A New Guidance Law Based on Information Fusion and Optimal Control of Structure Stochastic Jump System
Based on multisensor information fusion theory and optimal control theory of structure stochastic jump system,a new guidance law is proposed for air-to-air missiles based on information fusion of active radar and infrared sensor,and its validity is testified by analysis on simulation by building digital model of missiles.Compared with proportion navigation law and extended proportion navigation law based on radar or infrared through many Monte Carlo simulations,the results show that the new guidance law reduces errors of tracking target and has smooth trajectory and small over-load,and it is important to theory and engineering application.
multisensor information fusion structure stochastic jump system optimal control proportional navigation extended proportional navigation
Xianwei Zeng Yangwang Fang Youli Wu Hongqiang Wang Xiaobin Zhou Zenghui Xie
Department of Aviation Weapon Engineering University of Air Force Engineering Xian, Shaanxi Province, China
国际会议
2007 IEEE International Conference on Automation and Lofistics
山东济南
英文
2007-08-18(万方平台首次上网日期,不代表论文的发表时间)