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International Journal of Aerospace Engineering
Volume 2018, Article ID 9875462, 12 pages
https://doi.org/10.1155/2018/9875462
Research Article

Robust Smooth Sliding-Mode-Based Controller with Fixed-Time Convergence for Missiles considering Aerodynamic Uncertainty

School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China

Correspondence should be addressed to Jie Guo; nc.ude.tib@1891eijoug

Received 13 November 2017; Revised 6 March 2018; Accepted 22 March 2018; Published 14 June 2018

Academic Editor: Linda L. Vahala

Copyright © 2018 Yuhang Yun et al. 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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