Optimal Despin of a Tumbling Satellite with an Arbitrary Thruster Configuration, Inertia Matrix, and Cost Functional

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Title{Optimal Despin of a Tumbling Satellite with an Arbitrary Thruster Configuration, Inertia Matrix, and Cost Functional}
Publication TypeConference Paper
Year of Publication2010
AuthorsSheinfeld D, Rock SM
Conference NameProceedings of the 20th AAS/AIAA Space Flight Mechanics Meeting
PublisherAAS/AIAA
Conference LocationSan Diego
URLhttp://www.stanford.edu/group/arl/cgi-bin/drupal/sites/default/files/public/publications/SheinfeldR 2010.pdf

Last modified Sun, 17 Oct, 2010 at 21:30