FACT++  1.0
eect00.c
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1 #include "erfa.h"
2 
3 double eraEect00(double date1, double date2)
4 /*
5 ** - - - - - - - - - -
6 ** e r a E e c t 0 0
7 ** - - - - - - - - - -
8 **
9 ** Equation of the equinoxes complementary terms, consistent with
10 ** IAU 2000 resolutions.
11 **
12 ** Given:
13 ** date1,date2 double TT as a 2-part Julian Date (Note 1)
14 **
15 ** Returned (function value):
16 ** double complementary terms (Note 2)
17 **
18 ** Notes:
19 **
20 ** 1) The TT date date1+date2 is a Julian Date, apportioned in any
21 ** convenient way between the two arguments. For example,
22 ** JD(TT)=2450123.7 could be expressed in any of these ways,
23 ** among others:
24 **
25 ** date1 date2
26 **
27 ** 2450123.7 0.0 (JD method)
28 ** 2451545.0 -1421.3 (J2000 method)
29 ** 2400000.5 50123.2 (MJD method)
30 ** 2450123.5 0.2 (date & time method)
31 **
32 ** The JD method is the most natural and convenient to use in
33 ** cases where the loss of several decimal digits of resolution
34 ** is acceptable. The J2000 method is best matched to the way
35 ** the argument is handled internally and will deliver the
36 ** optimum resolution. The MJD method and the date & time methods
37 ** are both good compromises between resolution and convenience.
38 **
39 ** 2) The "complementary terms" are part of the equation of the
40 ** equinoxes (EE), classically the difference between apparent and
41 ** mean Sidereal Time:
42 **
43 ** GAST = GMST + EE
44 **
45 ** with:
46 **
47 ** EE = dpsi * cos(eps)
48 **
49 ** where dpsi is the nutation in longitude and eps is the obliquity
50 ** of date. However, if the rotation of the Earth were constant in
51 ** an inertial frame the classical formulation would lead to
52 ** apparent irregularities in the UT1 timescale traceable to side-
53 ** effects of precession-nutation. In order to eliminate these
54 ** effects from UT1, "complementary terms" were introduced in 1994
55 ** (IAU, 1994) and took effect from 1997 (Capitaine and Gontier,
56 ** 1993):
57 **
58 ** GAST = GMST + CT + EE
59 **
60 ** By convention, the complementary terms are included as part of
61 ** the equation of the equinoxes rather than as part of the mean
62 ** Sidereal Time. This slightly compromises the "geometrical"
63 ** interpretation of mean sidereal time but is otherwise
64 ** inconsequential.
65 **
66 ** The present function computes CT in the above expression,
67 ** compatible with IAU 2000 resolutions (Capitaine et al., 2002, and
68 ** IERS Conventions 2003).
69 **
70 ** Called:
71 ** eraFal03 mean anomaly of the Moon
72 ** eraFalp03 mean anomaly of the Sun
73 ** eraFaf03 mean argument of the latitude of the Moon
74 ** eraFad03 mean elongation of the Moon from the Sun
75 ** eraFaom03 mean longitude of the Moon's ascending node
76 ** eraFave03 mean longitude of Venus
77 ** eraFae03 mean longitude of Earth
78 ** eraFapa03 general accumulated precession in longitude
79 **
80 ** References:
81 **
82 ** Capitaine, N. & Gontier, A.-M., Astron. Astrophys., 275,
83 ** 645-650 (1993)
84 **
85 ** Capitaine, N., Wallace, P.T. and McCarthy, D.D., "Expressions to
86 ** implement the IAU 2000 definition of UT1", Astronomy &
87 ** Astrophysics, 406, 1135-1149 (2003)
88 **
89 ** IAU Resolution C7, Recommendation 3 (1994)
90 **
91 ** McCarthy, D. D., Petit, G. (eds.), IERS Conventions (2003),
92 ** IERS Technical Note No. 32, BKG (2004)
93 **
94 ** Copyright (C) 2013-2015, NumFOCUS Foundation.
95 ** Derived, with permission, from the SOFA library. See notes at end of file.
