Optimal Size and Location of Piezoelectric Actuator/Sensors: Practical Considerations
Author:
Affiliation:
1. King Saud University, Riyadh 11421, Saudi Arabia
2. State University of New York, Buffalo, New York 14260-4400
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.4557
Reference25 articles.
1. Tzou, H. S., and Anderson, G. L., Intelligent Structural Systems, Kluwer Academic, Norwell, MA, 1992, pp.75-244.
2. Detailed Models of Piezoceramic Actuation of Beams
3. Distributed piezoelectric-polymer active vibration control of a cantilever beam
4. Theory of laminated piezoelectric plates for the design of distributed sensors/actuators. Part I: Governing equations and reciprocal relationships
5. Lee, C. K. “Piezoelectric Laminates for Torsional and Bending Modal Control: Theory and Experiment,” Ph.D. Dissertation,Cornell Univ., Ithaca, NY, 1987.
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