Пожалуйста, используйте этот идентификатор, чтобы цитировать или ссылаться на этот ресурс:
http://hdl.handle.net/11701/2061
Полная запись метаданных
Поле DC | Значение | Язык |
---|---|---|
dc.contributor.author | Shmyrov, Alexander S. | - |
dc.contributor.author | Shymanchuk, Dzmitry | - |
dc.date.accessioned | 2016-04-12T06:46:03Z | - |
dc.date.available | 2016-04-12T06:46:03Z | - |
dc.date.issued | 2015 | - |
dc.identifier.isbn | 978-147996824-4 | - |
dc.identifier.uri | http://hdl.handle.net/11701/2061 | - |
dc.description.abstract | The use of the neighborhood of collinear libration point (L1 or L2) of the Sun-Earth system has long been of practical importance in connection with projects implemented by NASA and ESA. 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. For example, it may be used to solve the problem of comet and asteroid hazard to monitor space objects posing threat to the Earth. We offer a methodology for constructing control algorithms for the orbital motion of a celestial body. This methodology is based on the properties of a specially introduced phase variables function called hazard function. Numerical simulation results are given. © 2015 IEEE. | en_GB |
dc.language.iso | en | en_GB |
dc.publisher | Institute of Electrical and Electronics Engineers Inc. | en_GB |
dc.title | Maneuvering in near-Earth space with the use of the collinear libration points | en_GB |
dc.type | Article | en_GB |
Располагается в коллекциях: | Articles |
Файлы этого ресурса:
Файл | Описание | Размер | Формат | |
---|---|---|---|---|
Shmyrov_Shymanchuk_cT.pdf | 1,46 MB | Adobe PDF | Просмотреть/Открыть |
Все ресурсы в архиве электронных ресурсов защищены авторским правом, все права сохранены.