DSConverter.java

/* Copyright 2002-2020 CS GROUP
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 * 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.propagation.numerical;

import java.util.ArrayList;
import java.util.List;

import org.hipparchus.analysis.differentiation.DSFactory;
import org.hipparchus.analysis.differentiation.DerivativeStructure;
import org.hipparchus.geometry.euclidean.threed.FieldVector3D;
import org.hipparchus.geometry.euclidean.threed.Vector3D;
import org.orekit.attitudes.AttitudeProvider;
import org.orekit.attitudes.FieldAttitude;
import org.orekit.forces.ForceModel;
import org.orekit.orbits.FieldCartesianOrbit;
import org.orekit.orbits.FieldOrbit;
import org.orekit.propagation.FieldSpacecraftState;
import org.orekit.propagation.SpacecraftState;
import org.orekit.propagation.integration.AbstractDSConverter;
import org.orekit.utils.FieldAngularCoordinates;
import org.orekit.utils.FieldPVCoordinates;
import org.orekit.utils.ParameterDriver;
import org.orekit.utils.TimeStampedFieldAngularCoordinates;
import org.orekit.utils.TimeStampedFieldPVCoordinates;

/** Converter for states and parameters arrays.
 * @author Luc Maisonobe
 * @since 9.0
 * @deprecated as of 10.2, replace by {@link NumericalGradientConverter}
 */
@Deprecated
class DSConverter extends AbstractDSConverter {

    /** Dimension of the state. */
    private final int freeStateParameters;

    /** States with various number of additional parameters for force models. */
    private final List<FieldSpacecraftState<DerivativeStructure>> dsStates;

    /** Simple constructor.
     * @param state regular state
     * @param freeStateParameters number of free parameters, either 3 (position) or 6 (position-velocity)
     * @param provider provider to use if attitude needs to be recomputed
     */
    DSConverter(final SpacecraftState state, final int freeStateParameters, final AttitudeProvider provider) {

        super(freeStateParameters);
        this.freeStateParameters = freeStateParameters;

        // prepare derivation variables, position, optionally velocity
        final DSFactory factory = new DSFactory(freeStateParameters, 1);

        // position always has derivatives
        final Vector3D pos = state.getPVCoordinates().getPosition();
        final FieldVector3D<DerivativeStructure> posDS = new FieldVector3D<>(factory.variable(0, pos.getX()),
                                                                             factory.variable(1, pos.getY()),
                                                                             factory.variable(2, pos.getZ()));

        // velocity may have derivatives or not
        final Vector3D vel = state.getPVCoordinates().getVelocity();
        final FieldVector3D<DerivativeStructure> velDS;
        if (freeStateParameters > 3) {
            velDS = new FieldVector3D<>(factory.variable(3, vel.getX()),
                                        factory.variable(4, vel.getY()),
                                        factory.variable(5, vel.getZ()));
        } else {
            velDS = new FieldVector3D<>(factory.constant(vel.getX()),
                                        factory.constant(vel.getY()),
                                        factory.constant(vel.getZ()));
        }

        // acceleration never has derivatives
        final Vector3D acc = state.getPVCoordinates().getAcceleration();
        final FieldVector3D<DerivativeStructure> accDS = new FieldVector3D<>(factory.constant(acc.getX()),
                                                                             factory.constant(acc.getY()),
                                                                             factory.constant(acc.getZ()));

        // mass never has derivatives
        final DerivativeStructure dsM = factory.constant(state.getMass());

        final DerivativeStructure dsMu = factory.constant(state.getMu());

        final FieldOrbit<DerivativeStructure> dsOrbit =
                        new FieldCartesianOrbit<>(new TimeStampedFieldPVCoordinates<>(state.getDate(), posDS, velDS, accDS),
                                                  state.getFrame(), dsMu);

        final FieldAttitude<DerivativeStructure> dsAttitude;
        if (freeStateParameters > 3) {
            // compute attitude partial derivatives with respect to position/velocity
            dsAttitude = provider.getAttitude(dsOrbit, dsOrbit.getDate(), dsOrbit.getFrame());
        } else {
            // force model does not depend on attitude, don't bother recomputing it
            dsAttitude = new FieldAttitude<>(factory.getDerivativeField(), state.getAttitude());
        }

        // initialize the list with the state having 0 formce model parameters
        dsStates = new ArrayList<>();
        dsStates.add(new FieldSpacecraftState<>(dsOrbit, dsAttitude, dsM));

    }

    /** Get the state with the number of parameters consistent with force model.
     * @param forceModel force model
     * @return state with the number of parameters consistent with force model
     */
    public FieldSpacecraftState<DerivativeStructure> getState(final ForceModel forceModel) {

        // count the required number of parameters
        int nbParams = 0;
        for (final ParameterDriver driver : forceModel.getParametersDrivers()) {
            if (driver.isSelected()) {
                ++nbParams;
            }
        }

        // fill in intermediate slots
        while (dsStates.size() < nbParams + 1) {
            dsStates.add(null);
        }

        if (dsStates.get(nbParams) == null) {
            // it is the first time we need this number of parameters
            // we need to create the state
            final DSFactory factory = new DSFactory(freeStateParameters + nbParams, 1);
            final FieldSpacecraftState<DerivativeStructure> s0 = dsStates.get(0);

            // orbit
            final FieldPVCoordinates<DerivativeStructure> pv0 = s0.getPVCoordinates();
            final FieldOrbit<DerivativeStructure> dsOrbit =
                            new FieldCartesianOrbit<>(new TimeStampedFieldPVCoordinates<>(s0.getDate().toAbsoluteDate(),
                                                                                          extend(pv0.getPosition(),     factory),
                                                                                          extend(pv0.getVelocity(),     factory),
                                                                                          extend(pv0.getAcceleration(), factory)),
                                                      s0.getFrame(),
                                                      extend(s0.getMu(), factory));

            // attitude
            final FieldAngularCoordinates<DerivativeStructure> ac0 = s0.getAttitude().getOrientation();
            final FieldAttitude<DerivativeStructure> dsAttitude =
                            new FieldAttitude<>(s0.getAttitude().getReferenceFrame(),
                                                new TimeStampedFieldAngularCoordinates<>(dsOrbit.getDate(),
                                                                                         extend(ac0.getRotation(), factory),
                                                                                         extend(ac0.getRotationRate(), factory),
                                                                                         extend(ac0.getRotationAcceleration(), factory)));

            // mass
            final DerivativeStructure dsM = extend(s0.getMass(), factory);

            dsStates.set(nbParams, new FieldSpacecraftState<>(dsOrbit, dsAttitude, dsM));

        }

        return dsStates.get(nbParams);

    }

    /** Get the force model parameters.
     * @param state state as returned by {@link #getState(ForceModel)}
     * @param forceModel force model associated with the parameters
     * @return force model parameters
     * @since 9.0
     */
    public DerivativeStructure[] getParameters(final FieldSpacecraftState<DerivativeStructure> state,
                                               final ForceModel forceModel) {
        final DSFactory factory = state.getMass().getFactory();
        final ParameterDriver[] drivers = forceModel.getParametersDrivers();
        final DerivativeStructure[] parameters = new DerivativeStructure[drivers.length];
        int index = freeStateParameters;
        for (int i = 0; i < drivers.length; ++i) {
            parameters[i] = drivers[i].isSelected() ?
                            factory.variable(index++, drivers[i].getValue()) :
                            factory.constant(drivers[i].getValue());
        }
        return parameters;
    }

}