THE ELLIPTIC 3-BODY PROBLEM - TRIANGULAR SOLUTION

被引：0
|
作者：
TODORAN, I
ROMAN, R
机构：
[1] Astronomical Observatory, Cluj-napoca
来源：
ASTRONOMISCHE NACHRICHTEN | 1992年 / 313卷 / 05期
关键词：
CELESTIAL MECHANICS; 3-BODY PROBLEM;
D O I：
10.1002/asna.2113130510
中图分类号：
P1 [天文学];
学科分类号：
0704 ;
摘要：
The restricted three-body problem with eccentric orbit is reviewed and the positions of the triangular Lagrangian points (L4, L5) are determined. It is put in evidence the fact that L4 and L5 are situated at the corners of an isoscales triangle: AB = BC = 1 - e2/(1 + e cos v)4/3 and AC = 1 - e2/(1 + e cos v)
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页码：315 / 317
页数：3
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