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slalib/pm.f
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97
slalib/pm.f
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SUBROUTINE sla_PM (R0, D0, PR, PD, PX, RV, EP0, EP1, R1, D1)
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*+
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* - - -
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* P M
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* - - -
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*
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* Apply corrections for proper motion to a star RA,Dec
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* (double precision)
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*
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* References:
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* 1984 Astronomical Almanac, pp B39-B41.
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* (also Lederle & Schwan, Astron. Astrophys. 134,
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* 1-6, 1984)
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*
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* Given:
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* R0,D0 dp RA,Dec at epoch EP0 (rad)
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* PR,PD dp proper motions: RA,Dec changes per year of epoch
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* PX dp parallax (arcsec)
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* RV dp radial velocity (km/sec, +ve if receding)
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* EP0 dp start epoch in years (e.g. Julian epoch)
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* EP1 dp end epoch in years (same system as EP0)
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*
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* Returned:
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* R1,D1 dp RA,Dec at epoch EP1 (rad)
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*
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* Called:
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* sla_DCS2C spherical to Cartesian
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* sla_DCC2S Cartesian to spherical
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* sla_DRANRM normalize angle 0-2Pi
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*
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* Notes:
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*
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* 1 The proper motions in RA are dRA/dt rather than cos(Dec)*dRA/dt,
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* and are in the same coordinate system as R0,D0.
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*
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* 2 If the available proper motions are pre-FK5 they will be per
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* tropical year rather than per Julian year, and so the epochs
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* must both be Besselian rather than Julian. In such cases, a
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* scaling factor of 365.2422D0/365.25D0 should be applied to the
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* radial velocity before use.
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*
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* P.T.Wallace Starlink 19 January 2000
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*
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* Copyright (C) 2000 Rutherford Appleton Laboratory
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*
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* License:
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* This program is free software; you can redistribute it and/or modify
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* it under the terms of the GNU General Public License as published by
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* the Free Software Foundation; either version 2 of the License, or
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* (at your option) any later version.
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*
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* This program is distributed in the hope that it will be useful,
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* but WITHOUT ANY WARRANTY; without even the implied warranty of
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* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
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* GNU General Public License for more details.
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*
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* You should have received a copy of the GNU General Public License
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* along with this program (see SLA_CONDITIONS); if not, write to the
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* Free Software Foundation, Inc., 59 Temple Place, Suite 330,
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* Boston, MA 02111-1307 USA
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*
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*-
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IMPLICIT NONE
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DOUBLE PRECISION R0,D0,PR,PD,PX,RV,EP0,EP1,R1,D1
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* Km/s to AU/year multiplied by arcseconds to radians
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DOUBLE PRECISION VFR
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PARAMETER (VFR=(365.25D0*86400D0/149597870D0)*4.8481368111D-6)
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INTEGER I
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DOUBLE PRECISION sla_DRANRM
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DOUBLE PRECISION W,EM(3),T,P(3)
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* Spherical to Cartesian
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CALL sla_DCS2C(R0,D0,P)
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* Space motion (radians per year)
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W=VFR*RV*PX
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EM(1)=-PR*P(2)-PD*COS(R0)*SIN(D0)+W*P(1)
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EM(2)= PR*P(1)-PD*SIN(R0)*SIN(D0)+W*P(2)
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EM(3)= PD*COS(D0) +W*P(3)
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* Apply the motion
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T=EP1-EP0
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DO I=1,3
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P(I)=P(I)+T*EM(I)
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END DO
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* Cartesian to spherical
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CALL sla_DCC2S(P,R1,D1)
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R1=sla_DRANRM(R1)
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END
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