DYNAMICS OF A SPACECRAFT DURING EXTENSION OF FLEXIBLE APPENDAGES

被引：30
|
作者：
TSUCHIYA, K
机构：
来源：
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 1983年 / 6卷 / 02期
关键词：
D O I：
10.2514/3.56343
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：100 / 103
页数：4
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