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

Packages that use GroundStation

Package	Description
org.orekit.estimation.measurements	The measurements package defines everything that is related to orbit determination measurements.
org.orekit.estimation.measurements.filtering	This package provides measurement pre-processing filters.
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 GroundStation in org.orekit.estimation.measurements

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

Modifier and Type	Method	Description
GroundStation	BistaticRange.getEmitterStation()	Get the emitter ground station.
GroundStation	BistaticRangeRate.getEmitterStation()	Get the emitter ground station.
GroundStation	TurnAroundRange.getPrimaryStation()	Get the primary ground station from which measurement is performed.
GroundStation	FDOA.getPrimeStation()	Get the prime ground station, the one that gives the date of the measurement.
GroundStation	TDOA.getPrimeStation()	Get the prime ground station, the one that gives the date of the measurement.
GroundStation	BistaticRange.getReceiverStation()	Get the receiver ground station.
GroundStation	BistaticRangeRate.getReceiverStation()	Get the receiver ground station.
GroundStation	TurnAroundRange.getSecondaryStation()	Get the secondary ground station reflecting the signal.
GroundStation	FDOA.getSecondStation()	Get the second ground station, the one that gives the measurement.
GroundStation	TDOA.getSecondStation()	Get the second ground station, the one that gives the measurement.
GroundStation	GroundReceiverMeasurement.getStation()	Get the ground station from which measurement is performed.

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

Constructor	Description
AngularAzEl(GroundStation station, AbsoluteDate date, double[] angular, double[] sigma, double[] baseWeight, ObservableSatellite satellite)	Simple constructor.
AngularRaDec(GroundStation station, Frame referenceFrame, AbsoluteDate date, double[] angular, double[] sigma, double[] baseWeight, ObservableSatellite satellite)	Simple constructor.
BistaticRange(GroundStation emitter, GroundStation receiver, AbsoluteDate date, double range, double sigma, double baseWeight, ObservableSatellite satellite)	Simple constructor.
BistaticRangeRate(GroundStation emitter, GroundStation receiver, AbsoluteDate date, double rangeRate, double sigma, double baseWeight, ObservableSatellite satellite)	Simple constructor.
FDOA(GroundStation primeStation, GroundStation secondStation, double centreFrequency, AbsoluteDate date, double fdoa, double sigma, double baseWeight, ObservableSatellite satellite)	Simple constructor.
GroundReceiverMeasurement(GroundStation station, boolean twoWay, AbsoluteDate date, double[] observed, double[] sigma, double[] baseWeight, ObservableSatellite satellite)	Simple constructor.
GroundReceiverMeasurement(GroundStation station, boolean twoWay, AbsoluteDate date, double observed, double sigma, double baseWeight, ObservableSatellite satellite)	Simple constructor.
Range(GroundStation station, boolean twoWay, AbsoluteDate date, double range, double sigma, double baseWeight, ObservableSatellite satellite)	Simple constructor.
RangeRate(GroundStation station, AbsoluteDate date, double rangeRate, double sigma, double baseWeight, boolean twoway, ObservableSatellite satellite)	Simple constructor.
TDOA(GroundStation primeStation, GroundStation secondStation, AbsoluteDate date, double tdoa, double sigma, double baseWeight, ObservableSatellite satellite)	Simple constructor.
TurnAroundRange(GroundStation primaryStation, GroundStation secondaryStation, AbsoluteDate date, double turnAroundRange, double sigma, double baseWeight, ObservableSatellite satellite)	Simple constructor.

Uses of GroundStation in org.orekit.estimation.measurements.filtering

Constructors in org.orekit.estimation.measurements.filtering with parameters of type GroundStation

Constructor	Description
ElevationFilter(GroundStation station, double threshold)	Constructor.

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

Constructors in org.orekit.estimation.measurements.generation with parameters of type GroundStation

Constructor	Description
AngularAzElBuilder(CorrelatedRandomVectorGenerator noiseSource, GroundStation station, double[] sigma, double[] baseWeight, ObservableSatellite satellite)	Simple constructor.
AngularRaDecBuilder(CorrelatedRandomVectorGenerator noiseSource, GroundStation station, Frame referenceFrame, double[] sigma, double[] baseWeight, ObservableSatellite satellite)	Simple constructor.
BistaticRangeBuilder(CorrelatedRandomVectorGenerator noiseSource, GroundStation emitter, GroundStation receiver, double sigma, double baseWeight, ObservableSatellite satellite)	Simple constructor.
BistaticRangeRateBuilder(CorrelatedRandomVectorGenerator noiseSource, GroundStation emitter, GroundStation receiver, double sigma, double baseWeight, ObservableSatellite satellite)	Simple constructor.
FDOABuilder(CorrelatedRandomVectorGenerator noiseSource, GroundStation primeStation, GroundStation secondStation, double centreFrequency, double sigma, double baseWeight, ObservableSatellite satellite)	Simple constructor.
RangeBuilder(CorrelatedRandomVectorGenerator noiseSource, GroundStation station, boolean twoWay, double sigma, double baseWeight, ObservableSatellite satellite)	Simple constructor.
RangeRateBuilder(CorrelatedRandomVectorGenerator noiseSource, GroundStation station, boolean twoWay, double sigma, double baseWeight, ObservableSatellite satellite)	Simple constructor.
TDOABuilder(CorrelatedRandomVectorGenerator noiseSource, GroundStation primeStation, GroundStation secondStation, double sigma, double baseWeight, ObservableSatellite satellite)	Simple constructor.
TurnAroundRangeBuilder(CorrelatedRandomVectorGenerator noiseSource, GroundStation primaryStation, GroundStation secondaryStation, double sigma, double baseWeight, ObservableSatellite satellite)	Simple constructor.

