Path: Missions/LunarLanding
% Simulate the 2D landing problem and generate plots.
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Form:
Simulate2DLanding( t, beta, d, name )
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Inputs
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t (1,:) Time vector
beta (1,:) Thrust angle (rad)
d (.) Data structure describing spacecraft model
.x (4,1) Initial state (ex. [0;h;-u;0])
.g (1,1) Gravitational acceleration
.a (1,1) Thrust acceleration (m/s^2)
.n (1,1) Number of steps
name '' Name for the plots
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Outputs
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None
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Missions: LunarLanding/PropagateState Common: Graphics/Plot2D Common: Graphics/TimeLabl
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