An analytical review for the power system of a spacecraft-Reference-Cited by-同舟云学术

An analytical review for the power system of a spacecraft

Published:2022-06-10 Issue:2 Volume:14 Page:11-26
ISSN:2247-4528
Container-title:INCAS BULLETIN
language:en
Short-container-title:INCAS BULLETIN

Author:

CHATURVEDI Sudhir Kumar CHATURVEDI¹

Affiliation:

1. School of Engineering, UPES, Dehradun-248007, India, sudhir.chaturvedi@ddn.upes.ac.in

Abstract

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.

Publisher

INCAS - National Institute for Aerospace Research Elie Carafoli

Subject

Aerospace Engineering,Control and Systems Engineering

Reference10 articles.

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