Periapsis radius and velocity at periapsis to semi major axis and eccentricity - DEPRECATED
[sma, ecc] = CL_op_rpvp2ae(rp, vp [[, mu]])
This function is deprecated.
Replacement function: CL_kp_apsConvert
Use 'CL_kp_apsConvert("rp", rp, "vp", vp, ["sma", "ecc"])' instead of 'CL_op_rpvp2ae(rp, vp)'.
Computes semi major axis and eccentricity from periapsis radius and velocity at periapsis (elliptic and hyperbolic orbits).
Note:
The results are correct even if (rp,vp) are data that actually correspond to the apoapsis.
Periapsis radius [m] (1xN or 1x1)
Velocity at periapsis [m/s] (1xN or 1x1)
(optional) Gravitational constant [m^3/s^2] (default value is %CL_mu)
Semi major axis [m] (1xN)
Eccentricity (1xN)
CNES - DCT/SB