Path: Interplanetary/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 %
Interplanetary: Landers/LandingControlBilinear SCPro: DynamicalModels/RHSPointMass Common: Database/Constant Common: Graphics/Plot2D Common: Graphics/TimeLabl Common: MassProperties/Inertias Math: Integration/RK4 Math: Linear/Dot Math: Linear/Mag Math: Linear/Unit
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