On Stability of Orbit of Artificial Moon Moving around a Small Celestial Body Perturbed by an External Body

V. G. Pol; A. V. Simonov; K. G. Sukhanov

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On Stability of Orbit of Artificial Moon Moving around a Small Celestial Body Perturbed by an External Body

机译：人造卫星绕小天体绕扰动的轨道稳定性研究

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摘要

We examine the stability of the orbit of an artificial moon of a small celestial body in the presence of an external massive perturbing body in terms of the restricted three-body problem. The orbit of this moon is shown to be dependent on the shape of the small body and central gravitational field of the external body. We study how these factors interact with each other and how they affect the stability of the orbit.

机译：我们根据受限制的三体问题，研究了在外部巨大的扰动体的存在下，一个小天体的人造卫星的轨道的稳定性。该月球的轨道取决于小物体的形状和外部物体的中心重力场。我们研究了这些因素如何相互影响以及它们如何影响轨道的稳定性。

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来源
《Solar system research》 |2011年第7期|p.657-662|共6页
作者
V. G. Pol; A. V. Simonov; K. G. Sukhanov;
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作者单位

Lavochkin Research and Production Association, ul. Leningradskaya 24, Khimki, 141400 Russia;

Lavochkin Research and Production Association, ul. Leningradskaya 24, Khimki, 141400 Russia;

Lavochkin Research and Production Association, ul. Leningradskaya 24, Khimki, 141400 Russia;

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收录信息美国《科学引文索引》(SCI);
原文格式 PDF
正文语种 eng
中图分类
关键词
orbit stability; artificial satellite orbit; small celestial body;

机译：轨道稳定性人造卫星轨道;小天体;

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1. Periodic orbit-attitude solutions along planar orbits in a perturbed circular restricted three-body problem for the Earth-Moon system [J] . Bucci Lorenzo, Lavagna Michele, Guzzetti Davide, Acta astronautica . 2018,第JUNa期

机译：地球-月球系统摄动圆形受限三体问题中沿平面轨道的周期轨道姿态解
2. On the accuracy of approximation of motion of a small celestial body by intermediate perturbed orbits calculated on the basis of three position vectors and three observations [J] . Shefer V. A., Shefer O. V. Solar system research . 2016,第3期

机译：基于三个位置矢量和三个观测值计算的中间扰动轨道对小天体运动近似的准确性
3. On the Accuracy of Approximation of a Small Celestial Body Motion Using Intermediate Perturbed Orbits Calculated from Two Position Vectors and Three Observations [J] . Shefer V. A., Shefer O. V. Solar system research . 2015,第1期

机译：利用两个位置矢量和三个观测值计算的中间扰动轨道，对小天体运动的逼近精度
4. PERIODIC ORBIT-ATTITUDE SOLUTIONS ALONG PLANAR ORBITS IN A PERTURBED CIRCULAR RESTRICTED THREE-BODY PROBLEM FOR THE EARTH-MOON SYSTEM [C] . Lorenzo Bucci, Michele Lavagna, Davide Guzzetti, International astronautical congress . 2016

机译：地球-月球系统摄动圆约束三体问题中平面轨道的周期轨道-姿态解
5. Long-term Dynamical Behavior of Highly Perturbed Natural and Artificial Celestial Bodies. [D] . Rosengren, Aaron J. 2014

机译：高扰动的天然和人造天体的长期动力学行为。
6. Serpentinization and the Formation of H2 and CH4 on Celestial Bodies (Planets Moons Comets) [O] . N.G. Holm, C. Oze, O. Mousis, -1

机译：蛇纹石化和天体（行星卫星彗星）上H2和CH4的形成
7. On the accuracy of approximation of motion of a small celestial body by intermediate perturbed orbits calculated on the basis of three position vectors and three observations [O] . Шефер, Владимир Александрович, Шефер, Ольга Владимировна 2016

机译：基于三个位置矢量和三个观测值计算的中间扰动轨道对小天体运动近似的准确性
8. On the Stability of Regular Motions of Artificial Celestial Bodies [R] . Duboshin, G. N. 1960

机译：人工天体正则运动的稳定性

On Stability of Orbit of Artificial Moon Moving around a Small Celestial Body Perturbed by an External Body

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