1   /* Copyright 2002-2024 Mark Rutten
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    * Mark Rutten 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  
19  import java.util.Map;
20  
21  import org.hipparchus.random.CorrelatedRandomVectorGenerator;
22  import org.orekit.estimation.measurements.BistaticRange;
23  import org.orekit.estimation.measurements.EstimationModifier;
24  import org.orekit.estimation.measurements.GroundStation;
25  import org.orekit.estimation.measurements.ObservableSatellite;
26  import org.orekit.propagation.SpacecraftState;
27  import org.orekit.propagation.sampling.OrekitStepInterpolator;
28  import org.orekit.time.AbsoluteDate;
29  import org.orekit.utils.ParameterDriver;
30  
31  
32  /** Builder for {@link BistaticRange} measurements.
33   * @author Pascal Parraud
34   * @author Mark Rutten
35   * @since 11.2
36   */
37  public class BistaticRangeBuilder extends AbstractMeasurementBuilder<BistaticRange> {
38  
39      /** Emitter ground station. */
40      private final GroundStation emitter;
41  
42      /** Receiver ground station. */
43      private final GroundStation receiver;
44  
45      /** Satellite related to this builder.
46       * @since 12.0
47       */
48      private final ObservableSatellite satellite;
49  
50      /** Simple constructor.
51       * @param noiseSource noise source, may be null for generating perfect measurements
52       * @param emitter emitter ground station
53       * @param receiver receiver ground station, from which measurement is performed
54       * @param sigma theoretical standard deviation
55       * @param baseWeight base weight
56       * @param satellite satellite related to this builder
57       */
58      public BistaticRangeBuilder(final CorrelatedRandomVectorGenerator noiseSource,
59                                  final GroundStation emitter, final GroundStation receiver,
60                                  final double sigma, final double baseWeight,
61                                  final ObservableSatellite satellite) {
62          super(noiseSource, sigma, baseWeight, satellite);
63          this.emitter   = emitter;
64          this.receiver  = receiver;
65          this.satellite = satellite;
66      }
67  
68      /** {@inheritDoc} */
69      @Override
70      public BistaticRange build(final AbsoluteDate date, final Map<ObservableSatellite, OrekitStepInterpolator> interpolators) {
71  
72          final double sigma                  = getTheoreticalStandardDeviation()[0];
73          final double baseWeight             = getBaseWeight()[0];
74          final SpacecraftState[] relevant    = new SpacecraftState[] { interpolators.get(satellite).getInterpolatedState(date) };
75  
76          // create a dummy measurement
77          final BistaticRange dummy = new BistaticRange(emitter, receiver, relevant[0].getDate(),
78                                                        Double.NaN, sigma, baseWeight, satellite);
79          for (final EstimationModifier<BistaticRange> modifier : getModifiers()) {
80              dummy.addModifier(modifier);
81          }
82  
83          // set a reference date for parameters missing one
84          for (final ParameterDriver driver : dummy.getParametersDrivers()) {
85              if (driver.getReferenceDate() == null) {
86                  final AbsoluteDate start = getStart();
87                  final AbsoluteDate end   = getEnd();
88                  driver.setReferenceDate(start.durationFrom(end) <= 0 ? start : end);
89              }
90          }
91  
92          // estimate the perfect value of the measurement
93          double range = dummy.estimateWithoutDerivatives(relevant).getEstimatedValue()[0];
94  
95          // add the noise
96          final double[] noise = getNoise();
97          if (noise != null) {
98              range += noise[0];
99          }
100 
101         // generate measurement
102         final BistaticRange measurement = new BistaticRange(emitter, receiver, relevant[0].getDate(),
103                                                             range, sigma, baseWeight, satellite);
104         for (final EstimationModifier<BistaticRange> modifier : getModifiers()) {
105             measurement.addModifier(modifier);
106         }
107         return measurement;
108 
109     }
110 
111 }