RelativisticJ2ClockInterSatellitesRangeModifier.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
 * (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
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package org.orekit.estimation.measurements.modifiers;

import java.util.Collections;
import java.util.List;

import org.orekit.estimation.measurements.EstimatedMeasurement;
import org.orekit.estimation.measurements.EstimationModifier;
import org.orekit.estimation.measurements.InterSatellitesRange;
import org.orekit.utils.Constants;
import org.orekit.utils.ParameterDriver;

/**
 * Class modifying theoretical inter-satellites range measurements with relativistic J2 clock correction.
 * <p>
 * Relativistic clock correction of the effects caused by the oblateness of Earth on
 * the gravity potential.
 * </p>
 * <p>
 * The time delay caused by this effect is computed based on the orbital parameters of the
 * emitter's orbit.
 * </p>
 *
 * @author Louis Aucouturier
 * @since 11.2
 *
 * @see "Teunissen, Peter, and Oliver Montenbruck, eds. Springer handbook of global navigation
 * satellite systems. Chapter 19.2. Equation 19.18 Springer, 2017."
 */

public class RelativisticJ2ClockInterSatellitesRangeModifier extends AbstractRelativisticJ2ClockModifier implements EstimationModifier<InterSatellitesRange> {

    /**
     * Modifier constructor.
     * @param gm Earth gravitational constant (mu) in m³/s².
     * @param c20 Earth un-normalized second zonal coefficient (Signed J2 constant, is negative) (Typical value -1.0826e-3).
     * @param equatorialRadius Earth equatorial radius in m.
     */
    public RelativisticJ2ClockInterSatellitesRangeModifier(final double gm,
                                                           final double c20,
                                                           final double equatorialRadius) {
        super(gm, c20, equatorialRadius);
    }

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

    /** {@inheritDoc} */
    @Override
    public void modify(final EstimatedMeasurement<InterSatellitesRange> estimated) {
        // Relativistic effect
        final double dtJ2 = relativisticJ2Correction(estimated);

        // Update estimated value taking into account the relativistic effect.
        final double[] newValue = estimated.getEstimatedValue().clone();
        newValue[0] = newValue[0] - dtJ2 * Constants.SPEED_OF_LIGHT;
        estimated.setEstimatedValue(newValue);
    }

}