Optimal Control of Laminated Plate with Piezoelectric Sensor and Actuator Layers
β Scribed by Ray, M. C.
- Book ID
- 121787741
- Publisher
- American Institute of Aeronautics and Astronautics
- Year
- 1998
- Tongue
- English
- Weight
- 248 KB
- Volume
- 36
- Category
- Article
- ISSN
- 0001-1452
- DOI
- 10.2514/2.345
No coin nor oath required. For personal study only.
π SIMILAR VOLUMES
Vibration of a laminated composite plate is controlled by passive and active control methods. Stiffness change in composite structures by changes in laminate orientation is used as an example of a passive control method, negative velocity feedback control with the piezoelectric sensor/actuator is us
A&ret--We use the three-dimensional linear theory of elasticity to analyse the steady-state vibrations of a simply-supported rectangular linear elastic laminated plate with embedded PZT layers. Some of these PZT layers act as actuators while the remaining act as sensors. It is assumed that there is