InterSatellitesOneWayRangeRateBuilder.java

/* Copyright 2002-2024 Thales Alenia Space
 * 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
 * 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
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package org.orekit.estimation.measurements.generation;

import org.hipparchus.random.CorrelatedRandomVectorGenerator;
import org.orekit.estimation.measurements.EstimationModifier;
import org.orekit.estimation.measurements.ObservableSatellite;
import org.orekit.estimation.measurements.gnss.InterSatellitesOneWayRangeRate;
import org.orekit.propagation.SpacecraftState;
import org.orekit.propagation.sampling.OrekitStepInterpolator;
import org.orekit.time.AbsoluteDate;
import org.orekit.utils.ParameterDriver;

import java.util.Map;

/** Builder for {@link org.orekit.estimation.measurements.gnss.InterSatellitesOneWayRangeRate} measurements.
 * @author Luc Maisonobe
 * @since 12.1
 */
public class InterSatellitesOneWayRangeRateBuilder
    extends AbstractMeasurementBuilder<InterSatellitesOneWayRangeRate> {

    /** Satellite which receives the signal and performs the measurement. */
    private final ObservableSatellite local;

    /** Satellite which simply emits the signal. */
    private final ObservableSatellite remote;

    /** Simple constructor.
     * @param noiseSource noise source, may be null for generating perfect measurements
     * @param local satellite which receives the signal and performs the measurement
     * @param remote satellite which simply emits the signal
     * @param sigma theoretical standard deviation
     * @param baseWeight base weight
     */
    public InterSatellitesOneWayRangeRateBuilder(final CorrelatedRandomVectorGenerator noiseSource,
                                                 final ObservableSatellite local, final ObservableSatellite remote,
                                                 final double sigma, final double baseWeight) {
        super(noiseSource, sigma, baseWeight, local, remote);
        this.local  = local;
        this.remote = remote;
    }

    /** {@inheritDoc} */
    @Override
    public InterSatellitesOneWayRangeRate build(final AbsoluteDate date,
                                                final Map<ObservableSatellite, OrekitStepInterpolator> interpolators) {

        final double            sigma      = getTheoreticalStandardDeviation()[0];
        final double            baseWeight = getBaseWeight()[0];
        final SpacecraftState[] relevant   = new SpacecraftState[] {
            interpolators.get(local).getInterpolatedState(date),
            interpolators.get(remote).getInterpolatedState(date)
        };

        // create a dummy measurement
        final InterSatellitesOneWayRangeRate dummy = new InterSatellitesOneWayRangeRate(local, remote, relevant[0].getDate(),
                                                                                        Double.NaN, sigma, baseWeight);
        for (final EstimationModifier<InterSatellitesOneWayRangeRate> modifier : getModifiers()) {
            dummy.addModifier(modifier);
        }

        // set a reference date for parameters missing one
        for (final ParameterDriver driver : dummy.getParametersDrivers()) {
            if (driver.getReferenceDate() == null) {
                final AbsoluteDate start = getStart();
                final AbsoluteDate end   = getEnd();
                driver.setReferenceDate(start.durationFrom(end) <= 0 ? start : end);
            }
        }

        // estimate the perfect value of the measurement
        double rangeRate = dummy.estimateWithoutDerivatives(relevant).getEstimatedValue()[0];

        // add the noise
        final double[] noise = getNoise();
        if (noise != null) {
            rangeRate += noise[0];
        }

        // generate measurement
        final InterSatellitesOneWayRangeRate measurement = new InterSatellitesOneWayRangeRate(local, remote, relevant[0].getDate(),
                                                                                              rangeRate, sigma, baseWeight);
        for (final EstimationModifier<InterSatellitesOneWayRangeRate> modifier : getModifiers()) {
            measurement.addModifier(modifier);
        }
        return measurement;

    }

}