JACIII Vol.19 No.2 pp. 301-306
doi: 10.20965/jaciii.2015.p0301


Cooperative Salvo Attack Using Guidance Law of Multiple Missiles

Jie Zeng, Lihua Dou, and Bin Xin

School of Automation, Key Laboratory of Intelligent Control and Decision of Complex Systems, Beijing Institute of Technology
Zhong Guan Cun South Street, Haidian District, Beijing 100081, China

Corresponding author

June 15, 2014
December 18, 2014
March 20, 2015
cooperative guidance, multi-missiles, proportional navigation, impact time, feedback
In this article, a guidance problem for cooperative salvo attack of multiple missiles against a single stationary target is investigated. The proposed guidance law combines the well-known PNG law and cooperative acceleration command, which is based on the feedback of state error between the current missile and the mean value of participant missiles. The state variable in this paper is used as the approximate calculation of time-to-go. The cooperative acceleration command is designed to adjust the flight path and impact time, which leads the multi-missiles to hit the common target simultaneously. During the engagement, the velocities of missiles are not changed and presetting impact time is not needed. Simulation results show the effectiveness of the proposed guidance law.
Cite this article as:
J. Zeng, L. Dou, and B. Xin, “Cooperative Salvo Attack Using Guidance Law of Multiple Missiles,” J. Adv. Comput. Intell. Intell. Inform., Vol.19 No.2, pp. 301-306, 2015.
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