Uses of Class
org.orekit.estimation.measurements.ObservableSatellite
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Packages that use ObservableSatellite Package Description org.orekit.estimation.measurements The measurements package defines everything that is related to orbit determination measurements.org.orekit.estimation.measurements.generation This package provides Orbit Determination measurements generation.org.orekit.estimation.measurements.gnss This package provides methods to handle GNSS measurements. -
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Uses of ObservableSatellite in org.orekit.estimation.measurements
Methods in org.orekit.estimation.measurements that return types with arguments of type ObservableSatellite Modifier and Type Method Description List<ObservableSatellite>
AbstractMeasurement. getSatellites()
Get the satellites related to this measurement.List<ObservableSatellite>
ObservedMeasurement. getSatellites()
Get the satellites related to this measurement.Constructors in org.orekit.estimation.measurements with parameters of type ObservableSatellite Constructor Description AngularAzEl(GroundStation station, AbsoluteDate date, double[] angular, double[] sigma, double[] baseWeight, ObservableSatellite satellite)
Simple constructor.AngularRaDec(GroundStation station, Frame referenceFrame, AbsoluteDate date, double[] angular, double[] sigma, double[] baseWeight, ObservableSatellite satellite)
Simple constructor.BistaticRange(GroundStation emitter, GroundStation receiver, AbsoluteDate date, double range, double sigma, double baseWeight, ObservableSatellite satellite)
Simple constructor.BistaticRangeRate(GroundStation emitter, GroundStation receiver, AbsoluteDate date, double rangeRate, double sigma, double baseWeight, ObservableSatellite satellite)
Simple constructor.FDOA(GroundStation primeStation, GroundStation secondStation, double centreFrequency, AbsoluteDate date, double fdoa, double sigma, double baseWeight, ObservableSatellite satellite)
Simple constructor.GroundReceiverMeasurement(GroundStation station, boolean twoWay, AbsoluteDate date, double[] observed, double[] sigma, double[] baseWeight, ObservableSatellite satellite)
Simple constructor.GroundReceiverMeasurement(GroundStation station, boolean twoWay, AbsoluteDate date, double observed, double sigma, double baseWeight, ObservableSatellite satellite)
Simple constructor.InterSatellitesRange(ObservableSatellite local, ObservableSatellite remote, boolean twoWay, AbsoluteDate date, double range, double sigma, double baseWeight)
Simple constructor.Position(AbsoluteDate date, Vector3D position, double[][] covarianceMatrix, double baseWeight, ObservableSatellite satellite)
Constructor with full covariance matrix and all inputs.Position(AbsoluteDate date, Vector3D position, double[] sigmaPosition, double baseWeight, ObservableSatellite satellite)
Constructor with one vector for the standard deviation.Position(AbsoluteDate date, Vector3D position, double sigmaPosition, double baseWeight, ObservableSatellite satellite)
Constructor with one double for the standard deviation.PV(AbsoluteDate date, Vector3D position, Vector3D velocity, double[][] positionCovarianceMatrix, double[][] velocityCovarianceMatrix, double baseWeight, ObservableSatellite satellite)
Constructor with 2 smaller covariance matrices.PV(AbsoluteDate date, Vector3D position, Vector3D velocity, double[][] covarianceMatrix, double baseWeight, ObservableSatellite satellite)
Constructor with full covariance matrix and all inputs.PV(AbsoluteDate date, Vector3D position, Vector3D velocity, double[] sigmaPosition, double[] sigmaVelocity, double baseWeight, ObservableSatellite satellite)
Constructor with two vectors for the standard deviations.PV(AbsoluteDate date, Vector3D position, Vector3D velocity, double[] sigmaPV, double baseWeight, ObservableSatellite satellite)
Constructor with one vector for the standard deviations.PV(AbsoluteDate date, Vector3D position, Vector3D velocity, double sigmaPosition, double sigmaVelocity, double baseWeight, ObservableSatellite satellite)
Constructor with two double for the standard deviations.Range(GroundStation station, boolean twoWay, AbsoluteDate date, double range, double sigma, double baseWeight, ObservableSatellite satellite)
