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author | Joe Hunkeler <jhunkeler@gmail.com> | 2015-08-11 16:51:37 -0400 |
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committer | Joe Hunkeler <jhunkeler@gmail.com> | 2015-08-11 16:51:37 -0400 |
commit | 40e5a5811c6ffce9b0974e93cdd927cbcf60c157 (patch) | |
tree | 4464880c571602d54f6ae114729bf62a89518057 /math/slalib/ampqk.f | |
download | iraf-osx-40e5a5811c6ffce9b0974e93cdd927cbcf60c157.tar.gz |
Repatch (from linux) of OSX IRAF
Diffstat (limited to 'math/slalib/ampqk.f')
-rw-r--r-- | math/slalib/ampqk.f | 140 |
1 files changed, 140 insertions, 0 deletions
diff --git a/math/slalib/ampqk.f b/math/slalib/ampqk.f new file mode 100644 index 00000000..4bf95b69 --- /dev/null +++ b/math/slalib/ampqk.f @@ -0,0 +1,140 @@ + SUBROUTINE slAMPQ (RA, DA, AMPRMS, RM, DM) +*+ +* - - - - - - +* A M P Q +* - - - - - - +* +* Convert star RA,Dec from geocentric apparent to mean place +* +* The mean coordinate system is the post IAU 1976 system, +* loosely called FK5. +* +* Use of this routine is appropriate when efficiency is important +* and where many star positions are all to be transformed for +* one epoch and equinox. The star-independent parameters can be +* obtained by calling the slMAPA routine. +* +* Given: +* RA d apparent RA (radians) +* DA d apparent Dec (radians) +* +* AMPRMS d(21) star-independent mean-to-apparent parameters: +* +* (1) time interval for proper motion (Julian years) +* (2-4) barycentric position of the Earth (AU) +* (5-7) heliocentric direction of the Earth (unit vector) +* (8) (grav rad Sun)*2/(Sun-Earth distance) +* (9-11) ABV: barycentric Earth velocity in units of c +* (12) sqrt(1-v**2) where v=modulus(ABV) +* (13-21) precession/nutation (3,3) matrix +* +* Returned: +* RM d mean RA (radians) +* DM d mean Dec (radians) +* +* References: +* 1984 Astronomical Almanac, pp B39-B41. +* (also Lederle & Schwan, Astron. Astrophys. 134, +* 1-6, 1984) +* +* Note: +* +* Iterative techniques are used for the aberration and +* light deflection corrections so that the routines +* slAMP (or slAMPQ) and slMAP (or slMAPQ) are +* accurate inverses; even at the edge of the Sun's disc +* the discrepancy is only about 1 nanoarcsecond. +* +* Called: slDS2C, slDIMV, slDVDV, slDVN, slDC2S, +* slDA2P +* +* P.T.Wallace Starlink 7 May 2000 +* +* Copyright (C) 2000 Rutherford Appleton Laboratory +* +* License: +* This program is free software; you can redistribute it and/or modify +* it under the terms of the GNU General Public License as published by +* the Free Software Foundation; either version 2 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 General Public License for more details. +* +* You should have received a copy of the GNU General Public License +* along with this program (see SLA_CONDITIONS); if not, write to the +* Free Software Foundation, Inc., 51 Franklin Street, Fifth Floor, +* Boston, MA 02110-1301 USA +* +* Copyright (C) 1995 Association of Universities for Research in Astronomy Inc. +*- + + IMPLICIT NONE + + DOUBLE PRECISION RA,DA,AMPRMS(21),RM,DM + + INTEGER I,J + + DOUBLE PRECISION GR2E,AB1,EHN(3),ABV(3),P3(3),P2(3), + : AB1P1,P1DV,P1DVP1,P1(3),W,PDE,PDEP1,P(3) + + DOUBLE PRECISION slDVDV,slDA2P + + + +* Unpack scalar and vector parameters + GR2E = AMPRMS(8) + AB1 = AMPRMS(12) + DO I=1,3 + EHN(I) = AMPRMS(I+4) + ABV(I) = AMPRMS(I+8) + END DO + +* Apparent RA,Dec to Cartesian + CALL slDS2C(RA,DA,P3) + +* Precession and nutation + CALL slDIMV(AMPRMS(13),P3,P2) + +* Aberration + AB1P1 = AB1+1D0 + DO I=1,3 + P1(I) = P2(I) + END DO + DO J=1,2 + P1DV = slDVDV(P1,ABV) + P1DVP1 = 1D0+P1DV + W = 1D0+P1DV/AB1P1 + DO I=1,3 + P1(I) = (P1DVP1*P2(I)-W*ABV(I))/AB1 + END DO + CALL slDVN(P1,P3,W) + DO I=1,3 + P1(I) = P3(I) + END DO + END DO + +* Light deflection + DO I=1,3 + P(I) = P1(I) + END DO + DO J=1,5 + PDE = slDVDV(P,EHN) + PDEP1 = 1D0+PDE + W = PDEP1-GR2E*PDE + DO I=1,3 + P(I) = (PDEP1*P1(I)-GR2E*EHN(I))/W + END DO + CALL slDVN(P,P2,W) + DO I=1,3 + P(I) = P2(I) + END DO + END DO + +* Mean RA,Dec + CALL slDC2S(P,RM,DM) + RM = slDA2P(RM) + + END |