Uses of Interface
org.orekit.estimation.measurements.Observer
Packages that use Observer
Package
Description
The measurements package defines everything that is related to orbit
determination measurements.
This package provides Orbit Determination measurements generation.
This package provides methods to handle GNSS measurements.
This package provides measurement modifier.
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Uses of Observer in org.orekit.estimation.measurements
Classes in org.orekit.estimation.measurements that implement ObserverModifier and TypeClassDescriptionclassClass modeling a ground station that can perform some measurements.classClass that accepts a PVCoordinatesProvider for a space- based measurement receiver.Methods in org.orekit.estimation.measurements that return ObserverModifier and TypeMethodDescriptionfinal ObserverAbstractRangeRelatedMeasurement.getObserver()Get receiving object.AngularRaDec.getObserver()Getter for the observer.TurnAroundRange.getPrimaryObserver()Get the primary observer from which measurement is performed.TurnAroundRange.getSecondaryObserver()Get the secondary observer reflecting the signal.Constructors in org.orekit.estimation.measurements with parameters of type ObserverModifierConstructorDescriptionprotectedAbstractRangeRelatedMeasurement(Observer observer, AbsoluteDate date, double value, MeasurementQuality measurementQuality, boolean twoWay, 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, MeasurementQuality measurementQuality, 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, MeasurementQuality measurementQuality, 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, MeasurementQuality measurementQuality, 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, MeasurementQuality measurementQuality, SignalTravelTimeModel signalTravelTimeModel, ObservableSatellite satellite) Constructor.Range(Observer observer, boolean twoWay, AbsoluteDate date, double range, double sigma, double baseWeight, ObservableSatellite satellite) Simple constructor.Range(Observer observer, boolean twoWay, AbsoluteDate date, double range, MeasurementQuality measurementQuality, SignalTravelTimeModel signalTravelTimeModel, 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, MeasurementQuality measurementQuality, 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, MeasurementQuality measurementQuality, 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. -
Uses of Observer in org.orekit.estimation.measurements.generation
Methods in org.orekit.estimation.measurements.generation that return ObserverModifier and TypeMethodDescriptionAbstractBistaticBuilder.getEmitter()Getter for signal emitter.AngularRaDecBuilder.getObserver()Getter for the observer.AbstractBireceiverBuilder.getPrimeObserver()Getter for prime observer.AbstractBistaticBuilder.getReceiver()Getter for signal receiver.AbstractBireceiverBuilder.getSecondObserver()Getter for second observer.Constructors in org.orekit.estimation.measurements.generation with parameters of type ObserverModifierConstructorDescriptionprotectedAbstractBireceiverBuilder(Observer primeObserver, Observer secondObserver, MeasurementQuality measurementQuality, SignalTravelTimeModel signalTravelTimeModel, ObservableSatellite satellite) Simple constructor.protectedAbstractBistaticBuilder(Observer emitter, Observer receiver, MeasurementQuality measurementQuality, SignalTravelTimeModel signalTravelTimeModel, ObservableSatellite satellite) Simple constructor.AngularRaDecBuilder(Observer observer, Frame referenceFrame, MeasurementQuality measurementQuality, SignalTravelTimeModel signalTravelTimeModel, ObservableSatellite satellite) Simple constructor.BistaticRangeBuilder(Observer emitter, Observer receiver, double sigma, double baseWeight, ObservableSatellite satellite) Constructor with default signal travel time model.BistaticRangeBuilder(Observer emitter, Observer receiver, MeasurementQuality measurementQuality, SignalTravelTimeModel signalTravelTimeModel, ObservableSatellite