Low-Energy Sub-Optimal Low-Thrust Trajectories to Libration Points and Halo-Orbits

Abstract—: The paper considers the problem of calculating direct and low-energy, low-thrust trajectories to the libration points of the Earth–Moon system and to halo-orbits. A method for solving the problem is proposed. It consists of calculating stable manifolds of libration points or halo-orbits and calculating a low-thrust trajectory from an initial circular Earth orbit to the given point of this manifold using sub-optimal feedback control. With a fixed final mass of a spacecraft, the last stage of calculations is reduced to solving the Cauchy problem. The numerical examples are given for the calculation of direct and low-energy trajectories to libration points and to halo-orbits and the optimization of entry points to stable manifolds for low-energy trajectories. © 2019, Pleiades Publishing, Ltd.

Авторы
Редакторы
-
Журнал
Издательство
Maik Nauka Publishing / Springer SBM
Номер выпуска
5
Язык
Английский
Страницы
378-388
Статус
Опубликовано
Подразделение
-
Номер
-
Том
57
Год
2019
Организации
  • 1 Research Institute of Applied Mechanics and Electrodynamics, Moscow Aviation Institute, Moscow, 125993, Russian Federation
  • 2 Peoples Friendship University of Russia (RUDN University), Moscow, 117198, Russian Federation
Ключевые слова
-
Дата создания
24.12.2019
Дата изменения
24.12.2019
Постоянная ссылка
https://repository.rudn.ru/ru/records/article/record/55056/