Simple constructor.RangeRate(GroundStation station, AbsoluteDate date, double rangeRate, double sigma, double baseWeight, boolean twoway, ObservableSatellite satellite)
Simple constructor.TDOA(GroundStation primeStation, GroundStation secondStation, AbsoluteDate date, double tdoa, double sigma, double baseWeight, ObservableSatellite satellite)
Simple constructor.TurnAroundRange(GroundStation primaryStation, GroundStation secondaryStation, AbsoluteDate date, double turnAroundRange, double sigma, double baseWeight, ObservableSatellite satellite)
Simple constructor.Constructor parameters in org.orekit.estimation.measurements with type arguments of type ObservableSatellite Constructor Description AbstractMeasurement(AbsoluteDate date, double[] observed, double[] sigma, double[] baseWeight, List<ObservableSatellite> satellites)
Simple constructor, for multi-dimensional measurements.AbstractMeasurement(AbsoluteDate date, double observed, double sigma, double baseWeight, List<ObservableSatellite> satellites)
Simple constructor for mono-dimensional measurements. -
Uses of ObservableSatellite in org.orekit.estimation.measurements.generation
Methods in org.orekit.estimation.measurements.generation that return ObservableSatellite Modifier and Type Method Description ObservableSatellite
Generator. addPropagator(Propagator propagator)
Add a propagator.ObservableSatellite[]
AbstractMeasurementBuilder. getSatellites()
Get the satellites related to this measurement.ObservableSatellite[]
MeasurementBuilder. getSatellites()
Get the satellites related to this measurement.ObservableSatellite[]
MultiplexedMeasurementBuilder. getSatellites()
Get the satellites related to this measurement.Methods in org.orekit.estimation.measurements.generation with parameters of type ObservableSatellite Modifier and Type Method Description Propagator
Generator. getPropagator(ObservableSatellite satellite)
Get a registered propagator.Method parameters in org.orekit.estimation.measurements.generation with type arguments of type ObservableSatellite Modifier and Type Method Description EstimatedMeasurementBase<T>
AbstractMeasurementBuilder. build(AbsoluteDate date, Map<ObservableSatellite,OrekitStepInterpolator> interpolators)
Generate a single measurement.EstimatedMeasurementBase<T>
MeasurementBuilder. build(AbsoluteDate date, Map<ObservableSatellite,OrekitStepInterpolator> interpolators)
Generate a single measurement.EstimatedMeasurementBase<MultiplexedMeasurement>
MultiplexedMeasurementBuilder. build(AbsoluteDate date, Map<ObservableSatellite,OrekitStepInterpolator> interpolators)
Generate a single measurement.protected abstract T
AbstractMeasurementBuilder. buildObserved(AbsoluteDate date, Map<ObservableSatellite,OrekitStepInterpolator> interpolators)
Build a dummy observed measurement.protected AngularAzEl
AngularAzElBuilder. buildObserved(AbsoluteDate date, Map<ObservableSatellite,OrekitStepInterpolator> interpolators)
Build a dummy observed measurement.protected AngularRaDec
AngularRaDecBuilder. buildObserved(AbsoluteDate date, Map<ObservableSatellite,OrekitStepInterpolator> interpolators)
Build a dummy observed measurement.protected BistaticRange
BistaticRangeBuilder. buildObserved(AbsoluteDate date, Map<ObservableSatellite,OrekitStepInterpolator> interpolators)
Build a dummy observed measurement.protected BistaticRangeRate
BistaticRangeRateBuilder. buildObserved(AbsoluteDate date, Map<ObservableSatellite,OrekitStepInterpolator> interpolators)
Build a dummy observed measurement.protected FDOA
FDOABuilder. buildObserved(AbsoluteDate date, Map<ObservableSatellite,OrekitStepInterpolator> interpolators)
Build a dummy observed measurement.protected InterSatellitesOneWayRangeRate
InterSatellitesOneWayRangeRateBuilder. buildObserved(AbsoluteDate date, Map<ObservableSatellite,OrekitStepInterpolator> interpolators)
Build a dummy observed measurement.protected InterSatellitesPhase
InterSatellitesPhaseBuilder. buildObserved(AbsoluteDate date, Map<ObservableSatellite,OrekitStepInterpolator> interpolators)
Build a dummy observed measurement.protected InterSatellitesRange
InterSatellitesRangeBuilder. buildObserved(AbsoluteDate date, Map<ObservableSatellite,OrekitStepInterpolator> interpolators)
Build a dummy observed measurement.protected OneWayGNSSPhase
