Minimization and Fuel Economy of Hybrid Fuel Cell Electric Systems Based on Conventional Energy Management PI (Application for an aircraft)
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DOI:
https://doi.org/10.5281/zenodo.14897902Keywords:
MEA, Hybrid system, PEMFC, Classical PI strategy, SC, SOCAbstract
With the transition of the aviation industries to more electric aircraft (MEA), there is an
increase in the maximum electrical load observed by the main and emergency generators compared to
traditional aircraft. Therefore , the aircraft emergency system, consisting of an air turbine or air driven
generator (ADG), is highly concerned about the need to meet energy demand in critical situations,
especially at low speed where the power delivered is extremely low. Many aircraft manufacturers are
considering an alternative to replacing the air turbine with a hybrid fuel cell system, combined with
various sources.
The proposed model of the hybrid system of a more electric aircraft is implemented under MATLAB /
SIMULINK in order to simulate and study an energy management strategy known as the classic PI in
order to show the different behaviors of the power of a more electric aircraft according to the variations
of the fuel cell power and the SC power, as well as the SOC of the battery, the fuel consumption and the
DC bus voltage.
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