public class BistaticRange extends GroundReceiverMeasurement<BistaticRange>
The measurement is considered to be a signal:
The motion of the stations and the spacecraft during the signal flight time are taken into account.
Modifier and Type | Field and Description |
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static String |
MEASUREMENT_TYPE
Type of the measurement.
|
Constructor and Description |
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BistaticRange(GroundStation emitter,
GroundStation receiver,
AbsoluteDate date,
double range,
double sigma,
double baseWeight,
ObservableSatellite satellite)
Simple constructor.
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Modifier and Type | Method and Description |
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GroundStation |
getEmitterStation()
Get the emitter ground station.
|
GroundStation |
getReceiverStation()
Get the receiver ground station.
|
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.
|
computeCommonParametersWithDerivatives, computeCommonParametersWithout, getGroundStationCoordinates, getGroundStationPosition, getStation, isTwoWay
addModifier, addParameterDriver, estimate, estimateWithoutDerivatives, getBaseWeight, getCoordinates, getDate, getDimension, getModifiers, getObservedValue, getParametersDrivers, getSatellites, getTheoreticalStandardDeviation, isEnabled, setEnabled, signalTimeOfFlight, signalTimeOfFlight
clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait
getMeasurementType
compareTo
durationFrom
getNbParametersDriversValue, getParameterDriver, getParameters, getParameters, getParameters, getParameters, getParametersAllValues, getParametersAllValues, isSupported
public static final String MEASUREMENT_TYPE
public BistaticRange(GroundStation emitter, GroundStation receiver, AbsoluteDate date, double range, double sigma, double baseWeight, ObservableSatellite satellite)
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 measurementpublic GroundStation getEmitterStation()
public GroundStation getReceiverStation()
protected EstimatedMeasurementBase<BistaticRange> theoreticalEvaluationWithoutDerivatives(int iteration, int evaluation, SpacecraftState[] states)
The theoretical value does not have any modifiers applied.
theoreticalEvaluationWithoutDerivatives
in class AbstractMeasurement<BistaticRange>
iteration
- iteration numberevaluation
- evaluation numberstates
- orbital states at measurement dateAbstractMeasurement.estimate(int, int, SpacecraftState[])
protected EstimatedMeasurement<BistaticRange> theoreticalEvaluation(int iteration, int evaluation, SpacecraftState[] states)
The theoretical value does not have any modifiers applied.
theoreticalEvaluation
in class AbstractMeasurement<BistaticRange>
iteration
- iteration numberevaluation
- evaluation numberstates
- orbital states at measurement dateAbstractMeasurement.estimate(int, int, SpacecraftState[])
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