/*
*+
* 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 );
}