Halo-Orbit Formation in the Earth-Moon System by the Electric Propulsion Spacecraft

被引：0

作者：

Starinova, Olga ^{[1
]}

Kupczov, Vyacheslav ^{[1
]}

Gao, Changsheng ^{[2
]}

Hu, Yudon ^{[2
]}

Fain, Maksim ^{[1
]}

Khabibullin, Roman ^{[1
]}

机构：

[1] Samara Univ, Moscow Highway 34, Samara 443086, Russia

[2] HIT, 92 West Dazhi St, Harbin 150001, Heilongjiang, Peoples R China

来源：

ICNPAA 2018 WORLD CONGRESS: 12TH INTERNATIONAL CONFERENCE ON MATHEMATICAL PROBLEMS IN ENGINEERING, AEROSPACE AND SCIENCES | 2018年 / 2046卷

关键词：

D O I：

10.1063/1.5081579

中图分类号：

O1 [数学];

学科分类号：

0701 ; 070101 ;

摘要：

The problem of control laws, allowing the formation and maintenance of the required halo-orbit, is considered. The motion of the electric propulsion spacecraft is considered in the vicinity of the collinear libration points of the Earth-Moon system. The gravitational effects of the Earth, the Moon and the Sun are taken into account. The results are based on the simplified linearized models of the gravitational potential.

引用

页数：8

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