Path: LunarMissions/LunarLanding
% Spacecraft control during landing.
This implements a spacecraft control system for landing.
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Form:
d = LunarLandingControl; % default data
[d,dRHS] = LunarLandingControl( x, t, dRHS, d )
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Inputs
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x (20,1) State vector [r;v;q;w;m;inertia]
(km,km/s,-,rad/s,kg,kg-m^2)
t (1,1) Time (s)
dRHS (.) Data structure for the simulation. See RHSLunarLander
d (.) Data structure for the controller
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Outputs
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d (.) Data structure for the controller
dRHS (.) Data structure for the simulation.
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Interplanetary: Landers/LandingControlBilinear SCPro: ProControl/PID3Axis Common: Control/PIDMIMO Common: Quaternion/QTForm Common: Time/Date2JD Math: Linear/Mag Math: Linear/Unit
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