nm(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 L_n^s(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 L_n^s(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.
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.
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) - 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.
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.
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.
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.
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: Convert a 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, 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: Deprecated.
using this constructor may throw an exception if any given interpolator does not use AbstractFieldTimeInterpolator.DEFAULT_INTERPOLATION_POINTS and AbstractFieldTimeInterpolator.DEFAULT_EXTRAPOLATION_THRESHOLD_SEC. Use FieldSpacecraftStateInterpolator(int, double, Frame, FieldTimeInterpolator, FieldTimeInterpolator, FieldTimeInterpolator, FieldTimeInterpolator, FieldTimeInterpolator) instead.
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(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>, 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.
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(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.
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 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(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 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.
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.
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.
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.
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_ATTACHED - org.orekit.errors.OrekitMessages: FRAME_NOT_ATTACHED.
FrameAdapter - Class in org.orekit.utils: Adapter from Frame to ExtendedPVCoordinatesProvider.
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.
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.
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.FieldAbstractDetector: 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.FieldBooleanDetector
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.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.FieldLongitudeCrossingDetector: 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(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.AbstractDetector: 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.BooleanDetector
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.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.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.
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 Γ^m_n,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.
generateTLE() - Method in class org.orekit.files.ccsds.ndm.odm.omm.Omm: Generate TLE from OMM file.
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: 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.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.FieldDSSTThirdBodyDynamicContext: Get A = sqrt(μ * a).
getA() - Method in class org.orekit.propagation.SpacecraftState: Get the semi-major axis.
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.utils.FieldPVCoordinates: Gets the acceleration.
getAcceleration() - Method in class org.orekit.utils.PVCoordinates: Gets the acceleration.
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.
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.
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 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 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.
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.
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.DSSTThirdBodyDynamicContext: 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: Get direction cosine α for central body.
getAlpha() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements: Get direction cosine α for central body.
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.propagation.events.AltitudeDetector: Get the threshold altitude value.
getAltitude() - Method in class org.orekit.propagation.events.FieldAltitudeDetector: Get the threshold altitude value.
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.
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 n^th 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 A_p geomagnetic indices.
getAp(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation: Get the A_p geomagnetic indices.
getAp(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.NRLMSISE00InputParameters: Get the A_p 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.
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.
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.DragForce: 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 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 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.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 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.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(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 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.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.
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.
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.
getAx2oA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext: Get ax2oA = 2 * a / A .
getAx2oA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext: Get ax2oA = 2 * a / A .
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).
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.YawCompensation: Compute the base system state at given date, without compensation.
getBaseState(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawSteering: Compute the base system state at given date, without compensation.
getBaseState(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawCompensation: Compute the base system state at given date, without compensation.
getBaseState(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawSteering: Compute the base system state at given date, without compensation.
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.DSSTThirdBodyDynamicContext: 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: Get direction cosine β for central body.
getBeta() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements: Get direction cosine β for central body.
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.
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 B_n Word.
getBoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext: 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.DSSTZonalContext: Get B / A.
getBoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext: Get B / A.
getBoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext: Get B / A.
getBoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext: Get B / A.
getBoABpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext: 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.DSSTZonalContext: Get BoABpo = B / A(1 + B).
getBoABpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext: Get BoABpo = B / A(1 + B).
getBoABpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext: Get BoABpo = B / A(1 + B).
getBoABpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext: 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.propagation.events.FieldLatitudeCrossingDetector: 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.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.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.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.
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
getBodyOrientedFrame() - Method in interface org.orekit.bodies.CelestialBody: Get a body oriented, body centered frame.
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.
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.
getBuilders() - Method in class org.orekit.estimation.sequential.KalmanModel: Getter for the propagators.
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 C_2n,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.
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.
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.DSSTTesseralContext: Get Χ = 1 / sqrt(1 - e²) = 1 / B.
getChi() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext: Get Χ = 1 / sqrt(1 - e²) = 1 / B.
getChi2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext: Get Χ².
getChi2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext: Get Χ².
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 C_i^j.
getCij(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FourierCjSjCoefficients: Get the coefficient C_i^j.
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 C_j coefficient.
getCj(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient: Get the C_j 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: Get the realtime-derived receiver clock offset.
getClockAcceleration() - Method in class org.orekit.files.rinex.clock.RinexClock.ClockDataLine: Getter for the clock acceleration.
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.
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.DSSTTesseralContext: 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.FieldDSSTTesseralContext: 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(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: Get the value of the combined frequency in MHz.
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.
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.
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.KalmanModel: 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.
getCorrectedMeasurement() - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel: 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.KalmanModel: 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.
getCorrectedSpacecraftStates() - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel: 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.
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.KalmanModel: 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.
getCurrentDate() - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel: 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.KalmanModel: 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.
getCurrentMeasurementNumber() - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel: 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.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.DateTimeComponents: Get the date component.
getDate() - Method in class org.orekit.time.FieldAbsoluteDate: 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.
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 dC_j / dh coefficient.
getDcjDh(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient: Get the dC_j / dh coefficient.
getDcjDk(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient: Get the dC_j / dk coefficient.
getDcjDk(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient: Get the dC_j / 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.
