1 | /*
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2 | *+
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3 | * Name:
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4 | * palRvlsrk
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5 |
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6 | * Purpose:
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7 | * Velocity component in a given direction due to the Sun's motion
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8 | * with respect to an adopted kinematic Local Standard of Rest.
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9 |
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10 | * Language:
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11 | * Starlink ANSI C
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12 |
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13 | * Type of Module:
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14 | * Library routine
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15 |
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16 | * Invocation:
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17 | * double palRvlsrk( double r2000, double d2000 )
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18 |
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19 | * Arguments:
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20 | * r2000 = double (Given)
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21 | * J2000.0 mean RA (radians)
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22 | * d2000 = double (Given)
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23 | * J2000.0 mean Dec (radians)
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24 |
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25 | * Returned Value:
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26 | * Component of "standard" solar motion in direction R2000,D2000 (km/s).
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27 |
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28 | * Description:
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29 | * This function returns the velocity component in a given direction
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30 | * due to the Sun's motion with respect to an adopted kinematic
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31 | * Local Standard of Rest. The result is +ve when the Sun is receding
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32 | * from the given point on the sky.
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33 |
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34 | * Notes:
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35 | * - The Local Standard of Rest used here is one of several
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36 | * "kinematical" LSRs in common use. A kinematical LSR is the mean
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37 | * standard of rest of specified star catalogues or stellar
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38 | * populations. The Sun's motion with respect to a kinematical LSR
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39 | * is known as the "standard" solar motion.
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40 | * - There is another sort of LSR, the "dynamical" LSR, which is a
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41 | * point in the vicinity of the Sun which is in a circular orbit
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42 | * around the Galactic centre. The Sun's motion with respect to
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43 | * the dynamical LSR is called the "peculiar" solar motion. To
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44 | * obtain a radial velocity correction with respect to the
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45 | * dynamical LSR use the routine palRvlsrd.
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46 |
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47 | * Reference:
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48 | * - Delhaye (1965), in "Stars and Stellar Systems", vol 5, p73.
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49 |
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50 | * Authors:
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51 | * PTW: Pat Wallace (STFC)
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52 | * DSB: David Berry (JAC, Hawaii)
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53 | * {enter_new_authors_here}
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54 |
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55 | * History:
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56 | * 2012-02-16 (DSB):
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57 | * Initial version.
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58 | * Adapted with permission from the Fortran SLALIB library.
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59 | * {enter_further_changes_here}
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60 |
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61 | * Copyright:
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62 | * Copyright (C) 1995 Rutherford Appleton Laboratory
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63 | * Copyright (C) 2012 Science and Technology Facilities Council.
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64 | * All Rights Reserved.
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65 |
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66 | * Licence:
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67 | * This program is free software: you can redistribute it and/or
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68 | * modify it under the terms of the GNU Lesser General Public
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69 | * License as published by the Free Software Foundation, either
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70 | * version 3 of the License, or (at your option) any later
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71 | * version.
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72 | *
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73 | * This program is distributed in the hope that it will be useful,
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74 | * but WITHOUT ANY WARRANTY; without even the implied warranty of
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75 | * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
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76 | * GNU Lesser General Public License for more details.
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77 | *
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78 | * You should have received a copy of the GNU Lesser General
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79 | * License along with this program. If not, see
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80 | * <http://www.gnu.org/licenses/>.
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81 |
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82 | * Bugs:
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83 | * {note_any_bugs_here}
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84 | *-
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85 | */
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86 |
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87 | #include "pal.h"
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88 | #include "pal1sofa.h"
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89 |
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90 | double palRvlsrk( double r2000, double d2000 ){
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91 |
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92 | /* Local Variables: */
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93 | double vb[ 3 ];
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94 |
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95 | /*
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96 | * Standard solar motion (from Methods of Experimental Physics, ed Meeks,
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97 | * vol 12, part C, sec 6.1.5.2, p281):
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98 | *
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99 | * 20 km/s towards RA 18h Dec +30d (1900).
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100 | *
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101 | * The solar motion is expressed here in the form of a J2000.0
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102 | * equatorial Cartesian vector:
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103 | *
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104 | * VA(1) = X = -SPEED*COS(RA)*COS(DEC)
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105 | * VA(2) = Y = -SPEED*SIN(RA)*COS(DEC)
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106 | * VA(3) = Z = -SPEED*SIN(DEC)
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107 | */
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108 |
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109 | double va[ 3 ] = { -0.29000, +17.31726, -10.00141 };
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110 |
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111 | /* Convert given J2000 RA,Dec to x,y,z. */
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112 | eraS2c( r2000, d2000, vb );
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113 |
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114 | /* Compute dot product with Solar motion vector. */
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115 | return eraPdp( va, vb );
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116 | }
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