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Multiple-spacecraft reconfigurations through collision avoidance, bouncing, and stalemateWe consider constrained multiple-spacecraft reconfigurations outside of a gravity well in deep space. As opposed to the single-spacecraft scenario, such reconfigurations involve collision avoidance constraints that can be formalized and embedded in a nonconvex.
Document ID
20060040065
Acquisition Source
Jet Propulsion Laboratory
Document Type
Reprint (Version printed in journal)
External Source(s)
Authors
Kim, Y.
Mesbahi, M.
Hadaegh, F. Y.
Date Acquired
August 23, 2013
Publication Date
August 1, 2004
Publication Information
Publication: Journal of Optimization Theory and Applications
Volume: 122
Issue: 2
Distribution Limits
Public
Copyright
Other
Keywords
multiple spacecraft reconfiguration state-constrained optimal control bouncing
heuristic algorithm

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