DISTANT ORBITS AROUND MERCURY

被引：0

作者：

Ma, Xue ^{[1
]}

Li, Junfeng ^{[1
]}

Baoyin, Hexi ^{[1
]}

Zhang, Peng ^{[1
]}

Li, Jingyang ^{[1
]}

Chen, Yang ^{[1
]}

机构：

[1] Tsinghua Univ, Sch Aerosp, Beijing 100084, Peoples R China

来源：

FIRST IAA CONFERENCE ON DYNAMICS AND CONTROL OF SPACE SYSTEMS 2012, PTS I AND II | 2012年 / 145卷

关键词：

RESTRICTED 3-BODY PROBLEM; PERIODIC-ORBITS; STABILITY; MISSION;

D O I：

暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

For some low cost space missions to Mercury, distant orbits around the planet are studied. This research is carried out in the framework of the elliptic restricted three-body problem (ER3BP), because of the planet's non-negligible eccentricity. Two families of prograde and retrograde planar orbits in the CR3BP are chosen for their useful shapes or good performance of stability with high altitude, and we extend the study of these orbits to the ER3BP case. The stability of all above orbits around Mercury is investigated in this paper. Our research indicates that orbits within a large altitude range may keep certain shapes long enough for space missions.

引用

页码：231 / 239

页数：9

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