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On solving the problems of optimization of trajectories of many-revolution orbit transfers of spacecraftстатья
Информация о цитировании статьи получена из
Web of Science,
Scopus
Статья опубликована в журнале из списка Web of Science и/или Scopus
Дата последнего поиска статьи во внешних источниках: 18 июля 2013 г.
- Авторы: Ryzhov S.Yu, Grigoriev I.S.
- Журнал: Cosmic Research (English translation of Kosimicheskie Issledovaniya)
- Том: 44
- Номер: 3
- Год издания: 2006
- Издательство: Pleiades Publishing, Inc.
- Местоположение издательства: New York, USA
- Первая страница: 258
- Последняя страница: 267
- DOI: 10.1134/S0010952506030105
- Аннотация: The problem of optimal control over many-revolution spacecraft orbit transfers between circular coplanar orbits of satellites is considered. The spacecraft flight is controlled by a thrust vector of a jet engine with restricted thrust (JERT). The mass expenditure is minimized at a limited time of flight. The optimal control problem is solved based on the maximum principle. The boundary value problem of the maximum principle is solved numerically using the shooting method. A modified computation scheme of the shooting method is suggested (multi-point shooting), as well as a method (correlated with the scheme) of choosing the initial approximation with the use of a solution to the optimization problem in the impulse formulation. The scheme and method allow one to construct many-revolution spacecraft orbit transfers.
- Добавил в систему: Григорьев Илья Сергеевич