1 /* Copyright 2002-2025 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.data;
18
19 import org.hipparchus.CalculusFieldElement;
20
21 /** Class for tide terms.
22 * <p>
23 * BEWARE! For consistency with all the other Poisson series terms,
24 * the elements in γ, l, l', F, D and Ω are ADDED together to compute
25 * the argument of the term. In classical tides series, the computed
26 * argument is cGamma * γ - (cL * l + cLPrime * l' + cF * F + cD * D
27 * + cOmega * Ω). So at parsing time, the signs of cL, cLPrime, cF,
28 * cD and cOmega must already have been reversed so the addition
29 * performed here will work. This is done automatically when the
30 * parser has been configured with a call to {@link
31 * PoissonSeriesParser#withDoodson(int, int)} as the relationship
32 * between the Doodson arguments and the traditional Delaunay
33 * arguments ensures the proper sign is known.
34 * </p>
35 * @author Luc Maisonobe
36 */
37 class TideTerm extends SeriesTerm {
38
39 /** Coefficient for γ = GMST + π tide parameter. */
40 private final int cGamma;
41
42 /** Coefficient for mean anomaly of the Moon. */
43 private final int cL;
44
45 /** Coefficient for mean anomaly of the Sun. */
46 private final int cLPrime;
47
48 /** Coefficient for L - Ω where L is the mean longitude of the Moon. */
49 private final int cF;
50
51 /** Coefficient for mean elongation of the Moon from the Sun. */
52 private final int cD;
53
54 /** Coefficient for mean longitude of the ascending node of the Moon. */
55 private final int cOmega;
56
57 /** Build a tide term for nutation series.
58 * @param cGamma coefficient for γ = GMST + π tide parameter
59 * @param cL coefficient for mean anomaly of the Moon
60 * @param cLPrime coefficient for mean anomaly of the Sun
61 * @param cF coefficient for L - Ω where L is the mean longitude of the Moon
62 * @param cD coefficient for mean elongation of the Moon from the Sun
63 * @param cOmega coefficient for mean longitude of the ascending node of the Moon
64 */
65 TideTerm(final int cGamma,
66 final int cL, final int cLPrime, final int cF, final int cD, final int cOmega) {
67 this.cGamma = cGamma;
68 this.cL = cL;
69 this.cLPrime = cLPrime;
70 this.cF = cF;
71 this.cD = cD;
72 this.cOmega = cOmega;
73 }
74
75 /** {@inheritDoc} */
76 protected double argument(final BodiesElements elements) {
77 return cGamma * elements.getGamma() +
78 cL * elements.getL() + cLPrime * elements.getLPrime() + cF * elements.getF() +
79 cD * elements.getD() + cOmega * elements.getOmega();
80 }
81
82 /** {@inheritDoc} */
83 protected double argumentDerivative(final BodiesElements elements) {
84 return cGamma * elements.getGammaDot() +
85 cL * elements.getLDot() + cLPrime * elements.getLPrimeDot() + cF * elements.getFDot() +
86 cD * elements.getDDot() + cOmega * elements.getOmegaDot();
87 }
88
89 /** {@inheritDoc} */
90 protected <T extends CalculusFieldElement<T>> T argument(final FieldBodiesElements<T> elements) {
91 return elements.getGamma().multiply(cGamma).
92 add(elements.getL().multiply(cL)).
93 add(elements.getLPrime().multiply(cLPrime)).
94 add(elements.getF().multiply(cF)).
95 add(elements.getD().multiply(cD)).
96 add(elements.getOmega().multiply(cOmega));
97 }
98
99 /** {@inheritDoc} */
100 protected <T extends CalculusFieldElement<T>> T argumentDerivative(final FieldBodiesElements<T> elements) {
101 return elements.getGammaDot().multiply(cGamma).
102 add(elements.getLDot().multiply(cL)).
103 add(elements.getLPrimeDot().multiply(cLPrime)).
104 add(elements.getFDot().multiply(cF)).
105 add(elements.getDDot().multiply(cD)).
106 add(elements.getOmegaDot().multiply(cOmega));
107 }
108
109 }