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OREKIT (ORbits Extrapolation KIT) is a low level space dynamics library. It provides basic elements (orbits, dates, attitude, frames ...) and various algorithms to handle them (conversions, analytical and numerical propagation, pointing ...).

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/* Copyright 2002-2022 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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 * See the License for the specific language governing permissions and
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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.

 * 

* 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. *

* @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 > TimeStampedFieldPVCoordinates getTargetPV(final FieldPVCoordinatesProvider pvProv, final FieldAbsoluteDate date, final Frame frame) { final FieldTransform t = getBodyFrame().getTransformTo(frame, date); final FieldVector3D zero = FieldVector3D.getZero(date.getField()); final TimeStampedFieldPVCoordinates pv = new TimeStampedFieldPVCoordinates<>(date, new FieldVector3D<>(date.getField(), target), zero, zero); return t.transformPVCoordinates(pv); } }




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