An analytical review for the power system of a spacecraft

Electrical bus is needed for the operation of all active spacecraft systems and subsystems. In the spacecraft mechanism, the battery charging system and the bus storage continued with bus control, the conditioning and bus distribution is an essential part for keeping the spacecraft in working mode....

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Bibliographic Details
Published inINCAS bulletin Vol. 14; no. 2; pp. 11 - 26
Main Author CHATURVEDI, Sudhir Kumar CHATURVEDI
Format Journal Article
LanguageEnglish
Published Bucharest INCAS - National Institute for Aerospace Research "Elie Carafoli" 10.06.2022
National Institute for Aerospace Research “Elie Carafoli” - INCAS
Subjects
Batteries
Battery chargers
Charging
det
Electric power systems
Energy storage
eps
Heat
Photovoltaic cells
power regulation
Radiation
Scientific papers
solar array
Solar arrays
Solar collectors
Solar energy
Spacecraft
Spacecraft power supplies
Subsystems
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ISSN2066-8201
2247-4528
2247-4528
DOI10.13111/2066-8201.2022.14.2.2

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Summary:Electrical bus is needed for the operation of all active spacecraft systems and subsystems. In the spacecraft mechanism, the battery charging system and the bus storage continued with bus control, the conditioning and bus distribution is an essential part for keeping the spacecraft in working mode. In this paper, the discussion for electrical power system (EPS) analysis in the spacecraft body will be elaborated from the previous research papers on this subject covering the topics of solar array, solar array drive, over current and over voltage protection, battery charging and discharging, bus control, conversion.
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content type line 14
ISSN:2066-8201
2247-4528
2247-4528
DOI:10.13111/2066-8201.2022.14.2.2