Uses of Class
org.orekit.estimation.measurements.ObservableSatellite

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.

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
AbstractRangeRelatedMeasurement(Observer observer, AbsoluteDate date, double value, double sigma, double baseWeight, boolean twoWay, SignalTravelTimeModel signalTravelTimeModel, ObservableSatellite satellite)	Simple constructor.
AngularAzEl(GroundStation station, AbsoluteDate date, double[] angular, double[] sigma, double[] baseWeight, ObservableSatellite satellite)	Simple constructor.
AngularAzEl(GroundStation station, AbsoluteDate date, double[] angular, double[] sigma, double[] baseWeight, SignalTravelTimeModel signalTravelTimeModel, ObservableSatellite satellite)	Simple constructor.
AngularMeasurement(AbsoluteDate date, double[] angular, double[] sigma, double[] baseWeight, SignalTravelTimeModel signalTravelTimeModel, ObservableSatellite satellite)	Simple constructor.
AngularRaDec(Observer observer, Frame referenceFrame, AbsoluteDate date, double[] angular, double[] sigma, double[] baseWeight, ObservableSatellite satellite)	Simple constructor using default light time delay.
AngularRaDec(Observer observer, Frame referenceFrame, AbsoluteDate date, double[] angular, double[] sigma, double[] baseWeight, SignalTravelTimeModel signalTravelTimeModel, ObservableSatellite satellite)	Constructor.
BistaticRange(Observer emitter, Observer receiver, AbsoluteDate date, double range, double sigma, double baseWeight, ObservableSatellite satellite)	Simple constructor.
BistaticRange(Observer emitter, Observer receiver, AbsoluteDate date, double range, double sigma, double baseWeight, SignalTravelTimeModel signalTravelTimeModel, ObservableSatellite satellite)	Simple constructor.
BistaticRangeRate(Observer emitter, Observer receiver, AbsoluteDate date, double rangeRate, double sigma, double baseWeight, ObservableSatellite satellite)	Simple constructor.
BistaticRangeRate(Observer emitter, Observer receiver, AbsoluteDate date, double rangeRate, double sigma, double baseWeight, SignalTravelTimeModel signalTravelTimeModel, ObservableSatellite satellite)	Simple constructor.
FDOA(Observer primeObserver, Observer secondObserver, double centreFrequency, AbsoluteDate date, double fdoa, double sigma, double baseWeight, ObservableSatellite satellite)	Constructor with default signal travel time model.
FDOA(Observer primeObserver, Observer secondObserver, double centreFrequency, AbsoluteDate date, double fdoa, double sigma, double baseWeight, SignalTravelTimeModel signalTravelTimeModel, ObservableSatellite satellite)	Constructor.
InterSatellitesRange(ObservableSatellite local, ObservableSatellite remote, boolean twoWay, AbsoluteDate date, double range, double sigma, double baseWeight)	Simple constructor.
InterSatellitesRange(ObservableSatellite local, ObservableSatellite remote, boolean twoWay, AbsoluteDate date, double range, double sigma, double baseWeight, SignalTravelTimeModel signalTravelTimeModel)	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.
Position(AbsoluteDate date, Vector3D position, MeasurementQuality measurementQuality, ObservableSatellite satellite)	Constructor with full covariance matrix and all inputs.
PseudoMeasurement(AbsoluteDate date, double[] observed, MeasurementQuality measurementQuality, ObservableSatellite satellite)	Constructor with full covariance matrix and all inputs.
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.
PV(AbsoluteDate date, Vector3D position, Vector3D velocity, MeasurementQuality measurementQuality, ObservableSatellite satellite)	Constructor with full covariance matrix and all inputs.
Range(Observer observer, boolean twoWay, AbsoluteDate date, double range, double sigma, double baseWeight, ObservableSatellite satellite)	Simple constructor.
RangeRate(Observer observer, AbsoluteDate date, double rangeRate, double sigma, double baseWeight, boolean twoWay, ObservableSatellite satellite)	Simple constructor.
RangeRate(Observer observer, AbsoluteDate date, double rangeRate, double sigma, double baseWeight, boolean twoWay, SignalTravelTimeModel signalTravelTimeModel, ObservableSatellite satellite)	Simple constructor.
TDOA(Observer primeObserver, Observer secondObserver, AbsoluteDate date, double tdoa, double sigma, double baseWeight, ObservableSatellite satellite)	Constructor.
TDOA(Observer primeObserver, Observer secondObserver, AbsoluteDate date, double tdoa, double sigma, double baseWeight, SignalTravelTimeModel signalTravelTimeModel, ObservableSatellite satellite)	Constructor.
TurnAroundRange(Observer primaryObserver, Observer secondaryObserver, AbsoluteDate date, double turnAroundRange, double sigma, double baseWeight, ObservableSatellite satellite)	Simple constructor.
