Eigensystem synthesis for active flutter suppression on an oblique-wing aircraft

DOI10.2514/3.20253zbMath0658.93040OpenAlexW2078134349MaRDI QIDQ3807971

John J. Burken, Gurbux S. Alag

Publication date: 1987

Published in: Journal of Guidance, Control, and Dynamics (Search for Journal in Brave)

Full work available at URL: http://hdl.handle.net/2060/19860020396

zbMATH Keywords

output feedbackactive flutter suppressioneigensystem synthesisoblique-wing aircraft

Mathematics Subject Classification ID

Application models in control theory (93C95) Linear systems in control theory (93C05) Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10) Pole and zero placement problems (93B55) Synthesis problems (93B50) Eigenvalues, singular values, and eigenvectors (15A18) Control/observation systems governed by ordinary differential equations (93C15)

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