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| 1 |  |  |  |  |  |  | /* | 
| 2 |  |  |  |  |  |  | *+ | 
| 3 |  |  |  |  |  |  | *  Name: | 
| 4 |  |  |  |  |  |  | *     palRvlsrd | 
| 5 |  |  |  |  |  |  |  | 
| 6 |  |  |  |  |  |  | *  Purpose: | 
| 7 |  |  |  |  |  |  | *     Velocity component in a given direction due to the Sun's motion | 
| 8 |  |  |  |  |  |  | *     with respect to the dynamical Local Standard of Rest. | 
| 9 |  |  |  |  |  |  |  | 
| 10 |  |  |  |  |  |  | *  Language: | 
| 11 |  |  |  |  |  |  | *     Starlink ANSI C | 
| 12 |  |  |  |  |  |  |  | 
| 13 |  |  |  |  |  |  | *  Type of Module: | 
| 14 |  |  |  |  |  |  | *     Library routine | 
| 15 |  |  |  |  |  |  |  | 
| 16 |  |  |  |  |  |  | *  Invocation: | 
| 17 |  |  |  |  |  |  | *     double palRvlsrd( double r2000, double d2000 ) | 
| 18 |  |  |  |  |  |  |  | 
| 19 |  |  |  |  |  |  | *  Arguments: | 
| 20 |  |  |  |  |  |  | *     r2000 = double (Given) | 
| 21 |  |  |  |  |  |  | *        J2000.0 mean RA (radians) | 
| 22 |  |  |  |  |  |  | *     d2000 = double (Given) | 
| 23 |  |  |  |  |  |  | *        J2000.0 mean Dec (radians) | 
| 24 |  |  |  |  |  |  |  | 
| 25 |  |  |  |  |  |  | *  Returned Value: | 
| 26 |  |  |  |  |  |  | *     Component of "peculiar" solar motion in direction R2000,D2000 (km/s). | 
| 27 |  |  |  |  |  |  |  | 
| 28 |  |  |  |  |  |  | *  Description: | 
| 29 |  |  |  |  |  |  | *     This function returns the velocity component in a given direction | 
| 30 |  |  |  |  |  |  | *     due to the Sun's motion with respect to the dynamical Local Standard | 
| 31 |  |  |  |  |  |  | *     of Rest. The result is +ve when the Sun is receding from the given | 
| 32 |  |  |  |  |  |  | *     point on the sky. | 
| 33 |  |  |  |  |  |  |  | 
| 34 |  |  |  |  |  |  | *  Notes: | 
| 35 |  |  |  |  |  |  | *     - The Local Standard of Rest used here is the "dynamical" LSR, | 
| 36 |  |  |  |  |  |  | *     a point in the vicinity of the Sun which is in a circular orbit | 
| 37 |  |  |  |  |  |  | *     around the Galactic centre.  The Sun's motion with respect to the | 
| 38 |  |  |  |  |  |  | *     dynamical LSR is called the "peculiar" solar motion. | 
| 39 |  |  |  |  |  |  | *     - There is another type of LSR, called a "kinematical" LSR.  A | 
| 40 |  |  |  |  |  |  | *     kinematical LSR is the mean standard of rest of specified star | 
| 41 |  |  |  |  |  |  | *     catalogues or stellar populations, and several slightly different | 
| 42 |  |  |  |  |  |  | *     kinematical LSRs are in use.  The Sun's motion with respect to an | 
| 43 |  |  |  |  |  |  | *     agreed kinematical LSR is known as the "standard" solar motion. | 
| 44 |  |  |  |  |  |  | *     To obtain a radial velocity correction with respect to an adopted | 
| 45 |  |  |  |  |  |  | *     kinematical LSR use the routine palRvlsrk. | 
| 46 |  |  |  |  |  |  |  | 
| 47 |  |  |  |  |  |  | *  Reference: | 
| 48 |  |  |  |  |  |  | *     - Delhaye (1965), in "Stars and Stellar Systems", vol 5, p73. | 
| 49 |  |  |  |  |  |  |  | 
| 50 |  |  |  |  |  |  | *  Authors: | 
| 51 |  |  |  |  |  |  | *     PTW: Pat Wallace (STFC) | 
| 52 |  |  |  |  |  |  | *     DSB: David Berry (JAC, Hawaii) | 
| 53 |  |  |  |  |  |  | *     {enter_new_authors_here} | 
| 54 |  |  |  |  |  |  |  | 
| 55 |  |  |  |  |  |  | *  History: | 
| 56 |  |  |  |  |  |  | *     2012-02-16 (DSB): | 
| 57 |  |  |  |  |  |  | *        Initial version. | 
