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Characteristic Model-based Discrete-time Sliding Mode Control for Spacecraft with Variable Tilt of Flexible Structures

Lei Chen Yan Yan Chaoxu Mu Changyin Sun

自动化学报（英文版）2016，Vol.3Issue(1)：42-50,9.

Characteristic Model-based Discrete-time Sliding Mode Control for Spacecraft with Variable Tilt of Flexible Structures

Lei Chen ¹Yan Yan ¹Chaoxu Mu ²Changyin Sun¹

作者信息

1. School of Automation, Southeast University, Nanjing 210096, China
2. Department of Electrical Engineering and Automation, Tianjin University, Tianjin 300072, China
折叠

摘要

关键词

Spacecraft/attitude maneuver/characteristic model/sliding mode control/finite time

Key words

Spacecraft/attitude maneuver/characteristic model/sliding mode control/finite time

引用本文复制引用

Lei Chen,Yan Yan,Chaoxu Mu,Changyin Sun..Characteristic Model-based Discrete-time Sliding Mode Control for Spacecraft with Variable Tilt of Flexible Structures[J].自动化学报（英文版）,2016,3(1):42-50,9.

基金项目

This work was supported by National Natural Science Foundation of China (61125306,91016004),Ph.D.Programs Foundation of Ministry of Education of China (20110092110020,20120092110026),and in part by the Post-Doctoral Research Funds (1108000137,3208004602). （61125306,91016004）

自动化学报（英文版）

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ISSN：2329-9266

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