Adaptive feedback linearization for the control of a typical wing section with structural nonlinearity

DOI10.1023/A:1008323629064zbMath0948.74036OpenAlexW1550785508MaRDI QIDQ1307800

Thomas W. Strganac, Jeonghwan Ko, Andrew J. Kurdila

Publication date: 19 November 2000

Published in: Nonlinear Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1023/a:1008323629064

zbMATH Keywords

aeroelasticityLie algebraic methodsparameterizationclosed loop stabilityLa Salle's invariance principlestructural nonlinearityadaptive nonlinear feedback controlaeroservoelasticity

Mathematics Subject Classification ID

Control, switches and devices (``smart materials) in solid mechanics (74M05) Feedback control (93B52) Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10)

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