EFFECT OF A ROTOR ON ATTITUDE STABILITY OF A SATELLITE IN A CIRCULAR ORBIT

被引：18
|
作者：
KANE, TR
MINGORI, DL
机构：
来源：
AIAA JOURNAL | 1965年 / 3卷 / 05期
关键词：
D O I：
10.2514/3.3018
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
引用
收藏
页码：936 / &
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