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

Constructors in org.orekit.estimation.measurements.gnss with parameters of type GroundStation

Constructor	Description
Phase(GroundStation station, AbsoluteDate date, double phase, double wavelength, double sigma, double baseWeight, ObservableSatellite satellite, AmbiguityCache cache)	Simple constructor.
PhaseBuilder(CorrelatedRandomVectorGenerator noiseSource, GroundStation station, double wavelength, double sigma, double baseWeight, ObservableSatellite satellite, AmbiguityCache cache)	Simple constructor.

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

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

Modifier and Type	Method	Description
double	ParametricModelEffect.evaluate(GroundStation station, SpacecraftState state)	Evaluate the parametric model effect.
Gradient	ParametricModelEffectGradient.evaluate(GroundStation station, FieldSpacecraftState<Gradient> state, Gradient[] parameters)	Evaluate the parametric model effect.
static <T extends ObservedMeasurement<T>> void	RangeModifierUtil.modify(EstimatedMeasurement<T> estimated, ParameterDriversProvider parametricModel, AbstractGradientConverter converter, GroundStation 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, GroundStation station, ParametricModelEffect modelEffect, ParametricModelEffectGradient modelEffectGradient, EstimationModifier<T> modifier)	Apply a modifier to an estimated measurement.
static <T extends ObservedMeasurement<T>> void	RangeModifierUtil.modifyWithoutDerivatives(EstimatedMeasurementBase<T> estimated, GroundStation station, ParametricModelEffect modelEffect, EstimationModifier<T> modifier)	Apply a modifier to an estimated measurement.
static <T extends ObservedMeasurement<T>> void	RangeRateModifierUtil.modifyWithoutDerivatives(EstimatedMeasurementBase<T> estimated, GroundStation station, ParametricModelEffect modelEffect, EstimationModifier<T> modifier)	Apply a modifier to an estimated measurement.
static double[]	AberrationModifier.naturalToProper(double[] naturalRaDec, GroundStation station, AbsoluteDate date, Frame frame)	Natural to proper correction for aberration of light.
static double[]	AberrationModifier.naturalToProper(double[] naturalRaDec, GroundStation station, AbsoluteDate date, Frame frame, DataContext context)	Natural to proper correction for aberration of light.
static double[]	AberrationModifier.properToNatural(double[] properRaDec, GroundStation station, AbsoluteDate date, Frame frame)	Proper to natural correction for aberration of light.
static double[]	AberrationModifier.properToNatural(double[] properRaDec, GroundStation station, AbsoluteDate date, Frame frame, DataContext context)	Proper to natural correction for aberration of light.
protected <T extends CalculusFieldElement<T>> T	BaseRangeIonosphericDelayModifier.rangeErrorIonosphericModel(GroundStation station, FieldSpacecraftState<T> state, T[] parameters)	Compute the measurement error due to Ionosphere.
protected double	BaseRangeIonosphericDelayModifier.rangeErrorIonosphericModel(GroundStation station, SpacecraftState state)	Compute the measurement error due to Ionosphere.
<T extends CalculusFieldElement<T>> T	BaseRangeTroposphericDelayModifier.rangeErrorTroposphericModel(GroundStation station, FieldSpacecraftState<T> state, T[] parameters)	Compute the measurement error due to Troposphere.
double	BaseRangeTroposphericDelayModifier.rangeErrorTroposphericModel(GroundStation station, SpacecraftState state)	Compute the measurement error due to Troposphere.
protected <T extends CalculusFieldElement<T>> T	BaseRangeRateIonosphericDelayModifier.rangeRateErrorIonosphericModel(GroundStation station, FieldSpacecraftState<T> state, T[] parameters)	Compute the measurement error due to Ionosphere.
protected double	BaseRangeRateIonosphericDelayModifier.rangeRateErrorIonosphericModel(GroundStation station, SpacecraftState state)	Compute the measurement error due to Ionosphere.
protected <T extends CalculusFieldElement<T>> T	RangeRateIonosphericDelayModifier.rangeRateErrorIonosphericModel(GroundStation station, FieldSpacecraftState<T> state, T[] parameters)	Compute the measurement error due to Ionosphere.
protected double	RangeRateIonosphericDelayModifier.rangeRateErrorIonosphericModel(GroundStation station, SpacecraftState state)	Compute the measurement error due to Ionosphere.
<T extends CalculusFieldElement<T>> T	BaseRangeRateTroposphericDelayModifier.rangeRateErrorTroposphericModel(GroundStation station, FieldSpacecraftState<T> state, T[] parameters)	Compute the measurement error due to Troposphere.
double	BaseRangeRateTroposphericDelayModifier.rangeRateErrorTroposphericModel(GroundStation station, SpacecraftState state)	Compute the measurement error due to Troposphere.
<T extends CalculusFieldElement<T>> T	RangeRateTroposphericDelayModifier.rangeRateErrorTroposphericModel(GroundStation station, FieldSpacecraftState<T> state, T[] parameters)	Compute the measurement error due to Troposphere.
double	RangeRateTroposphericDelayModifier.rangeRateErrorTroposphericModel(GroundStation station, SpacecraftState state)	Compute the measurement error due to Troposphere.