/* *+ * Name: * palRvlg * Purpose: * Velocity component in a given direction due to Galactic rotation * and motion of the local group. * Language: * Starlink ANSI C * Type of Module: * Library routine * Invocation: * double palRvlg( double r2000, double d2000 ) * Arguments: * r2000 = double (Given) * J2000.0 mean RA (radians) * d2000 = double (Given) * J2000.0 mean Dec (radians) * Returned Value: * Component of SOLAR motion in direction R2000,D2000 (km/s). * Description: * This function returns the velocity component in a given * direction due to the combination of the rotation of the * Galaxy and the motion of the Galaxy relative to the mean * motion of the local group. The result is +ve when the Sun * is receding from the given point on the sky. * * Reference: * - IAU Trans 1976, 168, p201. * Authors: * PTW: Pat Wallace (STFC) * DSB: David Berry (JAC, Hawaii) * {enter_new_authors_here} * History: * 2012-02-16 (DSB): * Initial version. * Adapted with permission from the Fortran SLALIB library. * {enter_further_changes_here} * Copyright: * Copyright (C) 1995 Rutherford Appleton Laboratory * Copyright (C) 2012 Science and Technology Facilities Council. * All Rights Reserved. * Licence: * This program is free software: you can redistribute it and/or * modify it under the terms of the GNU Lesser General Public * License as published by the Free Software Foundation, either * version 3 of the License, or (at your option) any later * version. * * This program is distributed in the hope that it will be useful, * but WITHOUT ANY WARRANTY; without even the implied warranty of * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the * GNU Lesser General Public License for more details. * * You should have received a copy of the GNU Lesser General * License along with this program. If not, see * . * Bugs: * {note_any_bugs_here} *- */ #include "pal.h" #include "pal1sofa.h" double palRvlg( double r2000, double d2000 ){ /* Local Variables: */ double vb[ 3 ]; /* * * Solar velocity due to Galactic rotation and translation * * Speed = 300 km/s * * Apex = L2,B2 90deg, 0deg * = RA,Dec 21 12 01.1 +48 19 47 J2000.0 * * This is expressed in the form of a J2000.0 x,y,z vector: * * VA(1) = X = -SPEED*COS(RA)*COS(DEC) * VA(2) = Y = -SPEED*SIN(RA)*COS(DEC) * VA(3) = Z = -SPEED*SIN(DEC) */ double va[ 3 ] = { -148.23284, +133.44888, -224.09467 }; /* Convert given J2000 RA,Dec to x,y,z. */ eraS2c( r2000, d2000, vb ); /* Compute dot product with Solar motion vector. */ return eraPdp( va, vb ); }