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SLA_PRENUT - Precession-Nutation Matrix

ACTION:
Form the matrix of precession and nutation (SF2001).
CALL:
CALL sla_PRENUT (EPOCH, DATE, RMATPN)
GIVEN:

EPOCH D Julian Epoch for mean coordinates
DATE D Modified Julian Date (JD$-$2400000.5) for true coordinates
RETURNED:

RMATPN D(3,3) combined precession-nutation matrix
NOTES:
  1. The epoch and date are TDB. TT (or even UTC) will do.
  2. The matrix is in the sense:
    v$_{true}$ = M$\cdot$v$_{mean}$
    where v$_{true}$ is the star vector relative to the true equator and equinox of epoch DATE, M is the $3\times3$ matrix RMATPN and v$_{mean}$ is the star vector relative to the mean equator and equinox of epoch EPOCH.


next up previous 269
Next: SLA_PV2EL - Orbital Elements from Position/Velocity
Up: SUBPROGRAM SPECIFICATIONS
Previous: SLA_PRECL - Precession Matrix (latest)

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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