TargetPointing.java
/* Copyright 2002-2023 CS GROUP
* Licensed to CS GROUP (CS) under one or more
* contributor license agreements. See the NOTICE file distributed with
* this work for additional information regarding copyright ownership.
* CS licenses this file to You under the Apache License, Version 2.0
* (the "License"); you may not use this file except in compliance with
* the License. You may obtain a copy of the License at
*
* http://www.apache.org/licenses/LICENSE-2.0
*
* Unless required by applicable law or agreed to in writing, software
* distributed under the License is distributed on an "AS IS" BASIS,
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package org.orekit.attitudes;
import org.hipparchus.CalculusFieldElement;
import org.hipparchus.geometry.euclidean.threed.FieldVector3D;
import org.hipparchus.geometry.euclidean.threed.Vector3D;
import org.orekit.bodies.BodyShape;
import org.orekit.bodies.GeodeticPoint;
import org.orekit.frames.FieldTransform;
import org.orekit.frames.Frame;
import org.orekit.frames.Transform;
import org.orekit.time.AbsoluteDate;
import org.orekit.time.FieldAbsoluteDate;
import org.orekit.utils.FieldPVCoordinatesProvider;
import org.orekit.utils.PVCoordinatesProvider;
import org.orekit.utils.TimeStampedFieldPVCoordinates;
import org.orekit.utils.TimeStampedPVCoordinates;
/**
* This class handles target pointing attitude provider.
* <p>
* This class represents the attitude provider where the satellite z axis is
* pointing to a ground point target.</p>
* <p>
* The target position is defined in a body frame specified by the user.
* It is important to make sure this frame is consistent.
* </p>
* <p>
* The object <code>TargetPointing</code> is guaranteed to be immutable.
* </p>
* @see GroundPointing
* @author Véronique Pommier-Maurussane
*/
public class TargetPointing extends GroundPointing {
/** Target in body frame. */
private final Vector3D target;
/** Creates a new instance from body frame and target expressed in Cartesian coordinates.
* @param inertialFrame frame in which orbital velocities are computed
* @param bodyFrame body frame.
* @param target target position in body frame
* @since 7.1
*/
public TargetPointing(final Frame inertialFrame, final Frame bodyFrame, final Vector3D target) {
super(inertialFrame, bodyFrame);
this.target = target;
}
/** Creates a new instance from body shape and target expressed in geodetic coordinates.
* @param inertialFrame frame in which orbital velocities are computed
* @param targetGeo target defined as a geodetic point in body shape frame
* @param shape body shape
* @since 7.1
*/
public TargetPointing(final Frame inertialFrame, final GeodeticPoint targetGeo, final BodyShape shape) {
super(inertialFrame, shape.getBodyFrame());
// Transform target from geodetic coordinates to Cartesian coordinates
target = shape.transform(targetGeo);
}
/** {@inheritDoc} */
@Override
public TimeStampedPVCoordinates getTargetPV(final PVCoordinatesProvider pvProv,
final AbsoluteDate date, final Frame frame) {
final Transform t = getBodyFrame().getTransformTo(frame, date);
final TimeStampedPVCoordinates pv =
new TimeStampedPVCoordinates(date, target, Vector3D.ZERO, Vector3D.ZERO);
return t.transformPVCoordinates(pv);
}
/** {@inheritDoc} */
@Override
public <T extends CalculusFieldElement<T>> TimeStampedFieldPVCoordinates<T> getTargetPV(final FieldPVCoordinatesProvider<T> pvProv,
final FieldAbsoluteDate<T> date, final Frame frame) {
final FieldTransform<T> t = getBodyFrame().getTransformTo(frame, date);
final FieldVector3D<T> zero = FieldVector3D.getZero(date.getField());
final TimeStampedFieldPVCoordinates<T> pv =
new TimeStampedFieldPVCoordinates<>(date, new FieldVector3D<>(date.getField(), target), zero, zero);
return t.transformPVCoordinates(pv);
}
}