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).
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(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenTesseralLinear: Compute the value of the derivative dK_j^{-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 dK₀^{n, 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 dK_j^{-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 dK₀^{n, 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.
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.
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 dG_js / dα coefficient.
getdGjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Get the dG_js / dα coefficient.
getdGjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials: Get the dG_js / dβ coefficient.
getdGjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Get the dG_js / dβ coefficient.
getdGjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials: Get the dG_js / dh coefficient.
getdGjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Get the dG_js / dh coefficient.
getdGjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials: Get the dG_js / dk coefficient.
getdGjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Get the dG_js / dk coefficient.
getdGmsdAlpha(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials: Get the dG_ms^j / d_α coefficient.
getdGmsdAlpha(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials: Get the dG_ms^j / d_α coefficient.
getdGmsdBeta(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials: Get the dG_ms^j / d_β coefficient.
getdGmsdBeta(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials: Get the dG_ms^j / d_β coefficient.
getdGmsdh(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials: Get the dG_ms^j / d_h coefficient.
getdGmsdh(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials: Get the dG_ms^j / d_h coefficient.
getdGmsdk(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials: Get the dG_ms^j / d_k coefficient.
getdGmsdk(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials: Get the dG_ms^j / d_k coefficient.
getdHjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials: Get the dH_js / dα coefficient.
getdHjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Get the dH_js / dα coefficient.
getdHjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials: Get the dH_js / dβ coefficient.
getdHjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Get the dH_js / dβ coefficient.
getdHjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials: Get the dH_js / dh coefficient.
getdHjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Get the dH_js / dh coefficient.
getdHjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials: Get the dH_js / dk coefficient.
getdHjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Get the dH_js / dk coefficient.
getdHmsdAlpha(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials: Get the dH_ms^j / d_α coefficient.
getdHmsdAlpha(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials: Get the dH_ms^j / d_α coefficient.
getdHmsdBeta(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials: Get the dH_ms^j / d_β coefficient.
getdHmsdBeta(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials: Get the dH_ms^j / d_β coefficient.
getdHmsdh(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials: Get the dH_ms^j / d_h coefficient.
getdHmsdh(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials: Get the dH_ms^j / d_h coefficient.
getdHmsdk(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials: Get the dH_ms^j / d_k coefficient.
getdHmsdk(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials: Get the dH_ms^j / d_k 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 dI_js / dα coefficient.
getdIjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Get the dI_js / dα coefficient.
getdIjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials: Get the dI_js / dβ coefficient.
getdIjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Get the dI_js / dβ coefficient.
getdIjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials: Get the dI_js / dh coefficient.
getdIjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Get the dI_js / dh coefficient.
getdIjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials: Get the dI_js / dk coefficient.
getdIjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Get the dI_js / dk coefficient.
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.
getdJjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials: Get the dJ_js / dα coefficient.
getdJjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Get the dJ_js / dα coefficient.
getdJjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials: Get the dJ_js / dβ coefficient.
getdJjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Get the dJ_js / dβ coefficient.
getdJjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials: Get the dJ_js / dh coefficient.
getdJjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Get the dJ_js / dh coefficient.
getdJjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials: Get the dJ_js / dk coefficient.
getdJjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Get the dJ_js / dk coefficient.
getdLnsdGamma(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldLnsCoefficients: Get the value of dL_n^s / dγ (γ).
getdLnsdGamma(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.LnsCoefficients: Get the value of dL_n^s / 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 D_n^l(Χ).
getDnl(T, T, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.UpperBounds: Get the upper bound value D_n^l(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: Get the DragSensitive model valid at a date.
getDragSensitiveSpan(AbsoluteDate) - Method in class org.orekit.forces.drag.TimeSpanDragForce: 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: 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.
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 dS_j / dh coefficient.
getDsjDh(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient: Get the dS_j / dh coefficient.
getDsjDk(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient: Get the dS_j / dk coefficient.
getDsjDk(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient: Get the dS_j / 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.
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.
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.
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.
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.
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 E_n 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(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.
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 derivative.
getEquinoctialEx() - Method in class org.orekit.orbits.CircularOrbit: Get the first component of the equinoctial eccentricity vector derivative.
getEquinoctialEx() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the first component of the equinoctial eccentricity vector derivative.
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 derivative.
getEquinoctialEx() - Method in class org.orekit.orbits.Orbit: Get the first component of the equinoctial eccentricity vector derivative.
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.
getEquinoctialExDot() - Method in class org.orekit.orbits.CircularOrbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.FieldCartesianOrbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.FieldOrbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.KeplerianOrbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.Orbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.CartesianOrbit: Get the second component of the equinoctial eccentricity vector derivative.
getEquinoctialEy() - Method in class org.orekit.orbits.CircularOrbit: Get the second component of the equinoctial eccentricity vector derivative.
getEquinoctialEy() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the second component of the equinoctial eccentricity vector derivative.
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 derivative.
getEquinoctialEy() - Method in class org.orekit.orbits.Orbit: Get the second component of the equinoctial eccentricity vector derivative.
