Optimal Zero-Sliding Midcourse Guidance with an Observer for Missiles

摘要：

We address an observer-based optimal zero-sliding midcourse guidance for missiles with thrust vector control and divert control system for the interception of a theater ballistic missile. First, a 3 degree-of-freedom observer-based optimal zero-sliding midcourse guidance law is designed to minimize the control effort and to narrow the distance between the missile and the target. Then, the exponential stability of the overall system is analyzed thoroughly via Lyapunov stability theory. Finally, successful simulations are developed to verify the effectiveness of the proposed guidance law.

关键词： optimal control zero sliding observer based target tracking

作者: FK Yeh KY Kou CW Huang

作者单位: Chung Chou University of Science and Technology, Changhua National Central Police University, Taoyuan

会议类型: 国际会议

会议名称: The 31st Chinese Control Conference(第三十一届中国控制会议)

会议地点: 合肥

会议语种:英文

页码: 1018-1023

在线出版日期: 2012-07-01（万方平台首次上网日期，不代表论文的发表时间）