EXACT AND A NEW 1ST-ORDER SOLUTION FOR RELATIVE TRAJECTORIES OF A PROBE EJECTED FROM A SPACE STATION

被引：10

作者：

BERREEN, TF ^{[1
]}

CRISP, JDC ^{[1
]}

机构：

[1] MONASH UNIV,DEPT MECH ENGN,VICTORIA,AUSTRALIA

来源：

CELESTIAL MECHANICS | 1976年 / 13卷 / 01期

关键词：

D O I：

10.1007/BF01228535

中图分类号：

P1 [天文学];

学科分类号：

0704 ;

摘要：

引用

页码：75 / 88

页数：14

共 17 条

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ANTHONY, ML ;

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[2]

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[3]

CRISP JDC, 1962, ASTRONAUT ACTA, V8, P1

DEVRIES, JP .

[5]

Eades J. B. Jr., 1973, Celestial Mechanics, V7, P3, DOI 10.1007/BF01243506

[6]

EADES JB, 1972, 7227 AN MECH ASS INC

[7]

EGGLESTON JM, 1961, R87 NASA TR

[8] SECOND-ORDER SOLUTION TO ELLIPTICAL RENDEZVOUS PROBLEM [J].

EULER, EA ;

SHULMAN, Y .

[9]

HERRICK S, 1971, ASTRODYNAMICS, V1, P155

[10] RELATIVE TRAJECTORIES OF OBJECTS EJECTED FROM A NEAR SATELLITE [J].

KNOLLMAN, GC ;

PYRON, BO .