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SLA_PRENUT - Precession/Nutation Matrix   

ACTION:
Form the matrix of precession and nutation (IAU 1976, FK5).
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.
2.
The matrix is in the sense:
vtrue = M$\cdot$vmean
where vtrue is the star vector relative to the true equator and equinox of epoch DATE, M is the $3\times3$ matrix RMATPN and vmean is the star vector relative to the mean equator and equinox of epoch EPOCH.


next up previous
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
12 October 1999
E-mail:ptw@star.rl.ac.uk