SINGLE-AXIS SPACECRAFT ATTITUDE MANEUVERS USING AN OPTIMAL REACTION WHEEL POWER CRITERION

被引：5
|
作者：
SKAAR, SB
KRAIGE, LG
机构：
来源：
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 1982年 / 5卷 / 05期
关键词：
D O I：
10.2514/3.56200
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：543 / 544
页数：2
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