H0-n to EME2000 (J2000) transformation matrix
M=CL_fr_H0n2J2000Mat(lon,cjd,[,ut1_utc[,xp,yp[,dPsi,dEps[,conv]]]])
Computes the frame transformation matrix M from H0-n to EME2000.
By convention, multiplying M by coordinates relative to H0-n yields coordinates relative to EME2000.
See Reference Frames for more details on the definition of reference frames.
east longitude that defines the X axis of the H0-n frame [rad]
modified julian day from 1950.0 (UTC). Reference time for H0-n frame. (1xN)
(optional) ut1-utc [seconds] (default is 0) (1xN)
(optional) x polar coordinate [radians] (default is 0) (1xN)
(optional) y polar coordinate [radians] (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")
H0-n to EME200 transformation matrix (3x3xN)
CNES - DCT/SB