Remote Control Guidance Law Design U

時間:2023-04-27 19:35:42 航空航天論文 我要投稿
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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: 北京理工大學學報(英文版)  EI 英文刊名: JOURNAL OF BEIJING INSTITUTE OF TECHNOLOGY  年,卷(期): 2006 15(1)  分類號: V249.12  關鍵詞: remote control guidance law   variable structure control   sliding mode   reaching mode  

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