PlutoLander3D:

% 3D lander simulation.
 The spacecraft has 3-axis thruster control. Ideal attitude pointing is
 assumed. You must run LunarLanderCAD 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
%

Children:

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