Method of virtual trajectories for the design of gravity assisted missions

被引:0
|
作者
M. Yu. Ovchinnikov
S. P. Trofimov
M. G. Shirobokov
机构
[1] Keldysh Institute of Applied Mathematics of the Russian Academy of Sciences,
[2] Moscow Institute of Physics and Technology (State University),undefined
来源
Cosmic Research | 2013年 / 51卷
关键词
Transfer Time; Cosmic Research; Solar Sail; Planetary Orbit; Flight Trajectory;
D O I
暂无
中图分类号
学科分类号
摘要
A novel method of virtual trajectories is proposed for the design of multiple gravity assist trajectories. The database of virtual trajectories can be tabulated for any planetary sequence and used in subsequent calculations. Requirements for the mission duration and the launch date are taken into account during the iterative procedure of database screening and refinement. The results of applying the virtual trajectories method to the design of a mission to Uranus are presented.
引用
收藏
页码:439 / 451
页数:12
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