Robust LQR control for stall flutter suppression: A polytopic approach * *This material is based on research sponsored by the US Air Force Academy under agreement number FA7000-13-2-0002 and FA7000-13-2-0009. The authors would like to acknowledge funding from Dr. Douglas Smith through the Air Force Office of Scientific Research Flow Control and Interaction portfolio. The grant of computer resources by the DoD HPCMO is gratefully acknowledged. The views and conclusions contained herein are those of the authors and should not be interpreted as necessarily representing the official policies or endorsements, either expressed or implied, of the French and US Air Force Academies or the French and U.S. Governments.

Author:

Niel Fabien,Seuret Alexandre,Zaccarian Luca,Fagley Casey

Publisher

Elsevier BV

Subject

Control and Systems Engineering

Reference18 articles.

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3. Bifurcation behavior of airfoil undergoing stall flutter oscillations in low-speed wind tunnel;Dimitriadis;AIAA journal,2009

4. Cyber-physical flexible wing for aeroelastic investigations of stall and classical flutter;Fagley;Journal of Fluids and Structures,2016

5. Numerical methods for h2 related problems;Feron;In Proc. American Control Conf,1992

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