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Shock and Vibration
Volume 2018, Article ID 2870896, 11 pages
https://doi.org/10.1155/2018/2870896
Research Article

A Time-Domain Active Vibration Control Algorithm for Helicopter Based on a Prior Error Channel Identification Strategy

National Key Laboratory of Rotorcraft Aeromechanics, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

Correspondence should be addressed to Yang Lu; moc.361@gnayuljn

Received 7 August 2017; Revised 13 November 2017; Accepted 11 December 2017; Published 3 January 2018

Academic Editor: Enrico Zappino

Copyright © 2018 Yang Lu and Jianbo Feng. 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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