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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/nut.f | |
download | iraf-osx-40e5a5811c6ffce9b0974e93cdd927cbcf60c157.tar.gz |
Repatch (from linux) of OSX IRAF
Diffstat (limited to 'math/slalib/nut.f')
-rw-r--r-- | math/slalib/nut.f | 76 |
1 files changed, 76 insertions, 0 deletions
diff --git a/math/slalib/nut.f b/math/slalib/nut.f new file mode 100644 index 00000000..b3cbf192 --- /dev/null +++ b/math/slalib/nut.f @@ -0,0 +1,76 @@ + SUBROUTINE slNUT (DATE, RMATN) +*+ +* - - - - +* N U T +* - - - - +* +* Form the matrix of nutation for a given date - Shirai & Fukushima +* 2001 theory (double precision) +* +* Reference: +* Shirai, T. & Fukushima, T., Astron.J. 121, 3270-3283 (2001). +* +* Given: +* DATE d TDB (loosely ET) as Modified Julian Date +* (=JD-2400000.5) +* Returned: +* RMATN d(3,3) nutation matrix +* +* Notes: +* +* 1 The matrix is in the sense v(true) = rmatn * v(mean) . +* where v(true) is the star vector relative to the true equator and +* equinox of date and v(mean) is the star vector relative to the +* mean equator and equinox of date. +* +* 2 The matrix represents forced nutation (but not free core +* nutation) plus corrections to the IAU~1976 precession model. +* +* 3 Earth attitude predictions made by combining the present nutation +* matrix with IAU~1976 precession are accurate to 1~mas (with +* respect to the ICRS) for a few decades around 2000. +* +* 4 The distinction between the required TDB and TT is always +* negligible. Moreover, for all but the most critical applications +* UTC is adequate. +* +* Called: slNUTC, slDEUL +* +* Last revision: 1 December 2005 +* +* Copyright P.T.Wallace. All rights reserved. +* +* 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 DATE,RMATN(3,3) + + DOUBLE PRECISION DPSI,DEPS,EPS0 + + + +* Nutation components and mean obliquity + CALL slNUTC(DATE,DPSI,DEPS,EPS0) + +* Rotation matrix + CALL slDEUL('XZX',EPS0,-DPSI,-(EPS0+DEPS),RMATN) + + END |