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

Packages that use EstimatedMeasurementBase

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.
org.orekit.estimation.measurements.modifiers	This package provides measurement modifier.

Uses of EstimatedMeasurementBase in org.orekit.estimation.measurements

Subclasses of EstimatedMeasurementBase in org.orekit.estimation.measurements

Modifier and Type	Class	Description
class	EstimatedMeasurement<T extends ObservedMeasurement<T>>	Class holding an estimated theoretical value associated to an observed measurement.

Methods in org.orekit.estimation.measurements that return EstimatedMeasurementBase

Modifier and Type	Method	Description
EstimatedMeasurementBase<T>	AbstractMeasurement.estimateWithoutDerivatives(int iteration, int evaluation, SpacecraftState[] states)	Estimate the theoretical value of the measurement, without derivatives.
EstimatedMeasurementBase<T>	ObservedMeasurement.estimateWithoutDerivatives(int iteration, int evaluation, SpacecraftState[] states)	Estimate the theoretical value of the measurement, without derivatives.
default EstimatedMeasurementBase<T>	ObservedMeasurement.estimateWithoutDerivatives(SpacecraftState[] states)	Estimate the theoretical value of the measurement, without derivatives.
protected EstimatedMeasurementBase<T>	AbstractRangeRelatedMeasurement.initializeOneWayTheoreticalEvaluation(T measurement, int iteration, int evaluation, AbsoluteDate receptionDate, SpacecraftState state)	Compute participants for one-way case.
protected EstimatedMeasurementBase<T>	AbstractRangeRelatedMeasurement.initializeTwoWayTheoreticalEvaluation(T measurement, int iteration, int evaluation, AbsoluteDate receptionDate, SpacecraftState state)	Compute participants for two-way case.
protected EstimatedMeasurementBase<T>	AbstractMeasurement.theoreticalEvaluationWithoutDerivatives(int iteration, int evaluation, SpacecraftState[] states)	Estimate the theoretical value without derivatives.
protected EstimatedMeasurementBase<AngularAzEl>	AngularAzEl.theoreticalEvaluationWithoutDerivatives(int iteration, int evaluation, SpacecraftState[] states)	Estimate the theoretical value without derivatives.
protected EstimatedMeasurementBase<AngularRaDec>	AngularRaDec.theoreticalEvaluationWithoutDerivatives(int iteration, int evaluation, SpacecraftState[] states)	Estimate the theoretical value without derivatives.
protected EstimatedMeasurementBase<BistaticRange>	BistaticRange.theoreticalEvaluationWithoutDerivatives(int iteration, int evaluation, SpacecraftState[] states)	Estimate the theoretical value without derivatives.
protected EstimatedMeasurementBase<BistaticRangeRate>	BistaticRangeRate.theoreticalEvaluationWithoutDerivatives(int iteration, int evaluation, SpacecraftState[] states)	Estimate the theoretical value without derivatives.
protected EstimatedMeasurementBase<FDOA>	FDOA.theoreticalEvaluationWithoutDerivatives(int iteration, int evaluation, SpacecraftState[] states)	Estimate the theoretical value without derivatives.
protected EstimatedMeasurementBase<InterSatellitesRange>	InterSatellitesRange.theoreticalEvaluationWithoutDerivatives(int iteration, int evaluation, SpacecraftState[] states)	Estimate the theoretical value without derivatives.
protected EstimatedMeasurementBase<MultiplexedMeasurement>	MultiplexedMeasurement.theoreticalEvaluationWithoutDerivatives(int iteration, int evaluation, SpacecraftState[] states)	Estimate the theoretical value without derivatives.
protected EstimatedMeasurementBase<Position>	Position.theoreticalEvaluationWithoutDerivatives(int iteration, int evaluation, SpacecraftState[] states)	Estimate the theoretical value without derivatives.
protected EstimatedMeasurementBase<PV>	PV.theoreticalEvaluationWithoutDerivatives(int iteration, int evaluation, SpacecraftState[] states)	Estimate the theoretical value without derivatives.
protected EstimatedMeasurementBase<Range>	Range.theoreticalEvaluationWithoutDerivatives(int iteration, int evaluation, SpacecraftState[] states)	Estimate the theoretical value without derivatives.
protected EstimatedMeasurementBase<RangeRate>	RangeRate.theoreticalEvaluationWithoutDerivatives(int iteration, int evaluation, SpacecraftState[] states)	Estimate the theoretical value without derivatives.
protected EstimatedMeasurementBase<TDOA>	TDOA.theoreticalEvaluationWithoutDerivatives(int iteration, int evaluation, SpacecraftState[] states)	Estimate the theoretical value without derivatives.
protected EstimatedMeasurementBase<TurnAroundRange>	TurnAroundRange.theoreticalEvaluationWithoutDerivatives(int iteration, int evaluation, SpacecraftState[] states)	Estimate the theoretical value without derivatives.

