Solar sail orbits at artificial sun-Earth libration points

被引：50

作者：

Baoyin, H ^{[1
]}

McInnes, CR ^{[1
]}

机构：

[1] Univ Strathclyde, Dept Mech Engn, Glasgow G1 1XJ, Lanark, Scotland

来源：

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2005年 / 28卷 / 06期

关键词：

D O I：

10.2514/1.14598

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

A family of displaced solar sail orbits near the sun-Earth libration points was discussed. It was shown that periodic orbits can be developed that are displaced above or below the plane of the restricted three-body system. Several particular orbits were designed and their stability and controllability were discussed by means of numerical methods. The results indicate that this family of periodic orbits is usually unstable but completely controllable by use of the sail attitude or lightness number control.

引用

页码：1328 / 1331

页数：4

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