Battery Current and Temperature Mission Profiles for CubeSats at Low Earth Orbit
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21230%2F22%3A00357883" target="_blank" >RIV/68407700:21230/22:00357883 - isvavai.cz</a>
Result on the web
<a href="https://doi.org/10.1109/TAES.2022.3164867" target="_blank" >https://doi.org/10.1109/TAES.2022.3164867</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1109/TAES.2022.3164867" target="_blank" >10.1109/TAES.2022.3164867</a>
Alternative languages
Result language
angličtina
Original language name
Battery Current and Temperature Mission Profiles for CubeSats at Low Earth Orbit
Original language description
CubeSats, a branch of the space industry, has lately received great interest for being an affordable satellite platform. For proper functioning, they are nowadays practically dependent on Lithium-ion batteries as a power supply at moments, when there is not enough power generated by solar panels. Thus, batteries have to be thoroughly tested to ensure that they provide sufficient performance, lifetime and that they are safe. In other industry areas, such as electric vehicles, it is common to use mission profiles (often referred to as driving profiles) for battery testing to closely emulate conditions that are experienced in practice. However, mission profiles reflecting closely CubeSat conditions are not publicly available. Thus, this paper proposes a methodology to derive mission profiles, and resulting representative mission profiles, dedicated especially to battery testing. The proposed methodology is based on analyzed telemetry data from three GOMX CubeSats. At first, electrical current characteristics are obtained from the telemetry and are generalized across the satellites, to be subsequently used for the mission profile synthesis. The battery temperature is an important factor for the battery performance and lifetime, and it was identified to be very dynamic in CubeSats. Thus, a model describing battery temperature during their mission is proposed to enable generate realistic temperature mission profiles. Finally, the current and temperature profiles are synchronized to capture their mutual impact on the batteries, and they are formulated to be suitable for on-ground (laboratory) testing.
Czech name
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Czech description
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Classification
Type
J<sub>imp</sub> - Article in a specialist periodical, which is included in the Web of Science database
CEP classification
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OECD FORD branch
20201 - Electrical and electronic engineering
Result continuities
Project
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Continuities
I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace
Others
Publication year
2022
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Name of the periodical
IEEE Transactions on Aerospace and Electronic Systems
ISSN
0018-9251
e-ISSN
1557-9603
Volume of the periodical
58
Issue of the periodical within the volume
5
Country of publishing house
US - UNITED STATES
Number of pages
13
Pages from-to
4656-4668
UT code for WoS article
000866503000069
EID of the result in the Scopus database
2-s2.0-85127731721