satellite) Constructor.BistaticRangeRateBuilder(Observer emitter, Observer receiver, double sigma, double baseWeight, ObservableSatellite satellite) Constructor with default signal travel time model.BistaticRangeRateBuilder(Observer emitter, Observer receiver, MeasurementQuality measurementQuality, SignalTravelTimeModel signalTravelTimeModel, ObservableSatellite satellite) Simple constructor.FDOABuilder(Observer primeObserver, Observer secondObserver, double centreFrequency, double sigma, double baseWeight, ObservableSatellite satellite) Simple constructor.FDOABuilder(Observer primeObserver, Observer secondObserver, double centreFrequency, MeasurementQuality measurementQuality, SignalTravelTimeModel signalTravelTimeModel, ObservableSatellite satellite) Simple constructor.OneWayGNSSPhaseBuilder(ObservableSatellite local, Observer remote, double wavelength, double sigma, double baseWeight, AmbiguityCache cache) Simple constructor.OneWayGNSSPhaseBuilder(ObservableSatellite local, Observer remote, double wavelength, MeasurementQuality measurementQuality, SignalTravelTimeModel signalTravelTimeModel, AmbiguityCache cache) Simple constructor.OneWayGNSSRangeBuilder(ObservableSatellite local, Observer remote, double sigma, double baseWeight) Simple constructor.OneWayGNSSRangeBuilder(ObservableSatellite local, Observer remote, MeasurementQuality measurementQuality, SignalTravelTimeModel signalTravelTimeModel) Simple constructor.OneWayGNSSRangeRateBuilder(ObservableSatellite local, Observer remote, double sigma, double baseWeight) Simple constructor.OneWayGNSSRangeRateBuilder(ObservableSatellite local, Observer remote, MeasurementQuality measurementQuality, SignalTravelTimeModel signalTravelTimeModel) Simple constructor.RangeBuilder(Observer observer, boolean twoWay, double sigma, double baseWeight, ObservableSatellite satellite) Simple constructor.RangeBuilder(Observer observer, boolean twoWay, MeasurementQuality measurementQuality, SignalTravelTimeModel signalTravelTimeModel, ObservableSatellite satellite) Simple constructor.RangeRateBuilder(Observer observer, boolean twoWay, double sigma, double baseWeight, ObservableSatellite satellite) Simple constructor.RangeRateBuilder(Observer observer, boolean twoWay, MeasurementQuality measurementQuality, SignalTravelTimeModel signalTravelTimeModel, ObservableSatellite satellite) Simple constructor.TDOABuilder(Observer primeObserver, Observer secondObserver, double sigma, double baseWeight, ObservableSatellite satellite) Simple constructor.TDOABuilder(Observer primeObserver, Observer secondObserver, MeasurementQuality measurementQuality, SignalTravelTimeModel signalTravelTimeModel, ObservableSatellite satellite) Simple constructor.TurnAroundRangeBuilder(Observer primaryObserver, Observer secondaryObserver, double sigma, double baseWeight, ObservableSatellite satellite) Simple constructor.TurnAroundRangeBuilder(Observer primaryObserver, Observer secondaryObserver, MeasurementQuality measurementQuality, SignalTravelTimeModel signalTravelTimeModel, ObservableSatellite satellite) Simple constructor. -
Uses of Observer in org.orekit.estimation.measurements.gnss
Methods in org.orekit.estimation.measurements.gnss that return ObserverModifier and TypeMethodDescriptionfinal ObserverAbstractOneWayGNSS.getObserver()Observer object sending signal.final ObserverPhase.getObserver()Get receiving observer.Constructors in org.orekit.estimation.measurements.gnss with parameters of type ObserverModifierConstructorDescriptionprotectedAbstractOneWayGNSS(Observer observer, AbsoluteDate date, double[] observedValue, MeasurementQuality measurementQuality, SignalTravelTimeModel signalTravelTimeModel, ObservableSatellite local) Simple constructor.protectedAbstractOneWayGNSS(Observer observer, AbsoluteDate date, double observedValue, MeasurementQuality measurementQuality, SignalTravelTimeModel signalTravelTimeModel, ObservableSatellite local) Simple constructor.OneWayGNSSPhase(Observer observer, AbsoluteDate date, double phase, double wavelength, double sigma, double