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Shock and Vibration
Volume 2016 (2016), Article ID 2150493, 20 pages
http://dx.doi.org/10.1155/2016/2150493
Research Article

Observer Based Optimal Vibration Control of a Full Aircraft System Having Active Landing Gears and Biodynamic Pilot Model

1Department of Mechanical Engineering, Yildiz Technical University, Istanbul, Turkey
2Department of Mechatronics Engineering, Yildiz Technical University, Istanbul, Turkey

Received 28 March 2016; Revised 9 August 2016; Accepted 7 September 2016

Academic Editor: Mickaël Lallart

Copyright © 2016 Hakan Yazici and Mert Sever. 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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