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.
getEquinoctialEyDot() - Method in class org.orekit.orbits.CircularOrbit: Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldCartesianOrbit: Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldOrbit: Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.KeplerianOrbit: Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.Orbit: Get the second component of the equinoctial eccentricity vector.
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.KalmanModel: Get the current corrected estimate.
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.
getEstimate() - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel: 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.KalmanModel: 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.
getEstimatedMeasurementsParameters() - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel: 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.KalmanModel: 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.
getEstimatedOrbitalParameters() - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel: 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.KalmanModel: 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.
getEstimatedPropagationParameters() - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel: 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.
getEstimatedPropagators() - Method in class org.orekit.estimation.sequential.KalmanModel: Get the propagators estimated with the values set in the propagators builders.
getEstimatedPropagators() - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel: Get the propagators estimated with the values set in the propagators builders.
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.
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.forces.drag.TimeSpanDragForce: 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 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(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.
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
getFieldAuxiliaryElements() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldForceModelContext: Method to get the auxiliary elementsrelated to the ForceModelContext.
getFieldDate() - Method in class org.orekit.frames.FieldTransform: Get the date.
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.forces.drag.TimeSpanDragForce: 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 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
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.
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).
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.
getFirstSpan() - Method in class org.orekit.forces.drag.TimeSpanDragForce: 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.TimeSpanEstimatedTroposphericModel: 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.
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.
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.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.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 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(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.
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 F_T 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.DSSTThirdBodyDynamicContext: 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: Get direction cosine γ for central body.
getGamma() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements: Get direction cosine γ for central body.
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.
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.
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.
getGjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials: Get the G_js coefficient.
getGjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Get the G_js 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.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 G_ms^j coefficient.
getGmsj(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials: Get the G_ms^j 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.
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.
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.
getGradientConverter() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester: Get the gradient converter related to the analytical orbit propagator.
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 X_ell (i.e.
getHalfApertureAlongY() - Method in class org.orekit.geometry.fov.EllipticalFieldOfView: get the FOV half aperture angle for spreading along Y_ell (i.e.
getHaloOrbitalPeriod(double) - Method in class org.orekit.orbits.RichardsonExpansion: Return the orbital period of the Halo Orbit.
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 H_js coefficient.
getHjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Get the H_js 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 H_ms^j coefficient.
getHmsj(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials: Get the H_ms^j 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.StaticTransform: Get the identity static 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 I_js coefficient.
getIjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Get the I_js 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.
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.GroundReceiverCommonParametersWithDerivatives: 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.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.
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.
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.
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.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.
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.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.
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.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.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.
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.
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.
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 J_js coefficient.
getJjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Get the J_js 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.
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.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.
getLastObservedDate() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader: Gets the day (at data start) of the last observed data entry.
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.
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.
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).
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.
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.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).
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 l_n 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 L_n^s(γ).
getLns(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.LnsCoefficients: Get the value of L_n^s(γ).
getLNThirdString() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Get the GLONASS l_n 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
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.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.
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).
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.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: Get m2aoA = -2 * a / A.
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: Get m2aoA = -2 * a / A.
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.
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.DSSTPropagatorBuilder: Get the mass.
getMass() - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder: 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.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.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.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.
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.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 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 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.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.
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.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 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 interface org.orekit.propagation.events.FieldEventDetector: Get maximal number of iterations in the event time search.
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.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: Get mCo2AB = -C / 2AB.
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: Get mCo2AB = -C / 2AB.
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 da_i / dt.
getMeanElementRate(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: Computes the mean equinoctial elements rates da_i / dt.
getMeanElementRate(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel: Computes the mean equinoctial elements rates da_i / dt.
getMeanElementRate(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTJ2SquaredClosedForm: Computes the mean equinoctial elements rates da_i / dt.
getMeanElementRate(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction: Computes the mean equinoctial elements rates da_i / dt.
getMeanElementRate(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral: Computes the mean equinoctial elements rates da_i / dt.
getMeanElementRate(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody: Computes the mean equinoctial elements rates da_i / dt.
getMeanElementRate(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal: Computes the mean equinoctial elements rates da_i / 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 da_i / dt.
getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: Computes the mean equinoctial elements rates da_i / dt.
getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel: Computes the mean equinoctial elements rates da_i / dt.
getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTJ2SquaredClosedForm: Computes the mean equinoctial elements rates da_i / dt.
getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction: Computes the mean equinoctial elements rates da_i / dt.
getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral: Computes the mean equinoctial elements rates da_i / dt.
getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody: Computes the mean equinoctial elements rates da_i / dt.
getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal: Computes the mean equinoctial elements rates da_i / 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.DSSTTesseralContext: 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.DSSTZonalContext: 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.FieldDSSTTesseralContext: 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.forces.FieldDSSTZonalContext: 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: Get the value of the frequency in MHz.
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.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.DateComponents: Get the modified julian day.
getMJD() - Method in class org.orekit.time.UTCTAIOffset: Get the date of the start of the leap as Modified Julian Day.
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: Get μ / a .
getMoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext: Get μ / a .
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.
