Тип публикации: доклад, тезисы доклада, статья из сборника материалов конференций
Конференция: International Scientific Conference on Advanced Technologies in Aerospace, Mechanical and Automation Engineering, MIST: Aerospace 2019
Год издания: 2020
Идентификатор DOI: 10.1088/1757-899X/734/1/012034
Аннотация: In this paper, the mathematical analysis of spacecraft control cyclograms is considered. The proposed solution is applied to a ground-based control complex of spacecrafts, where a plenty of cyclograms is a part of the general technological control cycles of spacecrafts, which include the whole of spacecrafts system life cycle. The Показать полностьюproblem of ground control system software optimization is solved using static strategies and cost criteria. Spacecraft control processes cover all the system control cycle and regulate an execution of the information processing and control tasks in the ground-based and board control complexes. Analyzing characteristics of such the processes has ascertained a strong relation between spacecraft technological control cycles and their computer-based realization for the mentioned complexes. © Published under licence by IOP Publishing Ltd.
Журнал: IOP Conference Series: Materials Science and Engineering
Выпуск журнала: Vol. 734, Is. 1
ISSN журнала: 17578981
Издатель: Institute of Physics Publishing 012034