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Spacecraft thrust vector control during landing on the moon surfaceстатья
Информация о цитировании статьи получена из
Web of Science,
Scopus
Дата последнего поиска статьи во внешних источниках: 13 ноября 2019 г.
- Авторы: Matyushin M.M., Ovechko V.M., Razoumny Y.N., Skorobogatov O.P., Tyurina D.D., Baranova I.S.
- Сборник: Advances in the Astronautical Sciences
- Серия: Proceedings of 3rd International conferences on dynamics and control of space systems (DyCOSS, 30.05-01.06.2017, Moscow)
- Том: 161
- Год издания: 2017
- Первая страница: 181
- Последняя страница: 187
- Аннотация: The problem of optimal control of the thrust vector of a spacecraft power engine, making a decay and soft landing from the circular satellite orbit of the Moon to its surface, is considered. The maximum principle of L.S.Pontryagin was used to determine the control structure. An approach has been developed to determine the optimal thrust control programs for the power engine. The results of the trajectory calculation of a spacecraft landing on the lunar surface are presented.
- Добавил в систему: Баранова Ирина Сергеевна