Optimal deployment of satellite mega-constellation

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This paper proposes an optimization framework to deploy a large satellite constellation. The proposed framework consists of two phases: the mission viability evaluation phase and the optimal planning phase. The feasibility of the constellation deployment architecture with given resources is assessed in the first phase. The second phase uses mixed-integer linear programming to optimize the satellite deployment plan based on a dynamic logistics model. The effectiveness of the proposed framework is demonstrated through a case study for optimal deployment planning of a large satellite constellation.
Publisher
PERGAMON-ELSEVIER SCIENCE LTD
Issue Date
2023-01
Language
English
Article Type
Article
Citation

ACTA ASTRONAUTICA, v.202, pp.653 - 669

ISSN
0094-5765
DOI
10.1016/j.actaastro.2022.10.027
URI
http://hdl.handle.net/10203/302129
Appears in Collection
AE-Journal Papers(저널논문)
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