public class Phase extends AbstractMeasurement<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.
|
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 |
---|---|
GroundStation |
getStation()
Get the ground station from which measurement is performed.
|
double |
getWavelength()
Get the wavelength.
|
protected EstimatedMeasurement<Phase> |
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 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 valuewavelength
- phase observed value wavelength (m)sigma
- theoretical standard deviationbaseWeight
- base weightsatellite
- satellite related to this measurementpublic GroundStation getStation()
public double getWavelength()
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 © 2002-2019 CS Systèmes d'information. All rights reserved.