Uses of Class
org.orekit.estimation.measurements.EstimatedMeasurementBase
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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. -
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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 anobserved 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>
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 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 Constructor Description 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
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
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 protected <T extends ObservedMeasurement<T>>
voidAbstractShapiroBaseModifier. doModify(EstimationModifier<T> modifier, EstimatedMeasurementBase<T> estimated)
Modify measurement.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.void
AngularIonosphericDelayModifier. modifyWithoutDerivatives(EstimatedMeasurementBase<AngularAzEl> estimated)
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
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
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>>
voidRangeModifierUtil. modifyWithoutDerivatives(EstimatedMeasurementBase<T> estimated, GroundStation station, 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>>
voidRangeRateModifierUtil. modifyWithoutDerivatives(EstimatedMeasurementBase<T> estimated, GroundStation station, 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
ShapiroInterSatelliteRangeModifier. modifyWithoutDerivatives(EstimatedMeasurementBase<InterSatellitesRange> 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
ShapiroOneWayGNSSRangeModifier. modifyWithoutDerivatives(EstimatedMeasurementBase<OneWayGNSSRange> 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
ShapiroRangeModifier. modifyWithoutDerivatives(EstimatedMeasurementBase<Range> 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.
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