Methods in org.orekit.estimation.measurements that return types with arguments of type EstimatedMeasurementBase

Modifier and Type	Method	Description
List<EstimatedMeasurementBase<?>>	MultiplexedMeasurement.getEstimatedMeasurementsWithoutDerivatives()	Get the underlying estimated measurements without derivatives.

Methods in org.orekit.estimation.measurements with parameters of type EstimatedMeasurementBase

Modifier and Type	Method	Description
void	EstimationModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<T> estimated)	Apply a modifier to an estimated measurement without derivatives.

Constructors in org.orekit.estimation.measurements with parameters of type EstimatedMeasurementBase

Modifier	Constructor	Description
	EstimatedMeasurement(EstimatedMeasurementBase<T> estimatedMeasurementBase)	Constructor from measurement base.

Uses of EstimatedMeasurementBase in org.orekit.estimation.measurements.generation

Methods in org.orekit.estimation.measurements.generation that return EstimatedMeasurementBase

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.
default EstimatedMeasurementBase<T>	MeasurementBuilder.build(AbsoluteDate date, SpacecraftState[] states)	Generate a single measurement.
EstimatedMeasurementBase<MultiplexedMeasurement>	MultiplexedMeasurementBuilder.build(AbsoluteDate date, Map<ObservableSatellite,OrekitStepInterpolator> interpolators)	Generate a single measurement.

Methods in org.orekit.estimation.measurements.generation that return types with arguments of type EstimatedMeasurementBase

Modifier and Type	Method	Description
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.
SortedSet<EstimatedMeasurementBase<?>>	GatheringSubscriber.getGeneratedMeasurements()	Get generated measurements.

Methods in org.orekit.estimation.measurements.generation with parameters of type EstimatedMeasurementBase

Modifier and Type	Method	Description
void	GatheringSubscriber.handleGeneratedMeasurement(EstimatedMeasurementBase<?> measurement)	Handle a generated measurement.
void	GeneratedMeasurementSubscriber.handleGeneratedMeasurement(EstimatedMeasurementBase<?> measurement)	Handle a generated measurement.

Constructor parameters in org.orekit.estimation.measurements.generation with type arguments of type EstimatedMeasurementBase

Modifier	Constructor	Description
protected	AbstractScheduler(MeasurementBuilder<T> builder, DatesSelector selector, Predicate<EstimatedMeasurementBase<T>> filter)	Simple constructor.
	ContinuousScheduler(MeasurementBuilder<T> builder, DatesSelector selector, Predicate<EstimatedMeasurementBase<T>> filter)	Simple constructor.
	EventBasedScheduler(MeasurementBuilder<T> builder, DatesSelector selector, Predicate<EstimatedMeasurementBase<T>> filter, Propagator propagator, EventDetector detector, SignSemantic signSemantic)	Simple constructor.

Uses of EstimatedMeasurementBase in org.orekit.estimation.measurements.gnss

Methods in org.orekit.estimation.measurements.gnss that return EstimatedMeasurementBase

