Volume 23, Issue 6 No AccessIdentification and Control of Limit Cycle Oscillations in Aeroelastic SystemsThomas W. Strganac, Jeonghwan Ko, David E. Thompson and Andrew J. KurdilaThomas W. Strganac Texas A&M University, College Station, Texas 77843-3141Search for more papers by this author, Jeonghwan Ko Texas A&M University, College Station, Texas 77843-3141Search for more papers by this author, David E. Thompson Texas A&M University, College Station, Texas 77843-3141Search for more papers by this author and Andrew J. Kurdila University of Florida, Gainesville, Florida 32611-6250Search for more papers by this authorPublished Online:23 May 2012https://doi.org/10.2514/2.4664SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About Previous article Next article FiguresReferencesRelatedDetailsSee PDF for referencesCited byNonlinear modeling, characterization, and effectiveness of three-degree-of-freedom piezoaeroelastic energy harvestersMechanical Systems and Signal Processing, Vol. 189Nonlinear aeroelastic modeling and comparative studies of three degree of freedom wing-based systemsInternational Journal of Non-Linear Mechanics, Vol. 149Modulation and Annihilation of Aeroelastic Limit-Cycle Oscillations Using a Variable-Frequency Disturbance GeneratorMichael T. 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Strganac 23 May 2012 | Journal of Guidance, Control, and Dynamics, Vol. 27, No. 1Limit Cycle Oscillation Control of Aeroelastic System Using Model-Error Control SynthesisJongrae Kim and John Crassidis22 June 2012Estimating Nonlinearity Using Volterra Kernels in Feedback with Linear ModelsRick Lind and Richard Prazenica26 June 2012Analyses and Experiments of Suppression of Control Reversal Using a Wing Section with Multiple Control SurfacesGeorge Platanitis and Thomas Strganac26 June 2012Implications of cubic physical/aerodynamic non-linearities on the character of the flutter instability boundaryInternational Journal of Non-Linear Mechanics, Vol. 38, No. 2Flutter, Postflutter, and Control of a Supersonic Wing Section Piergiovanni Marzocca , Liviu Librescu and Walter A. Silva 23 May 2012 | Journal of Guidance, Control, and Dynamics, Vol. 25, No. 5Output Feedback Form and Adaptive Stabilization of a Nonlinear Aeroelastic System Sahjendra N. Singh and Ling Wang 23 May 2012 | Journal of Guidance, Control, and Dynamics, Vol. 25, No. 4Hybrid Fuzzy Sliding-Mode Control of an Aeroelastic System Chih-Min Lin and Chun-Fei Hsu 23 May 2012 | Journal of Guidance, Control, and Dynamics, Vol. 25, No. 4Structured Model Reference Adaptive Control for a Wing Section with Structural Nonlinearity19 August 2016 | Journal of Vibration and Control, Vol. 8, No. 5Open/Closed-Loop Nonlinear Aeroelasticity for Airfoils via Volterra Series ApproachPiergiovanni Marzocca, Walter Silva and Liviu Librescu26 June 2012Control of a Wing Section With Structural Nonlinearities Using Leading and Trailing Edge Control SurfacesGeorge Platanitis and Thomas Strganac26 June 2012Hierarchical Adaptive Controller for a Nonlinear Aeroelastic Wing Section with Multiple Control SurfacesNonlinear Robust Performance Analysis using Gradient-Based Optimisation - An Aeroelastic Case-StudyDecoupled fuzzy sliding-mode control of a nonlinear aeroelastic structure What's Popular Volume 23, Number 6November 2000 Crossmark TopicsAerodynamic PerformanceAerodynamicsAeroelasticityAeronautical EngineeringAeronauticsAvionicsControl SystemsControl TheoryFeedback ControlFluid DynamicsGuidance, Navigation, and Control SystemsNonlinear Control TheoryTransducers KeywordsNonlinear Aeroelastic SystemsFeedback LinearizationAdaptive Control MethodNonlinear SystemsHigh Performance AircraftAdaptive Control SystemsFreestream VelocityData AcquisitionAngle of AttackStructural NonlinearitiesPDF Published online23 May 2012