public class RangeRate extends AbstractMeasurement<RangeRate>
Constructor and Description |
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RangeRate(GroundStation station,
AbsoluteDate date,
double rangeRate,
double sigma,
double baseWeight,
boolean twoway,
ObservableSatellite satellite)
Simple constructor.
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Modifier and Type | Method and Description |
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GroundStation |
getStation()
Get the ground station from which measurement is performed.
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boolean |
isTwoWay()
Check if the instance represents a two-way measurement.
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protected EstimatedMeasurement<RangeRate> |
theoreticalEvaluation(int iteration,
int evaluation,
SpacecraftState[] states)
Estimate the theoretical value.
|
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 RangeRate(GroundStation station, AbsoluteDate date, double rangeRate, double sigma, double baseWeight, boolean twoway, ObservableSatellite satellite)
station
- ground station from which measurement is performeddate
- date of the measurementrangeRate
- observed value, m/ssigma
- theoretical standard deviationbaseWeight
- base weighttwoway
- if true, this is a two-way measurementsatellite
- satellite related to this measurementpublic boolean isTwoWay()
public GroundStation getStation()
protected EstimatedMeasurement<RangeRate> theoreticalEvaluation(int iteration, int evaluation, SpacecraftState[] states)
The theoretical value does not have any modifiers applied.
theoreticalEvaluation
in class AbstractMeasurement<RangeRate>
iteration
- iteration numberevaluation
- evaluation numberstates
- orbital states at measurement dateAbstractMeasurement.estimate(int, int, SpacecraftState[])
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