Modifier and Type	Method	Description
protected EstimatedMeasurementBase<InterSatellitesOneWayRangeRate>	InterSatellitesOneWayRangeRate.theoreticalEvaluationWithoutDerivatives(int iteration, int evaluation, SpacecraftState[] states)	Estimate the theoretical value without derivatives.
protected EstimatedMeasurementBase<InterSatellitesPhase>	InterSatellitesPhase.theoreticalEvaluationWithoutDerivatives(int iteration, int evaluation, SpacecraftState[] states)	Estimate the theoretical value without derivatives.
protected EstimatedMeasurementBase<OneWayGNSSPhase>	OneWayGNSSPhase.theoreticalEvaluationWithoutDerivatives(int iteration, int evaluation, SpacecraftState[] states)	Estimate the theoretical value without derivatives.
protected EstimatedMeasurementBase<OneWayGNSSRange>	OneWayGNSSRange.theoreticalEvaluationWithoutDerivatives(int iteration, int evaluation, SpacecraftState[] states)	Estimate the theoretical value without derivatives.
protected EstimatedMeasurementBase<OneWayGNSSRangeRate>	OneWayGNSSRangeRate.theoreticalEvaluationWithoutDerivatives(int iteration, int evaluation, SpacecraftState[] states)	Estimate the theoretical value without derivatives.
protected EstimatedMeasurementBase<Phase>	Phase.theoreticalEvaluationWithoutDerivatives(int iteration, int evaluation, SpacecraftState[] states)	Estimate the theoretical value without derivatives.

Methods in org.orekit.estimation.measurements.gnss with parameters of type EstimatedMeasurementBase

Modifier and Type	Method	Description
protected abstract Rotation	AbstractWindUp.emitterToInert(EstimatedMeasurementBase<T> estimated)	Compute rotation from emitter to inertial frame.
protected Rotation	InterSatellitesWindUp.emitterToInert(EstimatedMeasurementBase<InterSatellitesPhase> estimated)	Compute rotation from emitter to inertial frame.
protected Rotation	OneWayGNSSWindUp.emitterToInert(EstimatedMeasurementBase<OneWayGNSSPhase> estimated)	Compute rotation from emitter to inertial frame.
protected Rotation	WindUp.emitterToInert(EstimatedMeasurementBase<Phase> estimated)	Compute rotation from emitter to inertial frame.
void	AbstractWindUp.modifyWithoutDerivatives(EstimatedMeasurementBase<T> estimated)	Apply a modifier to an estimated measurement without derivatives.
protected abstract Rotation	AbstractWindUp.receiverToInert(EstimatedMeasurementBase<T> estimated)	Compute rotation from receiver to inertial frame.
protected Rotation	InterSatellitesWindUp.receiverToInert(EstimatedMeasurementBase<InterSatellitesPhase> estimated)	Compute rotation from receiver to inertial frame.
protected Rotation	OneWayGNSSWindUp.receiverToInert(EstimatedMeasurementBase<OneWayGNSSPhase> estimated)	Compute rotation from receiver to inertial frame.
protected Rotation	WindUp.receiverToInert(EstimatedMeasurementBase<Phase> estimated)	Compute rotation from receiver to inertial frame.

Uses of EstimatedMeasurementBase in org.orekit.estimation.measurements.modifiers

Methods in org.orekit.estimation.measurements.modifiers with parameters of type EstimatedMeasurementBase

