public class BistaticRange extends AbstractMeasurement<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.
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() |
GroundStation |
getReceiverStation() |
protected EstimatedMeasurement<BistaticRange> |
theoreticalEvaluation(int iteration,
int evaluation,
SpacecraftState[] states)
Estimate the theoretical value.
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addModifier, addParameterDriver, estimate, getBaseWeight, getCoordinates, getDate, getDimension, getModifiers, getObservedValue, getParametersDrivers, getSatellites, getTheoreticalStandardDeviation, isEnabled, setEnabled, signalTimeOfFlight, signalTimeOfFlight
clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait
compareTo
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 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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