| 1 | /*
|
|---|
| 2 | *+
|
|---|
| 3 | * Name:
|
|---|
| 4 | * palRdplan
|
|---|
| 5 |
|
|---|
| 6 | * Purpose:
|
|---|
| 7 | * Approximate topocentric apparent RA,Dec of a planet
|
|---|
| 8 |
|
|---|
| 9 | * Language:
|
|---|
| 10 | * Starlink ANSI C
|
|---|
| 11 |
|
|---|
| 12 | * Type of Module:
|
|---|
| 13 | * Library routine
|
|---|
| 14 |
|
|---|
| 15 | * Invocation:
|
|---|
| 16 | * void palRdplan( double date, int np, double elong, double phi,
|
|---|
| 17 | * double * ra, double * dec, double * diam );
|
|---|
| 18 |
|
|---|
| 19 | * Arguments:
|
|---|
| 20 | * date = double (Given)
|
|---|
| 21 | * MJD of observation (JD-2400000.5) in TDB. For all practical
|
|---|
| 22 | * purposes TT can be used instead of TDB, and for many applications
|
|---|
| 23 | * UT will do (except for the Moon).
|
|---|
| 24 | * np = int (Given)
|
|---|
| 25 | * Planet: 1 = Mercury
|
|---|
| 26 | * 2 = Venus
|
|---|
| 27 | * 3 = Moon
|
|---|
| 28 | * 4 = Mars
|
|---|
| 29 | * 5 = Jupiter
|
|---|
| 30 | * 6 = Saturn
|
|---|
| 31 | * 7 = Uranus
|
|---|
| 32 | * 8 = Neptune
|
|---|
| 33 | * else = Sun
|
|---|
| 34 | * elong = double (Given)
|
|---|
| 35 | * Observer's east longitude (radians)
|
|---|
| 36 | * phi = double (Given)
|
|---|
| 37 | * Observer's geodetic latitude (radians)
|
|---|
| 38 | * ra = double * (Returned)
|
|---|
| 39 | * RA (topocentric apparent, radians)
|
|---|
| 40 | * dec = double * (Returned)
|
|---|
| 41 | * Dec (topocentric apparent, radians)
|
|---|
| 42 | * diam = double * (Returned)
|
|---|
| 43 | * Angular diameter (equatorial, radians)
|
|---|
| 44 |
|
|---|
| 45 | * Description:
|
|---|
| 46 | * Approximate topocentric apparent RA,Dec of a planet, and its
|
|---|
| 47 | * angular diameter.
|
|---|
| 48 |
|
|---|
| 49 | * Authors:
|
|---|
| 50 | * PTW: Patrick T. Wallace
|
|---|
| 51 | * TIMJ: Tim Jenness (JAC, Hawaii)
|
|---|
| 52 | * {enter_new_authors_here}
|
|---|
| 53 |
|
|---|
| 54 | * Notes:
|
|---|
| 55 | * - Unlike with slaRdplan, Pluto is not supported.
|
|---|
| 56 | * - The longitude and latitude allow correction for geocentric
|
|---|
| 57 | * parallax. This is a major effect for the Moon, but in the
|
|---|
| 58 | * context of the limited accuracy of the present routine its
|
|---|
| 59 | * effect on planetary positions is small (negligible for the
|
|---|
| 60 | * outer planets). Geocentric positions can be generated by
|
|---|
| 61 | * appropriate use of the routines palDmoon and eraPlan94.
|
|---|
| 62 |
|
|---|
| 63 | * History:
|
|---|
| 64 | * 2012-03-07 (TIMJ):
|
|---|
| 65 | * Initial version, with some documentation from SLA/F.
|
|---|
| 66 | * Adapted with permission from the Fortran SLALIB library.
|
|---|
| 67 | * {enter_further_changes_here}
|
|---|
| 68 |
|
|---|
| 69 | * Copyright:
|
|---|
| 70 | * Copyright (C) 1997 Rutherford Appleton Laboratory
|
|---|
| 71 | * Copyright (C) 2012 Science and Technology Facilities Council.
