Ballistic optimization of the L1-L2 and L2-L1 low thrust transfers in the Earth-Moon system

被引：0

作者：

Fain, Maxim K. ^{[1
]}

Starinova, Olga L. ^{[1
]}

机构：

[1] Samara State Aerosp Univ, Spacecraft Dept, Samara, Russia

来源：

2015 7TH INTERNATIONAL CONFERENCE ON RECENT ADVANCES IN SPACE TECHNOLOGIES (RAST) | 2015年

关键词：

spacecraft; low thrust engine; ballistic optimization; interplanetary transfer; circular orbit; libration point; Earth-Moon system; NON-KEPLERIAN ORBITS; SOLAR SAIL; SPACECRAFT; PROPULSION; TRAJECTORIES; SIMULATION; LAWS;

D O I：

暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The paper outlines the optimization of the L1-L2 and L2-L1 missions using electric propulsion. The variational problem of the low thrust spacecraft transfer optimization with the optimization criterion as the total flight time is considered. The optimal control programs were obtained by using the Pontryagin's maximum principle. The optimization results were as follows: for a certain value of acceleration and exhaust velocity of the propulsion system, we determined optimal control programs, corresponding trajectories and minimal total flight times.

引用

页码：95 / 98

页数：4

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