Class OneWayGNSSPhase
- 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<OneWayGNSSPhase>
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- org.orekit.estimation.measurements.gnss.OneWayGNSSPhase
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- All Implemented Interfaces:
Comparable<ComparableMeasurement>
,ComparableMeasurement
,ObservedMeasurement<OneWayGNSSPhase>
,TimeStamped
,ParameterDriversProvider
public class OneWayGNSSPhase extends AbstractOneWayGNSSMeasurement<OneWayGNSSPhase>
One-way GNSS phase measurement.This class can be used in precise orbit determination applications for modeling a phase measurement between a GNSS satellite (emitter) and a LEO satellite (receiver).
The one-way GNSS phase 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
InterSatellitesPhase
measurement class. However, using the one-way GNSS phase measurement, the orbit and clock of the emitting GNSS satellite are NOT estimated simultaneously with LEO satellite coordinates.- Since:
- 10.3
- Author:
- Bryan Cazabonne
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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 OneWayGNSSPhase(PVCoordinatesProvider remote, String remoteName, QuadraticClockModel remoteClock, AbsoluteDate date, double phase, double wavelength, double sigma, double baseWeight, ObservableSatellite local, AmbiguityCache cache)
Simple constructor.
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Method Summary
All Methods Instance Methods Concrete Methods Modifier and Type Method Description AmbiguityDriver
getAmbiguityDriver()
Get the driver for phase ambiguity.double
getWavelength()
Get the wavelength.protected EstimatedMeasurement<OneWayGNSSPhase>
theoreticalEvaluation(int iteration, int evaluation, SpacecraftState[] states)
Estimate the theoretical value.protected EstimatedMeasurementBase<OneWayGNSSPhase>
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, setObservedValue, signalTimeOfFlightAdjustableEmitter, signalTimeOfFlightAdjustableEmitter, signalTimeOfFlightAdjustableEmitter, signalTimeOfFlightAdjustableEmitter, signalTimeOfFlightAdjustableReceiver, signalTimeOfFlightAdjustableReceiver, signalTimeOfFlightAdjustableReceiver, signalTimeOfFlightAdjustableReceiver
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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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OneWayGNSSPhase
public OneWayGNSSPhase(PVCoordinatesProvider remote, String remoteName, QuadraticClockModel remoteClock, AbsoluteDate date, double phase, double wavelength, double sigma, double baseWeight, ObservableSatellite local, AmbiguityCache cache)
Simple constructor.- Parameters:
remote
- provider for GNSS satellite which simply emits the signalremoteName
- name of the remoteremoteClock
- clock offset of the GNSS satellitedate
- date of the measurementphase
- observed value, in cycleswavelength
- phase observed value wavelength, in meterssigma
- theoretical standard deviationbaseWeight
- base weightlocal
- satellite which receives the signal and perform the measurementcache
- from which ambiguity drive should come- Since:
- 12.1
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Method Detail
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getWavelength
public double getWavelength()
Get the wavelength.- Returns:
- wavelength (m)
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getAmbiguityDriver
public AmbiguityDriver getAmbiguityDriver()
Get the driver for phase ambiguity.- Returns:
- the driver for phase ambiguity
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theoreticalEvaluationWithoutDerivatives
protected EstimatedMeasurementBase<OneWayGNSSPhase> 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:
theoreticalEvaluationWithoutDerivatives
in classAbstractMeasurement<OneWayGNSSPhase>
- 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<OneWayGNSSPhase> 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<OneWayGNSSPhase>
- 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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