Path: Orbit/OrbitManeuver
% Simulate a low-thrust orbit raising from an ISS orbit The strategy is to raise apogee, then correct for longitude of the ascending node then correct inclination. The width of the burn region is the allowable control band around the optimal true anomaly for each element change. See also: ISSOrbit, El2RV, RHSOrbit, LowThrustControl, RK4, TimeLabl, Plot2D ------------------------------------------------------------------------