Evaluation of impulsive maneuvers performed by active space object

The subject of this paper is the problem of estimating the maneuver parameters performed by an active space object between two consequent observations spans. Analytical and numerical-Analytical algorithms of estimating one-pulse and two-pulse maneuvers of short duration are proposed. Both coplanar and non-coplanar types of maneuvers are considered. The algorithm for estimating single-pulse maneuvers takes into account presence of significant errors in determining the initial and final orbits. The solution process has a geometric interpretation. Examples of calculation are presented for the series of maneuvers of the spacecraft in GEO. © 2017 Univelt Inc. All rights reserved.

Авторы
Agapov V.M. 1, 2 , Baranov A.A. 1, 3 , Karatunov M.O.3
Издательство
Univelt Inc.
Язык
Английский
Страницы
339-351
Статус
Опубликовано
Том
161
Год
2017
Организации
  • 1 Keldysh Institute of Applied Mathematics of Russian Academy of Science, 4, Miusskaya Sqr, Moscow, 125047, Russian Federation
  • 2 Peoples Friendship University of Russia (RUDN University), 6, Mikluho-Maklaya Str, Moscow, 117198, Russian Federation
  • 3 JSC Astronomical Research Center, 56 Entuziastov Str, Moscow, 111123, Russian Federation
Ключевые слова
Cobalt compounds; Dysprosium compounds; Orbits; Space flight; Active spaces; Analytical algorithms; Geometric interpretation; Maneuver parameter; Non-coplanar; Short durations; Single pulse; Solution process; Sulfur compounds
Дата создания
19.10.2018
Дата изменения
19.10.2018
Постоянная ссылка
https://repository.rudn.ru/ru/records/article/record/6121/
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