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.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.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.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.DSSTZonalContext: Get μ / a .
getMuoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext: Get 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 N^A 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.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.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 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 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.BDTScale: Get the name time scale.
getName() - Method in class org.orekit.time.GalileoScale: 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.GPSScale: Get the name time scale.
getName() - Method in class org.orekit.time.IRNSSScale: Get the name time scale.
getName() - Method in class org.orekit.time.QZSSScale: 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.TAIScale: 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.TTScale: 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: Get number of states for AdMethodType.EKF, AdMethodType.BATCH or AdMethodType.FILTER_SMOOTHER.
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>) - Method in class org.orekit.utils.ImmutableFieldTimeStampedCache: Get the entries surrounding a central date.
getNeighborsSize() - Method in interface org.orekit.utils.FieldTimeStampedCache: Get the fixed size of the lists returned by FieldTimeStampedCache.getNeighbors(FieldAbsoluteDate).
getNeighborsSize() - Method in class org.orekit.utils.ImmutableFieldTimeStampedCache: Get the fixed size of the lists returned by FieldTimeStampedCache.getNeighbors(FieldAbsoluteDate).
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.
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.
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: Create a NormalizedSphericalHarmonicsProvider from an UnnormalizedSphericalHarmonicsProvider.
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.
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.
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.time.OffsetModel: Offset at reference date in seconds (TAI minus UTC).
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.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.
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.
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.DSSTTesseralContext: Get 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.DSSTZonalContext: Get ooAB = 1 / (A * B).
getOoAB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext: 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.FieldDSSTZonalContext: 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.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.
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.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.
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.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.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: 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: 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: 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: 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: 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.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.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.SingleBodyAbsoluteAttraction: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.SingleBodyRelativeAttraction: 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.gravity.ThirdBodyAttraction: 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.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.EstimatedTroposphericModel: 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.MariniMurrayModel: 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.ModifiedSaastamoinenModel: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.ViennaOneModel: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.ViennaThreeModel: 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.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.KalmanModel: 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.
getPhysicalEstimatedCovarianceMatrix() - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel: 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.KalmanModel: 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.
getPhysicalEstimatedState() - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel: 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.KalmanModel: 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.
getPhysicalInnovationCovarianceMatrix() - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel: 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.KalmanModel: 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.
getPhysicalKalmanGain() - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel: 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.KalmanModel: 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).
getPhysicalMeasurementJacobian() - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel: 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.KalmanModel: 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.
getPhysicalStateTransitionMatrix() - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel: 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.
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 P_nm.
getPnm(int, int) - Method in class org.orekit.utils.LegendrePolynomials: Return the coefficient P_nm.
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.frames.TopocentricFrame: 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 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.
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.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.KalmanModel: 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.
getPredictedMeasurement() - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel: 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.KalmanModel: 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.
getPredictedSpacecraftStates() - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel: 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.GlobalPressureTemperature2Model: Returns the pressure at the station [hPa].
getPressure() - Method in class org.orekit.models.earth.weather.GlobalPressureTemperatureModel: Get the atmospheric pressure of the station depending its position.
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.
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.
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: Get an unmodifiable view of the propagators map.
getPropagators() - Method in class org.orekit.propagation.PropagatorsParallelizer: Get an unmodifiable list of the underlying mono-satellite propagators.
getPropulsionModel() - Method in class org.orekit.forces.maneuvers.Maneuver: Get the propulsion model.
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.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.
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.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.AbstractPropagator: 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 class org.orekit.propagation.integration.IntegratedEphemeris: Get the PVCoordinates of the body in the selected frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.numerical.NumericalPropagator: 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 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(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 class org.orekit.propagation.FieldAbstractPropagator: Get the FieldPVCoordinates of the body in the selected frame.
getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris: Get the FieldPVCoordinates of the body in the selected frame.
getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator: 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.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.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.
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.
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.
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(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.
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 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.
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.
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.
getRemainingDv() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties: Get the total ΔV remaining for spacecraft.
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 R^ε_n,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 R^ε_n,m,l(γ).
getRoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext: Get roa = R / a.
getRoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext: Get roa = R / a.
getRoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext: Get roa = R / a.
getRoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext: 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 class org.orekit.frames.FieldTransform: 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.
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.
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 N_a 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.
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.
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.
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 S_i^j.
getSij(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FourierCjSjCoefficients: Get the coefficient S_i^j.
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 S_j coefficient.
getSj(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient: Get the S_j 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: Create a new Marini-Murray model using a standard atmosphere model.
getStandardModel(double) - 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.GroundReceiverCommonParametersWithDerivatives: Get spacecraft state.
getState() - Method in class org.orekit.estimation.measurements.GroundReceiverCommonParametersWithoutDerivatives: 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.
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
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.
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.
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.
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.GroundPointing: 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.
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.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(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawCompensation: Compute the target point position/velocity in specified frame.
getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawSteering: 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.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.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawCompensation: Compute the target point position/velocity in specified frame.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawSteering: Compute the target point position/velocity in specified frame.
