Method for optimization of trajectories including gravitational maneuvers of a spacecraft with a solar sail

被引：0
|
作者：
P. V. Kazmerchuk
V. V. Malyshev
V. E. Usachev
机构：
[1] Technical University,Moscow State Institute of Aviation
来源：
Journal of Computer and Systems Sciences International | 2007年 / 46卷
关键词：
System Science International; Propulsion System; Angular Distance; Ecliptic Plane; Solar Sail;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
A method for simulation and optimization of flight trajectories including multiple maneuvers of spacecrafts equipped with a solar sail is considered. The proposed method provides a possibility of formation of the general approach to solution of optimization problems of interplanetary missions using a solar sail. The problems of optimization of flight trajectories to Mercury and to a vicinity of the Sun on the basis of the inexpensive conversion Dnepr launch vehicle are solved using the proposed method.
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收藏
页码：150 / 161
页数：11
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