电邮这篇文章 On Stability of Sattellite's Elliptical Orbit Motion for Cylindrical Precession of Lunar Type Resonance
- 作者: Churkina TE1
-
隶属关系:
- Moscow Aviation Institute
- 期: 编号 2 (2009)
- 页面: 5-13
- 栏目: Articles
- URL: https://journals.rcsi.science/2658-4670/article/view/328951
- ID: 328951
如何引用文章
全文:
详细
Stability of satellites elliptical orbit motion in the case of the cylindrical precession at
Lunar type resonance is under investigation. Stability regions at first approximation have
been obtained in the space of parameters of the problem (inertial parameter and eccentricity).
Nonlinear analysis is carried out in these regions. Analytical and numerical methods are used.
Lunar type resonance is under investigation. Stability regions at first approximation have
been obtained in the space of parameters of the problem (inertial parameter and eccentricity).
Nonlinear analysis is carried out in these regions. Analytical and numerical methods are used.
作者简介
T Churkina
Moscow Aviation InstituteКафедра теоретической механики; Московский авиационный институт; Moscow Aviation Institute
补充文件
