Examples
mean_kep = [7.e6; 1.e-4; 1; %pi/2; 0.2; 0.3] [mean_kep2,osc_kep] = CL_ex_lyddane(0,mean_kep,0); CL_ex_meanLyddane(osc_kep) // => mean_kep |  |  |
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 It has been replaced by "j1jn".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 [m]. Default is %CL_eqRad
(optional) Gravitational constant [m^3/s^2]. Default is %CL_mu
(optional) Vector of zonal harmonics. Default is %CL_j1jn (Nz x 1)
Mean orbital elements (6xN)
CNES - DCT/SB
mean_kep = [7.e6; 1.e-4; 1; %pi/2; 0.2; 0.3] [mean_kep2,osc_kep] = CL_ex_lyddane(0,mean_kep,0); CL_ex_meanLyddane(osc_kep) // => mean_kep | | |