Path: Missions/Pluto
% 3D lander simulation at Pluto. The spacecraft has 3-axis thruster control. Ideal attitude pointing is assumed. You must run PlutoLanderCAD first. An altimeter gives the altitude. The planet is assumed to be a perfect sphere. This demo demonstrates the bilinear tangent law for descent from a circular equatorial orbit. See also Constant, Plot2D, TimeLabl, Inertias, RK4, Dot, Mag, Unit, RHSPointMass, LandingControlBilinear %
AC: ACData/ACTConstants AerospaceUtils: Coord/QIToBDot SC: SCData/sCTConstants SCPro: DynamicalModels/RHSPointMass SCPro: Landers/BilinearTangentLaw SCPro: Landers/LandingControl SCPro: Landers/LandingControlBilinear SCPro: ProControl/PID3Axis Common: CommonData/Constants Common: CommonData/SwooshWatermark Common: CommonData/xSplashSmall Common: Control/C2DZOH Common: Control/C2DelZOH Common: Control/FResp Common: Control/GND Common: Control/GSS Common: Control/ND2SS Common: Control/PIDMIMO Common: Control/S2Damp Common: Control/SS2ND Common: Control/SizeABCD Common: Control/TrnsZero Common: Control/WPZ Common: Control/WReson Common: Control/ZFresp Common: Database/Constant Common: General/CellToMat Common: General/DeleteCell Common: General/MatToCell Common: General/Watermark Common: Graphics/LogLimit Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Common: Graphics/TextS Common: Graphics/TimeLabl Common: MassProperties/IC623X3 Common: MassProperties/Inertias Common: Quaternion/AU2Q Common: Quaternion/Q2AU Common: Quaternion/QMult Common: Quaternion/QPose Common: Quaternion/QTForm Common: Quaternion/U2Q Math: Geometry/Perpendicular Math: Integration/RK4 Math: Linear/ColCompR Math: Linear/Cross Math: Linear/DelLZ Math: Linear/Dot Math: Linear/DupVect Math: Linear/IsZero Math: Linear/Mag Math: Linear/RowCompU Math: Linear/SkewSymm Math: Linear/Unit
Back to the Missions Module page