Attitude Dynamics and Control for a Solar Sail with Individually Controllable Elements

被引：5
|
作者：
Luo, Tong [1 ]
Yao, Chuang [2 ]
Xu, Ming [1 ]
Qu, Qingyu [1 ]
机构：
[1] Beihang Univ, Sch Astronaut, Beijing 100191, Peoples R China
[2] Shanghai Inst Satellite Engn, Shanghai 201109, Peoples R China
来源：
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2019年 / 42卷 / 07期
基金：
中国国家自然科学基金;
关键词：
ORBITAL CONTROL; IKAROS;
D O I：
10.2514/1.G003957
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：1622 / 1629
页数：8
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