Remote Control Guidance Law Design Using Variable Structure Control
A method of sliding mode variable structure control for the missile body being a time varying system is presented. A remote control guidance law is designed. The method has strong robustness to target's maneuver. To reduce the chattering phenomena, quasi-sliding mode variable structure control method is used. Simulation results show that the proposed method has small miss distance for any kind of maneuvering targets and requires small control energy.
作 者： MENG Xiu-yun WANG Qi 作者单位： School of Mechatronic Engineering, Beijing Institute of Technology, Beijing 100081, China 刊 名： 北京理工大学学报(英文版) EI 英文刊名： JOURNAL OF BEIJING INSTITUTE OF TECHNOLOGY 年，卷(期)： 2006 15(1) 分类号： V249.12 关键词： remote control guidance law variable structure control sliding mode reaching mode