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Author:

Wang, M. (Wang, M..) | Liu, Q. (Liu, Q..) | Zhao, T. (Zhao, T..) | Liu, J. (Liu, J..)

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Scopus

Abstract:

Flexible deployment mechanisms are widely used in the aerospace field. During the satellite antenna's attitude adjustment and deployment process, vibration will greatly affect the accuracy of the satellite antenna profile after deployment. The finite element method (FEM) has the disadvantages of high calculation order, slow calculation speed and difficult optimization in the process of establishing the dynamic model of the flexible deployment mechanism. This paper uses the principle of the transfer matrix method to propose a calculation method for the natural frequency and vibration mode of a flexible deployment mechanism, which is used to calculate the vibration characteristics of a radial rib deployment antenna. Finally, its accuracy is verified by the finite element method (FEM). © Published under licence by IOP Publishing Ltd.

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Author Community:

  • [ 1 ] [Wang M.]Institute of Intelligent Monitoring and Diagnosis, College of Mechanical Engineering and Applied Electronics Technology, Beijing University of Technology, Beijing, 100124, China
  • [ 2 ] [Wang M.]Beijing Municipal Key Laboratory of EDM Technology, Beijing, 100191, China
  • [ 3 ] [Liu Q.]Institute of Intelligent Monitoring and Diagnosis, College of Mechanical Engineering and Applied Electronics Technology, Beijing University of Technology, Beijing, 100124, China
  • [ 4 ] [Zhao T.]Institute of Intelligent Monitoring and Diagnosis, College of Mechanical Engineering and Applied Electronics Technology, Beijing University of Technology, Beijing, 100124, China
  • [ 5 ] [Liu J.]Institute of Intelligent Monitoring and Diagnosis, College of Mechanical Engineering and Applied Electronics Technology, Beijing University of Technology, Beijing, 100124, China

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ISSN: 1757-8981

Year: 2020

Issue: 1

Volume: 926

Language: English

Cited Count:

WoS CC Cited Count: 0

SCOPUS Cited Count:

ESI Highly Cited Papers on the List: 0 Unfold All

WanFang Cited Count:

Chinese Cited Count:

30 Days PV: 13

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