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.GroundReceiverCommonParametersWithDerivatives: Get downlink delay.
getTauD() - Method in class org.orekit.estimation.measurements.GroundReceiverCommonParametersWithoutDerivatives: 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.GlobalPressureTemperature2Model: Returns the temperature at the station [K].
getTemperature() - Method in class org.orekit.models.earth.weather.GlobalPressureTemperatureModel: Get the atmospheric temperature of the station depending its position.
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.
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.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 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 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.
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.
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.
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.
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.
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.GroundReceiverCommonParametersWithDerivatives: Get transit position/velocity.
getTransitPV() - Method in class org.orekit.estimation.measurements.GroundReceiverCommonParametersWithoutDerivatives: Get transit position/velocity.
getTransitState() - Method in class org.orekit.estimation.measurements.GroundReceiverCommonParametersWithDerivatives: Get transit state.
getTransitState() - Method in class org.orekit.estimation.measurements.GroundReceiverCommonParametersWithoutDerivatives: 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.TimeSpanEstimatedTroposphericModel: 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.
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 U₁^j for Fourier index i.
getU1(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.UijVijCoefficients: Get the coefficient U₁^j for Fourier index i.
getU2(int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldUijVijCoefficients: Get the coefficient U₂^j for Fourier index = 1 (i == 0).
getU2(int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.UijVijCoefficients: Get the coefficient U₂^j 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.SpinStabilized: Get the underlying attitude provider.
getUnderlyingAttitudeProvider() - Method in class org.orekit.attitudes.YawCompensation: Get the underlying (ground pointing) attitude provider.
getUnderlyingAttitudeProvider() - Method in class org.orekit.attitudes.YawSteering: Get the underlying (ground pointing) 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.
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: Create an UnnormalizedSphericalHarmonicsProvider from a NormalizedSphericalHarmonicsProvider.
getUnnormalizedSnm(int, int) - Method in interface org.orekit.forces.gravity.potential.UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics: Get a spherical harmonic sine coefficient.
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 V₁^j for Fourier index i.
getV1(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.UijVijCoefficients: Get the coefficient V₁^j for Fourier index i.
getV2(int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldUijVijCoefficients: Get the coefficient V₂^j for Fourier index = 1 (i == 0).
getV2(int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.UijVijCoefficients: Get the coefficient V₂^j 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.
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 K_j^{-n-1, s}.
getValue(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenThirdBodyLinear: Compute the value of the Hansen coefficient K₀^{n, 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 P_l^v,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 P_l^v,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 K_j^{-n-1, s}.
getValue(int, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenThirdBodyLinear: Compute the value of the Hansen coefficient K₀^{n, 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 P_l^v,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 class org.orekit.frames.FieldTransform: 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 V_n,s^m coefficient from V_n,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.GlobalPressureTemperature2Model: Returns the water vapor pressure at the station [hPa].
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 enum org.orekit.gnss.Frequency: 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.
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: Get Χ = 1 / sqrt(1 - e²) = 1 / B.
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: Get Χ = 1 / sqrt(1 - e²) = 1 / B.
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 x_p parameter.
getXp() - Method in class org.orekit.frames.PoleCorrection: Get the x_p 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: Get Χ².
getXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext: Get Χ².
getXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext: Get Χ².
getXXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext: Get Χ³.
getXXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext: Get Χ³.
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 y_p parameter.
getYp() - Method in class org.orekit.frames.PoleCorrection: Get the y_p 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).
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.
GHIJjsPolynomials - Class in org.orekit.propagation.semianalytical.dsst.utilities: Compute the G_js, H_js, I_js and J_js 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 G_js, H_js, I_js and J_js polynomials.
GHmsjPolynomials - Class in org.orekit.propagation.semianalytical.dsst.utilities: Compute the G_ms^j and the H_ms^j 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 G_ms^j and H_ms^j 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.
GlobalPressureTemperature2Model - Class in org.orekit.models.earth.weather: The Global Pressure and Temperature 2 (GPT2) model.
GlobalPressureTemperature2Model(double, double, Geoid) - Constructor for class org.orekit.models.earth.weather.GlobalPressureTemperature2Model: Constructor with default supported names.
GlobalPressureTemperature2Model(String, double, double, Geoid) - Constructor for class org.orekit.models.earth.weather.GlobalPressureTemperature2Model: Constructor with supported names given by user.
GlobalPressureTemperature2Model(String, double, double, Geoid, DataProvidersManager, TimeScale) - Constructor for class org.orekit.models.earth.weather.GlobalPressureTemperature2Model: Constructor with supported names and source of GPT2 auxiliary data given by user.
GlobalPressureTemperatureModel - Class in org.orekit.models.earth.weather: The Global Pressure and Temperature model.
GlobalPressureTemperatureModel(double, double, Frame) - Constructor for class org.orekit.models.earth.weather.GlobalPressureTemperatureModel: Build a new instance.
GlobalPressureTemperatureModel(double, double, Frame, DataContext) - Constructor for class org.orekit.models.earth.weather.GlobalPressureTemperatureModel: 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 by 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.
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.
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.
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: 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(Frame) - Static method in enum org.orekit.files.ccsds.definitions.CelestialBodyFrame: Guesses names from ODM Table 5-3 and Annex A.
