File Coverage

erfasrc/src/ltecm.c
Criterion Covered Total %
statement 0 16 0.0
branch n/a
condition n/a
subroutine n/a
pod n/a
total 0 16 0.0


line stmt bran cond sub pod time code
1             #include "erfa.h"
2              
3 0           void eraLtecm(double epj, double rm[3][3])
4             /*
5             ** - - - - - - - - -
6             ** e r a L t e c m
7             ** - - - - - - - - -
8             **
9             ** ICRS equatorial to ecliptic rotation matrix, long-term.
10             **
11             ** Given:
12             ** epj double Julian epoch (TT)
13             **
14             ** Returned:
15             ** rm double[3][3] ICRS to ecliptic rotation matrix
16             **
17             ** Notes:
18             **
19             ** 1) The matrix is in the sense
20             **
21             ** E_ep = rm x P_ICRS,
22             **
23             ** where P_ICRS is a vector with respect to ICRS right ascension
24             ** and declination axes and E_ep is the same vector with respect to
25             ** the (inertial) ecliptic and equinox of epoch epj.
26             **
27             ** 2) P_ICRS is a free vector, merely a direction, typically of unit
28             ** magnitude, and not bound to any particular spatial origin, such
29             ** as the Earth, Sun or SSB. No assumptions are made about whether
30             ** it represents starlight and embodies astrometric effects such as
31             ** parallax or aberration. The transformation is approximately that
32             ** between mean J2000.0 right ascension and declination and ecliptic
33             ** longitude and latitude, with only frame bias (always less than
34             ** 25 mas) to disturb this classical picture.
35             **
36             ** 3) The Vondrak et al. (2011, 2012) 400 millennia precession model
37             ** agrees with the IAU 2006 precession at J2000.0 and stays within
38             ** 100 microarcseconds during the 20th and 21st centuries. It is
39             ** accurate to a few arcseconds throughout the historical period,
40             ** worsening to a few tenths of a degree at the end of the
41             ** +/- 200,000 year time span.
42             **
43             ** Called:
44             ** eraLtpequ equator pole, long term
45             ** eraLtpecl ecliptic pole, long term
46             ** eraPxp vector product
47             ** eraPn normalize vector
48             **
49             ** References:
50             **
51             ** Vondrak, J., Capitaine, N. and Wallace, P., 2011, New precession
52             ** expressions, valid for long time intervals, Astron.Astrophys. 534,
53             ** A22
54             **
55             ** Vondrak, J., Capitaine, N. and Wallace, P., 2012, New precession
56             ** expressions, valid for long time intervals (Corrigendum),
57             ** Astron.Astrophys. 541, C1
58             **
59             ** Copyright (C) 2013-2020, NumFOCUS Foundation.
60             ** Derived, with permission, from the SOFA library. See notes at end of file.
61             */
62             {
63             /* Frame bias (IERS Conventions 2010, Eqs. 5.21 and 5.33) */
64             const double dx = -0.016617 * ERFA_DAS2R,
65             de = -0.0068192 * ERFA_DAS2R,
66             dr = -0.0146 * ERFA_DAS2R;
67              
68             double p[3], z[3], w[3], s, x[3], y[3];
69              
70              
71             /* Equator pole. */
72 0           eraLtpequ(epj, p);
73              
74             /* Ecliptic pole (bottom row of equatorial to ecliptic matrix). */
75 0           eraLtpecl(epj, z);
76              
77             /* Equinox (top row of matrix). */
78 0           eraPxp(p, z, w);
79 0           eraPn(w, &s, x);
80              
81             /* Middle row of matrix. */
82 0           eraPxp(z, x, y);
83              
84             /* Combine with frame bias. */
85 0           rm[0][0] = x[0] - x[1]*dr + x[2]*dx;
86 0           rm[0][1] = x[0]*dr + x[1] + x[2]*de;
87 0           rm[0][2] = - x[0]*dx - x[1]*de + x[2];
88 0           rm[1][0] = y[0] - y[1]*dr + y[2]*dx;
89 0           rm[1][1] = y[0]*dr + y[1] + y[2]*de;
90 0           rm[1][2] = - y[0]*dx - y[1]*de + y[2];
91 0           rm[2][0] = z[0] - z[1]*dr + z[2]*dx;
92 0           rm[2][1] = z[0]*dr + z[1] + z[2]*de;
93 0           rm[2][2] = - z[0]*dx - z[1]*de + z[2];
94              
95 0           }
96             /*----------------------------------------------------------------------
97             **
98             **
99             ** Copyright (C) 2013-2020, NumFOCUS Foundation.
100             ** All rights reserved.
101             **
102             ** This library is derived, with permission, from the International
103             ** Astronomical Union's "Standards of Fundamental Astronomy" library,
104             ** available from http://www.iausofa.org.
105             **
106             ** The ERFA version is intended to retain identical functionality to
107             ** the SOFA library, but made distinct through different function and
108             ** file names, as set out in the SOFA license conditions. The SOFA
109             ** original has a role as a reference standard for the IAU and IERS,
110             ** and consequently redistribution is permitted only in its unaltered
111             ** state. The ERFA version is not subject to this restriction and
112             ** therefore can be included in distributions which do not support the
113             ** concept of "read only" software.
114             **
115             ** Although the intent is to replicate the SOFA API (other than
116             ** replacement of prefix names) and results (with the exception of
117             ** bugs; any that are discovered will be fixed), SOFA is not
118             ** responsible for any errors found in this version of the library.
119             **
120             ** If you wish to acknowledge the SOFA heritage, please acknowledge
121             ** that you are using a library derived from SOFA, rather than SOFA
122             ** itself.
123             **
124             **
125             ** TERMS AND CONDITIONS
126             **
127             ** Redistribution and use in source and binary forms, with or without
128             ** modification, are permitted provided that the following conditions
129             ** are met:
130             **
131             ** 1 Redistributions of source code must retain the above copyright
132             ** notice, this list of conditions and the following disclaimer.
133             **
134             ** 2 Redistributions in binary form must reproduce the above copyright
135             ** notice, this list of conditions and the following disclaimer in
136             ** the documentation and/or other materials provided with the
137             ** distribution.
138             **
139             ** 3 Neither the name of the Standards Of Fundamental Astronomy Board,
140             ** the International Astronomical Union nor the names of its
141             ** contributors may be used to endorse or promote products derived
142             ** from this software without specific prior written permission.
143             **
144             ** THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
145             ** "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
146             ** LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
147             ** FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
148             ** COPYRIGHT HOLDER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
149             ** INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
150             ** BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES;
151             ** LOSS OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER
152             ** CAUSED AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
153             ** LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
154             ** ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
155             ** POSSIBILITY OF SUCH DAMAGE.
156             **
157             */