Formation of high inclined orbits to the ecliptic by multiple gravity assist maneuvers
- 作者: Golubev Y.1, Grushevskii A.1, Koryanov V.1, Tuchin A.1, Tuchin D.1
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隶属关系:
- Keldysh Institute of Applied Mathematics
- 期: 卷 56, 编号 2 (2017)
- 页面: 275-299
- 栏目: Control Systems of Moving Objects
- URL: https://journals.rcsi.science/1064-2307/article/view/219858
- DOI: https://doi.org/10.1134/S1064230717020083
- ID: 219858
如何引用文章
详细
Methods for designing trajectories of spacecraft (SC) for missions that need to increase the inclination of their orbits to the ecliptic using energy-efficient gravity assist maneuvers (GAMs) around planets, their moons, and small Solar system bodies are developed. The focus is on the development of algorithms (taking into account accurate ephemerides) for designing chains of multiple GAMs that significantly raise the orbit of a SC above the plane of the ecliptic. Complete analytical formulas for the change of inclination as a result of a GAM in the general case of elliptic orbits of the SC and the partner planet are obtained.
作者简介
Yu. Golubev
Keldysh Institute of Applied Mathematics
编辑信件的主要联系方式.
Email: golubev@keldysh.ru
俄罗斯联邦, Moscow, 125047
A. Grushevskii
Keldysh Institute of Applied Mathematics
Email: golubev@keldysh.ru
俄罗斯联邦, Moscow, 125047
V. Koryanov
Keldysh Institute of Applied Mathematics
Email: golubev@keldysh.ru
俄罗斯联邦, Moscow, 125047
A. Tuchin
Keldysh Institute of Applied Mathematics
Email: golubev@keldysh.ru
俄罗斯联邦, Moscow, 125047
D. Tuchin
Keldysh Institute of Applied Mathematics
Email: golubev@keldysh.ru
俄罗斯联邦, Moscow, 125047
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