3-DIMENSIONAL RESPONSE CHARACTERISTICS FOR SPACECRAFT WITH DEPLOYING FLEXIBLE APPENDAGES

被引：21

作者：

LIPS, KW

MODI, VJ

机构：

来源：

JOURNAL OF GUIDANCE AND CONTROL | 1981年 / 4卷 / 06期

关键词：

D O I：

10.2514/3.56123

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：650 / 656

页数：7

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[5]

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[7]

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[8] GENERAL DYNAMICS OF A LARGE CLASS OF FLEXIBLE SATELLITE SYSTEMS [J].

LIPS, KW ;

MODI, VJ .

[9]

LIPS KW, 1980, THESIS U BRIT COLUMB

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MODI, VJ .

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