1   /* Copyright 2002-2026 CS GROUP
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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
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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
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16   */
17  package org.orekit.estimation.measurements.generation;
18  
19  import java.util.Map;
20  
21  import org.orekit.estimation.measurements.AngularRaDec;
22  import org.orekit.estimation.measurements.GroundStation;
23  import org.orekit.estimation.measurements.MeasurementQuality;
24  import org.orekit.estimation.measurements.ObservableSatellite;
25  import org.orekit.estimation.measurements.Observer;
26  import org.orekit.frames.Frame;
27  import org.orekit.propagation.sampling.OrekitStepInterpolator;
28  import org.orekit.signal.SignalTravelTimeModel;
29  import org.orekit.time.AbsoluteDate;
30  
31  /** Builder for {@link AngularRaDec} measurements.
32   * @author Luc Maisonobe
33   * @since 9.3
34   */
35  public class AngularRaDecBuilder extends AbstractSignalBasedBuilder<AngularRaDec> {
36  
37      /** Sensor. */
38      private final Observer observer;
39  
40      /** Reference frame in which the right ascension - declination angles are given. */
41      private final Frame referenceFrame;
42  
43      /** Simple constructor.
44       * @param station ground station from which measurement is performed
45       * @param referenceFrame Reference frame in which the right ascension - declination angles are given
46       * @param sigma theoretical standard deviation
47       * @param baseWeight base weight
48       * @param satellite satellite related to this builder
49       */
50      public AngularRaDecBuilder(final GroundStation station,
51                                 final Frame referenceFrame, final double[] sigma, final double[] baseWeight,
52                                 final ObservableSatellite satellite) {
53          this(station, referenceFrame, new MeasurementQuality(sigma, baseWeight), new SignalTravelTimeModel(), satellite);
54      }
55  
56      /** Simple constructor.
57       * @param observer sensor from which measurement is performed
58       * @param referenceFrame Reference frame in which the right ascension - declination angles are given
59       * @param measurementQuality measurement quality as used in estimation (in Orekit, the crossed-terms
60       *                           of the covariance matrix are only used by Kalman filters, not least squares)
61       * @param signalTravelTimeModel signal travel time model
62       * @param satellite satellite related to this builder
63       * @since 14.0
64       */
65      public AngularRaDecBuilder(final Observer observer,
66                                 final Frame referenceFrame, final MeasurementQuality measurementQuality,
67                                 final SignalTravelTimeModel signalTravelTimeModel, final ObservableSatellite satellite) {
68          super(measurementQuality, signalTravelTimeModel, satellite);
69          this.observer = observer;
70          this.referenceFrame = referenceFrame;
71      }
72  
73      /**
74       * Getter for the observer.
75       * @return observer
76       * @since 14.0
77       */
78      public Observer getObserver() {
79          return observer;
80      }
81  
82      /** {@inheritDoc} */
83      @Override
84      protected AngularRaDec buildObserved(final AbsoluteDate date,
85                                           final Map<ObservableSatellite, OrekitStepInterpolator> interpolators) {
86          return new AngularRaDec(observer, referenceFrame, date, new double[2], getMeasurementQuality(),
87                                  getSignalTravelTimeModel(), getSatellites()[0]);
88      }
89  
90  }