Investigation of the stability of orbits by using the adiabatic theory of motion in general relativity

被引：0
|
作者：
Toktarbay, S. [1 ]
Abishev, M. E. [1 ]
Talkhat, A. Z. [1 ]
Muratkhan, A. [1 ]
Kenzhebayeva, S. S. [1 ]
Abylayeva, A. Zh. [1 ]
机构：
[1] Al Farabi Kazakh Natl Univ, Dept Theoret & Nucl Phys, Alma Ata 050040, Kazakhstan
来源：
15TH MARCEL GROSSMANN MEETING, PT A | 2022年
关键词：
Restricted three-body problem; orbital stability; vector elements;
D O I：
暂无
中图分类号：
P1 [天文学];
学科分类号：
0704 ;
摘要：
We investigate the problem of the orbital stability of the motion of a test body in the restricted three-body problem, where all bodies have their own rotation. The stability of the orbits is investigated by using vector elements of orbits such as orbital moment and its time derivative. We show that it is possible to get some insight into the stability properties of the motion of test bodies.
引用
收藏
页码：500 / 504
页数：5
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