Abstract

In this paper we present a model for a plate-beam system to represent a bioinspired flexible wing. Using a Galerkin based finite element approximation to the system, we compute functional gains that can be used for sensor placement and show that a piezoceramic actuator on the beam can be used for camber control

Meeting Name

49th IEEE Conference on Decision and Control (2010: Dec. 15-17, Atlanta, GA)

Department(s)

Mathematics and Statistics

Keywords and Phrases

Mathematical model; Equations; Force; Biomembranes; Steady-state; Approximation methods

Document Type

Article - Conference proceedings

Document Version

Final Version

File Type

text

Language(s)

English

Rights

© 2010 Institute of Electrical and Electronics Engineers (IEEE), All rights reserved.

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