Advanced Search

Journal Navigation

Journal Home

Subscriptions

Archive

Contact Us

Table of Contents

SAGETRACK

Sign In to gain access to subscriptions and/or personal tools.
Journal of Intelligent Material Systems and Structures
This Article
Right arrow Full Text (PDF)
Right arrow References
Right arrow Alert me when this article is cited
Right arrow Alert me if a correction is posted
Right arrow Citation Map
Services
Right arrow Email this article to a friend
Right arrow Similar articles in this journal
Right arrow Alert me to new issues of the journal
Right arrow Add to Saved Citations
Right arrow Download to citation manager
Right arrowRequest Permissions
Right arrow Request Reprints
Right arrow Add to My Marked Citations
Citing Articles
Right arrow Citing Articles via HighWire
Right arrow Citing Articles via Google Scholar
Right arrow Citing Articles via Scopus
Google Scholar
Right arrow Articles by Raja, S.
Right arrow Articles by Rose, M.
Right arrow Search for Related Content
Social Bookmarking
 Add to CiteULike   Add to Complore   Add to Connotea   Add to Del.icio.us   Add to Digg   Add to Reddit   Add to Technorati   Add to Twitter  
What's this?

Piezothermoelastic Modeling and Active Vibration Control of Laminated Composite Beams

S. Raja

K. Rohwer

M. Rose

DLR, InstitutfUr Strukturmechanik, Lilienthalplatz 7, D-38108 Braunschweig, Germany

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 piezothermoelasticity. 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.

Journal of Intelligent Material Systems and Structures, Vol. 10, No. 11, 890-899 (1999)
DOI: 10.1106/GPPM-H4FU-8WUE-G63K


Add to CiteULike CiteULike   Add to Complore Complore   Add to Connotea Connotea   Add to Del.icio.us Del.icio.us   Add to Digg Digg   Add to Reddit Reddit   Add to Technorati Technorati   Add to Twitter Twitter    What's this?


This article has been cited by other articles:


Home page
Journal of Intelligent Material Systems and StructuresHome page
C. Ying and S. Zhifei
Exact Solutions of Functionally Gradient Piezothermoelastic Cantilevers and Parameter Identification
Journal of Intelligent Material Systems and Structures, June 1, 2005; 16(6): 531 - 539.
[Abstract] [PDF]


Home page
Journal of Reinforced Plastics and CompositesHome page
S. Raja, D. Dwarakanathan, P. K. Sinha, and G. Prathap
Bending Behavior of Piezo-Hygrothermo-Elastic Smart Laminated Composite Flat and Curved Plates with Active Control
Journal of Reinforced Plastics and Composites, February 1, 2004; 23(3): 265 - 290.
[Abstract] [PDF]


Home page
Journal of Reinforced Plastics and CompositesHome page
S. Raja, P. K. Sinha, and G. Prathap
Active Stiffening and Active Damping Effects on Closed Loop Vibration Control of Composite Beams and Plates
Journal of Reinforced Plastics and Composites, August 1, 2003; 22(12): 1101 - 1121.
[Abstract] [PDF]