Motion Tracking Sliding-Mode Guidance for Threat Avoidance of Homing Missile

摘要：

A new Guidance law based on motion tracking sliding- mode control method is presented for the terminal guidance of homing missile. This guidance law makes the line-of-sight (LOS) track an arbitrarily given signal so that own missile actuates effective maneuvers to avoid the threat from enemy missile and in mean while intercept the target accurately. Moreover, for a homing missile with passive seeker, the guidance law is able to enhance the obervability of bearings-only target tracking and is robust against target maneuvers and guidance parameter errors.

作者: Zhou Di Hu Hengzhang

作者单位: Department of Control Science and Engineering, Harbin Institute of Technology

会议类型: 国际会议

会议名称: 2007国际导航制导控制学术会议

会议地点: 北京

会议语种:英文

页码: 84-87

在线出版日期: 2007-11-04（万方平台首次上网日期，不代表论文的发表时间）