InertialProvider.java
/* Copyright 2002-2020 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.RealFieldElement;
import org.hipparchus.geometry.euclidean.threed.Rotation;
import org.orekit.annotation.DefaultDataContext;
import org.orekit.data.DataContext;
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;
/**
* This class handles an inertial attitude provider.
* <p>Instances of this class are guaranteed to be immutable.</p>
* @author Luc Maisonobe
*/
public class InertialProvider implements AttitudeProvider {
/** Dummy attitude provider, perfectly aligned with the EME2000 frame.
*
* <p>This field uses the {@link DataContext#getDefault() default data context}.
*
* @see #InertialProvider(Rotation, Frame)
* @see #InertialProvider(Frame)
*/
@DefaultDataContext
public static final InertialProvider EME2000_ALIGNED =
new InertialProvider(Rotation.IDENTITY);
/** Fixed satellite frame. */
private final Frame satelliteFrame;
/** Creates new instance.
*
* <p>This constructor uses the {@link DataContext#getDefault() default data context}.
*
* @param rotation rotation from EME2000 to the desired satellite frame
* @see #InertialProvider(Rotation, Frame)
*/
@DefaultDataContext
public InertialProvider(final Rotation rotation) {
this(rotation, DataContext.getDefault().getFrames().getEME2000());
}
/**
* Creates new instance aligned with the given frame.
*
* @param frame the reference frame for the attitude.
*/
public InertialProvider(final Frame frame) {
this(Rotation.IDENTITY, frame);
}
/**
* Creates new instance with a fixed attitude in the given frame.
*
* @param rotation rotation from {@code reference} to the desired satellite frame
* @param reference frame for {@code rotation}.
* @since 10.1
*/
public InertialProvider(final Rotation rotation,
final Frame reference) {
satelliteFrame =
new Frame(reference,
new Transform(AbsoluteDate.ARBITRARY_EPOCH, rotation), null, false);
}
/** {@inheritDoc} */
public Attitude getAttitude(final PVCoordinatesProvider pvProv,
final AbsoluteDate date, final Frame frame) {
final Transform t = frame.getTransformTo(satelliteFrame, date);
return new Attitude(date, frame, t.getRotation(), t.getRotationRate(), t.getRotationAcceleration());
}
/** {@inheritDoc} */
public <T extends RealFieldElement<T>>FieldAttitude<T> getAttitude(final FieldPVCoordinatesProvider<T> pvProv,
final FieldAbsoluteDate<T> date, final Frame frame) {
final FieldTransform<T> t = frame.getTransformTo(satelliteFrame, date);
return new FieldAttitude<>(date, frame, t.getRotation(), t.getRotationRate(), t.getRotationAcceleration());
}
}