Analysis of the possibilities for the creation of a relay system to control a multi-satellite orbital constellation
- Authors: Potyupkin A.Y.1, Kraskov V.V.1, Yakhutin S.A.1, Avramenko S.V.1
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Affiliations:
- JSC Russian Space Systems
- Issue: Vol 24, No 1 (2025)
- Pages: 45-55
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journal-vniispk.ru/2542-0453/article/view/311506
- DOI: https://doi.org/10.18287/2541-7533-2025-24-1-45-55
- ID: 311506
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Abstract
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.
About the authors
A. Yu. Potyupkin
JSC Russian Space Systems
Author for correspondence.
Email: Avramenko.sv@spacecorp.ru
Doctor of Science (Engineering), Professor, Senior Research Associate
Russian FederationV. V. Kraskov
JSC Russian Space Systems
Email: Kraskov.vv@spacecorp.ru
Deputy Chief of the Branch
Russian FederationS. A. Yakhutin
JSC Russian Space Systems
Email: Yakhutin.sa@spacecorp.ru
Director of Projects
Russian FederationS. V. Avramenko
JSC Russian Space Systems
Email: Avramenko.sv@spacecorp.ru
Candidate of Science (Engineering), Head of the Bureau
Russian FederationReferences
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