Path: LunarMissions/LunarMission
% Generates an Apollo lunar landing trajectory.
Type ApolloTrajectory for a demo.
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Form:
[r, v, a] = ApolloTrajectory( rTG, vTG, aTG, rG, vG, t )
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Inputs
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rTG (3,1) R target (m)
vTG (3,1) V target (m/s)
aG (3,1) Acceleration target(m/s^2)
rTG (3,1) R start (m)
vTG (3,1) V start (m/s)
t (1,:) Time (s)
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Outputs
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r (3,:) Position (m)
v (3,:) Velocity (m/s)
a (3,:) Acceleration (m/s^2)
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Reference: Klumpp, A. R. "Apollo Lunar Descent Guidance," Automatica,
Vol. 10, pp. 133-146, Pergamon Press, 1974.
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Common: Database/Constant Common: Graphics/Plot2D
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