The battery characterization and modelling of a Lithium-ion battery aimed at supporting the design of the energy storage system of an All-Electric Aircraft (AEA) is presented. Specifically, the developed model is employed to evaluate the energy and power performance of a battery pack designed for the AEA concept X- 57 Maxwell Mod.II. The preliminary battery pack sizing is performed referring to a project-flight mission-oriented to air city taxing. The evaluation of the design targets satisfaction has been ver ified through a simulation study based on the proposed battery modelling. The comparison between the simulation and preliminary results confirms the need of employing a battery dynamic model for designing AEA’s battery pack that satisfies all targets imposed.
Bossi, G., Floris, A., Campagna, N., Miceli, R., Damiano, A. (2023). Design of a Battery Pack for the Power System of an All-Electric Aircraft by Cell Characterization. In 2023 International Conference on Clean Electrical Power, ICCEP 2023 (pp. 76-82) [10.1109/iccep57914.2023.10247381].
Design of a Battery Pack for the Power System of an All-Electric Aircraft by Cell Characterization
Campagna, Nicola;Miceli, Rosario;
2023-01-01
Abstract
The battery characterization and modelling of a Lithium-ion battery aimed at supporting the design of the energy storage system of an All-Electric Aircraft (AEA) is presented. Specifically, the developed model is employed to evaluate the energy and power performance of a battery pack designed for the AEA concept X- 57 Maxwell Mod.II. The preliminary battery pack sizing is performed referring to a project-flight mission-oriented to air city taxing. The evaluation of the design targets satisfaction has been ver ified through a simulation study based on the proposed battery modelling. The comparison between the simulation and preliminary results confirms the need of employing a battery dynamic model for designing AEA’s battery pack that satisfies all targets imposed.
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