INFLUENCE OF FLEXIBLE APPENDAGES ON DUAL-SPIN SPACECRAFT DYNAMICS AND CONTROL

被引：23

作者：

GALE, AH

LIKINS, PW

机构：

来源：

关键词：

D O I：

10.2514/3.30101

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：1049 / &

共 17 条

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[6]

IORILLO AJ, 1965, NOV AM SOC MECH ENG

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Landon VD, 1964, J SPACECRAFT ROCKETS, V1, P682, DOI 10.2514/3.27725

[8]

Likins P.W., 1968, 19 INT ASTR C

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LIKINS, PW .

[10] ATTITUDE STABILITY CRITERIA FOR DUAL SPIN SPACECRAFT [J].

LIKINS, PW .