The repositioning maneuver of artificial earth satellite in a circular orbit with a supporting acceleration
Автор: Burdayev Mikhail Nikolayevich
Журнал: Программные системы: теория и приложения @programmnye-sistemy
Рубрика: Методы оптимизации и теория управления
Статья в выпуске: 4 (18) т.4, 2013 года.
Бесплатный доступ
The paper reveals the maneuver entity of reposition artificial satellite on a circular orbit with a supporting acceleration. A maneuver program implementation with using of constant thrust motors is found and proved. An energy efficiency of maneuver under various conditions of its implementation is determined. (in Russian)
Circular orbit, maneuver, satellite, supporting acceleration, trajectory
Короткий адрес: https://sciup.org/14335962
IDR: 14335962
Статья научная
