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Multicriterion structure/control design for optimal maneuverability and fault tolerance of flexible spacecraft

dc.contributor.authorLing, Jeren_US
dc.contributor.authorKabamba, Pierre T.en_US
dc.contributor.authorTaylor, Johnen_US
dc.date.accessioned2010-06-11T18:52:25Z
dc.date.available2010-06-11T18:52:25Z
dc.date.issued1992en_US
dc.identifier.citationLing, Jer; Kabamba, Pierre; Taylor, John (1992). "Multicriterion structure/control design for optimal maneuverability and fault tolerance of flexible spacecraft" AIAA-1992-4734, . <http://hdl.handle.net/2027.42/76986>en_US
dc.identifier.otherAIAA-1992-4734en_US
dc.identifier.urihttps://hdl.handle.net/2027.42/76986
dc.format.extent1032677 bytes
dc.format.extent3112 bytes
dc.format.mimetypeapplication/pdf
dc.format.mimetypetext/plain
dc.publisherAmerican Institute of Aeronautics and Astronauticsen_US
dc.titleMulticriterion structure/control design for optimal maneuverability and fault tolerance of flexible spacecraften_US
dc.typeArticleen_US
dc.subject.hlbsecondlevelAerospace Engineeringen_US
dc.subject.hlbtoplevelEngineeringen_US
dc.description.peerreviewedPeer Revieweden_US
dc.contributor.affiliationumMichigan Univ., Ann Arboren_US
dc.contributor.affiliationumMichigan Univ., Ann Arboren_US
dc.contributor.affiliationotherNSC, National Space Program Office, Taipei, Taiwanen_US
dc.description.bitstreamurlhttp://deepblue.lib.umich.edu/bitstream/2027.42/76986/1/AIAA-1992-4734-253.pdf
dc.owningcollnameInterdisciplinary and Peer-Reviewed


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