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: ProcessingState for NDM header.
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.
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.
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.
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.
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.
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<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.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>, 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.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 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 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(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.
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(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.
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.
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.
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.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.TimeStampedDoubleHermiteInterpolator: 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.
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: Constructor.
InterSatellitesPhaseAmbiguityModifier - Class in org.orekit.estimation.measurements.modifiers: Class modifying theoretical inter-satellites phase measurement with ambiguity.
InterSatellitesPhaseAmbiguityModifier(int, double) - Constructor for class org.orekit.estimation.measurements.modifiers.InterSatellitesPhaseAmbiguityModifier: 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: 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.
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.
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.
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 P_l^v,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.
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

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).
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.
KeplerianOrbit(double, double, double, double, double, double, 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.
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.
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 P_nm(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.
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.
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 L_n^s(γ).
LnsCoefficients(int, int, double[][], SortedMap<CoefficientsFactory.NSKey, Double>, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.LnsCoefficients: Create a set of L_n^s(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.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.
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.
LoveNumbers - Class in org.orekit.utils: Container for Love numbers.
LoveNumbers(double[][], double[][], double[][]) - Constructor for class org.orekit.utils.LoveNumbers: Simple constructor.
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: Epoch of the maneuver reference frame.
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: This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(double, GeodeticPoint, AbsoluteDate) - Method in interface org.orekit.models.earth.troposphere.MappingFunction: 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: With the Mendes Pavlis tropospheric model, the mapping function is not split into hydrostatic and wet component.
mappingFactors(double, GeodeticPoint, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.NiellMappingFunctionModel: This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(double, GeodeticPoint, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.ViennaOneModel: This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(double, GeodeticPoint, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.ViennaThreeModel: 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: This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(T, FieldGeodeticPoint<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.models.earth.troposphere.MappingFunction: 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: With the Mendes Pavlis tropospheric model, the mapping function is not split into hydrostatic and wet component.
mappingFactors(T, FieldGeodeticPoint<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(T, FieldGeodeticPoint<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.ViennaOneModel: 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.ViennaThreeModel: This method allows the computation of the hydrostatic and wet mapping functions.
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: Interface for mapping functions used in the tropospheric delay computation.
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.
MariniMurrayModel - Class in org.orekit.models.earth.troposphere: The Marini-Murray tropospheric delay model for laser ranging.
MariniMurrayModel(double, double, double, double) - Constructor for class org.orekit.models.earth.troposphere.MariniMurrayModel: 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.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).
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.CircularOrbit: Computes the eccentric latitude argument from the mean latitude argument.
meanToEccentric(double, double, double) - Static method in class org.orekit.orbits.EquinoctialOrbit: Computes the eccentric longitude argument from the mean longitude argument.
meanToEccentric(T, T, T) - Static method in class org.orekit.orbits.FieldCircularOrbit: Computes the eccentric latitude argument from the mean latitude argument.
meanToEccentric(T, T, T) - Static method in class org.orekit.orbits.FieldEquinoctialOrbit: Computes the eccentric longitude argument from the mean 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.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.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: 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.
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).
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.
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: Create a new Saastamoinen model for the troposphere using the given environmental conditions and table from the reference book.
ModifiedSaastamoinenModel(double, double, double, String) - Constructor for class org.orekit.models.earth.troposphere.ModifiedSaastamoinenModel: Create a new Saastamoinen model for the troposphere using the given environmental conditions.
ModifiedSaastamoinenModel(double, double, double, 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: Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<OneWayGNSSPhase>) - Method in class org.orekit.estimation.measurements.modifiers.OneWayGNSSPhaseAmbiguityModifier: Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<Phase>) - Method in class org.orekit.estimation.measurements.modifiers.PhaseAmbiguityModifier
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: Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<T>, ParameterDriversProvider, AbstractGradientConverter, GroundStation, ParametricModelEffect, ParametricModelEffectGradient) - Static method in class org.orekit.estimation.measurements.modifiers.RangeRateModifierUtil: Apply a modifier to an estimated measurement.
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
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<InterSatellitesPhase>) - Method in class org.orekit.estimation.measurements.modifiers.InterSatellitesPhaseAmbiguityModifier: 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: 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<Phase>) - Method in class org.orekit.estimation.measurements.modifiers.PhaseAmbiguityModifier
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>, GroundStation, ParametricModelEffect) - Static method in class org.orekit.estimation.measurements.modifiers.RangeModifierUtil: Apply a modifier to an estimated measurement.
modifyWithoutDerivatives(EstimatedMeasurementBase<T>, GroundStation, ParametricModelEffect) - 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_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.
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_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.
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.
newBundle(String, Locale, String, ClassLoader, boolean) - Method in class org.orekit.errors.OrekitMessages.UTF8Control
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.
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: 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.
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.
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.
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: Meta-data for Orbit Comprehensive Message.
