Panel flutter suppression by exact state transformations and feedback control using piezoelectric actuation is presented. A nonlinear control system is formulated for the nonlinear partial differential equation governing the dynamics of a simply supported rectangular panel with bonded piezoelectric layers based on the von Ka´rman large-deflection plate theory. Distributed piezoelectric actuators and sensors connected to processing networks are used as modal actuators and sensors to actively control panel vibrations. The control inputs are given by the electric fields required to drive the actuators based on piezoelectric actuation. Nonlinear feedback control laws are formulated through a transformation of the nonlinear system into an equivalent controllable linear system. The simulated results show that the resulting closed-loop system based on feedback linearized controllers effectively suppress panel flutter limit-cycle motions.
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ASME 2009 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference
August 30–September 2, 2009
San Diego, California, USA
Conference Sponsors:
- Design Engineering Division and Computers in Engineering Division
ISBN:
978-0-7918-4901-9
PROCEEDINGS PAPER
A Feedback Linearization Approach for Panel Flutter Suppression With Piezoelectric Actuation
Oluseyi O. Onawola,
Oluseyi O. Onawola
Auburn University, Auburn, AL
Search for other works by this author on:
S. C. Sinha
S. C. Sinha
Auburn University, Auburn, AL
Search for other works by this author on:
Oluseyi O. Onawola
Auburn University, Auburn, AL
S. C. Sinha
Auburn University, Auburn, AL
Paper No:
DETC2009-87697, pp. 1819-1828; 10 pages
Published Online:
July 29, 2010
Citation
Onawola, OO, & Sinha, SC. "A Feedback Linearization Approach for Panel Flutter Suppression With Piezoelectric Actuation." Proceedings of the ASME 2009 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference. Volume 4: 7th International Conference on Multibody Systems, Nonlinear Dynamics, and Control, Parts A, B and C. San Diego, California, USA. August 30–September 2, 2009. pp. 1819-1828. ASME. https://doi.org/10.1115/DETC2009-87697
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