Adaptive Sliding Mode Control for Missile Guidance Law

摘要：

　　The problem of missile interception is investigated in this paper.Sliding mode controllers are proposed for the design of guidance laws.Specially,the control design consists of the estimation of the target acceleration by adaptive scheme and thus it achieves the decrease of undesired chattering effectively.Also,simulation results are presented to illustrate the effectiveness of the control strategies.

关键词： Guidance law Sliding mode control Adaptive control

作者: Xiangyang Wu Shihua Bi Zheng Zhu Weinan Wu

作者单位: School of Aerospace Engineering,Beijing Institute of Technology,Beijing 100081,P.R.China;Beijing Ins School of Aerospace Engineering,Beijing Institute of Technology,Beijing 100081,P.R.China Beijing Institute of Specialized Machinery,Beijing 100143,P.R.China

会议类型: 国际会议

会议名称: The 33th Chinese Control Conference第33届中国控制会议

会议地点: 南京

会议语种:英文

页码: 960-965

在线出版日期: 2014-07-28（万方平台首次上网日期，不代表论文的发表时间）