CL_man_applyDv — Modification of osculating orbital elements after a maneuver defined in QSW frame.
kep_dv = CL_man_applyDv(kep,dv_local[,mu])
Maneuver is defined by its position (mean anomaly of kep) and its direction and modulus dv_local = [lambda;phi;norm] defined in the local orbital frame QSW with spheric coordinates : first parameter lambda is the in plane component (pi ~= towards planet and pi/2 = along velocity) second parameter phi is the out of plane component, positive towards the kinetic moment, third parameter is the norm
osculating keplerian parameters of original orbit in inertial frame [m,rad] (6xN)
maneuver in spheric coordinates in satellite local frame QSW [lambda;phi;|dv|] [rad,rad,m/s] (3xN)
(optionnal) geocentric gravitational constant [m^3/s^2] (default is %CL_mu)
osculating keplerian parameters of orbit in inertial frame after maneuver execution [m,rad] (6xN)