Adaptive sliding mode control for spacecraft attitude tracking system

被引：0
|
作者：
Li, Long [1 ]
Hou, Jian-Wen [2 ]
Shi, Xiao-Ping [1 ]
Yang, Jing [1 ]
机构：
[1] School of Astronautics, Harbin Institute of Technology, Harbin,150080, China
[2] Shanghai Academy of Spaceflight Technology, Shanghai,201109, China
来源：
Dianji yu Kongzhi Xuebao/Electric Machines and Control | 2015年 / 19卷 / 02期
关键词：
D O I：
10.15938/j.emc.2015.02.015
中图分类号：
学科分类号：
摘要：
13
引用
收藏
页码：96 / 100
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