Пожалуйста, используйте этот идентификатор, чтобы цитировать или ссылаться на этот ресурс:
http://hdl.handle.net/11701/2063
Полная запись метаданных
Поле DC | Значение | Язык |
---|---|---|
dc.contributor.author | Shmyrov, Alexander S. | - |
dc.contributor.author | Shymanchuk, Dzmitry | - |
dc.contributor.author | Sokolov, Leonid L. | - |
dc.date.accessioned | 2016-04-12T06:48:21Z | - |
dc.date.available | 2016-04-12T06:48:21Z | - |
dc.date.issued | 2015 | - |
dc.identifier.isbn | 978-146737698-3 | - |
dc.identifier.uri | http://hdl.handle.net/11701/2063 | - |
dc.description.abstract | This paper studies the problem of an intercept trajectory construction when using the neighborhood of the collinear libration point L1 of the Sun-Earth system. A celestial body motion is considered in a rotating frame within the Hill's problem of the circular restricted three-body problem. It is known that collinear libration points are unstable but its instability can be used as a positive factor for maneuvering a celestial body in the near-Earth space. Development methodology of control algorithms for the orbital motion of a celestial body when using the instability of collinear libration points is offered. The construction of an intercept trajectory is based on the properties of a specially introduced phase variables function, called 'hazard function'. The results of the numerical integration are graphically illustrated. © 2015 IEEE. | en_GB |
dc.language.iso | en | en_GB |
dc.publisher | Institute of Electrical and Electronics Engineers Inc. | en_GB |
dc.title | The interception problem of a celestial body with the use of the collinear libration points | en_GB |
Располагается в коллекциях: | Articles |
Файлы этого ресурса:
Файл | Описание | Размер | Формат | |
---|---|---|---|---|
shymanchuk.pdf | 3,04 MB | Adobe PDF | Просмотреть/Открыть |
Все ресурсы в архиве электронных ресурсов защищены авторским правом, все права сохранены.