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CL_ex_eckHech

Eckstein-Hechler propagation model - DEPRECATED

Calling Sequence

[mean_cir_t2, osc_cir_t2] = CL_ex_eckHech(t1, mean_cir_t1, t2 [, er, mu, j1jn])

Description

Parameters

t1:

Initial time [days] (1x1 or 1xN)

mean_cir_t1:

Mean orbital elements at time t1 (6x1 or 6xN).

t2:

Final time [days] (1xN or 1x1).

er:

(optional) Equatorial radius. Default: %CL_eqRad. [m] (1x1)

mu:

(optional) Gravitational constant. Default: %CL_mu. [m^3/s^2] (1x1)

j1jn:

(optional) Vector of zonal harmonics coefficients. Default: %CL_j1jn. [-] (Nzx1)

mean_cir_t2:

Mean orbital elements at t2 (6xN)

osc_cir_t2:

Osculating orbital elements at t2 (6xN)

Authors

See also

Examples

// Example 1: one orbit, several final time instants:
t1 = 12584;
mean_cir_t1 = [7.e6; 0; 1.e-3; 1; 0.1; 0.2];
t2 = 12587:1:12590
[mean_cir_t2,osc_cir_t2] = CL_ex_eckHech(t1,mean_cir_t1,t2)

// Example 2: one orbit, several final time instants:
t1 = 12584;
mean_cir_t1 = [7.e6; 0; 1.e-3; 0.1; 0.2; 0.3] * [1,1];
t2 = [12587, 12588];
[mean_cir_t2,osc_cir_t2] = CL_ex_eckHech(t1,mean_cir_t1,t2)

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