Multiple-spacecraft reconfiguration through collision avoidance, bouncing, and stalemate

We consider constrained multiple-spacecraft reconfigurations outside a gravity well in deep space. As opposed to the single-spacecraft scenario, such reconfigurations involve collision avoidance constraints that can be embedded in a nonconvex, state-constrained optimal control problem. Due to the di...

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Veröffentlicht in:Journal of optimization theory and applications 2004-08, Vol.122 (2), p.323-343
Hauptverfasser: KIM, Y, MESBAHI, M, HADAEGH, F. Y
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Sprache:eng
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