1 /* Copyright 2002-2022 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.numerical;
18
19 import java.util.List;
20
21 import org.hipparchus.linear.RealMatrix;
22 import org.orekit.orbits.Orbit;
23 import org.orekit.propagation.AbstractMatricesHarvester;
24 import org.orekit.propagation.SpacecraftState;
25 import org.orekit.utils.DoubleArrayDictionary;
26
27 /** Harvester between two-dimensional Jacobian matrices and one-dimensional {@link
28 * SpacecraftState#getAdditionalState(String) additional state arrays}.
29 * @author Luc Maisonobe
30 * @since 11.1
31 */
32 class NumericalPropagationHarvester extends AbstractMatricesHarvester {
33
34 /** Propagator bound to this harvester. */
35 private final NumericalPropagator propagator;
36
37 /** Columns names for parameters. */
38 private List<String> columnsNames;
39
40 /** Simple constructor.
41 * <p>
42 * The arguments for initial matrices <em>must</em> be compatible with the {@link org.orekit.orbits.OrbitType orbit type}
43 * and {@link org.orekit.orbits.PositionAngle position angle} that will be used by propagator
44 * </p>
45 * @param propagator propagator bound to this harvester
46 * @param stmName State Transition Matrix state name
47 * @param initialStm initial State Transition Matrix ∂Y/∂Y₀,
48 * if null (which is the most frequent case), assumed to be 6x6 identity
49 * @param initialJacobianColumns initial columns of the Jacobians matrix with respect to parameters,
50 * if null or if some selected parameters are missing from the dictionary, the corresponding
51 * initial column is assumed to be 0
52 */
53 NumericalPropagationHarvester(final NumericalPropagator propagator, final String stmName,
54 final RealMatrix initialStm, final DoubleArrayDictionary initialJacobianColumns) {
55 super(stmName, initialStm, initialJacobianColumns);
56 this.propagator = propagator;
57 this.columnsNames = null;
58 }
59
60 /** {@inheritDoc} */
61 @Override
62 protected double[][] getConversionJacobian(final SpacecraftState state) {
63
64 final double[][] dYdC = new double[STATE_DIMENSION][STATE_DIMENSION];
65
66 if (state.isOrbitDefined()) {
67 // make sure the state is in the desired orbit type
68 final Orbit orbit = propagator.getOrbitType().convertType(state.getOrbit());
69
70 // compute the Jacobian, taking the position angle type into account
71 orbit.getJacobianWrtCartesian(propagator.getPositionAngleType(), dYdC);
72 } else {
73 // for absolute PVA, parameters are already Cartesian
74 for (int i = 0; i < STATE_DIMENSION; ++i) {
75 dYdC[i][i] = 1.0;
76 }
77 }
78
79 return dYdC;
80
81 }
82
83 /** {@inheritDoc} */
84 @Override
85 public void freezeColumnsNames() {
86 columnsNames = getJacobiansColumnsNames();
87 }
88
89 /** {@inheritDoc} */
90 @Override
91 public List<String> getJacobiansColumnsNames() {
92 return columnsNames == null ? propagator.getJacobiansColumnsNames() : columnsNames;
93 }
94
95 }