Paper
13 May 2024 Modelling of unmanned aerial vehicle power battery considering temperature hysteresis effect and capacity loss
Chuang Cai, Wei Chen, Ping Yi, Liyang Lin
Author Affiliations +
Proceedings Volume 13159, Eighth International Conference on Energy System, Electricity, and Power (ESEP 2023); 131593X (2024) https://doi.org/10.1117/12.3024281
Event: Eighth International Conference on Energy System, Electricity and Power (ESEP 2023), 2023, Wuhan, China
Abstract
In order to improve the accuracy of the equivalent circuit model, on the basis of the second-order RC model, the effect of temperature on the hysteresis electromotive force is investigated and a temperature influence coefficient is added to the single-state model; the effect of temperature on the actual usable capacity of the battery is analyzed, and a correction coefficient considering the capacity loss is proposed. Finally, the dynamic current working condition is simulated and verified by experiments using the constructed model. The results show that the established model can fit the operating characteristics of the battery well, and the error with the experimental voltage is only about 20 mV, which is about 2.48% higher than that of the traditional second-order RC model.
(2024) Published by SPIE. Downloading of the abstract is permitted for personal use only.
Chuang Cai, Wei Chen, Ping Yi, and Liyang Lin "Modelling of unmanned aerial vehicle power battery considering temperature hysteresis effect and capacity loss", Proc. SPIE 13159, Eighth International Conference on Energy System, Electricity, and Power (ESEP 2023), 131593X (13 May 2024); https://doi.org/10.1117/12.3024281
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KEYWORDS
Batteries

Temperature metrology

Unmanned aerial vehicles

Circuit switching

Polarization

Resistance

Modeling

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