public class LofOffsetPointing extends AbstractGroundPointing
The attitude pointing law is defined by an attitude provider and the satellite axis vector chosen for pointing.
| Constructor and Description |
|---|
LofOffsetPointing(BodyShape shape,
AttitudeProvider attLaw,
Vector3D satPointingVectorIn)
Creates new instance.
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LofOffsetPointing(BodyShape shape,
AttitudeProvider attLaw,
Vector3D satPointingVectorIn,
Vector3D losInSatFrameVec,
Vector3D losNormalInSatFrameVec)
Constructor.
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| Modifier and Type | Method and Description |
|---|---|
Attitude |
getAttitude(PVCoordinatesProvider pvProv,
AbsoluteDate date,
Frame frame)
Compute the attitude corresponding to an orbital state.
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protected Vector3D |
getTargetPosition(PVCoordinatesProvider pvProv,
AbsoluteDate date,
Frame frame)
Compute the target ground point position in specified frame.
|
void |
setSpinDerivativesComputation(boolean computeSpinDerivatives)
Method to activate spin derivative computation.
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getBodyFrame, getBodyShape, getLosInSatFrame, getLosNormalInSatFrame, getTargetPVgetSpinDerivativesComputationclone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, waitcomputeSpinByFD, computeSpinDerivativeByFD, getAttitudepublic LofOffsetPointing(BodyShape shape, AttitudeProvider attLaw, Vector3D satPointingVectorIn)
shape - Body shapeattLaw - Attitude lawsatPointingVectorIn - satellite vector defining the pointing directionpublic LofOffsetPointing(BodyShape shape, AttitudeProvider attLaw, Vector3D satPointingVectorIn, Vector3D losInSatFrameVec, Vector3D losNormalInSatFrameVec)
shape - Body shapeattLaw - Attitude lawsatPointingVectorIn - satellite vector defining the pointing directionlosInSatFrameVec - LOS in satellite frame axislosNormalInSatFrameVec - LOS normal axis in satellite framepublic Attitude getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) throws PatriusException
getAttitude in interface AttitudeProvidergetAttitude in class AbstractGroundPointingpvProv - local position-velocity provider around current datedate - current dateframe - reference frame from which attitude is computedPatriusException - if attitude cannot be computed for provided dateprotected Vector3D getTargetPosition(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) throws PatriusException
getTargetPosition in class AbstractGroundPointingpvProv - provider for PV coordinatesdate - date at which target point is requestedframe - frame in which observed ground point should be providedPatriusException - if some specific error occurs,
such as no target reachedpublic void setSpinDerivativesComputation(boolean computeSpinDerivatives)
Spin derivatives computation applies to provided law attitudeLaw.
setSpinDerivativesComputation in interface AttitudeProvidersetSpinDerivativesComputation in class AbstractAttitudeLawcomputeSpinDerivatives - true if spin derivatives should be computedCopyright © 2025 CNES. All rights reserved.