source: trunk/FACT++/erfa/src/c2ibpn.c@ 18679

Last change on this file since 18679 was 18348, checked in by tbretz, 9 years ago
File size: 6.0 KB
Line 
1#include "erfa.h"
2
3void eraC2ibpn(double date1, double date2, double rbpn[3][3],
4 double rc2i[3][3])
5/*
6** - - - - - - - - - -
7** e r a C 2 i b p n
8** - - - - - - - - - -
9**
10** Form the celestial-to-intermediate matrix for a given date given
11** the bias-precession-nutation matrix. IAU 2000.
12**
13** Given:
14** date1,date2 double TT as a 2-part Julian Date (Note 1)
15** rbpn double[3][3] celestial-to-true matrix (Note 2)
16**
17** Returned:
18** rc2i double[3][3] celestial-to-intermediate matrix (Note 3)
19**
20** Notes:
21**
22** 1) The TT date date1+date2 is a Julian Date, apportioned in any
23** convenient way between the two arguments. For example,
24** JD(TT)=2450123.7 could be expressed in any of these ways,
25** among others:
26**
27** date1 date2
28**
29** 2450123.7 0.0 (JD method)
30** 2451545.0 -1421.3 (J2000 method)
31** 2400000.5 50123.2 (MJD method)
32** 2450123.5 0.2 (date & time method)
33**
34** The JD method is the most natural and convenient to use in
35** cases where the loss of several decimal digits of resolution
36** is acceptable. The J2000 method is best matched to the way
37** the argument is handled internally and will deliver the
38** optimum resolution. The MJD method and the date & time methods
39** are both good compromises between resolution and convenience.
40**
41** 2) The matrix rbpn transforms vectors from GCRS to true equator (and
42** CIO or equinox) of date. Only the CIP (bottom row) is used.
43**
44** 3) The matrix rc2i is the first stage in the transformation from
45** celestial to terrestrial coordinates:
46**
47** [TRS] = RPOM * R_3(ERA) * rc2i * [CRS]
48**
49** = RC2T * [CRS]
50**
51** where [CRS] is a vector in the Geocentric Celestial Reference
52** System and [TRS] is a vector in the International Terrestrial
53** Reference System (see IERS Conventions 2003), ERA is the Earth
54** Rotation Angle and RPOM is the polar motion matrix.
55**
56** 4) Although its name does not include "00", This function is in fact
57** specific to the IAU 2000 models.
58**
59** Called:
60** eraBpn2xy extract CIP X,Y coordinates from NPB matrix
61** eraC2ixy celestial-to-intermediate matrix, given X,Y
62**
63** References:
64** "Expressions for the Celestial Intermediate Pole and Celestial
65** Ephemeris Origin consistent with the IAU 2000A precession-
66** nutation model", Astron.Astrophys. 400, 1145-1154 (2003)
67**
68** n.b. The celestial ephemeris origin (CEO) was renamed "celestial
69** intermediate origin" (CIO) by IAU 2006 Resolution 2.
70**
71** McCarthy, D. D., Petit, G. (eds.), IERS Conventions (2003),
72** IERS Technical Note No. 32, BKG (2004)
73**
74** Copyright (C) 2013-2015, NumFOCUS Foundation.
75** Derived, with permission, from the SOFA library. See notes at end of file.
76*/
77{
78 double x, y;
79
80/* Extract the X,Y coordinates. */
81 eraBpn2xy(rbpn, &x, &y);
82
83/* Form the celestial-to-intermediate matrix (n.b. IAU 2000 specific). */
84 eraC2ixy(date1, date2, x, y, rc2i);
85
86 return;
87
88}
89/*----------------------------------------------------------------------
90**
91**
92** Copyright (C) 2013-2015, NumFOCUS Foundation.
93** All rights reserved.
94**
95** This library is derived, with permission, from the International
96** Astronomical Union's "Standards of Fundamental Astronomy" library,
97** available from http://www.iausofa.org.
98**
99** The ERFA version is intended to retain identical functionality to
100** the SOFA library, but made distinct through different function and
101** file names, as set out in the SOFA license conditions. The SOFA
102** original has a role as a reference standard for the IAU and IERS,
103** and consequently redistribution is permitted only in its unaltered
104** state. The ERFA version is not subject to this restriction and
105** therefore can be included in distributions which do not support the
106** concept of "read only" software.
107**
108** Although the intent is to replicate the SOFA API (other than
109** replacement of prefix names) and results (with the exception of
110** bugs; any that are discovered will be fixed), SOFA is not
111** responsible for any errors found in this version of the library.
112**
113** If you wish to acknowledge the SOFA heritage, please acknowledge
114** that you are using a library derived from SOFA, rather than SOFA
115** itself.
116**
117**
118** TERMS AND CONDITIONS
119**
120** Redistribution and use in source and binary forms, with or without
121** modification, are permitted provided that the following conditions
122** are met:
123**
124** 1 Redistributions of source code must retain the above copyright
125** notice, this list of conditions and the following disclaimer.
126**
127** 2 Redistributions in binary form must reproduce the above copyright
128** notice, this list of conditions and the following disclaimer in
129** the documentation and/or other materials provided with the
130** distribution.
131**
132** 3 Neither the name of the Standards Of Fundamental Astronomy Board,
133** the International Astronomical Union nor the names of its
134** contributors may be used to endorse or promote products derived
135** from this software without specific prior written permission.
136**
137** THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
138** "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
139** LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
140** FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
141** COPYRIGHT HOLDER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
142** INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
143** BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES;
144** LOSS OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER
145** CAUSED AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
146** LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
147** ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
148** POSSIBILITY OF SUCH DAMAGE.
149**
150*/
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