Lyddane propagation model - mean elements (mean = secular) - DEPRECATED
mean_kep = CL_ex_meanLyddane(osc_kep [, er, mu, j1jn])
This function is deprecated.
Replacement function: CL_ex_osc2mean
Computes the mean orbital elements from the osculating orbital elements, using Lyddane model.
The mean elements for this model include secular effects only.
Notes:
- The input argument "zonals" is deprecated as of CelestLab v3.0.0. It has been replaced by "j1jn".
See Propagation models for more details.
Osculating orbital elements (6xN)
(optional) Equatorial radius. Default: %CL_eqRad. [m] (1x1)
(optional) Gravitational constant. Default: %CL_mu. [m^3/s^2] (1x1)
(optional) Vector of zonal harmonics coefficients. Default: %CL_j1jn. [-] (Nzx1)
Mean orbital elements (6xN)
CNES - DCT/SB