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.frames;
18
19 import org.hipparchus.CalculusFieldElement;
20 import org.hipparchus.geometry.euclidean.threed.FieldRotation;
21 import org.hipparchus.geometry.euclidean.threed.RotationConvention;
22 import org.hipparchus.geometry.euclidean.threed.RotationOrder;
23 import org.orekit.time.FieldAbsoluteDate;
24 import org.orekit.time.TimeScalarFunction;
25 import org.orekit.time.TimeScales;
26 import org.orekit.time.TimeVectorFunction;
27 import org.orekit.utils.IERSConventions;
28
29 /** Provider for True of Date (ToD) frame.
30 * <p>This frame handles nutation effects according to selected IERS conventions.</p>
31 * <p>Transform is computed with reference to the {@link MODProvider Mean of Date} frame.</p>
32 * @author Pascal Parraud
33 */
34 class TODProvider implements FieldBasedTransformProvider, EOPBasedTransformProvider {
35
36 /** Conventions. */
37 private final IERSConventions conventions;
38
39 /** EOP history. */
40 private final EOPHistory eopHistory;
41
42 /** Function computing the mean obliquity. */
43 private final TimeScalarFunction obliquityFunction;
44
45 /** Function computing the nutation angles. */
46 private final TimeVectorFunction nutationFunction;
47
48
49 /**
50 * Simple constructor.
51 * @param conventions IERS conventions to apply
52 * @param eopHistory EOP history, or {@code null} if no correction should be
53 * applied.
54 * @param timeScales TAI time scale.
55 */
56 TODProvider(final IERSConventions conventions,
57 final EOPHistory eopHistory,
58 final TimeScales timeScales) {
59 this.conventions = conventions;
60 this.eopHistory = eopHistory;
61 this.obliquityFunction = conventions.getMeanObliquityFunction(timeScales);
62 this.nutationFunction =
63 conventions.getNutationFunction(timeScales);
64 }
65
66 /**
67 * Private constructor.
68 *
69 * @param conventions IERS conventions to use.
70 * @param eopHistory or {@code null} if no correction should be applied.
71 * @param obliquityFunction to use.
72 * @param nutationFunction to use.
73 */
74 private TODProvider(final IERSConventions conventions,
75 final EOPHistory eopHistory,
76 final TimeScalarFunction obliquityFunction,
77 final TimeVectorFunction nutationFunction) {
78 this.conventions = conventions;
79 this.eopHistory = eopHistory;
80 this.obliquityFunction = obliquityFunction;
81 this.nutationFunction = nutationFunction;
82 }
83
84 /** {@inheritDoc} */
85 @Override
86 public EOPHistory getEOPHistory() {
87 return eopHistory;
88 }
89
90 /** {@inheritDoc} */
91 @Override
92 public TODProvider getNonInterpolatingProvider() {
93 return new TODProvider(conventions, eopHistory.getEOPHistoryWithoutCachedTidalCorrection(),
94 obliquityFunction, nutationFunction);
95 }
96
97 /** Compute the complete nutation rotation.
98 * @param date current date
99 * @param <T> type of the field elements
100 * @return complete nutation rotation
101 */
102 public <T extends CalculusFieldElement<T>> FieldRotation<T> getRotation(final FieldAbsoluteDate<T> date) {
103
104 // compute nutation angles
105 final T[] angles = nutationFunction.value(date);
106
107 // compute the mean obliquity of the ecliptic
108 final T moe = obliquityFunction.value(date);
109
110 T dpsi = angles[0];
111 T deps = angles[1];
112 if (eopHistory != null) {
113 // apply the corrections for the nutation parameters
114 final T[] correction = eopHistory.getEquinoxNutationCorrection(date);
115 dpsi = dpsi.add(correction[0]);
116 deps = deps.add(correction[1]);
117 }
118
119 // compute the true obliquity of the ecliptic
120 final T toe = moe.add(deps);
121
122 // complete nutation
123 return new FieldRotation<>(RotationOrder.XZX, RotationConvention.FRAME_TRANSFORM,
124 moe, dpsi.negate(), toe.negate());
125
126 }
127
128 }