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The vibration suppression of solar panel based on smart structure
The Aeronautical Journal ( IF 1.4 ) Pub Date : 2020-06-22 , DOI: 10.1017/aer.2020.51
G. Ma , M. Xu , J. Tian , X. Kan

This paper provides a solution to the active vibration control of a microsatellite with two solar panels. At first, the microsatellite is processed as a finite element model containing a rigid body and two flexible bodies, according to the principles of mechanics, and that the dynamic characteristics are solved by modal analysis. Secondly, the equation involving vibration control is established according to the finite element calculation results. There are several actuators composed of macro fibre composite on the two solar panels for outputting control force. Furthermore, the control voltage for driving actuator is calculated by using fuzzy algorithm. It is clear that the smart structure consists of the flexible bodies and actuators. Finally, the closed-loop control simulation for suppressing harmful vibration is established. The simulation results illustrate that the responses to the external excitation are decreased significantly after adopting fuzzy control.

中文翻译:

基于智能结构的太阳能电池板振动抑制

本文提供了一种具有两个太阳能电池板的微型卫星的主动振动控制解决方案。首先,根据力学原理,将微卫星处理为一个包含一个刚体和两个柔性体的有限元模型,并通过模态分析求解其动力学特性。其次,根据有限元计算结果建立了涉及振动控制的方程。两块太阳能电池板上有多个由粗纤维复合材料组成的致动器,用于输出控制力。此外,驱动执行器的控制电压采用模糊算法计算。很明显,智能结构由柔性体和执行器组成。最后,建立了抑制有害振动的闭环控制仿真。
更新日期:2020-06-22
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