public abstract class GroundPointing extends AbstractAttitudeLaw
This class is a basic model for different kind of ground pointing attitude providers, such as : body center pointing, nadir pointing, target pointing, etc...
The object GroundPointing
is guaranteed to be immutable.
AttitudeProvider
,
Serialized FormModifier | Constructor and Description |
---|---|
protected |
GroundPointing(BodyShape shapeIn)
Default constructor.
|
Modifier and Type | Method and Description |
---|---|
Attitude |
getAttitude(PVCoordinatesProvider pvProv,
AbsoluteDate date,
Frame frame)
Compute the attitude corresponding to an orbital state.
|
Frame |
getBodyFrame()
Get the body frame.
|
BodyShape |
getBodyShape()
Get the body shape.
|
protected abstract Vector3D |
getTargetPoint(PVCoordinatesProvider pvProv,
AbsoluteDate date,
Frame frame)
Compute the target point in specified frame.
|
protected TimeStampedPVCoordinates |
getTargetPV(PVCoordinatesProvider pvProv,
AbsoluteDate date,
Frame frame)
Compute the target point position/velocity in specified frame.
|
getAttitude, getSpinDerivativesComputation, setSpinDerivativesComputation
protected GroundPointing(BodyShape shapeIn)
shapeIn
- the body shapepublic Attitude getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) throws PatriusException
pvProv
- local position-velocity provider around current datedate
- current dateframe
- reference frame from which attitude is computedPatriusException
- if attitude cannot be computedprotected abstract Vector3D getTargetPoint(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) throws PatriusException
pvProv
- 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 reachedprotected TimeStampedPVCoordinates getTargetPV(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) throws PatriusException
The default implementation use a simple centered two points finite differences scheme, it may be replaced by more accurate models in specialized implementations.
In the case where the point is computed at a date corresponding to the lower/upper bound of the ephemeris, the finite differences scheme used is either 1st order forward or backward.pvProv
- 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 final Frame getBodyFrame()
public final BodyShape getBodyShape()
Copyright © 2018 CNES. All Rights Reserved.