A Model Based Feedback Controller for Wing-Twist Via Piezoceramic Actuation

Cody W. Ray; Belinda A. Batten; John R. Singler

doi:10.1109/ACC.2011.5991258

A Model Based Feedback Controller for Wing-Twist Via Piezoceramic Actuation

Cody W. Ray
, Belinda A. Batten
, John R. Singler

Mathematics and Statistics

School of Chemical, Biological and Environmental Engineering, Oregon State University

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

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.

Original language	American English
Title of host publication	Proceedings of the 2011 American Control Conference, ACC 2011
Pages	2362-2367
Number of pages	6
DOIs	https://doi.org/10.1109/ACC.2011.5991258
State	Published - Jan 1 2011
Event	2011 American Control Conference, ACC 2011 - San Francisco, CA, United States Duration: Jun 29 2011 → Jul 1 2011

Publication series

Name	Proceedings of the 2011 American Control Conference (2011: June 29 - July 1, San Francisco, CA)

Conference

Conference	2011 American Control Conference, ACC 2011
Country/Territory	United States
City	San Francisco, CA
Period	6/29/11 → 7/1/11

ASJC Scopus Subject Areas

Electrical and Electronic Engineering

Disciplines

Mathematics
Statistics and Probability

Access to Document

10.1109/ACC.2011.5991258License: Unspecified

A Model Based Feedback Controller for Wing-Twist Via PiezoceramicFinal published version, 1.49 MBLicense: Unspecified

Cite this

A Model Based Feedback Controller for Wing-Twist Via Piezoceramic Actuation. / Ray, Cody W.; Batten, Belinda A.; Singler, John R.
Proceedings of the 2011 American Control Conference, ACC 2011. 2011. p. 2362-2367 5991258 (Proceedings of the 2011 American Control Conference (2011: June 29 - July 1, San Francisco, CA)).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

Ray, CW, Batten, BA & Singler, JR 2011, A Model Based Feedback Controller for Wing-Twist Via Piezoceramic Actuation. in Proceedings of the 2011 American Control Conference, ACC 2011., 5991258, Proceedings of the 2011 American Control Conference (2011: June 29 - July 1, San Francisco, CA), pp. 2362-2367, 2011 American Control Conference, ACC 2011, San Francisco, CA, United States, 6/29/11. https://doi.org/10.1109/ACC.2011.5991258

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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.",

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A Model Based Feedback Controller for Wing-Twist Via Piezoceramic Actuation

Abstract

Publication series

Conference

ASJC Scopus Subject Areas

Disciplines

Access to Document

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