Structured Model Reference Adaptive Control for a Wing Section with Structural Nonlinearity

DOI10.1177/107754602023710zbMath1032.74590OpenAlexW2143477296MaRDI QIDQ4443152

Thomas W. Strganac, John L. Junkins, Jeonghwan Ko, Maruthi Ram Akella, Andrew J. Kurdila

Publication date: 22 March 2004

Published in: Journal of Vibration and Control (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1177/107754602023710

zbMATH Keywords

limit cycle oscillationsstructural nonlinearityaeroservoelasticitywing sectionwind tunnel experimentsstructured model reference adaptive control method

Mathematics Subject Classification ID

Control, switches and devices (``smart materials) in solid mechanics (74M05) Nonlinear systems in control theory (93C10) Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10)

Related Items (2)

Unnamed Item ⋮ Detection of subcritical Hopf and fold bifurcations in an aeroelastic system via the describing function method

Cites Work

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• Adaptive feedback linearization for the control of a typical wing section with structural nonlinearity
• Chaotic motions of an airfoil with non-linear stiffness in incompressible flow
• Adaptive control of linearizable systems
• Nonlinear Control of a Prototypical Wing Section with Torsional Nonlinearity
• Control of wing rock motion using adaptive feedback linearization

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