In this paper we present a model for a rubber plate with piezoceramic actuators to represent a bioinspired flexible wing. Using a Galerkin based finite element approximation to the system, we compute a linear quadratic based tracking control for piezoelectric actuators placed along both leading and trailing edges. Using these piezoceramic devices, we demonstrate the effectiveness of model based feedback control in achieving a desired wing tip position; this modified shape is analogous to aircraft roll moment generation via wing twist.
J. R. Singler and B. A. Batten, "A Model Based Feedback Controller for Wing-Twist Via Piezoceramic Actuation," Proceedings of the 2011 American Control Conference (2011: June 29 - July 1, San Francisco, CA), Institute of Electrical and Electronics Engineers (IEEE), Jan 2011.
The definitive version is available at https://doi.org/10.1109/ACC.2011.5991258
2011 American Control Conference (2011: June 29 - July 1, San Francisco, CA)
Mathematics and Statistics
Article - Conference proceedings
© 2011 Institute of Electrical and Electronics Engineers (IEEE), All rights reserved.
01 Jan 2011