public class InterSatellitesPhase extends AbstractMeasurement<InterSatellitesPhase>
The measurement is considered to be a signal emitted from a remote satellite and received by a local satellite. Its value is the number of cycles between emission and reception. The motion of both spacecrafts 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 |
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static String |
AMBIGUITY_NAME
Name for ambiguity driver.
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Constructor and Description |
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InterSatellitesPhase(ObservableSatellite local,
ObservableSatellite remote,
AbsoluteDate date,
double phase,
double wavelength,
double sigma,
double baseWeight)
Constructor.
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Modifier and Type | Method and Description |
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ParameterDriver |
getAmbiguityDriver()
Get the driver for phase ambiguity.
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double |
getWavelength()
Get the wavelength.
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protected EstimatedMeasurement<InterSatellitesPhase> |
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 static final String AMBIGUITY_NAME
public InterSatellitesPhase(ObservableSatellite local, ObservableSatellite remote, AbsoluteDate date, double phase, double wavelength, double sigma, double baseWeight)
local
- satellite which receives the signal and performs the measurementremote
- emote satellite which simply emits the signaldate
- date of the measurementphase
- observed value (cycles)wavelength
- phase observed value wavelength (m)sigma
- theoretical standard deviationbaseWeight
- base weightpublic double getWavelength()
public ParameterDriver getAmbiguityDriver()
protected EstimatedMeasurement<InterSatellitesPhase> theoreticalEvaluation(int iteration, int evaluation, SpacecraftState[] states)
The theoretical value does not have any modifiers applied.
theoreticalEvaluation
in class AbstractMeasurement<InterSatellitesPhase>
iteration
- iteration numberevaluation
- evaluation numberstates
- orbital states at measurement dateAbstractMeasurement.estimate(int, int, SpacecraftState[])
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