Path: LunarMissions/LunarMission
% Lunar Mission Demo with Transfer and Insertion Simulate a mission from Earth orbit to lunar orbit. The spacecraft has 3 orthogonal reaction wheels and a single delta-v thruster. The mission takes five days for both the transfer and lunar insertion burn. It uses the default values from RHSLunarMission for a 6U CubeSat. The dimensions are 30 x 20 x 10 cm. If the user has the Optimization Toolbox, it will be used via LunarTargeting. See also Date2JD, LunarTargeting, LunarMissionControl, RHSLunarMission, PlanetPosJPL, LoadSGM150, RK4, EarthMoon, PlotLunarOrbit, Figui, Plot2D