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.help ecmat Jun99 "Slalib Package"
.nf
SUBROUTINE slECMA (DATE, RMAT)
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E C M A
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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.
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