baseWeight, ObservableSatellite local, AmbiguityCache cache) Simple constructor.OneWayGNSSPhase(Observer observer, AbsoluteDate date, double phase, double wavelength, MeasurementQuality measurementQuality, SignalTravelTimeModel signalTravelTimeModel, ObservableSatellite local, AmbiguityCache cache) Simple constructor.OneWayGNSSRange(Observer observer, AbsoluteDate date, double range, double sigma, double baseWeight, ObservableSatellite local) Simple constructor.OneWayGNSSRange(Observer observer, AbsoluteDate date, double range, MeasurementQuality measurementQuality, SignalTravelTimeModel signalTravelTimeModel, ObservableSatellite local) Simple constructor.OneWayGNSSRangeRate(Observer observer, AbsoluteDate date, double rangeRate, double sigma, double baseWeight, ObservableSatellite local) Simple constructor.OneWayGNSSRangeRate(Observer observer, AbsoluteDate date, double rangeRate, MeasurementQuality measurementQuality, SignalTravelTimeModel signalTravelTimeModel, ObservableSatellite local) Simple constructor.Phase(Observer observer, AbsoluteDate date, double phase, double wavelength, double sigma, double baseWeight, ObservableSatellite satellite, AmbiguityCache cache) Simple constructor.Phase(Observer observer, AbsoluteDate date, double phase, double wavelength, MeasurementQuality measurementQuality, SignalTravelTimeModel signalTravelTimeModel, ObservableSatellite satellite, AmbiguityCache cache) Simple constructor.PhaseBuilder(Observer observer, double wavelength, double sigma, double baseWeight, ObservableSatellite satellite, AmbiguityCache cache) Simple constructor.PhaseBuilder(Observer observer, double wavelength, MeasurementQuality measurementQuality, SignalTravelTimeModel signalTravelTimeModel, ObservableSatellite satellite, AmbiguityCache cache) Simple constructor. -
Uses of Observer in org.orekit.estimation.measurements.modifiers
Methods in org.orekit.estimation.measurements.modifiers that return ObserverModifier and TypeMethodDescriptionabstract ObserverPhaseCentersGroundReceiverBaseModifier.getObserver(EstimatedMeasurementBase<T> estimated) Retrieve observer.PhaseCentersPhaseModifier.getObserver(EstimatedMeasurementBase<Phase> estimated) PhaseCentersRangeModifier.getObserver(EstimatedMeasurementBase<Range> estimated) Retrieve observer.Methods in org.orekit.estimation.measurements.modifiers with parameters of type ObserverModifier and TypeMethodDescriptiondoubleParametricModelEffect.evaluate(Observer station, SpacecraftState state) Evaluate the parametric model effect.ParametricModelEffectGradient.evaluate(Observer station, FieldSpacecraftState<Gradient> state, Gradient[] parameters) Evaluate the parametric model effect.static <T extends ObservedMeasurement<T>>
voidOneWayGNSSRangeModifierUtil.modify(EstimatedMeasurement<T> estimated, ParameterDriversProvider parametricModel, AbstractGradientConverter converter, Observer gnssSatellite, ParametricModelEffect modelEffect, ParametricModelEffectGradient modelEffectGradient, EstimationModifier<T> modifier) Apply a modifier to an estimated measurement.static <T extends ObservedMeasurement<T>>
voidRangeModifierUtil.modify(EstimatedMeasurement<T> estimated, ParameterDriversProvider parametricModel, AbstractGradientConverter converter, Observer observer, ParametricModelEffect modelEffect, ParametricModelEffectGradient modelEffectGradient, EstimationModifier<T> modifier) Apply a modifier to an estimated measurement.static <T extends ObservedMeasurement<T>>
voidRangeRateModifierUtil.modify(EstimatedMeasurement<T> estimated, ParameterDriversProvider parametricModel, AbstractGradientConverter converter, Observer observer, ParametricModelEffect modelEffect, ParametricModelEffectGradient modelEffectGradient, EstimationModifier<T> modifier) Apply a modifier to an estimated measurement.static <T extends ObservedMeasurement<T>>
voidOneWayGNSSRangeModifierUtil.modifyWithoutDerivatives(EstimatedMeasurementBase<T> estimated, Observer gnssSatellite, ParametricModelEffect modelEffect, EstimationModifier<T> modifier) Apply a modifier to an estimated measurement.static <T extends ObservedMeasurement<T>>
