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Cooperative Guidance for Multimissile Salvo Attack

Cooperative Guidance for Multimissile Salvo Attack

作     者:Zhao Shiyu Zhou Rui 

作者机构:School of Automation Science and Electrical Engineering Beijing University of Aeronautics and Astronautics Beijing 100191 China 

出 版 物:《Chinese Journal of Aeronautics》 (中国航空学报(英文版))

年 卷 期:2008年第21卷第6期

页      面:533-539页

核心收录:

学科分类:08[工学] 0825[工学-航空宇航科学与技术] 

基  金:Foundation items: National Natural Science Foundation of China (60674103) Aeronautical Science Foundation of China (2006ZC51026) 

主  题:cooperative guidance impact time constraints multiple missiles salvo attack 

摘      要:Cooperative guidance problems of multiple missiles are considered in this article. A cooperative guidance scheme, where coordination algorithms and local guidance laws are combined together, is proposed. This scheme actually builds up a hierarchical cooperative guidance architecture, which may provide a general solution to the multimissile cooperative guidance problems. In the case of salvo attacks which require missiles to hit the target simultaneously, both centralized and distributed coordination algorithms are derived based on the impact-time-control guidance (ITCG) law. Numerical simulations are performed to demonstrate the effectiveness of the proposed approaches.

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