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The vibration suppression of solar panel based on smart structure

Part of: International Symposium on Smart Aircraft 2019 Collection Smart Aircraft

Published online by Cambridge University Press:  22 June 2020

G. Ma Open the ORCID record for G. Ma [Opens in a new window] ,
M. Xu ,
J. Tian  and
X. Kan
G. Ma*
Affiliation:
School of Mechatronic Engineering, Xi’an Technological University, Xi’an, China State Key Laboratory for Strength and Vibration of Mechanical Structures, School of Aerospace, Xi’an Jiaotong University, Xi’an, China
M. Xu
Affiliation:
State Key Laboratory for Strength and Vibration of Mechanical Structures, School of Aerospace, Xi’an Jiaotong University, Xi’an, China
J. Tian
Affiliation:
School of Mechatronic Engineering, Xi’an Technological University, Xi’an, China
X. Kan
Affiliation:
School of Mechanical and Precision Instrument Engineering, Xi’an University of Technology, Xi’an, China
*
qiuyexinjun@xatu.edu.cn
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Abstract

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.

Keywords

MicrosatelliteAVCsmart structureMFC

Information

Type
Research Article
Information
The Aeronautical Journal , Volume 125 , Issue 1283 , January 2021 , pp. 244 - 255
Copyright
© The Author(s), 2020. Published by Cambridge University Press on behalf of Royal Aeronautical Society

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References

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