Path: Interplanetary/Landers
% Lunar takeoff demo using bilinear tangent thrust programming.
Replicates the example in the reference.
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See also: BilinearTangentVector, FOrbCart, RK4, Plot2D
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Reference: Arthur E. Bryson, Jr., Y. C. Ho, "Applied Optimal Control:
Optimization, Estimation, and Control," Orbit, p. 85.
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Copyright (c) 2013-2014 Princeton Satellite Systems, Inc.
All rights reserved.
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Since version 2014.1
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