Anti-unwinding terminal sliding mode attitude tracking control for rigid spacecraft

被引：0
|
作者：
Su, Yuxin [1 ]
机构：
[1] Xidian Univ, Sch Electromech Engn, Xian 710071, Peoples R China
来源：
AUTOMATICA | 2023年 / 156卷
关键词：
Unwinding phenomenon; Rigid spacecraft; Quaternion; Attitude tracking control;
D O I：
10.1016/j.automatica.2023.111205
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
The proposed control of Dong et al. (2022) contains three flaws, making some of the claims questionable. (c) 2023 Published by Elsevier Ltd.
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页数：2
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