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International Journal of Aerospace Engineering
Volume 2017, Article ID 8181743, 18 pages
https://doi.org/10.1155/2017/8181743
Research Article

Tendon-Sheath Mechanisms in Flexible Membrane Wing Mini-UAVs: Control and Performance

School of Mechanical and Aerospace Engineering, Nanyang Technological University, 50 Nanyang Avenue, North Spine (N3), Singapore 639798

Correspondence should be addressed to Tegoeh Tjahjowidodo; gs.ude.utn@heogett

Received 9 February 2017; Accepted 1 June 2017; Published 24 July 2017

Academic Editor: Mahmut Reyhanoglu

Copyright © 2017 Tegoeh Tjahjowidodo and Shian Lee. 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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