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Mathematical Problems in Engineering
Volume 2015 (2015), Article ID 648231, 19 pages
http://dx.doi.org/10.1155/2015/648231
Research Article

Integrated Guidance and Control Method for the Interception of Maneuvering Hypersonic Vehicle Based on High Order Sliding Mode Approach

1College of Astronautics, Northwestern Polytechnical University, Xi’an 710072, China
2Flight Automation Control Research Institute, Xi’an 710065, China

Received 27 April 2015; Revised 26 July 2015; Accepted 29 July 2015

Academic Editor: Giuseppe Rega

Copyright © 2015 Kang Chen 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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