2023
DOI: 10.1016/j.egyai.2023.100233
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Prognostics for Lithium-ion batteries for electric Vertical Take-off and Landing aircraft using data-driven machine learning

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Cited by 14 publications
(5 citation statements)
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“…To cope with the wide operating range of EVs and always deliver reliable SOH estimation, there exist some early works to formulate the estimation task based on different usage profiles. Mitici et al [31] constructed the features based on the charge and discharge process and conducted a feature importance analysis. However, the highly dynamic discharging process and irregular charging profiles may hinder the performance of such a method in real-world EV applications.…”
Section: Introductionmentioning
confidence: 99%
“…To cope with the wide operating range of EVs and always deliver reliable SOH estimation, there exist some early works to formulate the estimation task based on different usage profiles. Mitici et al [31] constructed the features based on the charge and discharge process and conducted a feature importance analysis. However, the highly dynamic discharging process and irregular charging profiles may hinder the performance of such a method in real-world EV applications.…”
Section: Introductionmentioning
confidence: 99%
“…Nevertheless, the advantages of the PEMFCs make them perfect alternatives to fossil based power systems. Technical specifications related to different research topics of PEMFCs can be tracked in several publications [4][5][6][7].…”
Section: Introductionmentioning
confidence: 99%
“…Correspondingly, the typical eVTOL designs require a power-to-energy ratio (effective discharge rates) ranging from 10C to 60C with peak power required both at the beginning of the discharge cycle (low depth of discharge) and end of discharge (high depth of discharge) as shown schematically in Figure A. In specific power terms, these values can potentially exceed 1000 kW/kg depending on the mass of the payload, mission profile, and aircraft design. ,, …”
mentioning
confidence: 99%
“…In specific power terms, these values can potentially exceed 1000 kW/kg depending on the mass of the payload, mission profile, and aircraft design. 2,22,23 In recent years, significant research efforts have been directed toward enhancing the energy density, power output, and overall performance of LiBs. 24 However, the extreme power demands inherent to eVTOL operations necessitate a specialized investigation.…”
mentioning
confidence: 99%
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