Application of output feedback sliding mode control to active flutter suppression of two-dimensional airfoil

DOI10.1007/s11431-010-0099-zzbMath1383.74029OpenAlexW2073556002MaRDI QIDQ617154

Chen Song, Changchuan Xie, Zhi-Gang Wu, Chao Yang

Publication date: 21 January 2011

Published in: Science China. Technological Sciences (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s11431-010-0099-z

zbMATH Keywords

sliding mode controlaeroelasticityflutteroutput feedback controlairfoil

Mathematics Subject Classification ID

Feedback control (93B52) Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10) General aerodynamics and subsonic flows (76G25)

Related Items (2)

Analytical and Experimental Aeroelastic Wing Flutter Analysis and Suppression ⋮ Active control of hypersonic airfoil flutter via adaptive fuzzy sliding mode method

Cites Work

• Robust aeroelastic control of two-dimensional supersonic flapped wing systems

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