Fundamental arguments for nutation - DEPRECATED
[F,FP,FPP] = CL_mod_nutationArg(t [,flag])
This function is deprecated.
Computes the fundamental arguments for nutation (F) (Sun and Moon position), and their derivatives (FP,FPP).
F(1,:) -> l = Mean Anomaly of the Moon
F(2,:) -> l' = Mean Anomaly of the Sun
F(3,:) -> F = L - OMEGA (where L is the mean longitude of the moon)
F(4,:) -> D = Mean Elongation of the Moon from the Sun
F(5,:) -> OMEGA = Mean Longitude of the Ascending Node of the Moon
Time from 1st January 2000 12h in centuries (number of days / 36525), (TT time scale) (1xN)
(optional) "n" -> F only; "p" -> F and Fp; "s" -> F, Fp and Fpp (default depends on number of output variables)
Fundamental arguments for nutation (5xN) [rad]
(optional) First time derivative of F (5xN) [rad/s]
(optional) Second time derivative of F (5xN) [rad/s^2]
CNES - DCT/SB
1) IERS Conventions (1996), Dennis D. McCarthy