Class OneWayGNSSRangeRate
- java.lang.Object
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- org.orekit.estimation.measurements.AbstractMeasurement<T>
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- org.orekit.estimation.measurements.gnss.AbstractOnBoardMeasurement<T>
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- org.orekit.estimation.measurements.gnss.AbstractOneWayGNSSMeasurement<OneWayGNSSRangeRate>
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- org.orekit.estimation.measurements.gnss.OneWayGNSSRangeRate
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- All Implemented Interfaces:
Comparable<ComparableMeasurement>
,ComparableMeasurement
,ObservedMeasurement<OneWayGNSSRangeRate>
,TimeStamped
,ParameterDriversProvider
public class OneWayGNSSRangeRate extends AbstractOneWayGNSSMeasurement<OneWayGNSSRangeRate>
One-way GNSS range rate measurement.This class can be used in precise orbit determination applications for modeling a range rate measurement between a GNSS satellite (emitter) and a LEO satellite (receiver).
The one-way GNSS range rate measurement assumes knowledge of the orbit and the clock offset of the emitting GNSS satellite. For instance, it is possible to use a SP3 file or a GNSS navigation message to recover the satellite's orbit and clock.
This class is very similar to
InterSatellitesOneWayRangeRate
measurement class. However, using the one-way GNSS range measurement, the orbit and clock of the emitting GNSS satellite are NOT estimated simultaneously with LEO satellite coordinates.- Since:
- 12.1
- Author:
- Luc Maisonobe
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Field Summary
Fields Modifier and Type Field Description static String
MEASUREMENT_TYPE
Type of the measurement.
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Constructor Summary
Constructors Constructor Description OneWayGNSSRangeRate(PVCoordinatesProvider remote, double dtRemote, AbsoluteDate date, double rangeRate, double sigma, double baseWeight, ObservableSatellite local)
Simple constructor.OneWayGNSSRangeRate(PVCoordinatesProvider remote, QuadraticClockModel remoteClock, AbsoluteDate date, double rangeRate, double sigma, double baseWeight, ObservableSatellite local)
Simple constructor.
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Method Summary
All Methods Instance Methods Concrete Methods Modifier and Type Method Description protected EstimatedMeasurement<OneWayGNSSRangeRate>
theoreticalEvaluation(int iteration, int evaluation, SpacecraftState[] states)
Estimate the theoretical value.protected EstimatedMeasurementBase<OneWayGNSSRangeRate>
theoreticalEvaluationWithoutDerivatives(int iteration, int evaluation, SpacecraftState[] states)
Estimate the theoretical value without derivatives.-
Methods inherited from class org.orekit.estimation.measurements.gnss.AbstractOneWayGNSSMeasurement
getRemoteClock, getRemotePV, getRemotePV
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Methods inherited from class org.orekit.estimation.measurements.gnss.AbstractOnBoardMeasurement
computeCommonParametersWith, computeCommonParametersWithout, getRemoteClock
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Methods inherited from class org.orekit.estimation.measurements.AbstractMeasurement
addModifier, addParameterDriver, estimate, estimateWithoutDerivatives, getBaseWeight, getCoordinates, getDate, getDimension, getModifiers, getObservedValue, getParametersDrivers, getSatellites, getTheoreticalStandardDeviation, isEnabled, setEnabled, signalTimeOfFlight, signalTimeOfFlight, signalTimeOfFlight, signalTimeOfFlight, signalTimeOfFlight, signalTimeOfFlight
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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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OneWayGNSSRangeRate
public OneWayGNSSRangeRate(PVCoordinatesProvider remote, double dtRemote, AbsoluteDate date, double rangeRate, double sigma, double baseWeight, ObservableSatellite local)
Simple constructor.- Parameters:
remote
- provider for GNSS satellite which simply emits the signaldtRemote
- clock offset of the GNSS satellite, in secondsdate
- date of the measurementrangeRate
- observed valuesigma
- theoretical standard deviationbaseWeight
- base weightlocal
- satellite which receives the signal and perform the measurement
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OneWayGNSSRangeRate
public OneWayGNSSRangeRate(PVCoordinatesProvider remote, QuadraticClockModel remoteClock, AbsoluteDate date, double rangeRate, double sigma, double baseWeight, ObservableSatellite local)
Simple constructor.- Parameters:
remote
- provider for GNSS satellite which simply emits the signalremoteClock
- clock offset of the GNSS satellitedate
- date of the measurementrangeRate
- observed valuesigma
- theoretical standard deviationbaseWeight
- base weightlocal
- satellite which receives the signal and perform the measurement- Since:
- 12.1
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Method Detail
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theoreticalEvaluationWithoutDerivatives
protected EstimatedMeasurementBase<OneWayGNSSRangeRate> theoreticalEvaluationWithoutDerivatives(int iteration, int evaluation, SpacecraftState[] states)
Estimate the theoretical value without derivatives.The theoretical value does not have any modifiers applied.
- Specified by:
theoreticalEvaluationWithoutDerivatives
in classAbstractMeasurement<OneWayGNSSRangeRate>
- 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<OneWayGNSSRangeRate> theoreticalEvaluation(int iteration, int evaluation, SpacecraftState[] states)
Estimate the theoretical value.The theoretical value does not have any modifiers applied.
- Specified by:
theoreticalEvaluation
in classAbstractMeasurement<OneWayGNSSRangeRate>
- 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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