Path: Missions/LunarLanding
% Test fmincon against an analytical solution for the linear tangent law The test is for a lunar landing in 3D. The solution is in the moon fixed frame. Requires fmincon from the MATLAB Optimization Toolbox. % -------------------------------------------------------------------------- Copyright (c) 2015 Princeton Satellite Systems, Inc. All rights reserved. -------------------------------------------------------------------------- Since 2016.1 --------------------------------------------------------------------------
AC: ACData/ACTConstants Missions: LunarLanding/LandingConst3D Missions: LunarLanding/LandingCost3D Missions: LunarLanding/PropagateState3D Missions: LunarLanding/RHSPlanet3D Missions: LunarLanding/Simulate3DLanding Missions: LunarMission/PlanetWithTerrainPatch SC: Ephem/LoadLunarTopography SC: Ephem/RSHMoon SC: SCData/gltm2b SC: SCData/sCTConstants SCPro: Landers/BilinearTangentLaw Common: CommonData/Constants Common: CommonData/SwooshWatermark Common: CommonData/xSplashSmall Common: Database/Constant Common: General/CellToMat Common: General/DeBlankAll Common: General/DeBlankLT Common: General/DeleteCell Common: General/DispWithTitle Common: General/HasOptimizationToolbox Common: General/MatToCell Common: General/Watermark Common: Graphics/Mesh2 Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Common: Graphics/PrintFig Common: Graphics/TimeLabl Common: Graphics/TitleS Common: Graphics/XLabelS Common: Graphics/YLabelS Common: Graphics/ZLabelS Math: Analysis/PAL Math: Analysis/SCHarm Math: Integration/RK4 Math: Linear/DupVect Math: Linear/Factorl Math: Linear/Mag Math: Linear/Skew Math: Linear/Unit
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