RangeRateTroposphericDelayModifier.java

/* Copyright 2002-2022 CS GROUP
 * Licensed to CS GROUP (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
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 *
 *   http://www.apache.org/licenses/LICENSE-2.0
 *
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 * distributed under the License is distributed on an "AS IS" BASIS,
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package org.orekit.estimation.measurements.modifiers;

import org.hipparchus.CalculusFieldElement;
import org.orekit.attitudes.InertialProvider;
import org.orekit.estimation.measurements.EstimatedMeasurement;
import org.orekit.estimation.measurements.EstimationModifier;
import org.orekit.estimation.measurements.GroundStation;
import org.orekit.estimation.measurements.RangeRate;
import org.orekit.models.earth.troposphere.DiscreteTroposphericModel;
import org.orekit.propagation.FieldSpacecraftState;
import org.orekit.propagation.SpacecraftState;

/** Class modifying theoretical range-rate measurements with tropospheric delay.
 * The effect of tropospheric correction on the range-rate is directly computed
 * through the computation of the tropospheric delay difference with respect to
 * time.
 *
 * In general, for GNSS, VLBI, ... there is hardly any frequency dependence in the delay.
 * For SLR techniques however, the frequency dependence is sensitive.
 *
 * @author Joris Olympio
 * @since 8.0
 */
public class RangeRateTroposphericDelayModifier extends BaseRangeRateTroposphericDelayModifier implements EstimationModifier<RangeRate> {

    /** Two-way measurement factor. */
    private final double fTwoWay;

    /** Constructor.
     *
     * @param model  Tropospheric delay model appropriate for the current range-rate measurement method.
     * @param tw     Flag indicating whether the measurement is two-way.
     */
    public RangeRateTroposphericDelayModifier(final DiscreteTroposphericModel model, final boolean tw) {
        super(model);
        if (tw) {
            fTwoWay = 2.;
        } else {
            fTwoWay = 1.;
        }
    }

    /** Compute the measurement error due to Troposphere.
     * @param station station
     * @param state spacecraft state
     * @return the measurement error due to Troposphere
     */
    @Override
    public double rangeRateErrorTroposphericModel(final GroundStation station,
                                                  final SpacecraftState state) {
        return fTwoWay * super.rangeRateErrorTroposphericModel(station, state);
    }


    /** Compute the measurement error due to Troposphere.
     * @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
     */
    @Override
    public <T extends CalculusFieldElement<T>> T rangeRateErrorTroposphericModel(final GroundStation station,
                                                                                 final FieldSpacecraftState<T> state,
                                                                                 final T[] parameters) {
        return super.rangeRateErrorTroposphericModel(station, state, parameters).multiply(fTwoWay);
    }

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

        final RangeRate       measurement = estimated.getObservedMeasurement();
        final GroundStation   station     = measurement.getStation();
        final SpacecraftState state       = estimated.getStates()[0];

        RangeRateModifierUtil.modify(estimated, getTropoModel(),
                                     new ModifierGradientConverter(state, 6, new InertialProvider(state.getFrame())),
                                     station,
                                     this::rangeRateErrorTroposphericModel,
                                     this::rangeRateErrorTroposphericModel);


    }

}