The DOI matches its Crossref record; 7 of the 8 references it cites were found in a registry or an index.
Energy Storage Selection for LEO Satellites
Open accessAbstract
This paper presents two energy storage systems, based on chemical batteries and flywheels as the energy source of low earth orbit satellites in eclipse duration.Each system is designed and optimized with regard to energy requirement of a typical LEO satellite and various vital parameters in satellites which are discussed.The storage system and electronic interface are presented to give an adequate view for comparing them in different aspects.Afterwards, a comparison between these energy storage systems (ESSs) is applied considering their efficiency, reliability, weight, operational temperature and self-discharge dissipation (trickle charge).Finally, the conclusion presents the most recommended system in order of their capability.
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Citations
Cites
Supercapacitor Energy Storage for Wind Energy Applications
Abbey, C., & Joos, G. (2007) · IEEE Transactions on Industry Applications · doi:10.1109/tia.2007.895768 · Cited by 838
Power Management of a Stand-Alone Wind/Photovoltaic/Fuel Cell Energy System
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A Maximum Power Point Tracking System With Parallel Connection for PV Stand-Alone Applications
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Flywheel geometry design for improved energy storage using finite element analysis
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A flywheel energy storage system test on the International Space Station
Christopher, D. A., Beach, R., & Barton, J. R. (2002) · Intersociety Energy Conversion Engineering Conference · doi:10.1109/iecec.1997.656689 · Cited by 9
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1 of the 8 references couldn’t be matched to a known paper.
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- [16] M. A. Arslan, "Flywheel geometry design for improved energy storage using finite element analysis," ELSEVIER Trans. on Material and Design, 2007.
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A Comprehensive Review on Small Satellite Microgrids
Yaqoob, M., Lashab, A., Vasquez, J. C., Guerrero, J. M., Orchard, M. E., & Bintoudi, A. D. (2022) · IEEE Transactions on Power Electronics · doi:10.1109/tpel.2022.3175093 · Cited by 93
Windage loss characterisation for flywheel energy storage system: Model and experimental validation
Venturini, S., Cavallaro, S. P., & Vigliani, A. (2024) · Energy · doi:10.1016/j.energy.2024.132641 · Cited by 25
A Customize Battery Management Approach for Satellite
Hashmi, M. H., Affan, M., & Tandon, R. (2023) · International Carpathian Control Conference · doi:10.1109/iccc57093.2023.10178893 · Cited by 21
Chang, L., & Hu, Y. H. (2018) · Elsevier eBooks · doi:10.1016/b978-0-12-809597-3.00247-9 · Cited by 22
Boonmongkolras, P., Kim, S., Kim, Y. Y., Jeon, N. J., Lee, M. H., & Han, G. S. (2025) · Advanced Functional Materials · doi:10.1002/adfm.202525129 · Cited by 11
(2021) · Indonesian Journal of Aerospace · Cited by 6
Combined Power and Attitude Control System for Low Earth Orbit Satellites
Saad, A. I., Saad, N. H., & Ezzat, M. (2019) · International Middle East Power Systems Conference (MEPCON) · doi:10.1109/mepcon47431.2019.9008176 · Cited by 5
Behavior of an aqueous electrolyte supercapacitor under hypergravity
Khakzadeh, E., Ahadzadeh, I., Hosseini, M. G., & Golmohammadi, S. (2026) · Journal of Energy Storage · doi:10.1016/j.est.2026.121222 · Cited by 4
Improving the Satellite Power Supply Continuity using Flywheel Energy Storage System
El-Arwash, H. M., & Attalla, M. E. A. (2021) · ERJ Engineering Research Journal · doi:10.21608/erjm.2021.87309.1105 · Cited by 4
Optimizing the Connection Time for LEO Satellite Based on Dynamic Sensor Field
Truong, T. P., Tran, H. V., Huynh, H. X., & Pottier, B. (2016) · Lecture notes of the Institute for Computer Sciences, Social Informatics and Telecommunications Engineering · doi:10.1007/978-3-319-29236-6_36 · Cited by 3
Design Control and Power Management of Small Satellite Microgrids
Yaqoob, M. (2022) · VBN Forskningsportal (Aalborg Universitet) · doi:10.54337/aau527274534 · Cited by 3
Design of Battery Balancing Unit of Satellite Using BQ77PL900
Affan, M., Abdul‐Malek, Z., Sidik, M. A. B., Ali, M., Esa, M. R. M., Nawawi, Z., Munir, A., & Jambak, M. I. (2019) · doi:10.1109/icecos47637.2019.8984482 · Cited by 2
Chang, L., & Hu, Y. H. (2025) · Elsevier eBooks · doi:10.1016/b978-0-44-313219-3.00017-4
Metadata
- Authors
- Abdi, B., Alimardani, A., Ghasemi, R., & Mirtalaei, S. M. M.
- Affiliations
- Islamic Azad University, Tehran (IR)
- Venue
- International Journal of Machine Learning and Computing
- Publisher
- EJournal Publishing
- Published
- 2013
- Pages
- 287-290
- ISSN
- 2010-3700 (ISSN-L)
- OpenAlex
- W2319590269
- Cited by
- 13
- References
- 8
- Citations by year
- 2026: 1 · 2025: 2 · 2024: 1 · 2023: 1 · 2022: 2 · 2021: 2 · 2019: 2 · 2018: 1 · 2016: 1
- FWCI
- 0.54
- Type
- journal article
- Language
- en
- Open access
- bronze
- doi.org
- Locations
- International Journal of Machine Learning and Computing (publishedVersion)
- Topics
- Physical Sciences › Engineering › Aerospace Engineering › Spacecraft Design and Technology
- Physical Sciences › Engineering › Automotive Engineering › Battery Modeling and Management
- Physical Sciences › Engineering › Aerospace Engineering › Spacecraft Dynamics and Control
- Keywords
- energy storage systems, low Earth orbit satellites, chemical batteries, flywheel, eclipse duration, satellite power systems, self-discharge, storage reliability, operating temperature
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