Direct/aerodynamic force sliding mode variable structure compound control for terminal interceptor missile

摘要：

　　The compound control system of the side direct force and aerodynamic force of the terminal interceptor missile is studied.First, a compound control model of direct force and aerodynamic force is established.Then, based on the sliding mode variable structure control theory, a direct force/aerodynamic compound control system is designed.Finally, the design of the compound control system is verified by the simulation analysis.Compound control is able to make up for the lack of aerodynamic overload of missile terminal guidance, and improve the reaction time of the system.

关键词： Direct/aerodynamic force Sliding mode variable structure Compound control

作者: Jian-qiang ZHENG Qing-hua MA Shu-jun YANG Shuai-wei WANG

作者单位: Xian Advanced Control Technologies Research Institute, Xian 710065, China

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: 922-924

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）