public class Phase extends GroundReceiverMeasurement<Phase>
The measurement is considered to be a signal emitted from a spacecraft and received on a ground station. Its value is the number of cycles between emission and reception. The motion of both the station and the spacecraft during the signal flight time are taken into account. The date of the measurement corresponds to the reception on ground of the emitted signal.
| Modifier and Type | Field and Description |
|---|---|
static String |
AMBIGUITY_NAME
Name for ambiguity driver.
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static String |
MEASUREMENT_TYPE
Type of the measurement.
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| Constructor and Description |
|---|
Phase(GroundStation station,
AbsoluteDate date,
double phase,
double wavelength,
double sigma,
double baseWeight,
ObservableSatellite satellite)
Simple constructor.
|
| Modifier and Type | Method and Description |
|---|---|
ParameterDriver |
getAmbiguityDriver()
Get the driver for phase ambiguity.
|
double |
getWavelength()
Get the wavelength.
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protected EstimatedMeasurement<Phase> |
theoreticalEvaluation(int iteration,
int evaluation,
SpacecraftState[] states)
Estimate the theoretical value.
|
protected EstimatedMeasurementBase<Phase> |
theoreticalEvaluationWithoutDerivatives(int iteration,
int evaluation,
SpacecraftState[] states)
Estimate the theoretical value without derivatives.
|
computeCommonParametersWithDerivatives, computeCommonParametersWithout, getGroundStationCoordinates, getGroundStationPosition, getStation, isTwoWayaddModifier, addParameterDriver, estimate, estimateWithoutDerivatives, getBaseWeight, getCoordinates, getDate, getDimension, getModifiers, getObservedValue, getParametersDrivers, getSatellites, getTheoreticalStandardDeviation, isEnabled, setEnabled, signalTimeOfFlight, signalTimeOfFlightclone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, waitgetMeasurementTypecompareTodurationFromgetNbParametersDriversValue, getParameterDriver, getParameters, getParameters, getParameters, getParameters, getParametersAllValues, getParametersAllValues, isSupportedpublic static final String MEASUREMENT_TYPE
public static final String AMBIGUITY_NAME
public Phase(GroundStation station, AbsoluteDate date, double phase, double wavelength, double sigma, double baseWeight, ObservableSatellite satellite)
station - ground station from which measurement is performeddate - date of the measurementphase - observed value (cycles)wavelength - phase observed value wavelength (m)sigma - theoretical standard deviationbaseWeight - base weightsatellite - satellite related to this measurementpublic double getWavelength()
public ParameterDriver getAmbiguityDriver()
protected EstimatedMeasurementBase<Phase> theoreticalEvaluationWithoutDerivatives(int iteration, int evaluation, SpacecraftState[] states)
The theoretical value does not have any modifiers applied.
theoreticalEvaluationWithoutDerivatives in class AbstractMeasurement<Phase>iteration - iteration numberevaluation - evaluation numberstates - orbital states at measurement dateAbstractMeasurement.estimate(int, int, SpacecraftState[])protected EstimatedMeasurement<Phase> theoreticalEvaluation(int iteration, int evaluation, SpacecraftState[] states)
The theoretical value does not have any modifiers applied.
theoreticalEvaluation in class AbstractMeasurement<Phase>iteration - iteration numberevaluation - evaluation numberstates - orbital states at measurement dateAbstractMeasurement.estimate(int, int, SpacecraftState[])Copyright © 2002-2023 CS GROUP. All rights reserved.