Class BistaticRange
- java.lang.Object
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- org.orekit.estimation.measurements.AbstractMeasurement<T>
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- org.orekit.estimation.measurements.GroundReceiverMeasurement<T>
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- org.orekit.estimation.measurements.BistaticRange
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- All Implemented Interfaces:
Comparable<ComparableMeasurement>,ComparableMeasurement,ObservedMeasurement<BistaticRange>,TimeStamped,ParameterDriversProvider
public class BistaticRange extends GroundReceiverMeasurement<T>
Class modeling a bistatic range measurement using an emitter ground station and a receiver ground station.The measurement is considered to be a signal:
- Emitted from the emitter ground station
- Reflected on the spacecraft
- Received on the receiver ground station
The motion of the stations and the spacecraft during the signal flight time are taken into account.
- Since:
- 11.2
- Author:
- Mark Rutten
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Field Summary
Fields Modifier and Type Field Description static StringMEASUREMENT_TYPEType of the measurement.
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Constructor Summary
Constructors Constructor Description BistaticRange(GroundStation emitter, GroundStation receiver, AbsoluteDate date, double range, double sigma, double baseWeight, ObservableSatellite satellite)Simple constructor.BistaticRange(GroundStation emitter, GroundStation receiver, AbsoluteDate date, double range, double sigma, double baseWeight, SignalTravelTimeModel signalTravelTimeModel, ObservableSatellite satellite)Simple constructor.
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Method Summary
All Methods Instance Methods Concrete Methods Modifier and Type Method Description protected voidfillEstimation(Gradient quantity, Map<String,Integer> paramIndices, EstimatedMeasurement<T> estimated)Fill estimated measurements with value and derivatives.GroundStationgetEmitterStation()Get the emitter ground station.protected Gradient[]getFieldShifts(SpacecraftState[] states)Method computing consecutive Field time shifts of participants, starting from observation date.protected TimeStampedPVCoordinates[]getParticipants(SpacecraftState state)Method returning the full kinematic coordinates of signal participants at transmission dates.TwoLegsSignalTravelTimergetTwoLegsSignalTimer()Getter for the two legs timer.protected EstimatedMeasurement<BistaticRange>theoreticalEvaluation(int iteration, int evaluation, SpacecraftState[] states)Estimate the theoretical value.protected EstimatedMeasurementBase<BistaticRange>theoreticalEvaluationWithoutDerivatives(int iteration, int evaluation, SpacecraftState[] states)Estimate the theoretical value without derivatives.-
Methods inherited from class org.orekit.estimation.measurements.GroundReceiverMeasurement
computeEmissionDate, computeEmissionDateField, getCorrectedReceptionDate, getCorrectedReceptionDateField, getParameterIndices, getReceiverStation
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Methods inherited from class org.orekit.estimation.measurements.AbstractMeasurement
addModifier, addParameterDriver, addParametersDrivers, estimate, estimateWithoutDerivatives, getBaseWeight, getCoordinates, getDate, getDimension, getModifiers, getObservedValue, getParametersDrivers, getSatellites, getSignalTravelTimeModel, getTheoreticalStandardDeviation, isEnabled, isTwoWay, setEnabled, setObservedValue
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Methods inherited from class java.lang.Object
clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait
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Methods inherited from interface org.orekit.estimation.measurements.ComparableMeasurement
compareTo
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Methods inherited from interface org.orekit.estimation.measurements.ObservedMeasurement
estimateWithoutDerivatives, getMeasurementType
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Methods inherited from interface org.orekit.utils.ParameterDriversProvider
getNbParametersDriversValue, getParameterDriver, getParameters, getParameters, getParameters, getParameters, getParametersAllValues, getParametersAllValues, isSupported
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Methods inherited from interface org.orekit.time.TimeStamped
durationFrom
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Field Detail
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MEASUREMENT_TYPE
public static final String MEASUREMENT_TYPE
Type of the measurement.- See Also:
- Constant Field Values
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Constructor Detail
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BistaticRange
public BistaticRange(GroundStation emitter, GroundStation receiver, AbsoluteDate date, double range, double sigma, double baseWeight, ObservableSatellite satellite)
Simple constructor.- Parameters:
emitter- ground station from which transmission is performedreceiver- ground station from which measurement is performeddate- date of the measurementrange- observed valuesigma- theoretical standard deviationbaseWeight- base weightsatellite- satellite related to this measurement- Since:
- 11.2
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BistaticRange
public BistaticRange(GroundStation emitter, GroundStation receiver, AbsoluteDate date, double range, double sigma, double baseWeight, SignalTravelTimeModel signalTravelTimeModel, ObservableSatellite satellite)
Simple constructor.- Parameters:
emitter- ground station from which transmission is performedreceiver- ground station from which measurement is performeddate- date of the measurementrange- observed valuesigma- theoretical standard deviationbaseWeight- base weightsignalTravelTimeModel- signal travel time modelsatellite- satellite related to this measurement- Since:
- 14.0
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Method Detail
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theoreticalEvaluationWithoutDerivatives
protected EstimatedMeasurementBase<BistaticRange> theoreticalEvaluationWithoutDerivatives(int iteration, int evaluation, SpacecraftState[] states)
Estimate the theoretical value without derivatives. The default implementation uses the computation with derivatives and ought to be overwritten for performance.The theoretical value does not have any modifiers applied.
- Overrides:
theoreticalEvaluationWithoutDerivativesin classAbstractMeasurement<BistaticRange>- Parameters:
iteration- iteration numberevaluation- evaluation numberstates- orbital states at measurement date- Returns:
- theoretical value
- See Also:
AbstractMeasurement.estimate(int, int, SpacecraftState[])
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theoreticalEvaluation
protected EstimatedMeasurement<BistaticRange> theoreticalEvaluation(int iteration, int evaluation, SpacecraftState[] states)
Estimate the theoretical value.The theoretical value does not have any modifiers applied.
- Specified by:
theoreticalEvaluationin classAbstractMeasurement<BistaticRange>- Parameters:
iteration- iteration numberevaluation- evaluation numberstates- orbital states at measurement date- Returns:
- theoretical value
- See Also:
AbstractMeasurement.estimate(int, int, SpacecraftState[])
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getTwoLegsSignalTimer
public TwoLegsSignalTravelTimer getTwoLegsSignalTimer()
Getter for the two legs timer.- Returns:
- model
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getEmitterStation
public GroundStation getEmitterStation()
Get the emitter ground station.- Returns:
- emitter ground station
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getParticipants
protected TimeStampedPVCoordinates[] getParticipants(SpacecraftState state)
Method returning the full kinematic coordinates of signal participants at transmission dates.- Parameters:
state- observable state- Returns:
- signal participants
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getFieldShifts
protected Gradient[] getFieldShifts(SpacecraftState[] states)
Method computing consecutive Field time shifts of participants, starting from observation date.- Parameters:
states- observables- Returns:
- time shifts
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fillEstimation
protected void fillEstimation(Gradient quantity, Map<String,Integer> paramIndices, EstimatedMeasurement<T> estimated)
Fill estimated measurements with value and derivatives.- Parameters:
quantity- estimated quantityparamIndices- indices mapping parameter names to derivative indicesestimated- theoretical measurement class
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