Volume 28, Issue 3 No AccessSuppression of Control Reversal Using Leading- and Trailing-Edge Control SurfacesGeorge Platanitis and Thomas W. StrganacGeorge Platanitis Texas A&M University, College Station, Texas 77843-3141Search for more papers by this author and Thomas W. Strganac Texas A&M University, College Station, Texas 77843-3141Search for more papers by this authorPublished Online:23 May 2012https://doi.org/10.2514/1.6692SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About Previous article Next article FiguresReferencesRelatedDetailsSee PDF for referencesCited byIdentification of Dynamic Structural Properties of a Flexible Wing Through Distributed Bleed Flow ControlLuca De Beni, Gabriel Peyredieu du Charlat, Ari Glezer and Massimo Ruzzene20 June 2022Enhancing Flight Envelope for a Nonlinear Aeroelastic Wing-Section Using Adaptive Fuzzy Sliding Mode Control LawJournal of Aerospace Engineering, Vol. 35, No. 3Conventional and Unconventional Control Effectors for Load Alleviation in High-Aspect-Ratio-Wing AircraftDivya Sanghi, Cristina Riso, Carlos E. 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Singh26 February 2015 | Journal of Guidance, Control, and Dynamics, Vol. 38, No. 12Optimal Sizing and Configurations of the Control Surfaces for Active Aeroelastic ControlRichard N. Brown and Kumar V. Singh18 June 2015Adaptive Chebyshev Neural Control of a Multi-Input Aeroelastic System Despite Gust LoadPrince Ghorawat, Keum W. Lee and Sahjendra N. Singh18 June 2015TP Model Transformation as a Manipulation Tool for QLPV Analysis and Design29 January 2015 | Asian Journal of Control, Vol. 17, No. 2Aeroelastic Analysis and Optimization of Flexible Wing Aircraft with a Novel Control EffectorWrik Mallik, Rakesh K. Kapania and Joseph A. Schetz2 January 2015Effect of Embedded Control Surface Actuators on Active Aeroelastic ControlKumar V. Singh, Richard N. Brown and Raymond M. Kolonay2 January 2015Aeroelastic System Control by a Multiple Spoiler Actuation and MRAC SchemeMario Cassaro, Manuela Battipede, Pier Marzocca and Goodarz Ahmadi2 January 2015Active flutter suppression of a multiple-actuated-wing wind tunnel modelChinese Journal of Aeronautics, Vol. 27, No. 6Aeroelastic Wing Section Control via Relaxed Tensor Product Model Transformation FrameworkPéter Baranyi and Béla Takarics11 September 2014 | Journal of Guidance, Control, and Dynamics, Vol. 37, No. 5Robust Higher-Order Sliding-Mode Finite-Time Control of Aeroelastic SystemsKeum W. Lee and Sahjendra N. Singh11 September 2014 | Journal of Guidance, Control, and Dynamics, Vol. 37, No. 5Example for convex hull tightening increasing the feasible parameter region at Linear Matrix Inequality based control designInfluence of complexity relaxation and convex hull manipulation on LMI based control designWITHDRAWN: Active flutter suppression of a wind tunnel multiple-actuated-wing modelChinese Journal of Aeronautics, Vol. 32Recent advance in nonlinear aeroelastic analysis and control of the aircraftChinese Journal of Aeronautics, Vol. 27, No. 1Multi-Input Higher-order Sliding Mode Control of Aeroelastic Systems With Uncertainties and Gust LoadKeum W. Lee and Sahjendra N. Singh10 January 2014Novel Nonlinear Control Design for a Two-Dimensional Airfoil Under Unsteady FlowK. Zhang, Z. Wang, A. Behal and P. Marzocca30 October 2013 | Journal of Guidance, Control, and Dynamics, Vol. 36, No. 6Tensor-Product-Model-Based Control of a Three Degrees-of-Freedom Aeroelastic ModelBéla Takarics and Péter Baranyi3 September 2013 | Journal of Guidance, Control, and Dynamics, Vol. 36, No. 5Aileron Reversal of Nonuniform and Swept Composite Aircraft WingsKeun-Taek Kim and Ohseop Song28 May 2013 | Journal of Aircraft, Vol. 50, No. 3Control of a Wing Section Using Leading- and Trailing-Edge Flaps by L1 Adaptive Feedback Despite DisturbancesKeum Lee and Sahjendra Singh5 January 2013Adaptive control of a nonlinear aeroelastic systemAerospace Science and Technology, Vol. 15, No. 5Multi-Input Noncertainty-Equivalent Adaptive Control of an Aeroelastic System Keum W. Lee and Sahjendra N. Singh 23 May 2012 | Journal of Guidance, Control, and Dynamics, Vol. 33, No. 5Linear-Parameter-Varying Control of an Improved Three-Degree-of-Freedom Aeroelastic Model Zebb Prime , Ben Cazzolato , Con Doolan and Thomas Strganac 23 May 2012 | Journal of Guidance, Control, and Dynamics, Vol. 33, No. 2Robust Analysis of Active Flutter Suppression Using Multiple Control Surfaces via Second-Order Controllers17 September 2007Comparison of First- and Second-Order EMA Models for an Aeroservoelastic Wing with Multiple Control SurfacesYing Teng15 June 2012 What's Popular Volume 28, Number 3May 2005 Crossmark TopicsAeronauticsAircraft Components and StructureAircraft ControlAircraft DesignAircraft ManeuversAircraft Operations and TechnologyAircraft Stability and ControlAircraft Wing DesignAircraftsAirfoilAviationCombat AircraftFlight Control SurfacesMilitary AircraftMilitary AviationWing Configurations KeywordsControl ReversalActive Aeroelastic WingControl SurfacesActuatorsAeroelastic ResponseAircraft ManeuversAerostructureDynamic PressureLift CoefficientFreestream VelocityPDF Published online23 May 2012