Circular adapted to cartesian orbital elements
[pos,vel,jacob] = CL_oe_cir2car(cir [,mu])
Converts orbital elements adapted to near-circular orbits to cartesian orbital elements.
The transformation jacobian is optionally computed.
See Orbital elements for more details.
Orbital elements adapted to near-circular orbits [sma;ex;ey;inc;raan;alpha] [m,rad] (6xN)
position [X;Y;Z] [m] (3xN)
velocity [Vx;Vy;Vz] [m/s] (3xN)
(optional) Transformation jacobian (See Orbital elements for more details) (6x6xN)
CNES - DCT/SB
// // Example 1 cir = [7000.e3; 1e-4; 1e-4; 1; 2; %pi/2]; [pos,vel] = CL_oe_cir2car(cir); // Example 2 cir = [7000.e3; 1e-4; 1e-4; 1; 2; %pi/2]; [pos,vel,jacob1] = CL_oe_cir2car(cir); [cir2,jacob2] = CL_oe_car2cir(pos,vel); cir2 - cir // zero jacob2 * jacob1 // identity |  |  |