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(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(Frame) - Static method in class org.orekit.attitudes.FrameAlignedProvider: Creates an attitude provider aligned with the given frame.
of(AbsoluteDate, Rotation) - Static method in interface org.orekit.frames.StaticTransform: Create a new static transform from a rotation and zero 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(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>, 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(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(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.BDTScale: Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.GalileoScale: 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.GPSScale: Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.IRNSSScale: Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.QZSSScale: 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.TAIScale: 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.TTScale: 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.BDTScale: Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.GalileoScale: 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.GPSScale: Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.IRNSSScale: Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.QZSSScale: 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.TAIScale: 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.TTScale: 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.BDTScale: Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.GalileoScale: 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.GPSScale: Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.IRNSSScale: Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.QZSSScale: 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 class org.orekit.time.TAIScale: 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.TTScale: 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.
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.
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.
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.
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.
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.
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: Simple constructor.
OneWayGNSSPhaseAmbiguityModifier - Class in org.orekit.estimation.measurements.modifiers: Class modifying theoretical one-way GNSS phase measurement with ambiguity.
OneWayGNSSPhaseAmbiguityModifier(int, double) - Constructor for class org.orekit.estimation.measurements.modifiers.OneWayGNSSPhaseAmbiguityModifier: 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: 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.
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.
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: Keys for covariance history container entries.
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.
OrekitMessages.UTF8Control - Class in org.orekit.errors: Control class loading properties in UTF-8 encoding.
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.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.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.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.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.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.
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.
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.
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.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(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: 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: 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.FixedTroposphericDelay: 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.MariniMurrayModel: 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: 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.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.TimeSpanEstimatedTroposphericModel: 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: 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.ViennaThreeModel: Calculates the tropospheric 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.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(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: 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: 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.FixedTroposphericDelay: 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.MariniMurrayModel: 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: 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.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.TimeSpanEstimatedTroposphericModel: 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: 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.ViennaThreeModel: Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
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.
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: Simple constructor.
PHASE_MINUS_CODE - org.orekit.estimation.measurements.gnss.CombinationType: Phase minus code combination.
PhaseAmbiguityModifier - Class in org.orekit.estimation.measurements.modifiers: Class modifying theoretical phase measurement with ambiguity.
PhaseAmbiguityModifier(int, double) - Constructor for class org.orekit.estimation.measurements.modifiers.PhaseAmbiguityModifier: 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: 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.
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.
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: 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.
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.
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.
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].
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.
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.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.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.
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.
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) - 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).
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.
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.
RadiationSensitive - Interface in org.orekit.forces.radiation: Interface for spacecraft that are sensitive to radiation pressure forces.
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: 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: 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.
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.
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.
relativeMetadataData - org.orekit.files.ccsds.ndm.cdm.XmlSubStructureKey: Relative Metadata section.
relativeStateVector - org.orekit.files.ccsds.ndm.cdm.XmlSubStructureKey: Relative Metadata section.
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.
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.
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.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, 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.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.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, 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.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.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.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 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(FieldEventDetector<T>, FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.events.handlers.FieldEventHandler: 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.
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 an 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.
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.
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: Step handler picking up measurements for both SemiAnalyticalUnscentedKalmanEstimator and SemiAnalyticalKalmanEstimator.
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: Interface for both SemiAnalyticalUnscentedKalmanModel and SemiAnalyticalKalmanModel.
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.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 B_n 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: Set the realtime-derived receiver clock offset.
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.
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.
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 E_n 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.
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 F_T 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 l_n Word extracted from fifth string of the subframe.
setLNThirdString(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Set the GLONASS l_n 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.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.DSSTPropagatorBuilder: Set the initial mass.
setMass(double) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder: 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.
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 N^A 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: Set number of states for AdMethodType.EKF, AdMethodType.BATCH or AdMethodType.FILTER_SMOOTHER.
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.
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.
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.
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.
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.
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.
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.
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.
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(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.
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.
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: Rate random walk if AttitudeDeterminationKey.RATE_STATES is RateElementsType.GYRO_BIAS.
SIGMA_V - org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationKey: Angle random walk if AttitudeDeterminationKey.RATE_STATES is RateElementsType.GYRO_BIAS.
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(TimeStampedFieldPVCoordinates<T>, FieldVector3D<T>, FieldAbsoluteDate<T>) - 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: 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: Deprecated.
replaced by SingleParameterFitter(double, double, int, double...)
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.
SmallManeuverAnalyticalModel(SpacecraftState, 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_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.
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_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: String representation of the center of ephemeris coordinate system.
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, 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: Deprecated.
using this constructor may throw an exception if any given interpolator does not use AbstractTimeInterpolator.DEFAULT_INTERPOLATION_POINTS and AbstractTimeInterpolator.DEFAULT_EXTRAPOLATION_THRESHOLD_SEC. Use SpacecraftStateInterpolator(int, double, Frame, TimeInterpolator, TimeInterpolator, TimeInterpolator, TimeInterpolator, TimeInterpolator) instead.
SPAN - org.orekit.files.rinex.navigation.SbasId: Southern Positioning Augmentation System.
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<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).
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: Constructs a STKEphemerisFile.STKEphemerisSegment instance.
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.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).
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.
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: 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.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.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.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.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.
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: Time span atmospheric drag force model.
TimeSpanDragForce(Atmosphere, DragSensitive) - Constructor for class org.orekit.forces.drag.TimeSpanDragForce: 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: Constructor.
