org.orekit.estimation.measurements.gnss

Class InterSatellitesWindUp

java.lang.Object

org.orekit.estimation.measurements.gnss.AbstractWindUp<InterSatellitesPhase>

org.orekit.estimation.measurements.gnss.InterSatellitesWindUp

All Implemented Interfaces:

EstimationModifier<InterSatellitesPhase>, ParameterDriversProvider

public class InterSatellitesWindUp
extends AbstractWindUp<InterSatellitesPhase>

Modifier for wind-up effect in GNSS inter-satellites phase measurements.

Since:

12.0

Author:

Luc Maisonobe

See Also:

InterSatellitesWindUpFactory

Method Summary

Modifier and Type	Method and Description
protected org.hipparchus.geometry.euclidean.threed.Rotation	emitterToInert(EstimatedMeasurementBase<InterSatellitesPhase> estimated) Compute rotation from emitter to inertial frame.
protected org.hipparchus.geometry.euclidean.threed.Rotation	receiverToInert(EstimatedMeasurementBase<InterSatellitesPhase> estimated) Compute rotation from receiver to inertial frame.

Methods inherited from class org.orekit.estimation.measurements.gnss.AbstractWindUp

getParametersDrivers, modifyWithoutDerivatives

Methods inherited from class java.lang.Object

clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait

Methods inherited from interface org.orekit.estimation.measurements.EstimationModifier

modify

Methods inherited from interface org.orekit.utils.ParameterDriversProvider

getNbParametersDriversValue, getParameterDriver, getParameters, getParameters, getParameters, getParameters, getParametersAllValues, getParametersAllValues, isSupported

Method Detail

emitterToInert

protected org.hipparchus.geometry.euclidean.threed.Rotation emitterToInert(EstimatedMeasurementBase<InterSatellitesPhase> estimated)

Compute rotation from emitter to inertial frame.

Specified by:

emitterToInert in class AbstractWindUp<InterSatellitesPhase>

Parameters:

estimated - estimated measurement to modify

Returns:

rotation from emitter to inertial frame

receiverToInert

protected org.hipparchus.geometry.euclidean.threed.Rotation receiverToInert(EstimatedMeasurementBase<InterSatellitesPhase> estimated)

Compute rotation from receiver to inertial frame.

Specified by:

receiverToInert in class AbstractWindUp<InterSatellitesPhase>

Parameters:

estimated - estimated measurement to modify

Returns:

rotation from receiver to inertial frame