public class LofOffsetPointing extends GroundPointing
The attitude pointing law is defined by an attitude provider and the satellite axis vector chosen for pointing.
| Constructor and Description |
|---|
LofOffsetPointing(Frame inertialFrame,
BodyShape shape,
AttitudeProvider attLaw,
Vector3D satPointingVector)
Creates new instance.
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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 TimeStampedPVCoordinates |
getTargetPV(PVCoordinatesProvider pvProv,
AbsoluteDate date,
Frame frame)
Compute the target point position/velocity in specified frame.
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getBodyFramepublic LofOffsetPointing(Frame inertialFrame, BodyShape shape, AttitudeProvider attLaw, Vector3D satPointingVector) throws OrekitException
inertialFrame - frame in which orbital velocities are computedshape - Body shapeattLaw - Attitude lawsatPointingVector - satellite vector defining the pointing directionOrekitException - if the frame specified is not a pseudo-inertial framepublic Attitude getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) throws OrekitException
getAttitude in interface AttitudeProvidergetAttitude in class GroundPointingpvProv - local position-velocity provider around current datedate - current dateframe - reference frame from which attitude is computedOrekitException - if attitude cannot be computedprotected TimeStampedPVCoordinates getTargetPV(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) throws OrekitException
getTargetPV in class GroundPointingpvProv - provider for PV coordinatesdate - date at which target point is requestedframe - frame in which observed ground point should be providedOrekitException - if some specific error occurs,
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