CL_fr_teme2J2000Mat — TEME to J2000 matrix
M=CL_fr_teme2J2000Mat(cjdutc[,ut1_utc[,dPsi,dEps[,conv]]])
To convert a vector vect_J2000 to vect_TEME, you need to use the (hyper)matrix M' : vect_TEME = M' * vect_J2000
CNES Julian Date (1950) in TUC time (1xN)
(optional) ut1-utc [seconds] (default is 0) (1xN)
(optional) Nutation corrections [radians] (default is 0) (1xN)
(optional) Nutation corrections [radians] (default is 0) (1xN)
(optional) Convention IERS. Only iers 1996 (Lieske/Wahr) is implemented (default is "iers_1996")
TEME to EME2000 matrix (3x3xN)
1 IERS Conventions (1996), Dennis D. McCarthy
2 Explanatory Supplement to the Astronomical Almanac, Seidelman (1992)
3 Vallado, D.A., J.H. Seago, "The coordinate frames of the US Space Objects Catalogs", AIAA 2000-4025