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.

Авторы
Sheiretsky K.1 , Shkevov R.2 , Erokhin N. 3, 4
Журнал
Comptes Rendus de L'Academie Bulgare des Sciences
Издательство
Academic Publishing House
Номер выпуска
3
Язык
Английский
Страницы
411-418
Статус
Опубликовано
Ссылка
Внешняя ссылка
Том
70
Год
2017
Организации
  • 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
Ключевые слова
Asymptotic methods; Equatorial satellite; Satellite motion; Stationary points; Trajectory
Дата создания
19.10.2018
Дата изменения
19.10.2018
Постоянная ссылка
https://repository.rudn.ru/ru/records/article/record/6268/
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