| 58 |  |  |  |  |  |  | *        Adapted with permission from the Fortran SLALIB library. | 
| 59 |  |  |  |  |  |  | *     {enter_further_changes_here} | 
| 60 |  |  |  |  |  |  |  | 
| 61 |  |  |  |  |  |  | *  Copyright: | 
| 62 |  |  |  |  |  |  | *     Copyright (C) 1995 Rutherford Appleton Laboratory | 
| 63 |  |  |  |  |  |  | *     Copyright (C) 2012 Science and Technology Facilities Council. | 
| 64 |  |  |  |  |  |  | *     All Rights Reserved. | 
| 65 |  |  |  |  |  |  |  | 
| 66 |  |  |  |  |  |  | *  Licence: | 
| 67 |  |  |  |  |  |  | *     This program is free software: you can redistribute it and/or | 
| 68 |  |  |  |  |  |  | *     modify it under the terms of the GNU Lesser General Public | 
| 69 |  |  |  |  |  |  | *     License as published by the Free Software Foundation, either | 
| 70 |  |  |  |  |  |  | *     version 3 of the License, or (at your option) any later | 
| 71 |  |  |  |  |  |  | *     version. | 
| 72 |  |  |  |  |  |  | * | 
| 73 |  |  |  |  |  |  | *     This program is distributed in the hope that it will be useful, | 
| 74 |  |  |  |  |  |  | *     but WITHOUT ANY WARRANTY; without even the implied warranty of | 
| 75 |  |  |  |  |  |  | *     MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE.  See the | 
| 76 |  |  |  |  |  |  | *     GNU Lesser General Public License for more details. | 
| 77 |  |  |  |  |  |  | * | 
| 78 |  |  |  |  |  |  | *     You should have received a copy of the GNU Lesser General | 
| 79 |  |  |  |  |  |  | *     License along with this program.  If not, see | 
| 80 |  |  |  |  |  |  | *     . | 
| 81 |  |  |  |  |  |  |  | 
| 82 |  |  |  |  |  |  | *  Bugs: | 
| 83 |  |  |  |  |  |  | *     {note_any_bugs_here} | 
| 84 |  |  |  |  |  |  | *- | 
| 85 |  |  |  |  |  |  | */ | 
| 86 |  |  |  |  |  |  |  | 
| 87 |  |  |  |  |  |  | #include "pal.h" | 
| 88 |  |  |  |  |  |  | #include "pal1sofa.h" | 
| 89 |  |  |  |  |  |  |  | 
| 90 | 0 |  |  |  |  |  | double palRvlsrd( double r2000, double d2000 ){ | 
| 91 |  |  |  |  |  |  |  | 
| 92 |  |  |  |  |  |  | /* Local Variables: */ | 
| 93 |  |  |  |  |  |  | double vb[ 3 ]; | 
| 94 |  |  |  |  |  |  |  | 
| 95 |  |  |  |  |  |  | /* | 
| 96 |  |  |  |  |  |  | *  Peculiar solar motion from Delhaye 1965: in Galactic Cartesian | 
| 97 |  |  |  |  |  |  | *  coordinates (+9,+12,+7) km/s.  This corresponds to about 16.6 km/s | 
| 98 |  |  |  |  |  |  | *  towards Galactic coordinates L2 = 53 deg, B2 = +25 deg, or RA,Dec | 
| 99 |  |  |  |  |  |  | *  17 49 58.7 +28 07 04 J2000. | 
| 100 |  |  |  |  |  |  | * | 
| 101 |  |  |  |  |  |  | *  The solar motion is expressed here in the form of a J2000.0 | 
| 102 |  |  |  |  |  |  | *  equatorial Cartesian vector: | 
| 103 |  |  |  |  |  |  | * | 
| 104 |  |  |  |  |  |  | *      VA(1) = X = -SPEED*COS(RA)*COS(DEC) | 
| 105 |  |  |  |  |  |  | *      VA(2) = Y = -SPEED*SIN(RA)*COS(DEC) | 
| 106 |  |  |  |  |  |  | *      VA(3) = Z = -SPEED*SIN(DEC) | 
| 107 |  |  |  |  |  |  | */ | 
| 108 |  |  |  |  |  |  |  | 
| 109 | 0 |  |  |  |  |  | double va[ 3 ] = { +0.63823, +14.58542, -7.80116 }; | 
| 110 |  |  |  |  |  |  |  | 
| 111 |  |  |  |  |  |  | /* Convert given J2000 RA,Dec to x,y,z. */ | 
| 112 | 0 |  |  |  |  |  | eraS2c( r2000, d2000, vb ); | 
| 113 |  |  |  |  |  |  |  | 
| 114 |  |  |  |  |  |  | /* Compute dot product with Solar motion vector. */ | 
| 115 | 0 |  |  |  |  |  | return eraPdp( va, vb ); | 
| 116 |  |  |  |  |  |  | } |