Low-Thrust Transfer Between Circular Orbits Using Natural Precession

被引：24

作者：

Cerf, Max ^{[1
]}

机构：

[1] Airbus Def & Space, Mission Anal Dept, F-78130 Les Mureaux, France

来源：

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2016年 / 39卷 / 10期

关键词：

D O I：

10.2514/1.G001331

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The minimum-fuel low-thrust transfer between circular orbits is formulated using the Edelbaum averaged dynamics with the addition of the nodal precession due to the first zonal term. The extremal analysis shows that an optimal transfer is composed of three sequences in the regular case. The optimal control problem is solved by a shooting method with a costate guess derived from an approximate solution.

引用

页码：2232 / 2239

页数：8

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