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International Journal of Aerospace Engineering
Volume 2018 (2018), Article ID 7403639, 13 pages
https://doi.org/10.1155/2018/7403639
Research Article

A Two-Phased Guidance Law for Impact Angle Control with Seeker’s Field-of-View Limit

1Key Laboratory of Dynamic and Control of Flight Vehicle of the Ministry of Education, School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China
2Beijing Electro-Mechanical Engineering Institute, Beijing 100071, China

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

Received 25 July 2017; Revised 27 October 2017; Accepted 12 November 2017; Published 25 March 2018

Academic Editor: Hikmat Asadov

Copyright © 2018 Haoqiang Zhang 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.

How to Cite this Article

Haoqiang Zhang, Shengjing Tang, Jie Guo, and Wan Zhang, “A Two-Phased Guidance Law for Impact Angle Control with Seeker’s Field-of-View Limit,” International Journal of Aerospace Engineering, vol. 2018, Article ID 7403639, 13 pages, 2018. doi:10.1155/2018/7403639