Inertia-Free Minimum-Angular-Motion Detumbling Control of Spacecraft

被引：8
|
作者：
Feng, Xiao [1 ]
Jia, Yinghong [1 ]
Xu, Shijie [1 ]
机构：
[1] Beihang Univ, Sch Astronaut, 37 Xueyuan Rd, Beijing 100191, Peoples R China
来源：
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2019年 / 42卷 / 03期
关键词：
D O I：
10.2514/1.G003813
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
[No abstract available]
引用
收藏
页码：678 / 683
页数：6
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