RIGID BODY MODE POINTING ACCURACY AND STABILITY-CRITERIA FOR AN ORBITING SPACECRAFT

被引：2

作者：

SANDHU, GS ^{[1
]}

机构：

[1] TELEDYNE BROWN ENGN,ELECTR & ENGN DIV,HUNTSVILLE,AL 35800

来源：

JOURNAL OF SPACECRAFT AND ROCKETS | 1974年 / 11卷 / 08期

关键词：

D O I：

10.2514/3.62134

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：599 / 601

页数：3

共 28 条

[1] POINTING PERFORMANCE INVESTIGATION OF A MULTIPLE RIGID BODY SPACECRAFT
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[J]. IEEE TRANSACTIONS ON SYSTEMS MAN CYBERNETICS-SYSTEMS, 2023, 53 (03): : 1566 - 1572
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[7] 3-BODY ORBITAL STABILITY-CRITERIA FOR CIRCULAR RETROGRADE ORBITS
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[J]. MONTHLY NOTICES OF THE ROYAL ASTRONOMICAL SOCIETY, 1994, 266 (01) : 25 - 30
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[J]. OPTICAL ENGINEERING, 1997, 36 (05) : 1552 - 1561
[10] Line-of-sight pointing accuracy-stability analysis and computer simulation for small spacecraft
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[J]. ACQUISITION, TRACKING, AND POINTING X, 1996, 2739 : 62 - 76

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