Uses of Interface
org.orekit.estimation.measurements.Observer

Packages that use Observer

Package	Description
org.orekit.estimation.measurements	The measurements package defines everything that is related to orbit determination measurements.
org.orekit.estimation.measurements.modifiers	This package provides measurement modifier.

Uses of Observer in org.orekit.estimation.measurements

Classes in org.orekit.estimation.measurements that implement Observer

Modifier and Type	Class	Description
class	GroundStation	Class modeling a ground station that can perform some measurements.
class	ObserverSatellite	Class that accepts a PVCoordinatesProvider for a space- based measurement receiver.

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

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

Modifier and Type	Method	Description
double	ParametricModelEffect.evaluate(Observer station, SpacecraftState state)	Evaluate the parametric model effect.
Gradient	ParametricModelEffectGradient.evaluate(Observer station, FieldSpacecraftState<Gradient> state, Gradient[] parameters)	Evaluate the parametric model effect.
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.
static <T extends ObservedMeasurement<T>> void	RangeModifierUtil.modify(EstimatedMeasurement<T> estimated, ParameterDriversProvider parametricModel, AbstractGradientConverter converter, Observer station, ParametricModelEffect modelEffect, ParametricModelEffectGradient modelEffectGradient, EstimationModifier<T> modifier)	Apply a modifier to an estimated measurement.
static <T extends ObservedMeasurement<T>> void	RangeRateModifierUtil.modify(EstimatedMeasurement<T> estimated, ParameterDriversProvider parametricModel, AbstractGradientConverter converter, Observer station, ParametricModelEffect modelEffect, ParametricModelEffectGradient modelEffectGradient, EstimationModifier<T> modifier)	Apply a modifier to an estimated measurement.
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.
static <T extends ObservedMeasurement<T>> void	RangeModifierUtil.modifyWithoutDerivatives(EstimatedMeasurementBase<T> estimated, Observer station, ParametricModelEffect modelEffect, EstimationModifier<T> modifier)	Apply a modifier to an estimated measurement.
static <T extends ObservedMeasurement<T>> void	RangeRateModifierUtil.modifyWithoutDerivatives(EstimatedMeasurementBase<T> estimated, Observer station, ParametricModelEffect modelEffect, EstimationModifier<T> modifier)	Apply a modifier to an estimated measurement.
protected <T extends CalculusFieldElement<T>> T	BaseOneWayGNSSRangeIonosphericDelayModifier.oneWayGNSSErrorIonosphericModel(Observer observer, FieldSpacecraftState<T> state, T[] parameters)	Compute the measurement error due to Ionosphere.
protected double	BaseOneWayGNSSRangeIonosphericDelayModifier.oneWayGNSSErrorIonosphericModel(Observer observer, SpacecraftState state)	Compute the measurement error due to Ionosphere.
protected <T extends CalculusFieldElement<T>> T	BaseRangeIonosphericDelayModifier.rangeErrorIonosphericModel(Observer station, FieldSpacecraftState<T> state, T[] parameters)	Compute the measurement error due to Ionosphere.
protected double	BaseRangeIonosphericDelayModifier.rangeErrorIonosphericModel(Observer station, SpacecraftState state)	Compute the measurement error due to Ionosphere.
<T extends CalculusFieldElement<T>> T	BaseRangeTroposphericDelayModifier.rangeErrorTroposphericModel(Observer observer, FieldSpacecraftState<T> state, T[] parameters)	Compute the measurement error due to Troposphere.
double	BaseRangeTroposphericDelayModifier.rangeErrorTroposphericModel(Observer observer, SpacecraftState state)	Compute the measurement error due to Troposphere.
protected <T extends CalculusFieldElement<T>> T	BaseRangeRateIonosphericDelayModifier.rangeRateErrorIonosphericModel(Observer station, FieldSpacecraftState<T> state, T[] parameters)	Compute the measurement error due to Ionosphere.
protected double	BaseRangeRateIonosphericDelayModifier.rangeRateErrorIonosphericModel(Observer station, SpacecraftState state)	Compute the measurement error due to Ionosphere.
protected <T extends CalculusFieldElement<T>> T	RangeRateIonosphericDelayModifier.rangeRateErrorIonosphericModel(Observer station, FieldSpacecraftState<T> state, T[] parameters)	Compute the measurement error due to Ionosphere.
protected double	RangeRateIonosphericDelayModifier.rangeRateErrorIonosphericModel(Observer station, SpacecraftState state)	Compute the measurement error due to Ionosphere.
<T extends CalculusFieldElement<T>> T	BaseRangeRateTroposphericDelayModifier.rangeRateErrorTroposphericModel(Observer observer, FieldSpacecraftState<T> state, T[] parameters)	Compute the measurement error due to Troposphere.
double	BaseRangeRateTroposphericDelayModifier.rangeRateErrorTroposphericModel(Observer observer, SpacecraftState state)	Compute the measurement error due to Troposphere.
<T extends CalculusFieldElement<T>> T	RangeRateTroposphericDelayModifier.rangeRateErrorTroposphericModel(Observer station, FieldSpacecraftState<T> state, T[] parameters)	Compute the measurement error due to Troposphere.
double	RangeRateTroposphericDelayModifier.rangeRateErrorTroposphericModel(Observer station, SpacecraftState state)	Compute the measurement error due to Troposphere.