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

Packages that use EstimatedMeasurement

Package	Description
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	The measurements package defines everything that is related to orbit determination measurements.
org.orekit.estimation.measurements.gnss	This package provides methods to handle GNSS measurements.
org.orekit.estimation.measurements.modifiers	This package provides measurement modifier.
org.orekit.estimation.sequential	The sequential package provides an implementation of a Kalman Filter engine to perform an orbit determination.

Uses of EstimatedMeasurement in org.orekit.estimation.leastsquares

Methods in org.orekit.estimation.leastsquares that return types with arguments of type EstimatedMeasurement

Modifier and Type	Method	Description
Map<ObservedMeasurement<?>,EstimatedMeasurement<?>>	BatchLSEstimator.getLastEstimations()	Get the last estimations performed.

Methods in org.orekit.estimation.leastsquares with parameters of type EstimatedMeasurement

Modifier and Type	Method	Description
void	AbstractBatchLSModel.fetchEvaluatedMeasurement(int index, EstimatedMeasurement<?> evaluation)	Fetch a measurement that was evaluated during propagation.

Method parameters in org.orekit.estimation.leastsquares with type arguments of type EstimatedMeasurement

Modifier and Type	Method	Description
void	ModelObserver.modelCalled(Orbit[] orbits, Map<ObservedMeasurement<?>,EstimatedMeasurement<?>> estimations)	Notification callback for orbit changes.

Uses of EstimatedMeasurement in org.orekit.estimation.measurements

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

Modifier and Type	Method	Description
EstimatedMeasurement<T>	AbstractMeasurement.estimate(int iteration, int evaluation, SpacecraftState[] states)	Estimate the theoretical value of the measurement, with derivatives.
EstimatedMeasurement<T>	ObservedMeasurement.estimate(int iteration, int evaluation, SpacecraftState[] states)	Estimate the theoretical value of the measurement, with derivatives.
EstimatedMeasurement<?>	EstimationsProvider.getEstimatedMeasurement(int index)	Get one estimated measurement.
protected abstract EstimatedMeasurement<T>	AbstractRangeRelatedMeasurement.oneWayTheoreticalEvaluation(int iteration, int evaluation, FieldPVCoordinatesProvider<Gradient> observablePVProvider, SpacecraftState state, Map<String,Integer> paramIndices, int nbParams)	Evaluate measurement in one-way.
protected EstimatedMeasurement<Range>	Range.oneWayTheoreticalEvaluation(int iteration, int evaluation, FieldPVCoordinatesProvider<Gradient> satellitePVProvider, SpacecraftState state, Map<String,Integer> indices, int nbParams)	Evaluate measurement in one-way.
protected EstimatedMeasurement<RangeRate>	RangeRate.oneWayTheoreticalEvaluation(int iteration, int evaluation, FieldPVCoordinatesProvider<Gradient> satellitePVProvider, SpacecraftState state, Map<String,Integer> indices, int nbParams)	Evaluate measurement in one-way.
protected abstract EstimatedMeasurement<T>	AbstractMeasurement.theoreticalEvaluation(int iteration, int evaluation, SpacecraftState[] states)	Estimate the theoretical value.
protected EstimatedMeasurement<T>	AbstractRangeRelatedMeasurement.theoreticalEvaluation(int iteration, int evaluation, SpacecraftState[] states)	Estimate the theoretical value.
protected EstimatedMeasurement<AngularAzEl>	AngularAzEl.theoreticalEvaluation(int iteration, int evaluation, SpacecraftState[] states)	Estimate the theoretical value.
protected EstimatedMeasurement<AngularRaDec>	AngularRaDec.theoreticalEvaluation(int iteration, int evaluation, SpacecraftState[] states)	Estimate the theoretical value.
protected EstimatedMeasurement<BistaticRange>	BistaticRange.theoreticalEvaluation(int iteration, int evaluation, SpacecraftState[] states)	Estimate the theoretical value.
protected EstimatedMeasurement<BistaticRangeRate>	BistaticRangeRate.theoreticalEvaluation(int iteration, int evaluation, SpacecraftState[] states)	Estimate the theoretical value.
protected EstimatedMeasurement<FDOA>	FDOA.theoreticalEvaluation(int iteration, int evaluation, SpacecraftState[] states)	Estimate the theoretical value.
protected EstimatedMeasurement<InterSatellitesRange>	InterSatellitesRange.theoreticalEvaluation(int iteration, int evaluation, SpacecraftState[] states)	Estimate the theoretical value.
protected EstimatedMeasurement<MultiplexedMeasurement>	MultiplexedMeasurement.theoreticalEvaluation(int iteration, int evaluation, SpacecraftState[] states)	Estimate the theoretical value.
protected EstimatedMeasurement<Position>	Position.theoreticalEvaluation(int iteration, int evaluation, SpacecraftState[] states)	Estimate the theoretical value.
protected EstimatedMeasurement<PV>	PV.theoreticalEvaluation(int iteration, int evaluation, SpacecraftState[] states)	Estimate the theoretical value.
protected EstimatedMeasurement<TDOA>	TDOA.theoreticalEvaluation(int iteration, int evaluation, SpacecraftState[] states)	Estimate the theoretical value.
protected EstimatedMeasurement<TurnAroundRange>	TurnAroundRange.theoreticalEvaluation(int iteration, int evaluation, SpacecraftState[] states)	Estimate the theoretical value.
protected abstract EstimatedMeasurement<T>	AbstractRangeRelatedMeasurement.twoWayTheoreticalEvaluation(int iteration, int evaluation, FieldPVCoordinatesProvider<Gradient> observablePVProvider, SpacecraftState state, Map<String,Integer> paramIndices, int nbParams)	Evaluate measurement in two-way.
protected EstimatedMeasurement<Range>	Range.twoWayTheoreticalEvaluation(int iteration, int evaluation, FieldPVCoordinatesProvider<Gradient> satellitePVProvider, SpacecraftState state, Map<String,Integer> indices, int nbParams)	Evaluate measurement in two-way.
protected EstimatedMeasurement<RangeRate>	RangeRate.twoWayTheoreticalEvaluation(int iteration, int evaluation, FieldPVCoordinatesProvider<Gradient> satellitePVProvider, SpacecraftState state, Map<String,Integer> indices, int nbParams)	Evaluate measurement in two-way.

