Fully Actuated Flexible Spacecraft Attitude Control With Input Constraint

被引：0
|
作者：
Wang, Dian [1 ]
Wu, Yun-Hua [1 ]
Yue, Cheng-Fei [2 ,3 ]
Ma, Song-Jing [1 ]
机构：
[1] School of Astronautics, Nanjing University of Aeronautics and Astronautics, Nanjing,211100, China
[2] Institute of Space Science and Applied Technology, Harbin Institute of Technology, Shenzhen,518055, China
[3] National Key Laboratory of Micro-Spacecraft Rapid Design and Intelligent Cluster, Harbin Institute of Technology, Harbin,150001, China
来源：
Zidonghua Xuebao/Acta Automatica Sinica | 2024年 / 50卷 / 11期
关键词：
25;
D O I：
10.16383/j.aas.c230691
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：2177 / 2187
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