No AccessAdaptive Disturbance Rejection Control Using System Input-Output DataNilesh KulkarniNilesh KulkarniQSS Group, Inc., NASA Ames Research CenterSearch for more papers by this authorSession: GNC-30: Adaptive Aircraft ControlPublished Online:15 Jun 2012https://doi.org/10.2514/6.2006-6414SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byExperimental Validation of Metrics-Driven Enhanced-Safety (ME) Adaptive ControlJames Neidhoefer, Nilesh Kulkarni, Khalid Al-Ali, Jason Ryan and Abe Ishihara15 June 2012 What's Popular AIAA Guidance, Navigation, and Control Conference and Exhibit 21 August 2006 - 24 August 2006Keystone, Coloradohttps://doi.org/10.2514/6.2006-6414 Crossmark TopicsAircraft ControlAircraft Flight Control SystemAircraft Operations and TechnologyAircraft Stability and ControlAircraftsControl TheoryFeedback ControlGuidance, Navigation, and Control Systems KeywordsLinear Time Invariant SystemFeedback ControlNASA Ames Research CenterFlight ControlAeroplaneThree Degrees of FreedomAerospace SystemSpace StructuresFrequency DomainCombustorsDigital Topics Guidance, Navigation, and Control