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

Modifier and Type	Method	Description
List<EstimatedMeasurement<?>>	MultiplexedMeasurement.getEstimatedMeasurements()	Get the underlying estimated measurements.

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

Modifier and Type	Method	Description
protected void	AngularMeasurement.fillDerivatives(double[] firstAngleDerivatives, double[] secondAngleDerivatives, Map<String,Integer> paramIndices, EstimatedMeasurement<T> estimatedMeasurement)	Method filling derivatives in the estimated measurement.
protected void	AngularMeasurement.fillEstimatedMeasurement(Gradient firstAngle, Gradient secondAngle, Map<String,Integer> paramIndices, EstimatedMeasurement<T> estimatedMeasurement)	Method filling estimated measurement.
protected void	AbstractRangeRelatedMeasurement.fillEstimation(Gradient quantity, Map<String,Integer> paramIndices, EstimatedMeasurement<T> estimated)	Fill estimated measurements with value and derivatives.
default void	EstimationModifier.modify(EstimatedMeasurement<T> estimated)	Apply a modifier to an estimated measurement.

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

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

Modifier and Type	Method	Description
protected EstimatedMeasurement<InterSatellitesOneWayRangeRate>	InterSatellitesOneWayRangeRate.theoreticalEvaluation(int iteration, int evaluation, SpacecraftState[] states)	Estimate the theoretical value.
protected EstimatedMeasurement<InterSatellitesPhase>	InterSatellitesPhase.theoreticalEvaluation(int iteration, int evaluation, SpacecraftState[] states)	Estimate the theoretical value.
protected EstimatedMeasurement<OneWayGNSSPhase>	OneWayGNSSPhase.theoreticalEvaluation(int iteration, int evaluation, SpacecraftState[] states)	Estimate the theoretical value.
protected EstimatedMeasurement<OneWayGNSSRange>	OneWayGNSSRange.theoreticalEvaluation(int iteration, int evaluation, SpacecraftState[] states)	Estimate the theoretical value.
protected EstimatedMeasurement<OneWayGNSSRangeRate>	OneWayGNSSRangeRate.theoreticalEvaluation(int iteration, int evaluation, SpacecraftState[] states)	Estimate the theoretical value.
protected EstimatedMeasurement<Phase>	Phase.theoreticalEvaluation(int iteration, int evaluation, SpacecraftState[] states)	Estimate the theoretical value.

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

Modifier and Type	Method	Description
protected void	AbstractOneWayGNSS.fillDerivatives(Gradient observedValue, Map<String,Integer> indices, EstimatedMeasurement<T> estimated)	Method filling estimated measurement.

