Earth escape by ideal sail and solar-photon thrustor spacecraft

被引：23

作者：

Mengali, G ^{[1
]}

Quarta, AA ^{[1
]}

机构：

[1] Univ Pisa, Dept Aerosp Engn, I-56122 Pisa, Italy

来源：

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2004年 / 27卷 / 06期

关键词：

D O I：

10.2514/1.10637

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

Escape trajectories from geosynchronous transfer orbit for solar sails were investigated. A simple control, which maximizes the instantaneous rate of energy change, was derived using vector notation. The control law comprises both the case of an ideal flat sail and the case of a solar-photon thrustor spacecraft. The simulations indicate that the sun-sail position in the last few spirals has a significant effect on the efficiency of the escape trajectory.

引用

页码：1105 / 1108

页数：4

共 16 条

[1]

BATTIN R. H., 1987, AIAA ED SERIES, P387

[2] Technique for escape from geosynchronous transfer orbit using a solar sail [J].