Path: LunarMissions/LunarLanding
% Least Squares Optimization This demonstrates a least squares solution for lunar landing in 3D. The solution is in the moon fixed frame. See also RHSPlanet3D, LunarLandingTargetState, OrbitStateMatrices, FuelMassFromAccel, RK4, GlideSlope, TimeLabl % -------------------------------------------------------------------------- Copyright (c) 2014-2016 Princeton Satellite Systems, Inc. All rights reserved. -------------------------------------------------------------------------- Since 2016.1 --------------------------------------------------------------------------