Mathematical aspects of the motion of an equatorial satellite

The paper presents a study of the motion of an equatorial Earth satellite subject to inflow friction forces. Asymptotic methods have been used to analyze the derived equations. An approximate solution for the trajectory has been obtained, which has been used to study the satellite’s motion around its centre of mass. The stationary points have been determined and their stability examined. © 2017, Academic Publishing House. All rights reserved.

Authors
Sheiretsky K.1 , Shkevov R.2 , Erokhin N. 3, 4
Journal
Comptes Rendus de L'Academie Bulgare des Sciences
Publisher
Academic Publishing House
Number of issue
3
Language
English
Pages
411-418
Status
Published
Link
External link
Volume
70
Year
2017
Organizations
  • 1 University of National and World Economy, UNWE, Student Town, Sofia, 1700, Bulgaria
  • 2 Space Research and Technology Institute, Bulgarian Academy of Sciences, Acad. G. Bonchev St, Bl. 1, Sofia, 1113, Bulgaria
  • 3 Space Research Institute, Russian Academy of Sciences, 84/32 Profsoyuznaya St, Moscow, 117997, Russian Federation
  • 4 Peoples’ Friendship University of Russia, 3, Ordjonikidze St, Moscow, 115419, Russian Federation
Keywords
Asymptotic methods; Equatorial satellite; Satellite motion; Stationary points; Trajectory
Date of creation
19.10.2018
Date of change
19.10.2018
Short link
https://repository.rudn.ru/en/records/article/record/6268/
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