TurnAroundRange(Observer primaryObserver, Observer secondaryObserver, AbsoluteDate date, double turnAroundRange, double sigma, double baseWeight, SignalTravelTimeModel signalTravelTimeModel, ObservableSatellite satellite)	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, MeasurementQuality measurementQuality, 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.
SignalBasedMeasurement(AbsoluteDate date, boolean isTwoWay, double[] observedValue, MeasurementQuality measurementQuality, SignalTravelTimeModel signalTravelTimeModel, List<ObservableSatellite> satellites)	Simple constructor for measurements.
SignalBasedMeasurement(AbsoluteDate date, boolean isTwoWay, double observedValue, MeasurementQuality measurementQuality, SignalTravelTimeModel signalTravelTimeModel, List<ObservableSatellite> satellites)	Simple constructor for scalar 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	Generator.addPropagator(Propagator propagator, String name)	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
AbstractBireceiverBuilder(CorrelatedRandomVectorGenerator noiseSource, Observer primeObserver, Observer secondObserver, double sigma, double baseWeight, SignalTravelTimeModel signalTravelTimeModel, ObservableSatellite satellite)	Simple constructor.
AbstractBistaticBuilder(CorrelatedRandomVectorGenerator noiseSource, Observer emitter, Observer receiver, double sigma, double baseWeight, SignalTravelTimeModel signalTravelTimeModel, ObservableSatellite satellite)	Simple constructor.
AbstractMeasurementBuilder(CorrelatedRandomVectorGenerator noiseSource, double[] sigma, double[] baseWeight, ObservableSatellite... satellites)	Simple constructor.
AbstractMeasurementBuilder(CorrelatedRandomVectorGenerator noiseSource, double sigma, double baseWeight, ObservableSatellite... satellites)	Simple constructor.
AbstractSignalBasedBuilder(CorrelatedRandomVectorGenerator noiseSource, double[] sigma, double[] baseWeight, SignalTravelTimeModel signalTravelTimeModel, ObservableSatellite satellite)	Simple constructor for single observable satellite.
AbstractSignalBasedBuilder(CorrelatedRandomVectorGenerator noiseSource, double[] sigma, double[] baseWeight, SignalTravelTimeModel signalTravelTimeModel, ObservableSatellite[] satellites)	Simple constructor.
AngularAzElBuilder(CorrelatedRandomVectorGenerator noiseSource, GroundStation station, double[] sigma, double[] baseWeight, ObservableSatellite satellite)	Simple constructor.
AngularAzElBuilder(CorrelatedRandomVectorGenerator noiseSource, GroundStation station, double[] sigma, double[] baseWeight, SignalTravelTimeModel signalTravelTimeModel, ObservableSatellite satellite)	Simple constructor.
AngularRaDecBuilder(CorrelatedRandomVectorGenerator noiseSource, GroundStation station, Frame referenceFrame, double[] sigma, double[] baseWeight, ObservableSatellite satellite)	Simple constructor.
AngularRaDecBuilder(CorrelatedRandomVectorGenerator noiseSource, Observer observer, Frame referenceFrame, double[] sigma, double[] baseWeight, SignalTravelTimeModel signalTravelTimeModel, ObservableSatellite satellite)	Simple constructor.
BistaticRangeBuilder(CorrelatedRandomVectorGenerator noiseSource, Observer emitter, Observer receiver, double sigma, double baseWeight, ObservableSatellite satellite)	Constructor with default signal travel time model.
BistaticRangeBuilder(CorrelatedRandomVectorGenerator noiseSource, Observer emitter, Observer receiver, double sigma, double baseWeight, SignalTravelTimeModel signalTravelTimeModel, ObservableSatellite satellite)	Constructor.
BistaticRangeRateBuilder(CorrelatedRandomVectorGenerator noiseSource, Observer emitter, Observer receiver, double sigma, double baseWeight, ObservableSatellite satellite)	Constructor with default signal travel time model.
BistaticRangeRateBuilder(CorrelatedRandomVectorGenerator noiseSource, Observer emitter, Observer receiver, double sigma, double baseWeight, SignalTravelTimeModel signalTravelTimeModel, ObservableSatellite satellite)	Simple constructor.
FDOABuilder(CorrelatedRandomVectorGenerator noiseSource, Observer primeObserver, Observer secondObserver, double centreFrequency, double sigma, double baseWeight, ObservableSatellite satellite)	Simple constructor.
FDOABuilder(CorrelatedRandomVectorGenerator noiseSource, Observer primeObserver, Observer secondObserver, double centreFrequency, double sigma, double baseWeight, SignalTravelTimeModel signalTravelTimeModel, 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.
