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SLA_ECMAT - Form $\alpha,\delta\rightarrow\lambda,\beta$ Matrix

ACTION:
Form the equatorial to ecliptic rotation matrix (IAU 1980 theory).
CALL:
CALL sla_ECMAT (DATE, RMAT)
GIVEN:

DATE D TDB (formerly ET) as Modified Julian Date (JD$-$2400000.5)
RETURNED:

RMAT D(3,3) rotation matrix
NOTES:
  1. RMAT is matrix M in the expression v$_{ecl}$ = M$\cdot$v$_{equ}$.
  2. The equator, equinox and ecliptic are mean of date.
REFERENCE:
Murray, C.A., Vectorial Astrometry, section 4.3.


next up previous 269
Next: SLA_ECOR - RV & Time Corrns to Sun
Up: SUBPROGRAM SPECIFICATIONS
Previous: SLA_ECLEQ - Ecliptic to Equatorial

SLALIB --- Positional Astronomy Library
Starlink User Note 67
P. T. Wallace
19 December 2005
E-mail:ussc@star.rl.ac.uk

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