96 */
97 {
98 /* Time since J2000.0, in Julian centuries */
99  double t;
100 
101 /* Miscellaneous */
102  int i, j;
103  double a, s0, s1;
104 
105 /* Fundamental arguments */
106  double fa[14];
107 
108 /* Returned value. */
109  double eect;
110 
111 /* ----------------------------------------- */
112 /* The series for the EE complementary terms */
113 /* ----------------------------------------- */
114 
115  typedef struct {
116  int nfa[8]; /* coefficients of l,l',F,D,Om,LVe,LE,pA */
117  double s, c; /* sine and cosine coefficients */
118  } TERM;
119 
120 /* Terms of order t^0 */
121  static const TERM e0[] = {
122 
123  /* 1-10 */
124  {{ 0, 0, 0, 0, 1, 0, 0, 0}, 2640.96e-6, -0.39e-6 },
125  {{ 0, 0, 0, 0, 2, 0, 0, 0}, 63.52e-6, -0.02e-6 },
126  {{ 0, 0, 2, -2, 3, 0, 0, 0}, 11.75e-6, 0.01e-6 },
127  {{ 0, 0, 2, -2, 1, 0, 0, 0}, 11.21e-6, 0.01e-6 },
128  {{ 0, 0, 2, -2, 2, 0, 0, 0}, -4.55e-6, 0.00e-6 },
129  {{ 0, 0, 2, 0, 3, 0, 0, 0}, 2.02e-6, 0.00e-6 },
130  {{ 0, 0, 2, 0, 1, 0, 0, 0}, 1.98e-6, 0.00e-6 },
131  {{ 0, 0, 0, 0, 3, 0, 0, 0}, -1.72e-6, 0.00e-6 },
132  {{ 0, 1, 0, 0, 1, 0, 0, 0}, -1.41e-6, -0.01e-6 },
133  {{ 0, 1, 0, 0, -1, 0, 0, 0}, -1.26e-6, -0.01e-6 },
134 
135  /* 11-20 */
136  {{ 1, 0, 0, 0, -1, 0, 0, 0}, -0.63e-6, 0.00e-6 },
137  {{ 1, 0, 0, 0, 1, 0, 0, 0}, -0.63e-6, 0.00e-6 },
138  {{ 0, 1, 2, -2, 3, 0, 0, 0}, 0.46e-6, 0.00e-6 },
139  {{ 0, 1, 2, -2, 1, 0, 0, 0}, 0.45e-6, 0.00e-6 },
140  {{ 0, 0, 4, -4, 4, 0, 0, 0}, 0.36e-6, 0.00e-6 },
141  {{ 0, 0, 1, -1, 1, -8, 12, 0}, -0.24e-6, -0.12e-6 },
142  {{ 0, 0, 2, 0, 0, 0, 0, 0}, 0.32e-6, 0.00e-6 },
143  {{ 0, 0, 2, 0, 2, 0, 0, 0}, 0.28e-6, 0.00e-6 },
144  {{ 1, 0, 2, 0, 3, 0, 0, 0}, 0.27e-6, 0.00e-6 },
145  {{ 1, 0, 2, 0, 1, 0, 0, 0}, 0.26e-6, 0.00e-6 },
146 
147  /* 21-30 */
148  {{ 0, 0, 2, -2, 0, 0, 0, 0}, -0.21e-6, 0.00e-6 },
149  {{ 0, 1, -2, 2, -3, 0, 0, 0}, 0.19e-6, 0.00e-6 },
150  {{ 0, 1, -2, 2, -1, 0, 0, 0}, 0.18e-6, 0.00e-6 },
151  {{ 0, 0, 0, 0, 0, 8,-13, -1}, -0.10e-6, 0.05e-6 },
152  {{ 0, 0, 0, 2, 0, 0, 0, 0}, 0.15e-6, 0.00e-6 },
153  {{ 2, 0, -2, 0, -1, 0, 0, 0}, -0.14e-6, 0.00e-6 },
154  {{ 1, 0, 0, -2, 1, 0, 0, 0}, 0.14e-6, 0.00e-6 },
155  {{ 0, 1, 2, -2, 2, 0, 0, 0}, -0.14e-6, 0.00e-6 },
156  {{ 1, 0, 0, -2, -1, 0, 0, 0}, 0.14e-6, 0.00e-6 },
157  {{ 0, 0, 4, -2, 4, 0, 0, 0}, 0.13e-6, 0.00e-6 },
158 
159  /* 31-33 */
160  {{ 0, 0, 2, -2, 4, 0, 0, 0}, -0.11e-6, 0.00e-6 },
161  {{ 1, 0, -2, 0, -3, 0, 0, 0}, 0.11e-6, 0.00e-6 },
162  {{ 1, 0, -2, 0, -1, 0, 0, 0}, 0.11e-6, 0.00e-6 }
163  };
164 
165 /* Terms of order t^1 */
166  static const TERM e1[] = {
167  {{ 0, 0, 0, 0, 1, 0, 0, 0}, -0.87e-6, 0.00e-6 }
168  };
169 
170 /* Number of terms in the series */
171  const int NE0 = (int) (sizeof e0 / sizeof (TERM));
172  const int NE1 = (int) (sizeof e1 / sizeof (TERM));
173 
174 /*--------------------------------------------------------------------*/
175 
176 /* Interval between fundamental epoch J2000.0 and current date (JC). */
177  t = ((date1 - ERFA_DJ00) + date2) / ERFA_DJC;
178 
179 /* Fundamental Arguments (from IERS Conventions 2003) */
180 
181 /* Mean anomaly of the Moon. */
182  fa[0] = eraFal03(t);
183 
184 /* Mean anomaly of the Sun. */
185  fa[1] = eraFalp03(t);
186 
187 /* Mean longitude of the Moon minus that of the ascending node. */
188  fa[2] = eraFaf03(t);
189 
190 /* Mean elongation of the Moon from the Sun. */
191  fa[3] = eraFad03(t);
192 
193 /* Mean longitude of the ascending node of the Moon. */
194  fa[4] = eraFaom03(t);
195 
196 /* Mean longitude of Venus. */
197  fa[5] = eraFave03(t);
198 
199 /* Mean longitude of Earth. */
200  fa[6] = eraFae03(t);
201 
202 /* General precession in longitude. */
203  fa[7] = eraFapa03(t);
204 
205 /* Evaluate the EE complementary terms. */
206  s0 = 0.0;
207  s1 = 0.0;
208 
209  for (i = NE0-1; i >= 0; i--) {
210  a = 0.0;
211  for (j = 0; j < 8; j++) {
212  a += (double)(e0[i].nfa[j]) * fa[j];
213  }
214  s0 += e0[i].s * sin(a) + e0[i].c * cos(a);
