<< CL_ex_lyddaneMan Trajectory and maneuvers CL_ex_meanLyddane >>

CelestLab >> Trajectory and maneuvers > CL_ex_meanEckHech

CL_ex_meanEckHech

Eckstein Hechler orbit propagation analytical model (mean elements)

Calling Sequence

[mean_cir] = CL_ex_meanEckHech(osc_cir [,er,mu,zonals])

Description

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 value is %CL_mu)

zonals:

(optional) Vector of zonals coefficients J1 to Jn (troncated to J6) to be used (default is %CL_j1jn(1:6)) (Nz x 1)

mean_cir:

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

Authors

Bibliography

See also

Examples

osc_cir = [42166712;2.9e-3;1.2e-3;CL_deg2rad([97.2;125;5])];
mean_cir = CL_ex_meanEckHech(osc_cir)
// check
[mean_cir2,osc_cir2] = CL_ex_eckHech(0,mean_cir,0)
<< CL_ex_lyddaneMan Trajectory and maneuvers CL_ex_meanLyddane >>