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International Journal of Aerospace Engineering
Volume 2018, Article ID 5045740, 17 pages
https://doi.org/10.1155/2018/5045740
Research Article

Research on Microvibrations Generated by a Control Moment Gyroscope on a Flexible Interface Based on a Dynamic Substructure Method

School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

Correspondence should be addressed to Xiongfei Li; moc.361@8090il_iefgnoix

Received 20 July 2017; Accepted 15 January 2018; Published 8 April 2018

Academic Editor: Christopher J. Damaren

Copyright © 2018 Xiongfei Li and Wei Cheng. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

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