Path: Orbit/OrbitCoord
% Computes the eccentricity from apogee and perigee radii Since version 1. -------------------------------------------------------------------------- Form: e = RARP2E( rA, rP ) -------------------------------------------------------------------------- ------ Inputs ------ rA (1,m) Apogee radius rP (1,n) Perigee radius ------- Outputs ------- e (m,n) eccentricity --------------------------------------------------------------------------