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Discrete Dynamics in Nature and Society
Volume 2016, Article ID 6219609, 10 pages
http://dx.doi.org/10.1155/2016/6219609
Research Article

Guidance Law and Neural Control for Hypersonic Missile to Track Targets

School of Astronautics, Northwestern Polytechnical University, Xi’an 710072, China

Received 17 October 2015; Revised 22 December 2015; Accepted 14 January 2016

Academic Editor: Filippo Cacace

Copyright © 2016 Wenxing Fu 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.

Citations to this Article [1 citation]

The following is the list of published articles that have cited the current article.

  • Zijun Ren, Wenxing Fu, Jie Yan, and Bin Xu, “Discrete reconfigurable back-stepping attitude control of reentry hypersonic flight vehicle,” Advances in Mechanical Engineering, vol. 9, no. 4, pp. 168781401770390, 2017. View at Publisher · View at Google Scholar