No AccessSequential Loop Closure Based Adaptive Autopilot Design for a Hypersonic VehicleDaniel P. Wiese, Anuradha M. Annaswamy, Jonathan A. Muse, Michael A. Bolender and Eugene LavretskyDaniel P. WieseMassachusetts Institute of TechnologySearch for more papers by this author, Anuradha M. AnnaswamyMassachusetts Institute of TechnologySearch for more papers by this author, Jonathan A. MuseAir Force Research LaboratorySearch for more papers by this author, Michael A. BolenderAir Force Research LaboratorySearch for more papers by this author and Eugene LavretskyThe Boeing CompanySearch for more papers by this authorAIAA 2016-1379Session: H Infinity, Nonlinear, and Adaptive Flight ControlPublished Online:1 Jan 2016https://doi.org/10.2514/6.2016-1379SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookXLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byAdaptive Robust Servo LQR Control for Aircraft Under a Wide Range of Icing Conditions16 September 2024 | International Journal of Aeronautical and Space Sciences, Vol. 9Adaptive Control of Hypersonic Vehicles in the Presence of Rate LimitsJoseph E. Gaudio, Anuradha M. Annaswamy and Eugene Lavretsky7 January 2018Analytical decoupling control of a generic hypersonic vehicle based on internal model control1 Jul 2017Sequential Loop Closure Based Adaptive Output Feedback1 Jan 2017 | IEEE Access, Vol. 5 What's Popular AIAA Guidance, Navigation, and Control Conference 4-8 January 2016San Diego, California, USAhttps://doi.org/10.2514/6.2016-1379 CrossmarkInformationCopyright © 2016 by Daniel Wiese. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. TopicsAerodynamic PerformanceAerodynamicsAeronauticsAerospace SciencesAir NavigationAircrewAviationAvionicsCivil AviationCommercial AviationControl SystemsControl TheoryFeedback ControlGuidance, Navigation, and Control Systems KeywordsSequential Loop ClosureHypersonic VehiclesAutopilotClosed Loop Transfer FunctionAerodynamic CharacteristicsBlended Wing BodyScramjetElevator DeflectionFlight Path AngleFlight Control SystemDigital Topics Guidance, Navigation, and Control