Path: Orbit/OrbitSim
% Propagate an ECI state into the future with point mass orbit. Propagate an orbit around the Earth with no acceleration. Uses FOrbCart. -------------------------------------------------------------------------- Form: x = OrbitProp( x0, time ) -------------------------------------------------------------------------- ------ Inputs ------ x0 (6,1) Initial state [km; km/s] time (1,:) Time vector [sec] ------- Outputs ------- x (6,:) Time history of ECI states [km; km/s] -------------------------------------------------------------------------- See also: FOrbCart --------------------------------------------------------------------------