卫星太阳能帆板振动抑制研究  

A Study on the Active Vibration Control of Satellite Solar Panel Substrate

作　　者：刘安成[1] 吴大方[1] 高镇同[1] 黄海[2] 

机构地区：[1]北京航空航天大学飞行器设计与应用力学系,北京100083 [2]北京航空航天大学宇航学院,北京100083

出　　处：《实验力学》2002年第4期477-482,共6页Journal of Experimental Mechanics

基　　金：国家863项目(863-2-14-1-13)

摘　　要：太阳能帆板是给航天器提供能源的重要装置,以压电陶瓷为做动器的智能结构可以有效地抑制卫星太阳能帆板在太空中的振动.基于Hamilton变分原理,推导得到含多个压电陶瓷片的太阳能帆板模型的振动方程.制作了太阳能帆板振动主动控制实验系统,并对太阳能帆板模型进行振动主动控制实验.实验结果表明该控制系统可大幅度降低卫星太阳能帆板的振动,延长其使用寿命.Solar panel substrate is the important energy provider for the spacecraft, and its vibration can be effectively suppressed by the use of piezoelectric (PZT) actuators. Based on the extended Hamilton principle, the vibration equation of the solar panel substrate modal containing several PZT actuators is derived. An experimental system for vibration active control is designed according to the vibration equation, and the active vibration control experiment is performed. The experimental results show that the vibration of the solar panel substrate is reduced significantly and the life of the solar panel substrate is prolonged.

关 键 词：压电陶瓷 振动主动控制 太阳能帆板 智能结构 

分 类 号：TB535[理学—物理]