File Coverage

erfasrc/src/pn06.c
Criterion Covered Total %
statement 0 15 0.0
branch n/a
condition n/a
subroutine n/a
pod n/a
total 0 15 0.0


line stmt bran cond sub pod time code
1             #include "erfa.h"
2              
3 0           void eraPn06(double date1, double date2, double dpsi, double deps,
4             double *epsa,
5             double rb[3][3], double rp[3][3], double rbp[3][3],
6             double rn[3][3], double rbpn[3][3])
7             /*
8             ** - - - - - - - -
9             ** e r a P n 0 6
10             ** - - - - - - - -
11             **
12             ** Precession-nutation, IAU 2006 model: a multi-purpose function,
13             ** supporting classical (equinox-based) use directly and CIO-based use
14             ** indirectly.
15             **
16             ** Given:
17             ** date1,date2 double TT as a 2-part Julian Date (Note 1)
18             ** dpsi,deps double nutation (Note 2)
19             **
20             ** Returned:
21             ** epsa double mean obliquity (Note 3)
22             ** rb double[3][3] frame bias matrix (Note 4)
23             ** rp double[3][3] precession matrix (Note 5)
24             ** rbp double[3][3] bias-precession matrix (Note 6)
25             ** rn double[3][3] nutation matrix (Note 7)
26             ** rbpn double[3][3] GCRS-to-true matrix (Note 8)
27             **
28             ** Notes:
29             **
30             ** 1) The TT date date1+date2 is a Julian Date, apportioned in any
31             ** convenient way between the two arguments. For example,
32             ** JD(TT)=2450123.7 could be expressed in any of these ways,
33             ** among others:
34             **
35             ** date1 date2
36             **
37             ** 2450123.7 0.0 (JD method)
38             ** 2451545.0 -1421.3 (J2000 method)
39             ** 2400000.5 50123.2 (MJD method)
40             ** 2450123.5 0.2 (date & time method)
41             **
42             ** The JD method is the most natural and convenient to use in
43             ** cases where the loss of several decimal digits of resolution
44             ** is acceptable. The J2000 method is best matched to the way
45             ** the argument is handled internally and will deliver the
46             ** optimum resolution. The MJD method and the date & time methods
47             ** are both good compromises between resolution and convenience.
48             **
49             ** 2) The caller is responsible for providing the nutation components;
50             ** they are in longitude and obliquity, in radians and are with
51             ** respect to the equinox and ecliptic of date. For high-accuracy
52             ** applications, free core nutation should be included as well as
53             ** any other relevant corrections to the position of the CIP.
54             **
55             ** 3) The returned mean obliquity is consistent with the IAU 2006
56             ** precession.
57             **
58             ** 4) The matrix rb transforms vectors from GCRS to J2000.0 mean
59             ** equator and equinox by applying frame bias.
60             **
61             ** 5) The matrix rp transforms vectors from J2000.0 mean equator and
62             ** equinox to mean equator and equinox of date by applying
63             ** precession.
64             **
65             ** 6) The matrix rbp transforms vectors from GCRS to mean equator and
66             ** equinox of date by applying frame bias then precession. It is
67             ** the product rp x rb.
68             **
69             ** 7) The matrix rn transforms vectors from mean equator and equinox
70             ** of date to true equator and equinox of date by applying the
71             ** nutation (luni-solar + planetary).
72             **
73             ** 8) The matrix rbpn transforms vectors from GCRS to true equator and
74             ** equinox of date. It is the product rn x rbp, applying frame
75             ** bias, precession and nutation in that order.
76             **
77             ** 9) The X,Y,Z coordinates of the Celestial Intermediate Pole are
78             ** elements (3,1-3) of the GCRS-to-true matrix, i.e. rbpn[2][0-2].
79             **
80             ** 10) It is permissible to re-use the same array in the returned
81             ** arguments. The arrays are filled in the stated order.
