A Model based Feedback Controller for Wing-twist Via Piezoceramic Actuation

Author

Cody W. Ray
Belinda A. Batten
John R. Singler, Missouri University of Science and TechnologyFollow

Abstract

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. © 2011 AACC American Automatic Control Council.

Recommended Citation

C. W. Ray et al., "A Model based Feedback Controller for Wing-twist Via Piezoceramic Actuation," Proceedings of the American Control Conference, pp. 2362 - 2367, article no. 5991258, Institute of Electrical and Electronics Engineers, Sep 2011.

Department(s)

Mathematics and Statistics

International Standard Book Number (ISBN)

978-145770080-4

International Standard Serial Number (ISSN)

0743-1619

Document Type

Article - Conference proceedings

Document Version

Citation

File Type

text

Language(s)

English

Rights

© 2024 Institute of Electrical and Electronics Engineers, All rights reserved.

Publication Date

30 Sep 2011