Path: Missions/LunarLanding
% Least Squares Optimization This demonstrates a least squares solution for lunar landing in 3D. The solution is in the moon fixed frame. -------------------------------------------------------------------------- Copyright (c) 2014-2016 Princeton Satellite Systems, Inc. All rights reserved. -------------------------------------------------------------------------- Since 2016.1 --------------------------------------------------------------------------
AC: ACData/ACTConstants AerospaceUtils: Coord/LatLonAltToEF Missions: LunarLanding/FuelMassFromAccel Missions: LunarLanding/LunarLandingTargetState Missions: LunarLanding/OrbitStateMatrices Missions: LunarLanding/RHSPlanet3D Missions: LunarLanding/RHSPlanet3DToAB Orbit: OrbitCoord/SLR Orbit: OrbitMechanics/RVOrbGen SC: BasicOrbit/CP2I SC: BasicOrbit/E2M SC: BasicOrbit/E2Nu SC: BasicOrbit/M2E SC: BasicOrbit/M2EApp SC: BasicOrbit/M2EEl SC: BasicOrbit/M2EHy SC: BasicOrbit/Nu2E SC: BasicOrbit/Nu2M SC: BasicOrbit/Period SC: SCData/sCTConstants SCPro: ProTools/GlideSlope Common: CommonData/Constants Common: CommonData/SwooshWatermark Common: CommonData/xSplashSmall Common: Control/C2DZOH Common: Database/Constant Common: General/CellToMat Common: General/DeBlankLT Common: General/DeleteCell Common: General/DispWithTitle Common: General/MatToCell Common: General/Watermark Common: Graphics/Axis3D Common: Graphics/Mesh2 Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Common: Graphics/TimeLabl Common: Graphics/XLabelS Common: Graphics/YLabelS Common: Graphics/ZLabelS Math: Integration/RK4 Math: Linear/Cross Math: Linear/DupVect Math: Linear/Mag Math: Linear/Skew Math: Linear/Unit Math: Trigonometry/ACosD
Back to the Missions Module page