fr.cnes.sirius.patrius.attitudes

Class TargetPointing

java.lang.Object

fr.cnes.sirius.patrius.attitudes.AbstractAttitudeLaw

fr.cnes.sirius.patrius.attitudes.TargetPointing

All Implemented Interfaces:

AttitudeLaw, AttitudeProvider, Serializable

public class TargetPointing
extends AbstractAttitudeLaw

This class handles target pointing attitude provider.

This class represents the attitude provider where the satellite z axis is pointing to a ground point target.

The target position is defined in a body frame specified by the user. It is important to make sure this frame is consistent.

The object TargetPointing is guaranteed to be immutable.

Author:

Véronique Pommier-Maurussane

See Also:

Serialized Form

Constructor Summary

Constructors

Constructor and Description
TargetPointing(BodyPoint targetGeo) Creates a new instance from body shape and target expressed in geodetic coordinates.
TargetPointing(Frame bodyFrameIn, Vector3D targetIn) Creates a new instance from body frame and target expressed in cartesian coordinates.

Method Summary

Modifier and Type	Method and Description
Attitude	getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude corresponding to an orbital state.

Methods inherited from class fr.cnes.sirius.patrius.attitudes.AbstractAttitudeLaw

getSpinDerivativesComputation, setSpinDerivativesComputation

Methods inherited from class java.lang.Object

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

Methods inherited from interface fr.cnes.sirius.patrius.attitudes.AttitudeProvider

computeSpinByFD, computeSpinDerivativeByFD, getAttitude

Constructor Detail

TargetPointing

public TargetPointing(Frame bodyFrameIn,
                      Vector3D targetIn)

Creates a new instance from body frame and target expressed in cartesian coordinates.

Parameters:

bodyFrameIn - body frame.

targetIn - target position in body frame

TargetPointing

public TargetPointing(BodyPoint targetGeo)

Creates a new instance from body shape and target expressed in geodetic coordinates.

Parameters:

targetGeo - target defined as a geodetic point in body shape frame

Method Detail

getAttitude

public Attitude getAttitude(PVCoordinatesProvider pvProv,
                            AbsoluteDate date,
                            Frame frame)
                     throws PatriusException

Compute the attitude corresponding to an orbital state.

Parameters:

pvProv - local position-velocity provider around current date

date - current date

frame - reference frame from which attitude is computed

Returns:

attitude on the specified date and position-velocity state

Throws:

PatriusException - if attitude cannot be computed for provided date