COORDINATE TRANSFORMATION AND TRUNCATION FOR ROTATING SPACECRAFT WITH FLEXIBLE APPENDAGES

被引：1
|
作者：
LIKINS, P [1 ]
OHKAMI, Y [1 ]
机构：
[1] UNIV CALIF,LOS ANGELES,CA 90024
来源：
AIAA JOURNAL | 1975年 / 13卷 / 12期
关键词：
D O I：
10.2514/3.7042
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：1657 / 1665
页数：9
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