| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 757369 | Chinese Journal of Aeronautics | 2015 | 9 Pages |
Abstract
Thin-walled structures are sensitive to vibrate under even very small disturbances. In order to design a suitable controller for vibration suppression of thin-walled smart structures, an electro-mechanically coupled finite element (FE) model of smart structures is developed based on first-order shear deformation (FOSD) hypothesis. Considering the vibrations generated by various disturbances, which include free and forced vibrations, a PID control is implemented to damp both the free and forced vibrations. Additionally, an LQR optimal control is applied for comparison. The implemented control strategies are validated by a piezoelectric layered smart plate under various excitations.
Related Topics
Physical Sciences and Engineering
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Aerospace Engineering
Authors
Shunqi Zhang, Rüdiger Schmidt, Xiansheng Qin,