Logic-based Switching Control Strategy Design of a Spinning Missile with Blended Lateral Jets and Aerodynamic Fins

摘要：

In this paper, for a missile with blended lateral jets and aerodynamic fins, output tracking is realized by a switching control in a hybrid control architecture. The switching control strategy is divided into four phases in terms of practical guidance and control course. The switching conditions, from one phase to another, are given. Lateral jets and aerodynamic fins are adopted separately in respective phases. In the phase of lateral jets, model predictive control, based on Fliess functional expansion, is used to determine the firing logic, while in the phase of aerodynamic fins, asymptotic output tracking control, based on exact linearization, is used to design a continuous output tracking control law. Simulation results show the effectiveness of the proposed method.

作者: He Fenghua Ma Kemao Yao Yu Ma Jie

作者单位: Hefenghua is with Faculty of Control and Simulation Center,Harbin Institute of Technology,150080,China

会议类型: 国际会议

会议名称: The 2nd International Symposium on Systems and Control in Aeronautics and Astronautics(第二届航空航天系统与控制国际会议 ISSCAA 2008)

会议地点: 深圳

会议语种:英文

页码: 629-634

在线出版日期: 2008-12-10（万方平台首次上网日期，不代表论文的发表时间）