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
Interplanetary: Ephemeris/PlanetPosJPL LunarMissions: DynamicalModels/RHSLunarMission LunarMissions: LunarData/LoadSGM150 LunarMissions: LunarMission/LunarMissionControl LunarMissions: LunarMission/LunarTargeting LunarMissions: Visualization/EarthMoon LunarMissions: Visualization/PlotLunarOrbit SC: Ephem/InterpolateState SC: Ephem/SunV1 Common: GUIs/Figui Common: General/HasOptimizationToolbox Common: Graphics/Plot2D Common: Graphics/TimeLabl Common: Time/Date2JD Math: Integration/RK4 Math: Linear/Mag
Back to the LunarMissions Module page