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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