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Proceedings Paper

Proportional navigation law design of plane-symmetrical vehicle with terminal attack angle constraint for over target flight
Author(s): Bin Wu; Denggao Ji; Zhenxi Guo; Haibin Shen; Jianfei Zhang
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Paper Abstract

This article proposes a type of proportional navigation law design of plane-symmetrical vehicle with terminal attack angle constraint for over target flight. Firstly, the line of sight rotating rate and the velocity rotating rate model of the vehicle are expressed. Then, the attitude of the vehicle is constructed by the acceleration vector requirement of proportional navigation law. Accordingly, the guidance command uncertain issue can be avoided for plane-symmetrical vehicle over target flight. It guarantees high precision to hit the target. The effect and efficiency of the guidance law are shown by simulations of characteristic trajectories.

Paper Details

Date Published: 7 November 2016
PDF: 8 pages
Proc. SPIE 10141, Selected Papers of the Chinese Society for Optical Engineering Conferences held July 2016, 101410M (7 November 2016); doi: 10.1117/12.2256455
Show Author Affiliations
Bin Wu, Science and Technology on Space Physics Lab. (China)
Denggao Ji, Science and Technology on Space Physics Lab. (China)
Zhenxi Guo, Science and Technology on Space Physics Lab. (China)
Haibin Shen, Science and Technology on Space Physics Lab. (China)
Jianfei Zhang, Science and Technology on Space Physics Lab. (China)


Published in SPIE Proceedings Vol. 10141:
Selected Papers of the Chinese Society for Optical Engineering Conferences held July 2016
Yueguang Lv; Weimin Bao; Guangjun Zhang, Editor(s)

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