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：

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

页码：678 / 683

页数：6

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