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authorJoseph Hunkeler <jhunkeler@gmail.com>2015-07-08 20:46:52 -0400
committerJoseph Hunkeler <jhunkeler@gmail.com>2015-07-08 20:46:52 -0400
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+.help ecmat Jun99 "Slalib Package"
+.nf
+
+ SUBROUTINE slECMA (DATE, RMAT)
+
+ - - - - - -
+ E C M A
+ - - - - - -
+
+ Form the equatorial to ecliptic rotation matrix - IAU 1980 theory
+ (double precision)
+
+ Given:
+ DATE dp TDB (loosely ET) as Modified Julian Date
+ (JD-2400000.5)
+ Returned:
+ RMAT dp(3,3) matrix
+
+ Reference:
+ Murray,C.A., Vectorial Astrometry, section 4.3.
+
+ Note:
+ The matrix is in the sense V(ecl) = RMAT * V(equ); the
+ equator, equinox and ecliptic are mean of date.
+
+ Called: slDEUL
+
+ P.T.Wallace Starlink 23 August 1996
+
+ Copyright (C) 1996 Rutherford Appleton Laboratory
+ Copyright (C) 1995 Association of Universities for Research in Astronomy Inc.
+
+.fi
+.endhelp