IsotropicRadiationSingleCoefficient.java

/* Copyright 2002-2016 CS Systèmes d'Information
 * Licensed to CS Systèmes d'Information (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,
 * WITHOUT WARRANTIES OR CONDITIONS OF ANY KIND, either express or implied.
 * See the License for the specific language governing permissions and
 * limitations under the License.
 */
package org.orekit.forces.radiation;

import org.hipparchus.analysis.differentiation.DerivativeStructure;
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.Vector3D;
import org.hipparchus.util.FastMath;
import org.orekit.errors.OrekitException;
import org.orekit.errors.OrekitInternalError;
import org.orekit.errors.OrekitMessages;
import org.orekit.frames.Frame;
import org.orekit.time.AbsoluteDate;
import org.orekit.utils.ParameterDriver;
import org.orekit.utils.ParameterObserver;

/** This class represents the features of a simplified spacecraft.
 * <p>This model uses a single coefficient cr, considered to be
 * a {@link RadiationSensitive#REFLECTION_COEFFICIENT}.
 * </p>
 *
 * @see org.orekit.forces.BoxAndSolarArraySpacecraft
 * @see org.orekit.forces.drag.IsotropicDrag
 * @see IsotropicRadiationCNES95Convention
 * @author Luc Maisonobe
 * @since 7.1
 */
public class IsotropicRadiationSingleCoefficient implements RadiationSensitive {

    /** Parameters scaling factor.
     * <p>
     * We use a power of 2 to avoid numeric noise introduction
     * in the multiplications/divisions sequences.
     * </p>
     */
    private final double SCALE = FastMath.scalb(1.0, -3);

    /** Drivers for radiation pressure coefficient parameter. */
    private final ParameterDriver[] radiationParametersDrivers;

    /** Cross section (m²). */
    private final double crossSection;

    /** Reflection coefficient. */
    private double cr;

    /** Simple constructor.
     * @param crossSection Surface (m²)
     * @param cr reflection coefficient
     */
    public IsotropicRadiationSingleCoefficient(final double crossSection, final double cr) {
        this.radiationParametersDrivers = new ParameterDriver[1];
        try {
            // in some corner cases (unknown spacecraft, fuel leaks, active piloting ...)
            // the single coefficient may be arbitrary, and even negative
            radiationParametersDrivers[0] = new ParameterDriver(RadiationSensitive.REFLECTION_COEFFICIENT,
                                                                cr, SCALE,
                                                                Double.NEGATIVE_INFINITY, Double.POSITIVE_INFINITY);
            radiationParametersDrivers[0].addObserver(new ParameterObserver() {
                /** {@inheritDoc} */
                @Override
                public void valueChanged(final double previousValue, final ParameterDriver driver) {
                    IsotropicRadiationSingleCoefficient.this.cr = driver.getValue();
                }
            });
        } catch (OrekitException oe) {
            // this should never occur as valueChanged above never throws an exception
            throw new OrekitInternalError(oe);
        };

        this.crossSection = crossSection;
        this.cr           = cr;
    }

    /** {@inheritDoc} */
    @Override
    public ParameterDriver[] getRadiationParametersDrivers() {
        return radiationParametersDrivers.clone();
    }

    /** {@inheritDoc} */
    public Vector3D radiationPressureAcceleration(final AbsoluteDate date, final Frame frame, final Vector3D position,
                                                  final Rotation rotation, final double mass, final Vector3D flux) {
        return new Vector3D(crossSection * cr / mass, flux);
    }

    /** {@inheritDoc} */
    public FieldVector3D<DerivativeStructure> radiationPressureAcceleration(final AbsoluteDate date, final Frame frame, final FieldVector3D<DerivativeStructure> position,
                                                                            final FieldRotation<DerivativeStructure> rotation, final DerivativeStructure mass,
                                                                            final FieldVector3D<DerivativeStructure> flux) {
        return new FieldVector3D<DerivativeStructure>(mass.reciprocal().multiply(crossSection * cr), flux);
    }

    /** {@inheritDoc} */
    public FieldVector3D<DerivativeStructure> radiationPressureAcceleration(final AbsoluteDate date, final Frame frame, final Vector3D position,
                                                                            final Rotation rotation, final double mass,
                                                                            final Vector3D flux, final String paramName)
        throws OrekitException {

        final DerivativeStructure crDS;
        if (REFLECTION_COEFFICIENT.equals(paramName)) {
            crDS = new DerivativeStructure(1, 1, 0, cr);
        } else {
            throw new OrekitException(OrekitMessages.UNSUPPORTED_PARAMETER_NAME, paramName,
                                      ABSORPTION_COEFFICIENT + ", " + REFLECTION_COEFFICIENT);
        }

        return new FieldVector3D<DerivativeStructure>(crDS.multiply(crossSection / mass), flux);

    }

}