InterSatellitesRangeBuilder(CorrelatedRandomVectorGenerator noiseSource, ObservableSatellite local, ObservableSatellite remote, boolean twoWay, double sigma, double baseWeight, SignalTravelTimeModel signalTravelTimeModel)	Simple constructor.
OneWayGNSSPhaseBuilder(CorrelatedRandomVectorGenerator noiseSource, ObservableSatellite local, Observer remote, double wavelength, double sigma, double baseWeight, AmbiguityCache cache)	Simple constructor.
OneWayGNSSRangeBuilder(CorrelatedRandomVectorGenerator noiseSource, ObservableSatellite local, Observer remote, double sigma, double baseWeight)	Simple constructor.
OneWayGNSSRangeRateBuilder(CorrelatedRandomVectorGenerator noiseSource, ObservableSatellite local, Observer 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, Observer observer, boolean twoWay, double sigma, double baseWeight, ObservableSatellite satellite)	Simple constructor.
RangeRateBuilder(CorrelatedRandomVectorGenerator noiseSource, Observer observer, boolean twoWay, double sigma, double baseWeight, ObservableSatellite satellite)	Simple constructor.
TDOABuilder(CorrelatedRandomVectorGenerator noiseSource, Observer primeObserver, Observer secondObserver, double sigma, double baseWeight, ObservableSatellite satellite)	Simple constructor.
TDOABuilder(CorrelatedRandomVectorGenerator noiseSource, Observer primeObserver, Observer secondObserver, double sigma, double baseWeight, SignalTravelTimeModel signalTravelTimeModel, ObservableSatellite satellite)	Simple constructor.
TurnAroundRangeBuilder(CorrelatedRandomVectorGenerator noiseSource, Observer primaryObserver, Observer secondaryObserver, double sigma, double baseWeight, ObservableSatellite satellite)	Simple constructor.
TurnAroundRangeBuilder(CorrelatedRandomVectorGenerator noiseSource, Observer primaryObserver, Observer secondaryObserver, double sigma, double baseWeight, SignalTravelTimeModel signalTravelTimeModel, 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, MeasurementQuality measurementQuality, SignalTravelTimeModel signalTravelTimeModel, ObservableSatellite local, ObservableSatellite remote)	Constructor.
AbstractInterSatellitesMeasurement(AbsoluteDate date, double observed, MeasurementQuality measurementQuality, SignalTravelTimeModel signalTravelTimeModel, ObservableSatellite local, ObservableSatellite remote)	Constructor.
AbstractOneWayGNSS(Observer observer, AbsoluteDate date, double[] observedValue, MeasurementQuality measurementQuality, SignalTravelTimeModel signalTravelTimeModel, ObservableSatellite local)	Simple constructor.
AbstractOneWayGNSS(Observer observer, AbsoluteDate date, double observedValue, MeasurementQuality measurementQuality, SignalTravelTimeModel signalTravelTimeModel, ObservableSatellite local)	Simple constructor.
InterSatellitesOneWayRangeRate(ObservableSatellite local, ObservableSatellite remote, AbsoluteDate date, double rangeRate, double sigma, double baseWeight)	Constructor with default signal travel time model.
InterSatellitesOneWayRangeRate(ObservableSatellite local, ObservableSatellite remote, AbsoluteDate date, double rangeRate, double sigma, double baseWeight, SignalTravelTimeModel signalTravelTimeModel)	Constructor.
InterSatellitesPhase(ObservableSatellite local, ObservableSatellite remote, AbsoluteDate date, double phase, double wavelength, double sigma, double baseWeight, AmbiguityCache cache)	Constructor with default signal travel time model.
InterSatellitesPhase(ObservableSatellite local, ObservableSatellite remote, AbsoluteDate date, double phase, double wavelength, double sigma, double baseWeight, AmbiguityCache cache, SignalTravelTimeModel signalTravelTimeModel)	Constructor.
OneWayGNSSPhase(Observer observer, AbsoluteDate date, double phase, double wavelength, double sigma, double baseWeight, ObservableSatellite local, AmbiguityCache cache)	Simple constructor.
OneWayGNSSRange(Observer observer, AbsoluteDate date, double range, double sigma, double baseWeight, ObservableSatellite local)	Simple constructor.
OneWayGNSSRangeRate(Observer observer, AbsoluteDate date, double rangeRate, double sigma, double baseWeight, ObservableSatellite local)	Simple constructor.
Phase(Observer observer, AbsoluteDate date, double phase, double wavelength, double sigma, double baseWeight, ObservableSatellite satellite, AmbiguityCache cache)	Simple constructor.
PhaseBuilder(CorrelatedRandomVectorGenerator noiseSource, Observer observer, double wavelength, double sigma, double baseWeight, ObservableSatellite satellite, AmbiguityCache cache)	Simple constructor.