Frozen Orbits for a Solar Sail Around Mercury

被引：24
|
作者：
Tresaco, Eva [1 ]
Elipe, Antonio [1 ]
Carvalho, Jean Paulo S. [2 ]
机构：
[1] Ctr Univ Def Zaragoza, Inst Univ Matemat & Aplicac, Grp Mecan Espacial, Zaragoza 50090, Spain
[2] Univ Fed Reconcavo Bahia, Ctr Ciencia & Tecnol Energia & Sustentabilidad, BR-44380000 Cruz Das Almas, Brazil
来源：
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2016年 / 39卷 / 07期
关键词：
PERIODIC-ORBITS; SATELLITES; FAMILIES; EUROPA; MODEL;
D O I：
10.2514/1.G001510
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
A study provides a method for finding initial conditions for frozen orbits for a solar sail around Mercury. The use of propellantless propulsion systems like solar sails attracts the interest for scientific missions. Solar sails offer new challenging spacescience missions. They are considered for having artificial equilibrium points. These displaced periodic orbits near libration points can be used, for example, as an alert of geomagnetic storms. They allow to achieve long residence times in orbit, and also make feasible new observation missions based on the computation of geocentric sun-synchronous frozen orbits.
引用
收藏
页码：1657 / 1664
页数：8
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