TimeSpanEstimatedTroposphericModel - Class in org.orekit.models.earth.troposphere: Time span estimated tropospheric model.
TimeSpanEstimatedTroposphericModel(EstimatedTroposphericModel) - Constructor for class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel: Constructor with default UTC time scale.
TimeSpanEstimatedTroposphericModel(EstimatedTroposphericModel, TimeScale) - Constructor for class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel: 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: time-stamped version of AngularCoordinates.
TimeStampedAngularCoordinates(AbsoluteDate, FieldRotation) - 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.
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: time-stamped version of FieldAngularCoordinates.
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) - 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: time-stamped version of FieldPVCoordinates.
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) - 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: time-stamped version of PVCoordinates.
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) - 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, 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.
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.
toFieldPVCoordinatesProvider(Field<T>) - Method in interface org.orekit.utils.ExtendedPVCoordinatesProvider: Convert to a FieldPVCoordinatesProvider with a specific type.
toGeodetic(S2Point) - Method in class org.orekit.models.earth.tessellation.EllipsoidTessellator: Convert a point on the unit 2-sphere to geodetic coordinates.
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_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.
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.
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.BDTScale
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.GalileoScale
toString() - Method in class org.orekit.time.GLONASSScale
toString() - Method in class org.orekit.time.GMSTScale
toString() - Method in class org.orekit.time.GPSScale
toString() - Method in class org.orekit.time.IRNSSScale
toString() - Method in class org.orekit.time.QZSSScale
toString() - Method in class org.orekit.time.SatelliteClockScale
toString() - Method in class org.orekit.time.TAIScale
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.TTScale
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.
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.EstimatedTroposphericModel: 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: Convert to TimeStampedPVCoordinates.
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: Epoch of the trajectory reference frame.
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: Keys for rajectory state history container entries.
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, 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.
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].
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.CircularOrbit: Computes the eccentric latitude argument from the true latitude argument.
trueToEccentric(double, double, double) - Static method in class org.orekit.orbits.EquinoctialOrbit: Computes the eccentric longitude argument from the true longitude argument.
trueToEccentric(T, T, T) - Static method in class org.orekit.orbits.FieldCircularOrbit: Computes the eccentric latitude argument from the true latitude argument.
trueToEccentric(T, T, T) - Static method in class org.orekit.orbits.FieldEquinoctialOrbit: Computes the eccentric longitude argument from the true 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: 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<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_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.
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 by 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.
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.
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.
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(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.
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.
UTF8Control() - Constructor for class org.orekit.errors.OrekitMessages.UTF8Control: Empty constructor.
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.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.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.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.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.
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_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.
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.
ViennaOneModel - Class in org.orekit.models.earth.troposphere: The Vienna1 tropospheric delay model for radio techniques.
ViennaOneModel(double[], double[]) - Constructor for class org.orekit.models.earth.troposphere.ViennaOneModel: Build a new instance.
ViennaOneModel(double[], double[], TimeScale) - Constructor for class org.orekit.models.earth.troposphere.ViennaOneModel: Build a new instance.
ViennaThreeModel - Class in org.orekit.models.earth.troposphere: The Vienna3 tropospheric delay model for radio techniques.
ViennaThreeModel(double[], double[]) - Constructor for class org.orekit.models.earth.troposphere.ViennaThreeModel: Build a new instance.
ViennaThreeModel(double[], double[], TimeScale) - Constructor for class org.orekit.models.earth.troposphere.ViennaThreeModel: 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.
wasEndTagSeen() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser: Check if XML end tag has been seen.
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: Defines a surface meteorology model that can be used to compute the different weather parameters (pressure, temperature, ...).
weatherParameters(double, AbsoluteDate) - Method in class org.orekit.models.earth.weather.GlobalPressureTemperature2Model
weatherParameters(double, AbsoluteDate) - Method in class org.orekit.models.earth.weather.GlobalPressureTemperatureModel
weatherParameters(double, AbsoluteDate) - Method in interface org.orekit.models.earth.weather.WeatherModel: 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.
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.
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: Setup the event handler to call at event occurrences.
withHandler(FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldAbstractDetector: Setup the event handler to call at event occurrences.
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: Setup the maximum checking interval.
withMaxCheck(double) - Method in class org.orekit.propagation.events.FieldAbstractDetector: Setup the maximum checking interval.
withMaxCheck(AdaptableInterval) - Method in class org.orekit.propagation.events.AbstractDetector: Setup the maximum checking interval.
withMaxCheck(FieldAdaptableInterval<T>) - Method in class org.orekit.propagation.events.FieldAbstractDetector: Setup the maximum checking interval.
withMaxIter(int) - Method in class org.orekit.propagation.events.AbstractDetector: Setup the maximum number of iterations in the event time search.
withMaxIter(int) - Method in class org.orekit.propagation.events.FieldAbstractDetector: Setup 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: Setup the convergence threshold.
withThreshold(T) - Method in class org.orekit.propagation.events.FieldAbstractDetector: Setup 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_DEGREE_OR_ORDER - org.orekit.errors.OrekitMessages: WRONG_DEGREE_OR_ORDER.
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.

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