PhaseBuilder.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
* 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,
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package org.orekit.estimation.measurements.gnss;
import org.hipparchus.random.CorrelatedRandomVectorGenerator;
import org.orekit.estimation.measurements.EstimationModifier;
import org.orekit.estimation.measurements.GroundStation;
import org.orekit.estimation.measurements.ObservableSatellite;
import org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder;
import org.orekit.propagation.SpacecraftState;
import org.orekit.time.AbsoluteDate;
import org.orekit.utils.ParameterDriver;
/** Builder for {@link Phase} measurements.
* @author Luc Maisonobe
* @since 10.1
*/
public class PhaseBuilder extends AbstractMeasurementBuilder<Phase> {
/** Ground station from which measurement is performed. */
private final GroundStation station;
/** Wavelength of the phase observed value [m]. */
private final double wavelength;
/** Simple constructor.
* @param noiseSource noise source, may be null for generating perfect measurements
* @param station ground station from which measurement is performed
* @param wavelength phase observed value wavelength (m)
* @param sigma theoretical standard deviation
* @param baseWeight base weight
* @param satellite satellite related to this builder
*/
public PhaseBuilder(final CorrelatedRandomVectorGenerator noiseSource,
final GroundStation station, final double wavelength,
final double sigma, final double baseWeight,
final ObservableSatellite satellite) {
super(noiseSource, sigma, baseWeight, satellite);
this.station = station;
this.wavelength = wavelength;
}
/** {@inheritDoc} */
@Override
public Phase build(final SpacecraftState[] states) {
final ObservableSatellite satellite = getSatellites()[0];
final double sigma = getTheoreticalStandardDeviation()[0];
final double baseWeight = getBaseWeight()[0];
final SpacecraftState[] relevant = new SpacecraftState[] { states[satellite.getPropagatorIndex()] };
// create a dummy measurement
final Phase dummy = new Phase(station, relevant[0].getDate(), Double.NaN, wavelength, sigma, baseWeight, satellite);
for (final EstimationModifier<Phase> 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 phase = dummy.estimate(0, 0, relevant).getEstimatedValue()[0];
// add the noise
final double[] noise = getNoise();
if (noise != null) {
phase += noise[0];
}
// generate measurement
final Phase measurement = new Phase(station, relevant[0].getDate(), phase, wavelength, sigma, baseWeight, satellite);
for (final EstimationModifier<Phase> modifier : getModifiers()) {
measurement.addModifier(modifier);
}
return measurement;
}
}