Analytical eclipse calculation for circular orbits
res = CL_gm_eclipseCir(sma, inc, raan, alpha_sun, delta_sun [[, er, mu]])
Computes various ress that characterize the portion of the orbit path where the satellite is in the shadow of the planet.
Notes:
This function is actually an interface to CL_gm_eclipse, which is called with zero values for eccentricity and argument of periapsis).
See CL_gm_eclipse for more details.
Semi-major axis. [m] (1xN)
Inclination. [rad] (1xN)
Right ascension of ascending node. [rad] (1xN)
Sun right ascension. [rad] (1xN)
Sun declination. [rad] (1xN)
(optional) Equatorial radius. Default: %CL_eqRad. [m] (1x1)
(optional) Gravitational constant. Default: %CL_mu. [m^3/s^2] (1x1)
(structure) Results (see description above). [rad or sec] (each field is 1xN)
CNES - DCT/SB