Class FDOA
java.lang.Object
org.orekit.estimation.measurements.AbstractMeasurement<FDOA>
org.orekit.estimation.measurements.SignalBasedMeasurement<FDOA>
org.orekit.estimation.measurements.FDOA
- All Implemented Interfaces:
Comparable<ComparableMeasurement>,ComparableMeasurement,ObservedMeasurement<FDOA>,TimeStamped,ParameterDriversProvider
Class modeling a Frequency Difference of Arrival measurement with a satellite as emitter
and two ground stations as receivers.
FDOA measures the difference in signal arrival frequency between the emitter and receivers, corresponding to a difference in range-rate from the two receivers to the emitter.
The date of the measurement corresponds to the reception of the signal by the prime station.
The measurement corresponds to the frequency of the signal received at the prime station at
the date of the measurement minus the frequency of the signal received at the second station:
fdoa = f1 - f2
The motion of the stations and the satellite during the signal flight time are taken into account.
- Since:
- 12.0
- Author:
- Mark Rutten
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Field Summary
Fields -
Constructor Summary
ConstructorsConstructorDescriptionFDOA(Observer primeObserver, Observer secondObserver, double centreFrequency, AbsoluteDate date, double fdoa, double sigma, double baseWeight, ObservableSatellite satellite) Constructor with default signal travel time model.FDOA(Observer primeObserver, Observer secondObserver, double centreFrequency, AbsoluteDate date, double fdoa, MeasurementQuality measurementQuality, SignalTravelTimeModel signalTravelTimeModel, ObservableSatellite satellite) Constructor. -
Method Summary
Modifier and TypeMethodDescriptionprotected Gradient[]computeDelays(SpacecraftState[] states) Compute signal delays (always positive).protected voidfillEstimation(Gradient quantity, Map<String, Integer> paramIndices, EstimatedMeasurement<FDOA> estimated) Fill estimated measurements with value and derivatives.doubleGet centre frequency of carrier wave.Get the prime observer, the one that receives the signal first.Deprecated.Get the second observer, the one that gives the measurement.Deprecated.as of 14.0, replaced bygetSecondObserver()protected EstimatedMeasurement<FDOA> theoreticalEvaluation(int iteration, int evaluation, SpacecraftState[] states) Estimate the theoretical value.protected EstimatedMeasurementBase<FDOA> theoreticalEvaluationWithoutDerivatives(int iteration, int evaluation, SpacecraftState[] states) Estimate the theoretical value without derivatives.Methods inherited from class org.orekit.estimation.measurements.SignalBasedMeasurement
getSignalTravelTimeModel, isTwoWayMethods inherited from class org.orekit.estimation.measurements.AbstractMeasurement
addModifier, addParameterDriver, addParametersDrivers, estimate, estimateWithoutDerivatives, getCoordinates, getDate, getMeasurementQuality, getModifiers, getObservedValue, getParameterIndices, getParametersDrivers, getSatellites, isEnabled, setEnabled, setObservedValueMethods inherited from class java.lang.Object
clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, waitMethods inherited from interface org.orekit.estimation.measurements.ComparableMeasurement
compareToMethods inherited from interface org.orekit.estimation.measurements.ObservedMeasurement
estimateWithoutDerivatives, getBaseWeight, getDimension, getMeasurementType, getTheoreticalStandardDeviationMethods inherited from interface org.orekit.utils.ParameterDriversProvider
getNbParametersDriversValue, getParameterDriver, getParameters, getParameters, getParameters, getParameters, getParametersAllValues, getParametersAllValues, isSupportedMethods inherited from interface org.orekit.time.TimeStamped
durationFrom
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Field Details
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MEASUREMENT_TYPE
Type of the measurement.- See Also:
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Constructor Details
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FDOA
public FDOA(Observer primeObserver, Observer secondObserver, double centreFrequency, AbsoluteDate date, double fdoa, double sigma, double baseWeight, ObservableSatellite satellite) Constructor with default signal travel time model.- Parameters:
primeObserver- observer that gives the date of the measurementsecondObserver- observer that gives the measurementcentreFrequency- satellite emitter frequency (Hz)date- date of the measurementfdoa- observed value (Hz)sigma- theoretical standard deviationbaseWeight- base weightsatellite- satellite related to this measurement
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FDOA
public FDOA(Observer primeObserver, Observer secondObserver, double centreFrequency, AbsoluteDate date, double fdoa, MeasurementQuality measurementQuality, SignalTravelTimeModel signalTravelTimeModel, ObservableSatellite satellite) Constructor.- Parameters:
primeObserver- observer that gives the date of the measurementsecondObserver- observer that gives the measurementcentreFrequency- satellite emitter frequency (Hz)date- date of the measurementfdoa- observed value (Hz)measurementQuality- measurement quality data as used in orbit determinationsignalTravelTimeModel- signal travel time modelsatellite- satellite related to this measurement- Since:
- 14.0
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Method Details
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getCentreFrequency
public double getCentreFrequency()Get centre frequency of carrier wave.- Returns:
- frequency value (Hz)
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theoreticalEvaluationWithoutDerivatives
protected EstimatedMeasurementBase<FDOA> 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<FDOA>- Parameters:
iteration- iteration numberevaluation- evaluation numberstates- orbital states at measurement date- Returns:
- theoretical value
- See Also:
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theoreticalEvaluation
protected EstimatedMeasurement<FDOA> theoreticalEvaluation(int iteration, int evaluation, SpacecraftState[] states) Estimate the theoretical value.The theoretical value does not have any modifiers applied.
- Specified by:
theoreticalEvaluationin classAbstractMeasurement<FDOA>- Parameters:
iteration- iteration numberevaluation- evaluation numberstates- orbital states at measurement date- Returns:
- theoretical value
- See Also:
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getPrimeStation
Deprecated.as of 14.0, replaced bygetPrimeObserver()Get the prime ground station, the one that receives the signal first.- Returns:
- prime ground station
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getPrimeObserver
Get the prime observer, the one that receives the signal first.- Returns:
- prime observer
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getSecondStation
Deprecated.as of 14.0, replaced bygetSecondObserver()Get the second ground station, the one that receives the signal first.- Returns:
- second ground station
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getSecondObserver
Get the second observer, the one that gives the measurement.- Returns:
- second observer
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computeDelays
Compute signal delays (always positive).- Parameters:
states- observed states- Returns:
- delays (to prime and second sensors)
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fillEstimation
protected void fillEstimation(Gradient quantity, Map<String, Integer> paramIndices, EstimatedMeasurement<FDOA> 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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getPrimeObserver()