Propagation of a chaser relatively to a target, with impulsives maneuvers - DEPRECATED
[t,rel_pos_vel] = CL_cw_impulPropa(t_ini,rel_pos_vel_ini,... man_dates,man,alt,t_end,... [delta_t,ballistic_coef_chaser,ballistic_coef_target,er,mu])
Computes the position and velocity vector of a chaser relative to a target when impulsive maneuvres are performed by the chaser.
The output argument rel_pos_vel contains the positions and velocities of the chaser relative to the target in the target's LVLH reference frame at the times t.
If no ballistic coefficients are given, acceleration due to drag is not taken into account.
Initial time [seconds] (1x1)
Initial position and velocity vector of chaser in target's LVLH frame [X;Y;Z;Vx;Vy;Vz] [m;m/s] (6x1)
Maneuvers times [seconds] (1xM)
Velocity increments [dvx, dvy, dvz] [m/s] (3xM)
Altitude of target [m]
Final time [seconds] (1x1)
(optional) Time step [s] (default is 100)
(optional) Ballistic coefficient of chaser : S*cx/m S=equivalent drag surface, cx = drag coefficient, m = mass [m^2/kg] (default is 0)
(optional) Ballistic coefficient of target : S*cx/m S=equivalent drag surface, cx = drag coefficient, m = mass [m^2/kg] (default is 0)
(optional) Equatorial radius [m] (default is %CL_eqRad)
(optional) Gravitational constant [m^3/s^2] (default value is %CL_mu)
Computation times [seconds] (1xN)
Position and velocity vectors of chaser in target's LVLH frame at corresponding times [X;Y;Z;Vx;Vy;Vz] [m,m/s] (6xN)
CNES - DCT/SB
1) Mecanique spatiale, CNES - Cepadues 1995, Tome II
t_ini = 0; rel_pos_vel_ini = [0;0;0;0;0;0]; alt = 450.e3; ballistic_coef_chaser = 100 * 1 / 20.e3; ballistic_coef_target = 200 * 1 / 400.e3; t_end = 4*3600; // 4 hours of ballistic propagation delta_t = 100; // 100 seconds time step man_dates = 100; man = [1;0;0]; [t,rel_pos_vel] = CL_cw_impulPropa(t_ini, .. rel_pos_vel_ini,man_dates,man,alt,t_end,delta_t, .. ballistic_coef_chaser,ballistic_coef_target) |  |  |