Analysis of the possibilities for the creation of a relay system to control a multi-satellite orbital constellation

The paper shows the relevance of a space relay system when creating multi-satellite orbital constellations of spacecraft. The parameters of an advanced space relay system for controlling a multi-satellite orbital constellation of spacecraft are studied taking into account the structure of the spacec...

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Bibliographic Details
Main Authors: A. Yu. Potyupkin, V. V. Kraskov, S. A. Yakhutin, S. V. Avramenko
Format: Article
Language:English
Published: Samara National Research University 2025-04-01
Series:Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение
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Online Access:https://journals.ssau.ru/vestnik/article/viewFile/28380/11193
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Summary:The paper shows the relevance of a space relay system when creating multi-satellite orbital constellations of spacecraft. The parameters of an advanced space relay system for controlling a multi-satellite orbital constellation of spacecraft are studied taking into account the structure of the spacecraft technological control cycle. A space relay system in low and medium Earth orbits is proposed as a dynamic telecommunication system to provide control of a large number of spacecraft. Necessary conditions are formulated to complete the spacecraft technological control cycle with a given quality including the realization of multiple access methods. The proposed space relay system is considered as a queuing system. An example of calculating the parameters of a geostationary space relay system in the case of using multi-beam antenna system as a queuing system is given.
ISSN:2542-0453
2541-7533