Research on Midcourse Maneuvering Penetration Guidance Law of Ballistic Missile Based on Genetic Algorithm
The maneuvering penetration guidance law in the middle-course flight of the strategic missile is developed by simulation method in this paper. A maneuvering penetration scheme based on detect system is presented and researched. Based on calculation to maneuvering penetration time with Genetic Algorithm, a new type of optimal penetration guidance law is presented. The optimal, earliest and latest maneuvering penetration time calculating optimization models are designed. Finally, the penetration-interception simulated system based on those models is built, the simulation experiments show the guidance law feasible and effective, and its results are analyzed.
maneuvering penetration strategic missile penetration guidance law Genetic Algorithm
XIAN Yong SI Wen-hui
Xian Research Institute of Hi-Tech,Hongqing Town Xian,Shaanxi Province,P.R China
国际会议
上海
英文
1091-1094
2009-11-20（万方平台首次上网日期，不代表论文的发表时间）