Path: Interplanetary/MissionAnaluysis
% Perform an optimal 2D transfer from Earth to Mars orbits. This performs a discrete optimization of a linearized system using Simplex. The mass of the spacecraft (and the acceleration) is assumed to be constant. See also Constant, BarPlot, NewFig, TimeLabl, TitleS, XLabelS, YLabelS, Mag, OptimalTrajectory, LTSpiral, LinOrb, Planets % ------------------------------------------------------------------------------- Copyright (c) 2002 Princeton Satellite Systems, Inc. All rights reserved. -------------------------------------------------------------------------------