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Shock and Vibration
Volume 2015, Article ID 348971, 11 pages
http://dx.doi.org/10.1155/2015/348971
Research Article

GPC-Based Gust Response Alleviation for Aircraft Model Adapting to Various Flow Velocities in the Wind Tunnel

School of Aeronautic Science and Engineering, Beihang University, Beijing 100191, China

Received 21 February 2015; Revised 27 April 2015; Accepted 17 May 2015

Academic Editor: Sakdirat Kaewunruen

Copyright © 2015 Yuting Dai and Chao Yang. 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.

How to Cite this Article

Yuting Dai and Chao Yang, “GPC-Based Gust Response Alleviation for Aircraft Model Adapting to Various Flow Velocities in the Wind Tunnel,” Shock and Vibration, vol. 2015, Article ID 348971, 11 pages, 2015. https://doi.org/10.1155/2015/348971.