压电驱动器用于薄板型结构振动主动控制研究

ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2001, Vol. 22 ›› Issue (2): 109-112.

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ACTIVE VIBRATION CONTROL OF THIN PLATE WITH PIEZOELECTRIC ACTUATORS

CHEN Wei min, GUAND De, LI Min, ZHU De chao

Dept. of Flight Vehicle Design and Applied Mechanics, Beijing University of Aeronautics and Astraunotics, Beijing 100083, China

Received:1999-12-09 Revised:2000-05-30 Online:2001-04-25 Published:2001-04-25

Abstract

Abstract:

Analysis and experiments of the active vibration control to a plate with piezoelectric actuators are summarized. Both velocity feedback and linear quadratic Gauss(LQG) control were analyzed and tested. Digital control systems were designed and tested. Calculated and tested results are compared. The effect of mechanical electric coupling was also investigated.

Key words: piezoelectric actuator, coupling of mechanics electricity, damping, velocity feedback, optimal control

CLC Number:

V214.33
V249

CHEN Wei min;GUAND De;LI Min;ZHU De chao . ACTIVE VIBRATION CONTROL OF THIN PLATE WITH PIEZOELECTRIC ACTUATORS[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2001, 22(2): 109-112.

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ACTIVE VIBRATION CONTROL OF THIN PLATE WITH PIEZOELECTRIC ACTUATORS

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