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Mathematical Problems in Engineering
Volume 2013, Article ID 313197, 11 pages
http://dx.doi.org/10.1155/2013/313197
Research Article

Optimal Ascent Guidance for Air-Breathing Launch Vehicle Based on Optimal Trajectory Correction

Key Laboratory of Ministry of Education for Image Processing and Intelligent Control, School of Automation, Huazhong University of Science and Technology, Wuhan 430074, China

Received 14 October 2013; Revised 28 October 2013; Accepted 28 October 2013

Academic Editor: Hui Zhang

Copyright © 2013 Xuefang Lu 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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