1   /* Copyright 2002-2026 CS GROUP
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.propagation.conversion;
18  
19  import org.orekit.attitudes.AttitudeProvider;
20  import org.orekit.estimation.leastsquares.AbstractBatchLSModel;
21  import org.orekit.estimation.leastsquares.ModelObserver;
22  import org.orekit.estimation.measurements.ObservedMeasurement;
23  import org.orekit.orbits.Orbit;
24  import org.orekit.orbits.OrbitalParameterFactory;
25  import org.orekit.orbits.OrbitalParameters;
26  import org.orekit.propagation.Propagator;
27  import org.orekit.utils.ParameterDriversList;
28  
29  import java.util.List;
30  
31  /** This interface is the top-level abstraction to build propagators for conversion.
32   * @author Pascal Parraud
33   * @since 6.0
34   */
35  public interface PropagatorBuilder extends Cloneable {
36  
37      /** Build a propagator.
38       * @param normalizedParameters normalized values for the selected parameters
39       * @return an initialized propagator
40       */
41      Propagator buildPropagator(double[] normalizedParameters);
42  
43      /** Build a propagator from current value of selected normalized parameters.
44       * @return an initialized propagator
45       */
46      default Propagator buildPropagator() {
47          return buildPropagator(getSelectedNormalizedParameters());
48      }
49  
50      /** Build a new batch least squares model.
51       * @param builders builders to use for propagation
52       * @param measurements measurements
53       * @param estimatedMeasurementsParameters estimated measurements parameters
54       * @param observer observer to be notified at model calls
55       * @return a new model for the Batch Least Squares orbit determination
56       * @since 12.0
57       */
58      AbstractBatchLSModel buildLeastSquaresModel(PropagatorBuilder[] builders,
59                                                  List<ObservedMeasurement<?>> measurements,
60                                                  ParameterDriversList estimatedMeasurementsParameters,
61                                                  ModelObserver observer);
62  
63      /** Get the current value of selected normalized parameters.
64       * @return current value of selected normalized parameters
65       */
66      double[] getSelectedNormalizedParameters();
67  
68      /**
69       * Get the attitude provider.
70       *
71       * @return the attitude provider
72       * @since 13.0
73       */
74      AttitudeProvider getAttitudeProvider();
75  
76      /** Get the orbital parameters factory.
77       * @return orbital parameters factory
78       * @since 14.0
79       */
80      OrbitalParameterFactory<? extends OrbitalParameters> getOrbitalParameterFactory();
81  
82      /** Get the initial mass.
83       * @return the mass (kg)
84       * @since 13.0
85       */
86      double getMass();
87  
88      /** Get the drivers for the configurable propagation parameters.
89       * <p>
90       * The parameters typically correspond to force models.
91       * </p>
92       * @return drivers for the configurable propagation parameters
93       * @since 8.0
94       */
95      ParameterDriversList getPropagationParametersDrivers();
96  
97      /** Reset the orbit in the propagator builder.
98       * @param newOrbit New orbit to set in the propagator builder
99       * @since 12.0
100      */
101     void resetOrbit(Orbit newOrbit);
102 
103 }