ATTITUDE DYNAMICS OF SATELLITES WITH FLEXIBLE APPENDAGES - BRIEF REVIEW

被引：82

作者：

MODI, VJ ^{[1
]}

机构：

[1] UNIV BRITISH COLUMBIA,VANCOUVER,BRITISH COLUMBI,CANADA

来源：

JOURNAL OF SPACECRAFT AND ROCKETS | 1974年 / 11卷 / 11期

关键词：

D O I：

10.2514/3.62172

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：743 / 751

页数：9

相关论文

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