Panel flutter suppression by exact state transformations and feedback control using piezoelectric actuation is presented. A nonlinear control system is designed for a simply supported rectangular panel with bonded piezoelectric layers based on the von Kármán large-deflection plate theory. The governing nonlinear partial differential equation for the panel is reduced to a set of ordinary differential equations using a two mode approximation. 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 discretized 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.
Skip Nav Destination
e-mail: seyionawola@gmail.com
e-mail: ssinha@eng.auburn.edu
Article navigation
July 2011
Research Papers
A Feedback Linearization Approach for Panel Flutter Suppression With Piezoelectric Actuation
Oluseyi O. Onawola,
Oluseyi O. Onawola
Nonlinear Systems Research Laboratory,
e-mail: seyionawola@gmail.com
Auburn University
, Auburn, AL 36849
Search for other works by this author on:
S. C. Sinha
S. C. Sinha
ASME Fellow
Nonlinear Systems Research Laboratory,
e-mail: ssinha@eng.auburn.edu
Auburn University
, Auburn, AL 36849
Search for other works by this author on:
Oluseyi O. Onawola
Nonlinear Systems Research Laboratory,
Auburn University
, Auburn, AL 36849e-mail: seyionawola@gmail.com
S. C. Sinha
ASME Fellow
Nonlinear Systems Research Laboratory,
Auburn University
, Auburn, AL 36849e-mail: ssinha@eng.auburn.edu
J. Comput. Nonlinear Dynam. Jul 2011, 6(3): 031006 (8 pages)
Published Online: December 16, 2010
Article history
Received:
October 20, 2009
Revised:
July 2, 2010
Online:
December 16, 2010
Published:
December 16, 2010
Citation
Onawola, O. O., and Sinha, S. C. (December 16, 2010). "A Feedback Linearization Approach for Panel Flutter Suppression With Piezoelectric Actuation." ASME. J. Comput. Nonlinear Dynam. July 2011; 6(3): 031006. https://doi.org/10.1115/1.4002391
Download citation file:
Get Email Alerts
Numerical Simulation Method for the Rain-Wind Induced Vibration of the Three-Dimensional Flexible Stay Cable
J. Comput. Nonlinear Dynam
A Numerical Study for Nonlinear Time-Space Fractional Reaction-Diffusion Model of Fourth-Order
J. Comput. Nonlinear Dynam (March 2025)
An Investigation of Dynamic Behavior of Electric Vehicle Gear Trains
J. Comput. Nonlinear Dynam (March 2025)
Nonlinear Dynamic Analysis Framework for Slender Structures Using the Modal Rotation Method
J. Comput. Nonlinear Dynam (March 2025)
Related Articles
An Anti-Windup Design for Linear System With Asymptotic Tracking Subjected to Actuator Saturation
J. Dyn. Sys., Meas., Control (June,2000)
Receding Horizon Control for Constrained Markovian Jump Linear Systems With Bounded Disturbance
J. Dyn. Sys., Meas., Control (January,2011)
Nonfragile H ∞ Output Feedback Controller Design for Linear Systems
J. Dyn. Sys., Meas., Control (March,2003)
H ∞ Control for Continuous-Time Switched Linear Systems
J. Dyn. Sys., Meas., Control (July,2010)
Related Proceedings Papers
Related Chapters
QP Based Encoder Feedback Control
Robot Manipulator Redundancy Resolution
Norms of Feedback Systems
Robust Control: Youla Parameterization Approach
Feedback-Aided Minimum Joint Motion
Robot Manipulator Redundancy Resolution