SpinStabilized.java

/* Copyright 2002-2024 CS GROUP
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 * 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
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 *   http://www.apache.org/licenses/LICENSE-2.0
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package org.orekit.attitudes;

import org.hipparchus.CalculusFieldElement;
import org.hipparchus.geometry.euclidean.threed.FieldRotation;
import org.hipparchus.geometry.euclidean.threed.FieldVector3D;
import org.hipparchus.geometry.euclidean.threed.Rotation;
import org.hipparchus.geometry.euclidean.threed.RotationConvention;
import org.hipparchus.geometry.euclidean.threed.Vector3D;
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 a spin stabilized attitude provider.
 * <p>Spin stabilized laws are handled as wrappers for an underlying
 * non-rotating law. This underlying law is typically an instance
 * of {@link CelestialBodyPointed} with the pointing axis equal to
 * the rotation axis, but can in fact be anything.</p>
 * <p>Instances of this class are guaranteed to be immutable.</p>
 * @author Luc Maisonobe
 */
public class SpinStabilized implements AttitudeProviderModifier {

    /** Underlying non-rotating attitude provider.  */
    private final AttitudeProvider nonRotatingLaw;

    /** Start date of the rotation. */
    private final AbsoluteDate start;

    /** Rotation axis in satellite frame. */
    private final Vector3D axis;

    /** Spin rate in radians per seconds. */
    private final double rate;

    /** Spin vector. */
    private final Vector3D spin;

    /** Creates a new instance.
     * @param nonRotatingLaw underlying non-rotating attitude provider
     * @param start start date of the rotation
     * @param axis rotation axis in satellite frame
     * @param rate spin rate in radians per seconds
     */
    public SpinStabilized(final AttitudeProvider nonRotatingLaw,
                          final AbsoluteDate start,
                          final Vector3D axis, final double rate) {
        this.nonRotatingLaw = nonRotatingLaw;
        this.start          = start;
        this.axis           = axis;
        this.rate           = rate;
        this.spin           = new Vector3D(rate / axis.getNorm(), axis);
    }

    /** {@inheritDoc} */
    public AttitudeProvider getUnderlyingAttitudeProvider() {
        return nonRotatingLaw;
    }

    /** {@inheritDoc} */
    public Attitude getAttitude(final PVCoordinatesProvider pvProv,
                                final AbsoluteDate date, final Frame frame) {

        // get attitude from underlying non-rotating law
        final Attitude base = nonRotatingLaw.getAttitude(pvProv, date, frame);
        final Transform baseTransform = new Transform(date, base.getOrientation());

        // compute spin transform due to spin from reference to current date
        final Transform spinInfluence =
            new Transform(date,
                          new Rotation(axis,
                                       rate * date.durationFrom(start),
                                       RotationConvention.FRAME_TRANSFORM),
                          spin);

        // combine the two transforms
        final Transform combined = new Transform(date, baseTransform, spinInfluence);

        // build the attitude
        return new Attitude(date, frame,
                            combined.getRotation(), combined.getRotationRate(), combined.getRotationAcceleration());

    }

    /** {@inheritDoc} */
    public <T extends CalculusFieldElement<T>> FieldAttitude<T> getAttitude(final FieldPVCoordinatesProvider<T> pvProv,
                                                                        final FieldAbsoluteDate<T> date,
                                                                        final Frame frame) {

        // get attitude from underlying non-rotating law
        final FieldAttitude<T> base = nonRotatingLaw.getAttitude(pvProv, date, frame);
        final FieldTransform<T> baseTransform = new FieldTransform<>(date, base.getOrientation());

        // compute spin transform due to spin from reference to current date
        final FieldTransform<T> spinInfluence =
            new FieldTransform<>(date,
                                 new FieldRotation<>(new FieldVector3D<>(date.getField(), axis),
                                                     date.durationFrom(start).multiply(rate),
                                                     RotationConvention.FRAME_TRANSFORM),
                                 new FieldVector3D<>(date.getField(), spin));

        // combine the two transforms
        final FieldTransform<T> combined = new FieldTransform<>(date, baseTransform, spinInfluence);

        // build the attitude
        return new FieldAttitude<>(date, frame,
                                   combined.getRotation(), combined.getRotationRate(), combined.getRotationAcceleration());

    }

}