OneWayGNSSPhaseBuilder.java

  1. /* Copyright 2002-2024 Luc Maisonobe
  2.  * Licensed to CS GROUP (CS) under one or more
  3.  * contributor license agreements.  See the NOTICE file distributed with
  4.  * this work for additional information regarding copyright ownership.
  5.  * CS licenses this file to You under the Apache License, Version 2.0
  6.  * (the "License"); you may not use this file except in compliance with
  7.  * the License.  You may obtain a copy of the License at
  8.  *
  9.  *   http://www.apache.org/licenses/LICENSE-2.0
  10.  *
  11.  * Unless required by applicable law or agreed to in writing, software
  12.  * distributed under the License is distributed on an "AS IS" BASIS,
  13.  * WITHOUT WARRANTIES OR CONDITIONS OF ANY KIND, either express or implied.
  14.  * See the License for the specific language governing permissions and
  15.  * limitations under the License.
  16.  */
  17. package org.orekit.estimation.measurements.generation;

  18. import java.util.Map;
  19. import java.util.function.ToDoubleFunction;

  20. import org.hipparchus.random.CorrelatedRandomVectorGenerator;
  21. import org.orekit.estimation.measurements.EstimationModifier;
  22. import org.orekit.estimation.measurements.ObservableSatellite;
  23. import org.orekit.estimation.measurements.gnss.OneWayGNSSPhase;
  24. import org.orekit.propagation.SpacecraftState;
  25. import org.orekit.propagation.sampling.OrekitStepInterpolator;
  26. import org.orekit.time.AbsoluteDate;
  27. import org.orekit.utils.ParameterDriver;


  28. /** Builder for {@link OneWayGNSSPhase} measurements.
  29.  * @author Luc Maisonobe
  30.  * @since 12.0
  31.  */
  32. public class OneWayGNSSPhaseBuilder extends AbstractMeasurementBuilder<OneWayGNSSPhase> {

  33.     /** Wavelength of the phase observed value [m]. */
  34.     private final double wavelength;

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

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

  39.     /** Clock model of the remote satellite that provides clock offset. */
  40.     private ToDoubleFunction<AbsoluteDate> remoteClockModel;

  41.     /** Simple constructor.
  42.      * @param noiseSource noise source, may be null for generating perfect measurements
  43.      * @param local satellite which receives the signal and performs the measurement
  44.      * @param remote satellite which simply emits the signal
  45.      * @param remoteClockModel clock model of the remote satellite that provides clock offset
  46.      * @param wavelength phase observed value wavelength (m)
  47.      * @param sigma theoretical standard deviation
  48.      * @param baseWeight base weight
  49.      */
  50.     public OneWayGNSSPhaseBuilder(final CorrelatedRandomVectorGenerator noiseSource,
  51.                                   final ObservableSatellite local, final ObservableSatellite remote,
  52.                                   final ToDoubleFunction<AbsoluteDate> remoteClockModel,
  53.                                   final double wavelength, final double sigma, final double baseWeight) {
  54.         super(noiseSource, sigma, baseWeight, local, remote);
  55.         this.wavelength       = wavelength;
  56.         this.local            = local;
  57.         this.remote           = remote;
  58.         this.remoteClockModel = remoteClockModel;
  59.     }

  60.     /** {@inheritDoc} */
  61.     @Override
  62.     public OneWayGNSSPhase build(final AbsoluteDate date, final Map<ObservableSatellite, OrekitStepInterpolator> interpolators) {

  63.         final double sigma               = getTheoreticalStandardDeviation()[0];
  64.         final double baseWeight          = getBaseWeight()[0];
  65.         final SpacecraftState[] relevant = new SpacecraftState[] {
  66.             interpolators.get(local).getInterpolatedState(date),
  67.             interpolators.get(remote).getInterpolatedState(date)
  68.         };
  69.         final double offset              = remoteClockModel.applyAsDouble(date);

  70.         // create a dummy measurement
  71.         final OneWayGNSSPhase dummy = new OneWayGNSSPhase(interpolators.get(remote), offset, date,
  72.                                                           Double.NaN, wavelength, sigma, baseWeight, local);
  73.         for (final EstimationModifier<OneWayGNSSPhase> modifier : getModifiers()) {
  74.             dummy.addModifier(modifier);
  75.         }

  76.         // set a reference date for parameters missing one
  77.         for (final ParameterDriver driver : dummy.getParametersDrivers()) {
  78.             if (driver.getReferenceDate() == null) {
  79.                 final AbsoluteDate start = getStart();
  80.                 final AbsoluteDate end   = getEnd();
  81.                 driver.setReferenceDate(start.durationFrom(end) <= 0 ? start : end);
  82.             }
  83.         }

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

  86.         // add the noise
  87.         final double[] noise = getNoise();
  88.         if (noise != null) {
  89.             phase += noise[0];
  90.         }

  91.         // generate measurement
  92.         final OneWayGNSSPhase measurement = new OneWayGNSSPhase(interpolators.get(remote), offset, date,
  93.                                                                 phase, wavelength, sigma, baseWeight, local);
  94.         for (final EstimationModifier<OneWayGNSSPhase> modifier : getModifiers()) {
  95.             measurement.addModifier(modifier);
  96.         }
  97.         return measurement;

  98.     }

  99. }