Comparison Study of Electric Power System Architectures for CubeSat

Amarendra Edpuganti; Vinod Khadkikar; Hatem Zeineldin; Mohamed S. Elmoursi; Mohamed Al Hosani

doi:10.1109/PESGRE45664.2020.9070355

Comparison Study of Electric Power System Architectures for CubeSat

Amarendra Edpuganti
, Vinod Khadkikar
, Hatem Zeineldin
, Mohamed S. Elmoursi
, Mohamed Al Hosani

Electrical Engineering

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

10 Scopus citations

Abstract

CubeSats have been widely used for space research due to lower cost and faster development. Electric power system (EPS) is one of the key subsystem of CubeSat which powers all the other subsystems. The successful mission of CubeSat requires highly efficient and reliable EPS as there is no possibility of maintenance after launch. The main objective of this paper is to study and compare floating battery and non-floating battery EPS architectures in terms of system efficiency and reliability. The comparison study is done based on the data of MYSAT-I which is an 1U CubeSat launched by Khalifa University. The comparison study concludes that floating battery EPS is most suitable for CubeSats.

Original language	British English
Title of host publication	2020 IEEE International Conference on Power Electronics, Smart Grid and Renewable Energy, PESGRE 2020
Publisher	Institute of Electrical and Electronics Engineers Inc.
ISBN (Electronic)	9781728142517
DOIs	https://doi.org/10.1109/PESGRE45664.2020.9070355
State	Published - Jan 2020
Event	2020 IEEE International Conference on Power Electronics, Smart Grid and Renewable Energy, PESGRE 2020 - Cochin, India Duration: 2 Jan 2020 → 4 Jan 2020

Publication series

Name	2020 IEEE International Conference on Power Electronics, Smart Grid and Renewable Energy, PESGRE 2020

Conference

Conference	2020 IEEE International Conference on Power Electronics, Smart Grid and Renewable Energy, PESGRE 2020
Country/Territory	India
City	Cochin
Period	2/01/20 → 4/01/20

UN SDGs

This output contributes to the following UN Sustainable Development Goals (SDGs)

SDG 7 Affordable and Clean Energy

Keywords

CubeSat
Dc to dc converters
Electric power system
Nanosatellites

Access to Document

10.1109/PESGRE45664.2020.9070355

OpenUrl availability

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Edpuganti, A., Khadkikar, V., Zeineldin, H., Elmoursi, M. S., & Hosani, M. A. (2020). Comparison Study of Electric Power System Architectures for CubeSat. In 2020 IEEE International Conference on Power Electronics, Smart Grid and Renewable Energy, PESGRE 2020 Article 9070355 (2020 IEEE International Conference on Power Electronics, Smart Grid and Renewable Energy, PESGRE 2020). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/PESGRE45664.2020.9070355

Edpuganti, Amarendra ; Khadkikar, Vinod ; Zeineldin, Hatem et al. / Comparison Study of Electric Power System Architectures for CubeSat. 2020 IEEE International Conference on Power Electronics, Smart Grid and Renewable Energy, PESGRE 2020. Institute of Electrical and Electronics Engineers Inc., 2020. (2020 IEEE International Conference on Power Electronics, Smart Grid and Renewable Energy, PESGRE 2020).

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title = "Comparison Study of Electric Power System Architectures for CubeSat",

abstract = "CubeSats have been widely used for space research due to lower cost and faster development. Electric power system (EPS) is one of the key subsystem of CubeSat which powers all the other subsystems. The successful mission of CubeSat requires highly efficient and reliable EPS as there is no possibility of maintenance after launch. The main objective of this paper is to study and compare floating battery and non-floating battery EPS architectures in terms of system efficiency and reliability. The comparison study is done based on the data of MYSAT-I which is an 1U CubeSat launched by Khalifa University. The comparison study concludes that floating battery EPS is most suitable for CubeSats.",

keywords = "CubeSat, Dc to dc converters, Electric power system, Nanosatellites",

author = "Amarendra Edpuganti and Vinod Khadkikar and Hatem Zeineldin and Elmoursi, \{Mohamed S.\} and Hosani, \{Mohamed Al\}",

note = "Publisher Copyright: {\textcopyright} 2020 IEEE.; 2020 IEEE International Conference on Power Electronics, Smart Grid and Renewable Energy, PESGRE 2020 ; Conference date: 02-01-2020 Through 04-01-2020",

year = "2020",

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doi = "10.1109/PESGRE45664.2020.9070355",

language = "British English",

series = "2020 IEEE International Conference on Power Electronics, Smart Grid and Renewable Energy, PESGRE 2020",

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Edpuganti, A, Khadkikar, V , Zeineldin, H , Elmoursi, MS & Hosani, MA 2020, Comparison Study of Electric Power System Architectures for CubeSat. in 2020 IEEE International Conference on Power Electronics, Smart Grid and Renewable Energy, PESGRE 2020., 9070355, 2020 IEEE International Conference on Power Electronics, Smart Grid and Renewable Energy, PESGRE 2020, Institute of Electrical and Electronics Engineers Inc., 2020 IEEE International Conference on Power Electronics, Smart Grid and Renewable Energy, PESGRE 2020, Cochin, India, 2/01/20. https://doi.org/10.1109/PESGRE45664.2020.9070355

Comparison Study of Electric Power System Architectures for CubeSat. / Edpuganti, Amarendra; Khadkikar, Vinod ; Zeineldin, Hatem et al.
2020 IEEE International Conference on Power Electronics, Smart Grid and Renewable Energy, PESGRE 2020. Institute of Electrical and Electronics Engineers Inc., 2020. 9070355 (2020 IEEE International Conference on Power Electronics, Smart Grid and Renewable Energy, PESGRE 2020).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

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T1 - Comparison Study of Electric Power System Architectures for CubeSat

AU - Edpuganti, Amarendra

AU - Khadkikar, Vinod

AU - Zeineldin, Hatem

AU - Elmoursi, Mohamed S.

AU - Hosani, Mohamed Al

PY - 2020/1

Y1 - 2020/1

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AB - CubeSats have been widely used for space research due to lower cost and faster development. Electric power system (EPS) is one of the key subsystem of CubeSat which powers all the other subsystems. The successful mission of CubeSat requires highly efficient and reliable EPS as there is no possibility of maintenance after launch. The main objective of this paper is to study and compare floating battery and non-floating battery EPS architectures in terms of system efficiency and reliability. The comparison study is done based on the data of MYSAT-I which is an 1U CubeSat launched by Khalifa University. The comparison study concludes that floating battery EPS is most suitable for CubeSats.

KW - CubeSat

KW - Dc to dc converters

KW - Electric power system

KW - Nanosatellites

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M3 - Conference contribution

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Edpuganti A, Khadkikar V , Zeineldin H , Elmoursi MS, Hosani MA. Comparison Study of Electric Power System Architectures for CubeSat. In 2020 IEEE International Conference on Power Electronics, Smart Grid and Renewable Energy, PESGRE 2020. Institute of Electrical and Electronics Engineers Inc. 2020. 9070355. (2020 IEEE International Conference on Power Electronics, Smart Grid and Renewable Energy, PESGRE 2020). doi: 10.1109/PESGRE45664.2020.9070355

Comparison Study of Electric Power System Architectures for CubeSat

Abstract

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UN SDGs

Keywords

Access to Document

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