source: trunk/FACT++/pal/palMapqkz.c@ 19966

Last change on this file since 19966 was 18712, checked in by tbretz, 8 years ago
Updated to PAL 0.9.7 (adds mainly light deflection to abberation which was previously missing)
File size: 4.8 KB
Line 
1/*
2*+
3* Name:
4* palMapqkz
5
6* Purpose:
7* Quick mean to apparent place (no proper motion or parallax).
8
9* Language:
10* Starlink ANSI C
11
12* Type of Module:
13* Library routine
14
15* Invocation:
16* void palMapqkz( double rm, double dm, double amprms[21],
17* double *ra, double *da )
18
19* Arguments:
20* rm = double (Given)
21* Mean RA (radians).
22* dm = double (Given)
23* Mean Dec (radians).
24* amprms = double[21] (Given)
25* Star-independent mean-to-apparent parameters (see palMappa):
26* (0-3) not used
27* (4-6) heliocentric direction of the Earth (unit vector)
28* (7) not used
29* (8-10) abv: barycentric Earth velocity in units of c
30* (11) sqrt(1-v^2) where v=modulus(abv)
31* (12-20) precession/nutation (3,3) matrix
32* ra = double * (Returned)
33* Apparent RA (radians).
34* da = double * (Returned)
35* Apparent Dec (radians).
36
37* Description:
38* Quick mean to apparent place: transform a star RA,dec from
39* mean place to geocentric apparent place, given the
40* star-independent parameters, and assuming zero parallax
41* and proper motion.
42*
43* Use of this function is appropriate when efficiency is important
44* and where many star positions, all with parallax and proper
45* motion either zero or already allowed for, and all referred to
46* the same equator and equinox, are to be transformed for one
47* epoch. The star-independent parameters can be obtained by
48* calling the palMappa function.
49*
50* The corresponding function for the case of non-zero parallax
51* and proper motion is palMapqk.
52
53* Notes:
54* - The reference systems and timescales used are IAU 2006.
55* - The mean place rm, dm and the vectors amprms[1-3] and amprms[4-6]
56* are referred to the mean equinox and equator of the epoch
57* specified when generating the precession/nutation matrix
58* amprms[12-20]. In the call to palMappa (q.v.) normally used
59* to populate amprms, this epoch is the first argument (eq).
60* - The vector amprms(4-6) is referred to the mean equinox and
61* equator of epoch eq.
62* - Strictly speaking, the routine is not valid for solar-system
63* sources, though the error will usually be extremely small.
64* However, to prevent gross errors in the case where the
65* position of the Sun is specified, the gravitational
66* deflection term is restrained within about 920 arcsec of the
67* centre of the Sun's disc. The term has a maximum value of
68* about 1.85 arcsec at this radius, and decreases to zero as
69* the centre of the disc is approached.
70
71* Authors:
72* PTW: Pat Wallace (STFC)
73* {enter_new_authors_here}
74
75* History:
76* 2012-02-13 (PTW):
77* Initial version.
78* Adapted with permission from the Fortran SLALIB library.
79* {enter_further_changes_here}
80
81* Copyright:
82* Copyright (C) 1999 Rutherford Appleton Laboratory
83* Copyright (C) 2012 Science and Technology Facilities Council.
84* All Rights Reserved.
85
86* Licence:
87* This program is free software: you can redistribute it and/or
88* modify it under the terms of the GNU Lesser General Public
89* License as published by the Free Software Foundation, either
90* version 3 of the License, or (at your option) any later
91* version.
92*
93* This program is distributed in the hope that it will be useful,
94* but WITHOUT ANY WARRANTY; without even the implied warranty of
95* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
96* GNU Lesser General Public License for more details.
97*
98* You should have received a copy of the GNU Lesser General
99* License along with this program. If not, see
100* <http://www.gnu.org/licenses/>.
101
102* Bugs:
103* {note_any_bugs_here}
104*-
105*/
106
107#include "pal.h"
108#include "pal1sofa.h"
109
110void palMapqkz ( double rm, double dm, double amprms[21], double *ra,
111 double *da ){
112
113/* Local Variables: */
114 int i;
115 double ab1, abv[3], p[3], w, p1dv, p2[3], p3[3];
116 double gr2e, pde, pdep1, ehn[3], p1[3];
117
118/* Unpack scalar and vector parameters. */
119 ab1 = amprms[11];
120 gr2e = amprms[7];
121 for( i = 0; i < 3; i++ ) {
122 abv[i] = amprms[i+8];
123 ehn[i] = amprms[i+4];
124 }
125
126/* Spherical to x,y,z. */
127 eraS2c( rm, dm, p );
128
129/* Light deflection (restrained within the Sun's disc) */
130 pde = eraPdp( p, ehn );
131 pdep1 = pde + 1.0;
132 w = gr2e / ( pdep1 > 1.0e-5 ? pdep1 : 1.0e-5 );
133 for( i = 0; i < 3; i++) {
134 p1[i] = p[i] + w * ( ehn[i] - pde * p[i] );
135 }
136
137/* Aberration. */
138 p1dv = eraPdp( p1, abv );
139 w = 1.0 + p1dv / ( ab1 + 1.0 );
140 for( i = 0; i < 3; i++ ) {
141 p2[i] = ( ( ab1 * p1[i] ) + ( w * abv[i] ) );
142 }
143
144/* Precession and nutation. */
145 eraRxp( (double(*)[3]) &amprms[12], p2, p3 );
146
147/* Geocentric apparent RA,dec. */
148 eraC2s( p3, ra, da );
149 *ra = eraAnp( *ra );
150}
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