| 1 | /* | 
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| 2 | *+ | 
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| 3 | *  Name: | 
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| 4 | *     palAmpqk | 
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| 5 |  | 
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| 6 | *  Purpose: | 
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| 7 | *     Convert star RA,Dec from geocentric apparent to mean place. | 
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| 8 |  | 
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| 9 | *  Language: | 
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| 10 | *     Starlink ANSI C | 
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| 11 |  | 
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| 12 | *  Type of Module: | 
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| 13 | *     Library routine | 
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| 14 |  | 
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| 15 | *  Invocation: | 
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| 16 | *     void palAmpqk ( double ra, double da, double amprms[21], | 
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| 17 | *                     double *rm, double *dm ) | 
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| 18 |  | 
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| 19 | *  Arguments: | 
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| 20 | *     ra = double (Given) | 
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| 21 | *        Apparent RA (radians). | 
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| 22 | *     da = double (Given) | 
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| 23 | *        Apparent Dec (radians). | 
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| 24 | *     amprms = double[21] (Given) | 
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| 25 | *        Star-independent mean-to-apparent parameters (see palMappa): | 
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| 26 | *        (0)      time interval for proper motion (Julian years) | 
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| 27 | *        (1-3)    barycentric position of the Earth (AU) | 
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| 28 | *        (4-6)    not used | 
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| 29 | *        (7)      not used | 
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| 30 | *        (8-10)   abv: barycentric Earth velocity in units of c | 
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| 31 | *        (11)     sqrt(1-v*v) where v=modulus(abv) | 
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| 32 | *        (12-20)  precession/nutation (3,3) matrix | 
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| 33 | *     rm = double (Returned) | 
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| 34 | *        Mean RA (radians). | 
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| 35 | *     dm = double (Returned) | 
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| 36 | *        Mean Dec (radians). | 
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| 37 |  | 
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| 38 | *  Description: | 
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| 39 | *     Convert star RA,Dec from geocentric apparent to mean place. The "mean" | 
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| 40 | *     coordinate system is in fact close to ICRS. Use of this function | 
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| 41 | *     is appropriate when efficiency is important and where many star | 
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| 42 | *     positions are all to be transformed for one epoch and equinox.  The | 
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| 43 | *     star-independent parameters can be obtained by calling the palMappa | 
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| 44 | *     function. | 
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| 45 |  | 
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| 46 | *  Authors: | 
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| 47 | *     PTW: Pat Wallace (STFC) | 
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| 48 | *     {enter_new_authors_here} | 
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| 49 |  | 
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| 50 | *  History: | 
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| 51 | *     2012-02-13 (PTW): | 
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| 52 | *        Initial version. | 
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| 53 | *        Adapted with permission from the Fortran SLALIB library. | 
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| 54 | *     {enter_further_changes_here} | 
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| 55 |  | 
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| 56 | *  Copyright: | 
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| 57 | *     Copyright (C) 2000 Rutherford Appleton Laboratory | 
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| 58 | *     Copyright (C) 2012 Science and Technology Facilities Council. | 
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| 59 | *     All Rights Reserved. | 
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| 60 |  | 
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| 61 | *  Licence: | 
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| 62 | *     This program is free software: you can redistribute it and/or | 
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| 63 | *     modify it under the terms of the GNU Lesser General Public | 
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| 64 | *     License as published by the Free Software Foundation, either | 
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| 65 | *     version 3 of the License, or (at your option) any later | 
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| 66 | *     version. | 
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| 67 | * | 
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| 68 | *     This program is distributed in the hope that it will be useful, | 
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| 69 | *     but WITHOUT ANY WARRANTY; without even the implied warranty of | 
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| 70 | *     MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE.  See the | 
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| 71 | *     GNU Lesser General Public License for more details. | 
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| 72 | * | 
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| 73 | *     You should have received a copy of the GNU Lesser General | 
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| 74 | *     License along with this program.  If not, see | 
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| 75 | *     <http://www.gnu.org/licenses/>. | 
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| 76 |  | 
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| 77 | *  Bugs: | 
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| 78 | *     {note_any_bugs_here} | 
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| 79 | *- | 
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| 80 | */ | 
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| 81 |  | 
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| 82 | #include "pal.h" | 
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| 83 | #include "pal1sofa.h" | 
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| 84 |  | 
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| 85 | void palAmpqk ( double ra, double da, double amprms[21], double *rm, | 
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| 86 | double *dm ){ | 
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| 87 |  | 
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| 88 | /* Local Variables: */ | 
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| 89 | double ab1;                 /* sqrt(1-v*v) where v=modulus of Earth vel */ | 
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| 90 | double abv[3];              /* Earth velocity wrt SSB (c, FK5) */ | 
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| 91 | double p1[3], p2[3], p3[3]; /* work vectors */ | 
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| 92 | double ab1p1, p1dv, p1dvp1, w; | 
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| 93 | int i, j; | 
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| 94 |  | 
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| 95 | /* Unpack some of the parameters */ | 
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| 96 | ab1  = amprms[11]; | 
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| 97 | for( i = 0; i < 3; i++ ) { | 
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| 98 | abv[i] = amprms[i + 8]; | 
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| 99 | } | 
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| 100 |  | 
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| 101 | /* Apparent RA,Dec to Cartesian */ | 
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| 102 | eraS2c( ra, da, p3 ); | 
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| 103 |  | 
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| 104 | /* Precession and nutation */ | 
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| 105 | eraTrxp( (double(*)[3]) &rms[12], p3, p2 ); | 
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| 106 |  | 
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| 107 | /* Aberration */ | 
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| 108 | ab1p1 = ab1 + 1.0; | 
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| 109 | for( i = 0; i < 3; i++ ) { | 
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| 110 | p1[i] = p2[i]; | 
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| 111 | } | 
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| 112 | for( j = 0; j < 2; j++ ) { | 
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| 113 | p1dv = eraPdp( p1, abv ); | 
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| 114 | p1dvp1 = 1.0 + p1dv; | 
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| 115 | w = 1.0 + p1dv / ab1p1; | 
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| 116 | for( i = 0; i < 3; i++ ) { | 
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| 117 | p1[i] = ( p1dvp1 * p2[i] - w * abv[i] ) / ab1; | 
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| 118 | } | 
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| 119 | eraPn( p1, &w, p3 ); | 
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| 120 | for( i = 0; i < 3; i++ ) { | 
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| 121 | p1[i] = p3[i]; | 
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| 122 | } | 
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| 123 | } | 
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| 124 |  | 
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| 125 | /* Mean RA,Dec */ | 
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| 126 | eraC2s( p1, rm, dm ); | 
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| 127 | *rm = eraAnp( *rm ); | 
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| 128 | } | 
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