82             **
83             ** Called:
84             ** eraPfw06 bias-precession F-W angles, IAU 2006
85             ** eraFw2m F-W angles to r-matrix
86             ** eraCr copy r-matrix
87             ** eraTr transpose r-matrix
88             ** eraRxr product of two r-matrices
89             **
90             ** References:
91             **
92             ** Capitaine, N. & Wallace, P.T., 2006, Astron.Astrophys. 450, 855
93             **
94             ** Wallace, P.T. & Capitaine, N., 2006, Astron.Astrophys. 459, 981
95             **
96             ** Copyright (C) 2013-2019, NumFOCUS Foundation.
97             ** Derived, with permission, from the SOFA library. See notes at end of file.
98             */
99             {
100             double gamb, phib, psib, eps, r1[3][3], r2[3][3], rt[3][3];
101              
102              
103             /* Bias-precession Fukushima-Williams angles of J2000.0 = frame bias. */
104 0           eraPfw06(ERFA_DJM0, ERFA_DJM00, &gamb, &phib, &psib, &eps);
105              
106             /* B matrix. */
107 0           eraFw2m(gamb, phib, psib, eps, r1);
108 0           eraCr(r1, rb);
109              
110             /* Bias-precession Fukushima-Williams angles of date. */
111 0           eraPfw06(date1, date2, &gamb, &phib, &psib, &eps);
112              
113             /* Bias-precession matrix. */
114 0           eraFw2m(gamb, phib, psib, eps, r2);
115 0           eraCr(r2, rbp);
116              
117             /* Solve for precession matrix. */
118 0           eraTr(r1, rt);
119 0           eraRxr(r2, rt, rp);
120              
121             /* Equinox-based bias-precession-nutation matrix. */
122 0           eraFw2m(gamb, phib, psib + dpsi, eps + deps, r1);
123 0           eraCr(r1, rbpn);
124              
125             /* Solve for nutation matrix. */
126 0           eraTr(r2, rt);
127 0           eraRxr(r1, rt, rn);
128              
129             /* Obliquity, mean of date. */
130 0           *epsa = eps;
131              
132 0           return;
133              
134             }
135             /*----------------------------------------------------------------------
136             **
137             **
138             ** Copyright (C) 2013-2019, NumFOCUS Foundation.
139             ** All rights reserved.
140             **
141             ** This library is derived, with permission, from the International
142             ** Astronomical Union's "Standards of Fundamental Astronomy" library,
143             ** available from http://www.iausofa.org.
144             **
145             ** The ERFA version is intended to retain identical functionality to
146             ** the SOFA library, but made distinct through different function and
147             ** file names, as set out in the SOFA license conditions. The SOFA
148             ** original has a role as a reference standard for the IAU and IERS,
149             ** and consequently redistribution is permitted only in its unaltered
150             ** state. The ERFA version is not subject to this restriction and
151             ** therefore can be included in distributions which do not support the
152             ** concept of "read only" software.
153             **
154             ** Although the intent is to replicate the SOFA API (other than
155             ** replacement of prefix names) and results (with the exception of
156             ** bugs; any that are discovered will be fixed), SOFA is not
157             ** responsible for any errors found in this version of the library.
158             **
159             ** If you wish to acknowledge the SOFA heritage, please acknowledge
160             ** that you are using a library derived from SOFA, rather than SOFA
161             ** itself.
162             **
163             **
164             ** TERMS AND CONDITIONS
165             **
166             ** Redistribution and use in source and binary forms, with or without
167             ** modification, are permitted provided that the following conditions
168             ** are met:
169             **
170             ** 1 Redistributions of source code must retain the above copyright
171             ** notice, this list of conditions and the following disclaimer.
172             **
173             ** 2 Redistributions in binary form must reproduce the above copyright
174             ** notice, this list of conditions and the following disclaimer in
175             ** the documentation and/or other materials provided with the
176             ** distribution.
177             **
178             ** 3 Neither the name of the Standards Of Fundamental Astronomy Board,
179             ** the International Astronomical Union nor the names of its
180             ** contributors may be used to endorse or promote products derived
181             ** from this software without specific prior written permission.
182             **
183             ** THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
184             ** "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
185             ** LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
186             ** FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
187             ** COPYRIGHT HOLDER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
188             ** INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
189             ** BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES;
190             ** LOSS OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER
191             ** CAUSED AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
192             ** LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
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194             ** POSSIBILITY OF SUCH DAMAGE.
195             **
196             */