Evaluation of the initial phase range for transfers in the vicinity of a large space debris

The paper is concerned with the problem of finding the initial phase range for transfers in the vicinity of a large size space debris. We give algorithms for determination of both the optimal phase range, for which the transfer costs are minimal, and the admissible phase range, for which a transfer can begin earlier, but all the available budget of summary characteristic velocity will be exhausted. The proposed solutions include analytical and semi-analytical formulae that significantly simplify the precise numerical calculations providing very good first approximation. © IAEME Publication.

Авторы
Baranov A. 1, 3 , Budyansky A. 3, 2 , Grishko D.2
Издательство
IAEME Publication
Номер выпуска
769-777
Язык
Английский
Страницы
769-777
Статус
Опубликовано
Том
9
Год
2018
Организации
  • 1 Keldysh Institute of Applied Mathematics, Russian Academy of Sciences, Bauman Moscow State Technical University, Moscow, Russian Federation
  • 2 Bauman Moscow State Technical University, Moscow, Russian Federation
  • 3 People’s Friendship University, Moscow, Russian Federation
Ключевые слова
Admissible Phase Range; Large Space Debris; Optimal Phase Range; Orbital Maneuvers; Orbital Transfers; Rendezvous In Orbit
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