|
|---|
| 72 | * All Rights Reserved.
|
|---|
| 73 |
|
|---|
| 74 | * Licence:
|
|---|
| 75 | * This program is free software; you can redistribute it and/or
|
|---|
| 76 | * modify it under the terms of the GNU General Public License as
|
|---|
| 77 | * published by the Free Software Foundation; either version 3 of
|
|---|
| 78 | * the License, or (at your option) any later version.
|
|---|
| 79 | *
|
|---|
| 80 | * This program is distributed in the hope that it will be
|
|---|
| 81 | * useful, but WITHOUT ANY WARRANTY; without even the implied
|
|---|
| 82 | * warranty of MERCHANTABILITY or FITNESS FOR A PARTICULAR
|
|---|
| 83 | * PURPOSE. See the GNU General Public License for more details.
|
|---|
| 84 | *
|
|---|
| 85 | * You should have received a copy of the GNU General Public License
|
|---|
| 86 | * along with this program; if not, write to the Free Software
|
|---|
| 87 | * Foundation, Inc., 51 Franklin Street, Fifth Floor, Boston,
|
|---|
| 88 | * MA 02110-1301, USA.
|
|---|
| 89 |
|
|---|
| 90 | * Bugs:
|
|---|
| 91 | * {note_any_bugs_here}
|
|---|
| 92 | *-
|
|---|
| 93 | */
|
|---|
| 94 |
|
|---|
| 95 | #include <math.h>
|
|---|
| 96 |
|
|---|
| 97 | #include "pal.h"
|
|---|
| 98 | #include "palmac.h"
|
|---|
| 99 | #include "pal1sofa.h"
|
|---|
| 100 |
|
|---|
| 101 | void palRdplan( double date, int np, double elong, double phi,
|
|---|
| 102 | double * ra, double * dec, double * diam ) {
|
|---|
| 103 |
|
|---|
| 104 | /* AU in km */
|
|---|
| 105 | const double AUKM = 1.49597870e8;
|
|---|
| 106 |
|
|---|
| 107 | /* Equatorial radii (km) */
|
|---|
| 108 | const double EQRAU[] = {
|
|---|
| 109 | 696000.0, /* Sun */
|
|---|
| 110 | 2439.7,
|
|---|
| 111 | 6051.9,
|
|---|
| 112 | 1738,
|
|---|
| 113 | 3397,
|
|---|
| 114 | 71492,
|
|---|
| 115 | 60268,
|
|---|
| 116 | 25559,
|
|---|
| 117 | 24764
|
|---|
| 118 | };
|
|---|
| 119 |
|
|---|
| 120 | /* Local variables */
|
|---|
| 121 | int i, j;
|
|---|
| 122 | double stl;
|
|---|
| 123 | double vgm[6];
|
|---|
| 124 | double v[6];
|
|---|
| 125 | double rmat[3][3];
|
|---|
| 126 | double vse[6];
|
|---|
| 127 | double vsg[6];
|
|---|
| 128 | double vsp[6];
|
|---|
| 129 | double vgo[6];
|
|---|
| 130 | double dx,dy,dz,r,tl;
|
|---|
| 131 |
|
|---|
| 132 | /* Classify np */
|
|---|
| 133 | if (np < 0 || np > 8 ) np=0; /* Sun */
|
|---|
| 134 |
|
|---|
| 135 | /* Approximate local sidereal time */
|
|---|
| 136 | stl = palGmst( date - palDt( palEpj(date)) / 86400.0) + elong;
|
|---|
| 137 |
|
|---|
| 138 | /* Geocentre to Moon (mean of date) */
|
|---|
| 139 | palDmoon( date, v );
|
|---|
| 140 |
|
|---|
| 141 | /* Nutation to true of date */
|
|---|
| 142 | palNut( date, rmat );
