Terminal sliding mode guidance law with impact angle constraints

摘要：

　　In this article, a guidance law is developed using the terminal sliding model control theory.The law can generate high-performance when intercepts maneuvering targets.A sliding model estimator also be presented to estimate the line-of-sight angle rate which the guidance law is required.According to the Lyapunov theory, the guidance law can be converge to zero is proved.Several simulations are made to validate the effectiveness of proposed guidance law.

关键词： Terminal sliding mode control Guidance law Guided projectile

作者: Jun GUAN Wen-jun YI Dan-dan YUAN Zhen-dong LIANG

作者单位: School of Automation, Nanjing University of Science & Technology, Nanjing, Jiangsu, China;National K National Key Laboratory of Transient Physics, Nanjing University of Science & Technology, Nanjing, J

会议类型: 国际会议

会议名称: 2018 International Conference on Defence Technology (2018国际防务技术会议)

会议地点: 北京

会议语种:英文

页码: 925-929

在线出版日期: 2018-10-21（万方平台首次上网日期，不代表论文的发表时间）