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   作者單位： School of Mechatronic Engineering, Beijing Institute of Technology, Beijing 100081, China  刊 名： 北京理工大學(xué)學(xué)報(bào)(英文版)  EI 英文刊名： JOURNAL OF BEIJING INSTITUTE OF TECHNOLOGY  年，卷(期)： 2006 15(1)  分類號(hào)： V249.12  關(guān)鍵詞： remote control guidance law   variable structure control   sliding mode   reaching mode  

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