voidRangeModifierUtil.modifyWithoutDerivatives(EstimatedMeasurementBase<T> estimated, Observer observer, ParametricModelEffect modelEffect, EstimationModifier<T> modifier) Apply a modifier to an estimated measurement.static <T extends ObservedMeasurement<T>>
voidRangeRateModifierUtil.modifyWithoutDerivatives(EstimatedMeasurementBase<T> estimated, Observer observer, ParametricModelEffect modelEffect, EstimationModifier<T> modifier) Apply a modifier to an estimated measurement.static double[]AberrationModifier.naturalToProper(double[] naturalRaDec, Observer observer, AbsoluteDate date, Frame frame) Natural to proper correction for aberration of light.static double[]AberrationModifier.naturalToProper(double[] naturalRaDec, Observer observer, AbsoluteDate date, Frame frame, DataContext context) Natural to proper correction for aberration of light.protected <T extends CalculusFieldElement<T>>
TBaseOneWayGNSSRangeIonosphericDelayModifier.oneWayGNSSErrorIonosphericModel(Observer observer, FieldSpacecraftState<T> state, T[] parameters) Compute the measurement error due to Ionosphere.protected doubleBaseOneWayGNSSRangeIonosphericDelayModifier.oneWayGNSSErrorIonosphericModel(Observer observer, SpacecraftState state) Compute the measurement error due to Ionosphere.static double[]AberrationModifier.properToNatural(double[] properRaDec, Observer observer, AbsoluteDate date, Frame frame) Proper to natural correction for aberration of light.static double[]AberrationModifier.properToNatural(double[] properRaDec, Observer observer, AbsoluteDate date, Frame frame, DataContext context) Proper to natural correction for aberration of light.protected <T extends CalculusFieldElement<T>>
TBaseRangeIonosphericDelayModifier.rangeErrorIonosphericModel(Observer station, FieldSpacecraftState<T> state, T[] parameters) Compute the measurement error due to Ionosphere.protected doubleBaseRangeIonosphericDelayModifier.rangeErrorIonosphericModel(Observer station, SpacecraftState state) Compute the measurement error due to Ionosphere.<T extends CalculusFieldElement<T>>
TBaseRangeTroposphericDelayModifier.rangeErrorTroposphericModel(Observer observer, FieldSpacecraftState<T> state, T[] parameters) Compute the measurement error due to Troposphere.doubleBaseRangeTroposphericDelayModifier.rangeErrorTroposphericModel(Observer observer, SpacecraftState state) Compute the measurement error due to Troposphere.protected <T extends CalculusFieldElement<T>>
TBaseRangeRateIonosphericDelayModifier.rangeRateErrorIonosphericModel(Observer station, FieldSpacecraftState<T> state, T[] parameters) Compute the measurement error due to Ionosphere.protected doubleBaseRangeRateIonosphericDelayModifier.rangeRateErrorIonosphericModel(Observer station, SpacecraftState state) Compute the measurement error due to Ionosphere.protected <T extends CalculusFieldElement<T>>
TRangeRateIonosphericDelayModifier.rangeRateErrorIonosphericModel(Observer observer, FieldSpacecraftState<T> state, T[] parameters) Compute the measurement error due to Ionosphere.protected doubleRangeRateIonosphericDelayModifier.rangeRateErrorIonosphericModel(Observer observer, SpacecraftState state) Compute the measurement error due to Ionosphere.<T extends CalculusFieldElement<T>>
TBaseRangeRateTroposphericDelayModifier.rangeRateErrorTroposphericModel(Observer observer, FieldSpacecraftState<T> state, T[] parameters) Compute the measurement error due to Troposphere.doubleBaseRangeRateTroposphericDelayModifier.rangeRateErrorTroposphericModel(Observer observer, SpacecraftState state) Compute the measurement error due to Troposphere.<T extends CalculusFieldElement<T>>
TRangeRateTroposphericDelayModifier.rangeRateErrorTroposphericModel(Observer observer, FieldSpacecraftState<T> state, T[] parameters) Compute the measurement error due to Troposphere.doubleRangeRateTroposphericDelayModifier.rangeRateErrorTroposphericModel(Observer observer, SpacecraftState state) Compute the measurement error due to Troposphere.