On-off Guidance Law Design for Exo-atmospheric Interceptor via Nonsmooth Linear Lipschitz Thresholds

摘要：

On-off guidance law design problem of terminal guidance system is studied for exo-atmospheric interceptor with pulse divert thrusters.Nonsmooth linear Lipschitz thresholds are constructed due to the relative motion equations of the missile and the target.The dynamics of the closed-loop system is described in the sense of Filippovs differential inclusion since the pulse control input is discontinuous,thus the stability of the terminal guidance system is analyzed with contingent cone criteria in the frame of nonsmooth analysis.Finally,the validity of the method and its superiority in decreasing the on-off counts of the divert thruster are illustrated by a numerical simulation.

作者: HUO Xin YANG Baoqing XIE Ruiqiang YAO Yu

作者单位: Control and Simulation Center,Harbin Institute of Technology,Harbin 150080,P.R.China

会议类型: 国际会议

会议名称: The 30th Chinese Control Conference(第三十届中国控制会议)

会议地点: 烟台

会议语种:英文

页码: 1-5

在线出版日期: 2011-07-01（万方平台首次上网日期，不代表论文的发表时间）