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Piezothermoelastic Modeling and Active Vibration Control of Laminated Composite Beams

Raja, S. and Rohwer, K. and Rose, M. (2000) Piezothermoelastic Modeling and Active Vibration Control of Laminated Composite Beams. Journal of Intelligent Material Systems and Structures, 10 (11), pp. 890-899.

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Abstract

A generalized piezothermoelastic finite element formulation of a laminated beam with embedded piezoelectric material as distributed actuators/sensors is presented. Electromechanical and electrothermal couplings are incorporated using the linear equations of piezothermoeleasticity. Inclusion of temperature and electric potential as state variables along with mechanical displacement permits a unified representation of multiple fields coupling in finite element formulations. A two noded 3-D beam element is derived using first order shear deformation theory to model direct and coupled effects. Eigenstructure assignment technique using output feedback is employed in the controller design, which is subsequently adopted to actively control the first three modes of a cantilever PZT/Steel/PZT beam. The desired eigenfrequencies are placed exactly and the tip motion of the beam is significantly reduced by shaping the eigenvectors of the closed-loop system. Control spillover effect is minimized by optimally selecting the actuator/sensor locations and optimizing the damping factors of the desired closed-loop eigenvalues.

Document Type:Article
Additional Information: LIDO-Berichtsjahr=2000,
Title:Piezothermoelastic Modeling and Active Vibration Control of Laminated Composite Beams
Authors:
AuthorsInstitution or Email of Authors
Raja, S.UNSPECIFIED
Rohwer, K.UNSPECIFIED
Rose, M.UNSPECIFIED
Date:2000
Journal or Publication Title:Journal of Intelligent Material Systems and Structures
Refereed publication:Yes
In ISI Web of Science:Yes
Volume:10
Page Range:pp. 890-899
Status:Published
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:Aeronautics
DLR - Program:L DT - Drehflüglertechnologien
DLR - Research theme (Project):UNSPECIFIED
Location: Braunschweig
Institutes and Institutions:Institute of Composite Structures and Adaptive Systems > Institut für Strukturmechanik
Deposited By: Sibylle Wolff
Deposited On:16 Sep 2005
Last Modified:14 Jan 2010 15:59

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