ACTIVE ATTITUDE-CONTROL OF A SPINNING SYMMETRICAL SATELLITE IN AN ELLIPTIC ORBIT

被引：4

|

作者：

CALICO, RA

YEAKEL, GS

机构：

来源：

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 1983年 / 6卷 / 04期

关键词：

D O I：

10.2514/3.19836

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

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收藏

页码：315 / 320

页数：6

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