Keplerian to cartesian orbital elements
[pos_car,vel_car[,jacob]] = CL_oe_kep2car(kep[,mu])
Converts classical keplerian orbital elements to position and velocity for an elliptic, hyperbolic or parabolic orbit.
The transformation jacobian is optionally computed.
See Orbital elements for more details
classical keplerian parameters [sma;ecc;inc;pom;raan;anm] [m,rad] (6xN)
(optional) gravitational constant. [m^3/s^2] (default value is %CL_mu)
position [X;Y;Z] [m] (3xN)
velocity [Vx;Vy;Vz] [m/s] (3xN)
(optional) transformation jacobian d(X,Y,Z,Vx,Vy,Vz)/d(sma,ecc,inc,pom,raan,anm) (6x6xN)
1) CNES - MSLIB FORTRAN 90, Volume V (mv_kep_car)
CNES - DCT/SB