Informations about Eckstein-Hechler orbit propagation analytical model - DEPRECATED
infos = CL_ex_eckHechInfos(mean_cir [, er, mu, j1jn])
This function is deprecated.
Replacement function: CL_ex_getInfo
Computes data related to Eckstein Hechler orbit propagation analytical model.
These data are:
- Eccentricity vector of frozen orbit
- Secular drifts of some angular orbital elements
The output is a structure with the following fields:
- infos.exf: Mean eccentricity vector x-component of frozen orbit
- infos.eyf: Mean eccentricity vector y-component of frozen orbit
- infos.dgomdt: Secular drift of mean right ascension of ascending node [rad/s]
- infos.dpsodt: Secular drift of mean argument of latitude [rad/s]
Note:
The outputs only depend on semi major-axis and inclination.
See CL_ex_eckHech for more details on the propagation model.
Warning :
- The input argument "zonals" is deprecated as of CelestLab v3.0.0. It has been replaced by "j1jn".
Mean 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 truncated at order 6 (J1 to J6). Default: %CL_j1jn(1:6). [-] (6x1)
(structure) Data for the given orbital elements (containing (1xN) vectors)
CNES - DCT/SB