|
|---|
| 143 | eraRxp( rmat, v, vgm );
|
|---|
| 144 | eraRxp( rmat, &(v[3]), &(vgm[3]) );
|
|---|
| 145 |
|
|---|
| 146 | /* Moon? */
|
|---|
| 147 | if (np == 3) {
|
|---|
| 148 |
|
|---|
| 149 | /* geocentre to Moon (true of date) */
|
|---|
| 150 | for (i=0; i<6; i++) {
|
|---|
| 151 | v[i] = vgm[i];
|
|---|
| 152 | }
|
|---|
| 153 |
|
|---|
| 154 | } else {
|
|---|
| 155 |
|
|---|
| 156 | /* Not moon: precession/nutation matrix J2000 to date */
|
|---|
| 157 | palPrenut( 2000.0, date, rmat );
|
|---|
| 158 |
|
|---|
| 159 | /* Sun to Earth-Moon Barycentre (J2000) */
|
|---|
| 160 | palPlanet( date, 3, v, &j );
|
|---|
| 161 |
|
|---|
| 162 | /* Precession and nutation to date */
|
|---|
| 163 | eraRxp( rmat, v, vse );
|
|---|
| 164 | eraRxp( rmat, &(v[3]), &(vse[3]) );
|
|---|
| 165 |
|
|---|
| 166 | /* Sun to geocentre (true of date) */
|
|---|
| 167 | for (i=0; i<6; i++) {
|
|---|
| 168 | vsg[i] = vse[i] - 0.012150581 * vgm[i];
|
|---|
| 169 | }
|
|---|
| 170 |
|
|---|
| 171 | /* Sun ? */
|
|---|
| 172 | if (np == 0) {
|
|---|
| 173 |
|
|---|
| 174 | /* Geocentre to Sun */
|
|---|
| 175 | for (i=0; i<6; i++) {
|
|---|
| 176 | v[i] = -vsg[i];
|
|---|
| 177 | }
|
|---|
| 178 |
|
|---|
| 179 | } else {
|
|---|
| 180 |
|
|---|
| 181 | /* Sun to Planet (J2000) */
|
|---|
| 182 | palPlanet( date, np, v, &j );
|
|---|
| 183 |
|
|---|
| 184 | /* Precession and nutation to date */
|
|---|
| 185 | eraRxp( rmat, v, vsp );
|
|---|
| 186 | eraRxp( rmat, &(v[3]), &(vsp[3]) );
|
|---|
| 187 |
|
|---|
| 188 | /* Geocentre to planet */
|
|---|
| 189 | for (i=0; i<6; i++) {
|
|---|
| 190 | v[i] = vsp[i] - vsg[i];
|
|---|
| 191 | }
|
|---|
| 192 |
|
|---|
| 193 | }
|
|---|
| 194 |
|
|---|
| 195 | }
|
|---|
| 196 |
|
|---|
| 197 | /* Refer to origina at the observer */
|
|---|
| 198 | palPvobs( phi, 0.0, stl, vgo );
|
|---|
| 199 | for (i=0; i<6; i++) {
|
|---|
| 200 | v[i] -= vgo[i];
|
|---|
| 201 | }
|
|---|
| 202 |
|
|---|
| 203 | /* Geometric distance (AU) */
|
|---|
| 204 | dx = v[0];
|
|---|
| 205 | dy = v[1];
|
|---|
| 206 | dz = v[2];
|
|---|
| 207 | r = sqrt( dx*dx + dy*dy + dz*dz );
|
|---|
| 208 |
|
|---|
| 209 | /* Light time */
|
|---|
| 210 | tl = PAL__CR * r;
|
|---|
| 211 |
|
|---|
| 212 | /* Correct position for planetary aberration */
|
|---|
| 213 | for (i=0; i<3; i++) {
|
|---|
| 214 | v[i] -= tl * v[i+3];
|
|---|
| 215 | }
|
|---|
| 216 |
|
|---|
| 217 | /* To RA,Dec */
|
|---|
| 218 | eraC2s( v, ra, dec );
|
|---|
| 219 | *ra = eraAnp( *ra );
|
|---|
| 220 |
|
|---|
| 221 | /* Angular diameter (radians) */
|
|---|
| 222 | *diam = 2.0 * asin( EQRAU[np] / (r * AUKM ) );
|
|---|
| 223 |
|
|---|
| 224 | }
|
|---|