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

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

Modifier and Type	Method	Description
void	AberrationModifier.modify(EstimatedMeasurement<AngularRaDec> estimated)	Apply a modifier to an estimated measurement.
void	Bias.modify(EstimatedMeasurement<T> estimated)	Apply a modifier to an estimated measurement.
void	BistaticRangeIonosphericDelayModifier.modify(EstimatedMeasurement<BistaticRange> estimated)	Apply a modifier to an estimated measurement.
void	BistaticRangeRateIonosphericDelayModifier.modify(EstimatedMeasurement<BistaticRangeRate> estimated)	Apply a modifier to an estimated measurement.
void	BistaticRangeRateTroposphericDelayModifier.modify(EstimatedMeasurement<BistaticRangeRate> estimated)	Apply a modifier to an estimated measurement.
void	BistaticRangeTroposphericDelayModifier.modify(EstimatedMeasurement<BistaticRange> estimated)	Apply a modifier to an estimated measurement.
void	DynamicOutlierFilter.modify(EstimatedMeasurement<T> estimated)	Apply a modifier to an estimated measurement.
void	OneWayGNSSRangeIonosphericDelayModifier.modify(EstimatedMeasurement<OneWayGNSSRange> estimated)	Apply a modifier to an estimated measurement.
static <T extends ObservedMeasurement<T>> void	OneWayGNSSRangeModifierUtil.modify(EstimatedMeasurement<T> estimated, ParameterDriversProvider parametricModel, AbstractGradientConverter converter, Observer gnssSatellite, ParametricModelEffect modelEffect, ParametricModelEffectGradient modelEffectGradient, EstimationModifier<T> modifier)	Apply a modifier to an estimated measurement.
void	PhaseIonosphericDelayModifier.modify(EstimatedMeasurement<Phase> estimated)
void	PhaseTroposphericDelayModifier.modify(EstimatedMeasurement<Phase> estimated)	Apply a modifier to an estimated measurement.
void	RangeIonosphericDelayModifier.modify(EstimatedMeasurement<Range> estimated)	Apply a modifier to an estimated measurement.
static <T extends ObservedMeasurement<T>> void	RangeModifierUtil.modify(EstimatedMeasurement<T> estimated, ParameterDriversProvider parametricModel, AbstractGradientConverter converter, Observer observer, ParametricModelEffect modelEffect, ParametricModelEffectGradient modelEffectGradient, EstimationModifier<T> modifier)	Apply a modifier to an estimated measurement.
void	RangeRateIonosphericDelayModifier.modify(EstimatedMeasurement<RangeRate> estimated)	Apply a modifier to an estimated measurement.
static <T extends ObservedMeasurement<T>> void	RangeRateModifierUtil.modify(EstimatedMeasurement<T> estimated, ParameterDriversProvider parametricModel, AbstractGradientConverter converter, Observer observer, ParametricModelEffect modelEffect, ParametricModelEffectGradient modelEffectGradient, EstimationModifier<T> modifier)	Apply a modifier to an estimated measurement.
void	RangeRateTroposphericDelayModifier.modify(EstimatedMeasurement<RangeRate> estimated)	Apply a modifier to an estimated measurement.
void	RangeTroposphericDelayModifier.modify(EstimatedMeasurement<Range> estimated)	Apply a modifier to an estimated measurement.
void	TDOAIonosphericDelayModifier.modify(EstimatedMeasurement<TDOA> estimated)
void	TDOATroposphericDelayModifier.modify(EstimatedMeasurement<TDOA> estimated)	Apply a modifier to an estimated measurement.
void	TurnAroundRangeIonosphericDelayModifier.modify(EstimatedMeasurement<TurnAroundRange> estimated)
void	TurnAroundRangeTroposphericDelayModifier.modify(EstimatedMeasurement<TurnAroundRange> estimated)	Apply a modifier to an estimated measurement.

Uses of EstimatedMeasurement in org.orekit.estimation.sequential

Methods in org.orekit.estimation.sequential that return EstimatedMeasurement

Modifier and Type	Method	Description
EstimatedMeasurement<?>	KalmanEstimation.getCorrectedMeasurement()	Get the estimated measurement.
EstimatedMeasurement<?>	SemiAnalyticalKalmanModel.getCorrectedMeasurement()	Get the estimated measurement.
EstimatedMeasurement<?>	SemiAnalyticalUnscentedKalmanModel.getCorrectedMeasurement()	Get the estimated measurement.
EstimatedMeasurement<?>	KalmanEstimation.getPredictedMeasurement()	Get the predicted measurement.
EstimatedMeasurement<?>	SemiAnalyticalKalmanModel.getPredictedMeasurement()	Get the predicted measurement.
EstimatedMeasurement<?>	SemiAnalyticalUnscentedKalmanModel.getPredictedMeasurement()	Get the predicted measurement.

Methods in org.orekit.estimation.sequential with parameters of type EstimatedMeasurement

Modifier and Type	Method	Description
static <T extends ObservedMeasurement<T>> void	KalmanEstimatorUtil.applyDynamicOutlierFilter(EstimatedMeasurement<T> measurement, RealMatrix innovationCovarianceMatrix)	Set and apply a dynamic outlier filter on a measurement.
static RealVector	KalmanEstimatorUtil.computeInnovationVector(EstimatedMeasurement<?> predicted)	Compute the unnormalized innovation vector from the given predicted measurement.
static RealVector	KalmanEstimatorUtil.computeInnovationVector(EstimatedMeasurement<?> predicted, double[] sigma)	Compute the normalized innovation vector from the given predicted measurement.