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A Numerical Comparison of Inertia-Free Attitude Control Laws for a Spacecraft with a Discrete Flexible Mode

dc.contributor.authorCamblor, Marcen_US
dc.contributor.authorXie, Antaien_US
dc.contributor.authorCruz, Gerardoen_US
dc.contributor.authorEsteban, Sergioen_US
dc.contributor.authorLee, Taeyoungen_US
dc.contributor.authorBernstein, Dennisen_US
dc.date.accessioned2014-04-10T14:50:52Z
dc.date.available2014-04-10T14:50:52Z
dc.date.issued2013en_US
dc.identifier.citationAIAA Guidance, Navigation, and Control (GNC) Conference <http://hdl.handle.net/2027.42/106484>en_US
dc.identifier.otherAIAA2013-4562
dc.identifier.urihttps://hdl.handle.net/2027.42/106484
dc.publisherPeer Revieweden_US
dc.titleA Numerical Comparison of Inertia-Free Attitude Control Laws for a Spacecraft with a Discrete Flexible Modeen_US
dc.typeArticleen_US
dc.subject.hlbsecondlevelArticleen_US
dc.subject.hlbsecondlevelAerospace Engineeringen_US
dc.subject.hlbtoplevelEngineeringen_US
dc.description.peerreviewedPeer Revieweden_US
dc.description.bitstreamurlhttp://deepblue.lib.umich.edu/bitstream/2027.42/106484/1/AIAA2013-4562.pdf
dc.identifier.doi10.2514/6.2013-4562en_US
dc.identifier.sourceAmerican Institute of Aeronautics and Astronauticsen_US
dc.owningcollnameAerospace Engineering, Department of


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