No AccessNonlinear Multiple-Time-Scale Attitude Control of a Rigid Spacecraft with Uncertain InertiasDipanjan Saha and John ValasekDipanjan SahaTexas A&M UniversitySearch for more papers by this author and John ValasekTexas A&M UniversitySearch for more papers by this authorAIAA 2019-0932Session: Attitude ControlPublished Online:6 Jan 2019https://doi.org/10.2514/6.2019-0932SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byRobust H-infinity Controller for a Single-axis Spacecraft Rotation What's Popular AIAA Scitech 2019 Forum 7-11 January 2019San Diego, Californiahttps://doi.org/10.2514/6.2019-0932 CrossmarkInformationCopyright © 2019 by Dipanjan Saha and John Valasek. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. TopicsActuatorsAeronauticsAerospace SciencesAir NavigationAstrodynamicsAstronauticsAttitude ControlAvionicsControl TheoryFeedback ControlGuidance, Navigation, and Control SystemsNonlinear Control TheoryOptimal Control TheorySpacecraft Guidance and Control KeywordsSpacecraft ModelsControl Moment GyrosActuatorsLyapunov AnalysisSingular PerturbationAttitude TrackingEuler AnglesStrict Feedback FormSix Degree of FreedomNonlinear SystemsPDF Topics Guidance, Navigation, and Control