CL_ex_meanEckHech

Description

• This function is deprecated.

  Replacement function: CL_ex_osc2mean

• Computes the mean orbital elements from the osculating orbital elements, using Eckstein-Hechler model.

• 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 It has been replaced by "j1jn".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.

Parameters

osc_cir:

Osculating circular-adapted elements [sma;ex;ey;inc;raan;pom+anm] (6xN)

er:

(optional) Equatorial radius [m]. Default is %CL_eqRad

mu:

(optional) Gravitational constant [m^3/s^2]. Default is %CL_mu

j1jn:

(optional) Vector of zonal harmonics. Default is %CL_j1jn (Nz x 1)

mean_cir:

Mean circular-adapted elements [sma;ex;ey;inc;raan;pom+anm] (6xN)

Authors

• CNES - DCT/SB

See also

• CL_ex_meanEckHech

Examples

mean_cir = [7.e6; 0; 1.e-3; 1; 0.2; 0.3] [mean_cir2,osc_cir] = CL_ex_eckHech(0,mean_cir,0); CL_ex_meanEckHech(osc_cir) // => mean_cir