METHOD OF EARTH-POINTING ATTITUDE-CONTROL FOR ELLIPTIC ORBITS

被引：3

作者：

CONNELL, GM

机构：

来源：

AIAA JOURNAL | 1972年 / 10卷 / 03期

关键词：

D O I：

10.2514/3.6574

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：258 / &

共 10 条

[1]

Beletskii V.V., 1966, TT6751366 NASA

[2]

BELETSKII VV, 1966, TTF429 NASA

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[4] ATTITUDE CONTROL OF A SATELLITE IN AN ELLIPTIC ORBIT [J].

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[5] RESPONSE OF A 2-BODY GRAVITY GRADIENT SYSTEM IN A SLIGHTLY ECCENTRIC ORBIT [J].

CLARK, JPC .

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[6] INFINITE DETERMINANT METHODS FOR STABILITY ANALYSIS OF PERIODIC-COEFFICIENT DIFFERENTIAL EQUATIONS [J].

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LIKINS, PW .

AIAA JOURNAL, 1970, 8 (04) :680-&

[7] PERIODIC SOLUTIONS ASSOCIATED WITH GRAVITY-GRADIENT-ORIENTED SYSTEM .2. STABILITY ANALYSIS [J].

MODI, VJ ;

BRERETON, RC .

AIAA JOURNAL, 1969, 7 (08) :1465-&

[8] PERIODIC SOLUTIONS ASSOCIATED WITH GRAVITY-GRADIENT-ORIENTED SYSTEM .I. ANALYTICAL AND NUMERICAL DETERMINATION [J].

MODI, VJ ;

BRERETON, RC .

AIAA JOURNAL, 1969, 7 (07) :1217-&

[9]

OCONNOR BJ, 1969, J SPACECRAFT ROCKETS, V6, P225

[10]

SAATY T, 1964, NONLINEAR MATHEMATIC, P217

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