Modifier and Type	Method	Description
abstract Observer	PhaseCentersGroundReceiverBaseModifier.getObserver(EstimatedMeasurementBase<T> estimated)	Retrieve observer.
Observer	PhaseCentersPhaseModifier.getObserver(EstimatedMeasurementBase<Phase> estimated)
Observer	PhaseCentersRangeModifier.getObserver(EstimatedMeasurementBase<Range> estimated)	Retrieve observer.
void	AberrationModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<AngularRaDec> estimated)	Apply a modifier to an estimated measurement without derivatives.
protected void	AbstractRelativisticClockOnBoardRangeRateModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<T> estimated, double aLocal, double rLocal, double aRemote, double rRemote)	Apply relativistic frequency deviation.
protected void	AbstractShapiroPhaseModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<T> estimated, double wavelength)	Modify the theoretical phase measurement without derivatives, given the wavelength.
void	AbstractShapiroRangeModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<T> estimated)	Apply a modifier to an estimated measurement without derivatives.
void	AngularIonosphericDelayModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<AngularAzEl> estimated)	Apply a modifier to an estimated measurement without derivatives.
void	AngularRadioRefractionModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<AngularAzEl> estimated)
void	Bias.modifyWithoutDerivatives(EstimatedMeasurementBase<T> estimated)	Apply a modifier to an estimated measurement without derivatives.
void	BistaticRangeIonosphericDelayModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<BistaticRange> estimated)	Apply a modifier to an estimated measurement without derivatives.
void	BistaticRangeRateIonosphericDelayModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<BistaticRangeRate> estimated)	Apply a modifier to an estimated measurement without derivatives.
void	BistaticRangeRateTroposphericDelayModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<BistaticRangeRate> estimated)	Apply a modifier to an estimated measurement without derivatives.
void	BistaticRangeTroposphericDelayModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<BistaticRange> estimated)	Apply a modifier to an estimated measurement without derivatives.
void	DynamicOutlierFilter.modifyWithoutDerivatives(EstimatedMeasurementBase<T> estimated)	Apply a modifier to an estimated measurement without derivatives.
void	MeasurementNoise.modifyWithoutDerivatives(EstimatedMeasurementBase<T> estimated)	Apply a modifier to an estimated measurement without derivatives.
void	OnBoardAntennaInterSatellitesPhaseModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<InterSatellitesPhase> estimated)
void	OnBoardAntennaInterSatellitesRangeModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<InterSatellitesRange> estimated)	Apply a modifier to an estimated measurement without derivatives.
void	OnBoardAntennaOneWayGNSSPhaseModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<OneWayGNSSPhase> estimated)	Apply a modifier to an estimated measurement without derivatives.
void	OnBoardAntennaOneWayGNSSRangeModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<OneWayGNSSRange> estimated)	Apply a modifier to an estimated measurement without derivatives.
void	OnBoardAntennaTurnAroundRangeModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<TurnAroundRange> estimated)	Apply a modifier to an estimated measurement without derivatives.
void	OneWayGNSSRangeIonosphericDelayModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<OneWayGNSSRange> estimated)	Apply a modifier to an estimated measurement without derivatives.
static <T extends ObservedMeasurement<T>> void	OneWayGNSSRangeModifierUtil.modifyWithoutDerivatives(EstimatedMeasurementBase<T> estimated, Observer gnssSatellite, ParametricModelEffect modelEffect, EstimationModifier<T> modifier)	Apply a modifier to an estimated measurement.
void	OutlierFilter.modifyWithoutDerivatives(EstimatedMeasurementBase<T> estimated)	Apply a modifier to an estimated measurement without derivatives.
void	PhaseCentersPhaseModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<Phase> estimated)	Apply a modifier to an estimated measurement without derivatives.
void	PhaseCentersRangeModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<Range> estimated)	Apply a modifier to an estimated measurement without derivatives.
void	PhaseIonosphericDelayModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<Phase> estimated)
void	PhaseTroposphericDelayModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<Phase> estimated)	Apply a modifier to an estimated measurement without derivatives.
void	RangeIonosphericDelayModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<Range> estimated)	Apply a modifier to an estimated measurement without derivatives.
static <T extends ObservedMeasurement<T>> void	RangeModifierUtil.modifyWithoutDerivatives(EstimatedMeasurementBase<T> estimated, Observer observer, ParametricModelEffect modelEffect, EstimationModifier<T> modifier)	Apply a modifier to an estimated measurement.
void	RangeRateIonosphericDelayModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<RangeRate> estimated)	Apply a modifier to an estimated measurement without derivatives.
static <T extends ObservedMeasurement<T>> void	RangeRateModifierUtil.modifyWithoutDerivatives(EstimatedMeasurementBase<T> estimated, Observer observer, ParametricModelEffect modelEffect, EstimationModifier<T> modifier)	Apply a modifier to an estimated measurement.
void	RangeRateTroposphericDelayModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<RangeRate> estimated)	Apply a modifier to an estimated measurement without derivatives.
void	RangeTroposphericDelayModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<Range> estimated)	Apply a modifier to an estimated measurement without derivatives.
void	RelativisticClockInterSatellitesOneWayRangeRateModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<InterSatellitesOneWayRangeRate> estimated)	Apply a modifier to an estimated measurement without derivatives.
void	RelativisticClockInterSatellitesPhaseModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<InterSatellitesPhase> estimated)	Apply a modifier to an estimated measurement without derivatives.
void	RelativisticClockInterSatellitesRangeModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<InterSatellitesRange> estimated)	Apply a modifier to an estimated measurement without derivatives.
void	RelativisticClockOneWayGNSSPhaseModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<OneWayGNSSPhase> estimated)	Apply a modifier to an estimated measurement without derivatives.
void	RelativisticClockOneWayGNSSRangeModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<OneWayGNSSRange> estimated)	Apply a modifier to an estimated measurement without derivatives.
void	RelativisticClockOneWayGNSSRangeRateModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<OneWayGNSSRangeRate> estimated)	Apply a modifier to an estimated measurement without derivatives.
void	RelativisticClockPhaseModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<Phase> estimated)	Apply a modifier to an estimated measurement without derivatives.
void	RelativisticClockRangeModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<Range> estimated)	Apply a modifier to an estimated measurement without derivatives.
void	RelativisticClockRangeRateModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<RangeRate> estimated)	Apply a modifier to an estimated measurement without derivatives.
void	RelativisticJ2ClockInterSatellitesPhaseModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<InterSatellitesPhase> estimated)	Apply a modifier to an estimated measurement without derivatives.
void	RelativisticJ2ClockInterSatellitesRangeModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<InterSatellitesRange> estimated)	Apply a modifier to an estimated measurement without derivatives.
void	RelativisticJ2ClockOneWayGNSSPhaseModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<OneWayGNSSPhase> estimated)	Apply a modifier to an estimated measurement without derivatives.
void	RelativisticJ2ClockOneWayGNSSRangeModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<OneWayGNSSRange> estimated)	Apply a modifier to an estimated measurement without derivatives.
void	RelativisticJ2ClockPhaseModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<Phase> estimated)	Apply a modifier to an estimated measurement without derivatives.
void	RelativisticJ2ClockRangeModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<Range> estimated)	Apply a modifier to an estimated measurement without derivatives.
void	ShapiroInterSatellitePhaseModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<InterSatellitesPhase> estimated)	Apply a modifier to an estimated measurement without derivatives.
void	ShapiroOneWayGNSSPhaseModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<OneWayGNSSPhase> estimated)	Apply a modifier to an estimated measurement without derivatives.
void	ShapiroPhaseModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<Phase> estimated)	Apply a modifier to an estimated measurement without derivatives.
void	TDOAIonosphericDelayModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<TDOA> estimated)
void	TDOATroposphericDelayModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<TDOA> estimated)	Apply a modifier to an estimated measurement without derivatives.
void	TurnAroundRangeIonosphericDelayModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<TurnAroundRange> estimated)
void	TurnAroundRangeTroposphericDelayModifier.modifyWithoutDerivatives(EstimatedMeasurementBase<TurnAroundRange> estimated)	Apply a modifier to an estimated measurement without derivatives.
double	PhaseCentersGroundReceiverBaseModifier.oneWayDistanceModification(EstimatedMeasurementBase<T> estimated)	Compute distance modification for one way measurement.
double	PhaseCentersInterSatellitesBaseModifier.oneWayDistanceModification(EstimatedMeasurementBase<T> estimated)	Compute distance modification for one way measurement.
double	PhaseCentersOneWayGNSSBaseModifier.oneWayDistanceModification(EstimatedMeasurementBase<T> estimated)	Compute distance modification for one way measurement.
protected double	AbstractRelativisticClockModifier.relativisticCorrection(EstimatedMeasurementBase<?> estimated)	Computes the relativistic clock correction.
protected double	AbstractRelativisticJ2ClockModifier.relativisticJ2Correction(EstimatedMeasurementBase<?> estimated)	Computes the relativistic J2 clock time delay correction.
double	PhaseCentersGroundReceiverBaseModifier.twoWayDistanceModification(EstimatedMeasurementBase<T> estimated)	Apply a modifier to a two-way range measurement.
double	PhaseCentersInterSatellitesBaseModifier.twoWayDistanceModification(EstimatedMeasurementBase<InterSatellitesRange> estimated)	Compute distance modification for two way measurement.