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Attitude stabilization of a rigid spacecraft using two momentum wheel actuators
dc.contributor.authorKrishnan, Hariharanen_US
dc.contributor.authorMcClamroch, N. Harrisen_US
dc.contributor.authorReyhanoglu, Mahmuten_US
dc.date.accessioned2010-06-11T18:51:38Z
dc.date.available2010-06-11T18:51:38Z
dc.date.issued1995en_US
dc.identifier.citationKrishnan, Hariharan; Mcclamroch, N. H.; Reyhanoglu, Mahmut (1995). "Attitude stabilization of a rigid spacecraft using two momentum wheel actuators" Journal of Guidance, Control, and Dynamics, vol.18 no.2 (256-263). <http://hdl.handle.net/2027.42/76974>en_US
dc.identifier.issn0731-5090en_US
dc.identifier.urihttps://hdl.handle.net/2027.42/76974
dc.format.extent1004576 bytes
dc.format.extent3112 bytes
dc.format.mimetypeapplication/pdf
dc.format.mimetypetext/plain
dc.publisherAmerican Institute of Aeronautics and Astronauticsen_US
dc.titleAttitude stabilization of a rigid spacecraft using two momentum wheel actuatorsen_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.affiliationotherNational Univ. of Singapore, Singaporeen_US
dc.contributor.affiliationotherKing Fahad Univ. of Petroleum and Minerals, Dhahran, Saudi Arabiaen_US
dc.description.bitstreamurlhttp://deepblue.lib.umich.edu/bitstream/2027.42/76974/1/AIAA-21378-217.pdf
dc.identifier.doi10.2514/3.21378en_US
dc.identifier.sourceJournal of Guidance, Control, and Dynamicsen_US
dc.owningcollnameInterdisciplinary and Peer-Reviewed


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