215  }
216 
217  for (i = NE1-1; i >= 0; i--) {
218  a = 0.0;
219  for (j = 0; j < 8; j++) {
220  a += (double)(e1[i].nfa[j]) * fa[j];
221  }
222  s1 += e1[i].s * sin(a) + e1[i].c * cos(a);
223  }
224 
225  eect = (s0 + s1 * t ) * ERFA_DAS2R;
226 
227  return eect;
228 
229 }
230 /*----------------------------------------------------------------------
231 **
232 **
233 ** Copyright (C) 2013-2015, NumFOCUS Foundation.
234 ** All rights reserved.
235 **
236 ** This library is derived, with permission, from the International
237 ** Astronomical Union's "Standards of Fundamental Astronomy" library,
238 ** available from http://www.iausofa.org.
239 **
240 ** The ERFA version is intended to retain identical functionality to
241 ** the SOFA library, but made distinct through different function and
242 ** file names, as set out in the SOFA license conditions. The SOFA
243 ** original has a role as a reference standard for the IAU and IERS,
244 ** and consequently redistribution is permitted only in its unaltered
245 ** state. The ERFA version is not subject to this restriction and
246 ** therefore can be included in distributions which do not support the
247 ** concept of "read only" software.
248 **
249 ** Although the intent is to replicate the SOFA API (other than
250 ** replacement of prefix names) and results (with the exception of
251 ** bugs; any that are discovered will be fixed), SOFA is not
252 ** responsible for any errors found in this version of the library.
253 **
254 ** If you wish to acknowledge the SOFA heritage, please acknowledge
255 ** that you are using a library derived from SOFA, rather than SOFA
256 ** itself.
257 **
258 **
259 ** TERMS AND CONDITIONS
260 **
261 ** Redistribution and use in source and binary forms, with or without
262 ** modification, are permitted provided that the following conditions
263 ** are met:
264 **
265 ** 1 Redistributions of source code must retain the above copyright
266 ** notice, this list of conditions and the following disclaimer.
267 **
268 ** 2 Redistributions in binary form must reproduce the above copyright
269 ** notice, this list of conditions and the following disclaimer in
270 ** the documentation and/or other materials provided with the
271 ** distribution.
272 **
273 ** 3 Neither the name of the Standards Of Fundamental Astronomy Board,
274 ** the International Astronomical Union nor the names of its
275 ** contributors may be used to endorse or promote products derived
276 ** from this software without specific prior written permission.
277 **
278 ** THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
279 ** "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
280 ** LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
281 ** FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
282 ** COPYRIGHT HOLDER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
283 ** INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
284 ** BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES;
285 ** LOSS OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER
286 ** CAUSED AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
287 ** LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
288 ** ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
289 ** POSSIBILITY OF SUCH DAMAGE.
290 **
291 */
#define ERFA_DJ00
Definition: erfam.h:87
double eraFae03(double t)
Definition: fae03.c:3
double eraFapa03(double t)
Definition: fapa03.c:3
double eraFal03(double t)
Definition: fal03.c:3
int i
Definition: db_dim_client.c:21
#define ERFA_DAS2R
Definition: erfam.h:60
double eraFaom03(double t)
Definition: faom03.c:3
double eraFad03(double t)
Definition: fad03.c:3
double eraFaf03(double t)
Definition: faf03.c:3
double eraFalp03(double t)
Definition: falp03.c:3
#define ERFA_DJC
Definition: erfam.h:81
TT t
Definition: test_client.c:26
double eraEect00(double date1, double date2)
Definition: eect00.c:3
double eraFave03(double t)
Definition: fave03.c:3