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Volume 26 Issue 1
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Journal of Beijing University of Aeronautics and Astronautics  > 2000  >  26(1): 87-90.
FANG You-liang, WU Zhe. Active Vibration Control of Smart Plate with SelfSensing Piezoelectric Actuators[J]. Journal of Beijing University of Aeronautics and Astronautics, 2000, 26(1): 87-90. (in Chinese)
Citation: FANG You-liang, WU Zhe. Active Vibration Control of Smart Plate with SelfSensing Piezoelectric Actuators[J]. Journal of Beijing University of Aeronautics and Astronautics, 2000, 26(1): 87-90. (in Chinese)
shu

Active Vibration Control of Smart Plate with SelfSensing Piezoelectric Actuators

  • Beijing University of Aeronautics and Astronautics,Dept. of Flight Vehicle Design and Applied Mechanics

  • Received Date: 23 Oct 1998
  • Publish Date: 31 Jan 2000
    Abstract
  • For the four laterals simply supported plate, the transverse deflection of plate is expanded over the modal shapes, the electroelastic model with self-sensing actuators plate is given, and the current is considered as output variable of measurement equation. Generalized modal coordinates being state variables, LQG and H∞control is proceeded using the state space equation. In this paper, a self-sensing thin plate with three pairs piezoelectric films is bonded on the surface of base structure, the H∞ control solution is compared with that of LQG control. Singular value curve of system is given, velocity and displacement responses of one location in the plate are drawn, and applied voltages for actuators are given. The simulation solution illustrates the effectiveness of the control method in this paper.

     

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    • References(1)
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