Convex Programming Approach to Powered Descent Guidance for Mars Landing

We present a convex programming algorithm for the numerical solution of the minimum fuel powered descent guidance problem associated with Mars pinpoint landing. Our main contribution is the formulation of the trajectory optimization problem, which has nonconvex control constraints, as a finite-dimen...

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Veröffentlicht in:	Journal of guidance, control, and dynamics control, and dynamics, 2007-09, Vol.30 (5), p.1353-1366
Hauptverfasser:	Acikmese, Behcet, Ploen, Scott R
Format:	Artikel
Sprache:	eng
Schlagworte:	Accuracy Algorithms Applied sciences Computer science control theory systems Control system synthesis Control theory. Systems Convex analysis Convexity Copyright Exact sciences and technology Explicit knowledge Laboratories Mars Mars landing Optimization Velocity
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