TDOATroposphericDelayModifier.java

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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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package org.orekit.estimation.measurements.modifiers;

import java.util.List;

import org.hipparchus.CalculusFieldElement;
import org.hipparchus.Field;
import org.hipparchus.geometry.euclidean.threed.FieldVector3D;
import org.hipparchus.geometry.euclidean.threed.Vector3D;
import org.orekit.attitudes.FrameAlignedProvider;
import org.orekit.estimation.measurements.EstimatedMeasurement;
import org.orekit.estimation.measurements.EstimatedMeasurementBase;
import org.orekit.estimation.measurements.EstimationModifier;
import org.orekit.estimation.measurements.GroundStation;
import org.orekit.estimation.measurements.TDOA;
import org.orekit.models.earth.troposphere.DiscreteTroposphericModel;
import org.orekit.propagation.FieldSpacecraftState;
import org.orekit.propagation.SpacecraftState;
import org.orekit.utils.Constants;
import org.orekit.utils.ParameterDriver;

/** Class modifying theoretical TDOA measurements with tropospheric delay.
 * <p>
 * The effect of tropospheric correction on the TDOA is a time delay computed
 * directly from the difference in tropospheric delays for each downlink.
 * </p><p>
 * Tropospheric delay is not frequency dependent for signals up to 15 GHz.
 * </p>
 * @author Pascal Parraud
 * @since 11.2
 */
public class TDOATroposphericDelayModifier implements EstimationModifier<TDOA> {

    /** Tropospheric delay model. */
    private final DiscreteTroposphericModel tropoModel;

    /** Constructor.
     *
     * @param model tropospheric model appropriate for the current TDOA measurement method.
     */
    public TDOATroposphericDelayModifier(final DiscreteTroposphericModel model) {
        tropoModel = model;
    }

    /** Compute the measurement error due to Troposphere on a single downlink.
     * @param station station
     * @param state spacecraft state
     * @return the measurement error due to Troposphere (s)
     */
    private double timeErrorTroposphericModel(final GroundStation station, final SpacecraftState state) {
        final Vector3D position = state.getPosition();

        // elevation
        final double elevation =
                        station.getBaseFrame().getTrackingCoordinates(position, state.getFrame(), state.getDate()).
                        getElevation();

        // only consider measurements above the horizon
        if (elevation > 0) {
            // Delay in meters
            final double delay = tropoModel.pathDelay(elevation, station.getBaseFrame().getPoint(),
                                                      tropoModel.getParameters(state.getDate()), state.getDate());
            // return delay in seconds
            return delay / Constants.SPEED_OF_LIGHT;
        }

        return 0;
    }

    /** Compute the measurement error due to Troposphere on a single downlink.
     * @param <T> type of the element
     * @param station station
     * @param state spacecraft state
     * @param parameters tropospheric model parameters
     * @return the measurement error due to Troposphere (s)
     */
    private <T extends CalculusFieldElement<T>> T timeErrorTroposphericModel(final GroundStation station,
                                                                             final FieldSpacecraftState<T> state,
                                                                             final T[] parameters) {
        // Field
        final Field<T> field = state.getDate().getField();
        final T zero         = field.getZero();

        // elevation
        final FieldVector3D<T> pos = state.getPosition();
        final T elevation =
                        station.getBaseFrame().getTrackingCoordinates(pos, state.getFrame(), state.getDate()).
                        getElevation();

        // only consider measurements above the horizon
        if (elevation.getReal() > 0) {
            // delay in meters
            final T delay = tropoModel.pathDelay(elevation, station.getBaseFrame().getPoint(field),
                                                 parameters, state.getDate());
            // return delay in seconds
            return delay.divide(Constants.SPEED_OF_LIGHT);
        }

        return zero;
    }

    /** {@inheritDoc} */
    @Override
    public List<ParameterDriver> getParametersDrivers() {
        return tropoModel.getParametersDrivers();
    }

    /** {@inheritDoc} */
    @Override
    public void modifyWithoutDerivatives(final EstimatedMeasurementBase<TDOA> estimated) {

        final TDOA            measurement   = estimated.getObservedMeasurement();
        final GroundStation   primeStation  = measurement.getPrimeStation();
        final GroundStation   secondStation = measurement.getSecondStation();

        TDOAModifierUtil.modifyWithoutDerivatives(estimated,  primeStation, secondStation, this::timeErrorTroposphericModel);

    }

    /** {@inheritDoc} */
    @Override
    public void modify(final EstimatedMeasurement<TDOA> estimated) {

        final TDOA            measurement   = estimated.getObservedMeasurement();
        final GroundStation   primeStation  = measurement.getPrimeStation();
        final GroundStation   secondStation = measurement.getSecondStation();
        final SpacecraftState state         = estimated.getStates()[0];

        TDOAModifierUtil.modify(estimated, tropoModel,
                                new ModifierGradientConverter(state, 6, new FrameAlignedProvider(state.getFrame())),
                                primeStation, secondStation,
                                this::timeErrorTroposphericModel,
                                this::timeErrorTroposphericModel);

    }

}