Solution of the problem of time-energy minimization in orbital transfer via the improved SPEA

被引：0
|
作者：
Wang, S [1 ]
Dai, JH [1 ]
机构：
[1] Univ Natl Def Sci & Technol, Coll Astronaut & Mat Engn, Changsha 410073, Peoples R China
来源：
CHINESE ASTRONOMY AND ASTROPHYSICS | 2003年 / 27卷 / 04期
关键词：
celestial mechanics; methods : numerical;
D O I：
暂无
中图分类号：
P1 [天文学];
学科分类号：
0704 ;
摘要：
In this paper, we present an improved version of a multi-objective evolutionary algorithm known as SPEA, which has a high capability for solving problems defined in a large size space. We applied the algorithm to solve the problem of minimization of time-energy of orbital transfer, which often appears in space missions. The computational results show that the algorithm is valid and efficient.
引用
收藏
页码：447 / 453
页数：7
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