OneWayGNSSPhaseBuilder. buildObserved(AbsoluteDate date, Map<ObservableSatellite,OrekitStepInterpolator> interpolators)
Build a dummy observed measurement.protected OneWayGNSSRange
OneWayGNSSRangeBuilder. buildObserved(AbsoluteDate date, Map<ObservableSatellite,OrekitStepInterpolator> interpolators)
Build a dummy observed measurement.protected OneWayGNSSRangeRate
OneWayGNSSRangeRateBuilder. buildObserved(AbsoluteDate date, Map<ObservableSatellite,OrekitStepInterpolator> interpolators)
Build a dummy observed measurement.protected Position
PositionBuilder. buildObserved(AbsoluteDate date, Map<ObservableSatellite,OrekitStepInterpolator> interpolators)
Build a dummy observed measurement.protected PV
PVBuilder. buildObserved(AbsoluteDate date, Map<ObservableSatellite,OrekitStepInterpolator> interpolators)
Build a dummy observed measurement.protected Range
RangeBuilder. buildObserved(AbsoluteDate date, Map<ObservableSatellite,OrekitStepInterpolator> interpolators)
Build a dummy observed measurement.protected RangeRate
RangeRateBuilder. buildObserved(AbsoluteDate date, Map<ObservableSatellite,OrekitStepInterpolator> interpolators)
Build a dummy observed measurement.protected TDOA
TDOABuilder. buildObserved(AbsoluteDate date, Map<ObservableSatellite,OrekitStepInterpolator> interpolators)
Build a dummy observed measurement.protected TurnAroundRange
TurnAroundRangeBuilder. buildObserved(AbsoluteDate date, Map<ObservableSatellite,OrekitStepInterpolator> interpolators)
Build a dummy observed measurement.SortedSet<EstimatedMeasurementBase<T>>
AbstractScheduler. generate(Map<ObservableSatellite,OrekitStepInterpolator> interpolators)
Generate a sequence of measurements.SortedSet<EstimatedMeasurementBase<T>>
Scheduler. generate(Map<ObservableSatellite,OrekitStepInterpolator> interpolators)
Generate a sequence of measurements.Constructors in org.orekit.estimation.measurements.generation with parameters of type ObservableSatellite Constructor Description AbstractMeasurementBuilder(CorrelatedRandomVectorGenerator noiseSource, double[] sigma, double[] baseWeight, ObservableSatellite... satellites)
Simple constructor.AbstractMeasurementBuilder(CorrelatedRandomVectorGenerator noiseSource, double sigma, double baseWeight, ObservableSatellite... satellites)
Simple constructor.AngularAzElBuilder(CorrelatedRandomVectorGenerator noiseSource, GroundStation station, double[] sigma, double[] baseWeight, ObservableSatellite satellite)
Simple constructor.AngularRaDecBuilder(CorrelatedRandomVectorGenerator noiseSource, GroundStation station, Frame referenceFrame, double[] sigma, double[] baseWeight, ObservableSatellite satellite)
Simple constructor.BistaticRangeBuilder(CorrelatedRandomVectorGenerator noiseSource, GroundStation emitter, GroundStation receiver, double sigma, double baseWeight, ObservableSatellite satellite)
Simple constructor.BistaticRangeRateBuilder(CorrelatedRandomVectorGenerator noiseSource, GroundStation emitter, GroundStation receiver, double sigma, double baseWeight, ObservableSatellite satellite)
Simple constructor.FDOABuilder(CorrelatedRandomVectorGenerator noiseSource, GroundStation primeStation, GroundStation secondStation, double centreFrequency, double sigma, double baseWeight, ObservableSatellite satellite)
Simple constructor.InterSatellitesOneWayRangeRateBuilder(CorrelatedRandomVectorGenerator noiseSource, ObservableSatellite local, ObservableSatellite remote, double sigma, double baseWeight)
Simple constructor.InterSatellitesPhaseBuilder(CorrelatedRandomVectorGenerator noiseSource, ObservableSatellite local, ObservableSatellite remote, double wavelength, double sigma, double baseWeight, AmbiguityCache cache)
Simple constructor.InterSatellitesRangeBuilder(CorrelatedRandomVectorGenerator noiseSource, ObservableSatellite local, ObservableSatellite remote, boolean twoWay, double sigma, double baseWeight)
Simple constructor.OneWayGNSSPhaseBuilder(CorrelatedRandomVectorGenerator noiseSource, ObservableSatellite local, ObservableSatellite remote, double wavelength, double sigma, double baseWeight, AmbiguityCache cache)
Simple constructor.OneWayGNSSRangeBuilder(CorrelatedRandomVectorGenerator noiseSource, ObservableSatellite local, ObservableSatellite remote, double sigma, double baseWeight)
Simple constructor.OneWayGNSSRangeRateBuilder(CorrelatedRandomVectorGenerator noiseSource, ObservableSatellite local, ObservableSatellite remote, double sigma, double baseWeight)
Simple constructor.PositionBuilder(CorrelatedRandomVectorGenerator noiseSource, double sigma, double baseWeight, ObservableSatellite satellite)
Simple constructor.PVBuilder(CorrelatedRandomVectorGenerator noiseSource, double sigmaPosition, double sigmaVelocity, double baseWeight, ObservableSatellite satellite)
Simple constructor.RangeBuilder(CorrelatedRandomVectorGenerator noiseSource, GroundStation station, boolean twoWay, double sigma, double baseWeight, ObservableSatellite satellite)
Simple constructor.RangeRateBuilder(CorrelatedRandomVectorGenerator noiseSource, GroundStation station, boolean twoWay, double sigma, double baseWeight, ObservableSatellite satellite)
Simple constructor.TDOABuilder(CorrelatedRandomVectorGenerator noiseSource, GroundStation primeStation, GroundStation secondStation, double sigma, double baseWeight, ObservableSatellite satellite)
Simple constructor.TurnAroundRangeBuilder(CorrelatedRandomVectorGenerator noiseSource, GroundStation primaryStation, GroundStation secondaryStation, double sigma, double baseWeight, ObservableSatellite satellite)
Simple constructor. -
Uses of ObservableSatellite in org.orekit.estimation.measurements.gnss
Method parameters in org.orekit.estimation.measurements.gnss with type arguments of type ObservableSatellite Modifier and Type Method Description protected Phase
PhaseBuilder. buildObserved(AbsoluteDate date, Map<ObservableSatellite,OrekitStepInterpolator> interpolators)
Build a dummy observed measurement.Constructors in org.orekit.estimation.measurements.gnss with parameters of type ObservableSatellite Constructor Description AbstractInterSatellitesMeasurement(AbsoluteDate date, double observed, double sigma, double baseWeight, ObservableSatellite local, ObservableSatellite remote)
Constructor.AbstractOneWayGNSSMeasurement(PVCoordinatesProvider remotePV, QuadraticClockModel remoteClock, AbsoluteDate date, double range, double sigma, double baseWeight, ObservableSatellite local)
Simple constructor.InterSatellitesOneWayRangeRate(ObservableSatellite local, ObservableSatellite remote, AbsoluteDate date, double rangeRate, double sigma, double baseWeight)
Constructor.InterSatellitesPhase(ObservableSatellite local, ObservableSatellite remote, AbsoluteDate date, double phase, double wavelength, double sigma, double baseWeight, AmbiguityCache cache)
Constructor.OneWayGNSSPhase(PVCoordinatesProvider remote, String remoteName, QuadraticClockModel remoteClock, AbsoluteDate date, double phase, double wavelength, double sigma, double baseWeight, ObservableSatellite local, AmbiguityCache cache)
Simple constructor.OneWayGNSSRange(PVCoordinatesProvider remote, double dtRemote, AbsoluteDate date, double range, double sigma, double baseWeight, ObservableSatellite local)
Simple constructor.OneWayGNSSRange(PVCoordinatesProvider remote, QuadraticClockModel remoteClock, AbsoluteDate date, double range, double sigma, double baseWeight, ObservableSatellite local)
Simple constructor.OneWayGNSSRangeRate(PVCoordinatesProvider remote, double dtRemote, AbsoluteDate date, double rangeRate, double sigma, double baseWeight, ObservableSatellite local)
Simple constructor.OneWayGNSSRangeRate(PVCoordinatesProvider remote, QuadraticClockModel remoteClock, AbsoluteDate date, double rangeRate, double sigma, double baseWeight, ObservableSatellite local)
Simple constructor.Phase(GroundStation station, AbsoluteDate date, double phase, double wavelength, double sigma, double baseWeight, ObservableSatellite satellite, AmbiguityCache cache)
Simple constructor.PhaseBuilder(CorrelatedRandomVectorGenerator noiseSource, GroundStation station, double wavelength, double sigma, double baseWeight, ObservableSatellite satellite, AmbiguityCache cache)
Simple constructor.Constructor parameters in org.orekit.estimation.measurements.gnss with type arguments of type ObservableSatellite Constructor Description AbstractOnBoardMeasurement(AbsoluteDate date, double observed, double sigma, double baseWeight, List<ObservableSatellite> satellites)
Constructor.
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