4.7 Article

Fuzzy-based optimal energy management strategy of series hybrid-electric propulsion system for UAVs

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JOURNAL OF ENERGY STORAGE
卷 68, 期 -, 页码 -

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ELSEVIER
DOI: 10.1016/j.est.2023.107712

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Equivalent consumption minimum strategy; Energy management; Fuzzy logic control; Hybrid-electric propulsion system; Unmanned aerial vehicle

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Hybrid-electric propulsion system (HEPS) is gaining attention in UAVs for its potential to reduce fuel consumption and emissions. This study introduces a fuzzy logic control-equivalent consumption minimum strategy (FLC-ECMS) that improves energy management in HEPS. Simulation tests show that HEPS-equipped hybrid UAVs can significantly decrease fuel consumption and emissions, while maintaining battery state of charge (SOC) and reducing SOC difference. This research provides insights into optimal energy management for HEPS in UAVs, highlighting the importance of UAVs in reducing environmental impacts.
Hybrid-electric propulsion system (HEPS) has gained significant attention in unmanned aerial vehicles (UAVs) due to its potential to significantly reduce fuel consumption and pollutant emissions. Effective energy management strategies are crucial in ensuring the efficient operation of HEPS in UAVs, as they involve multiple power and energy sources. While conventional equivalent consumption minimum strategy (ECMS) is effective in distributing engine and battery output power, it struggles to maintain the battery's state of charge (SOC) within desired levels in case of engine failure. The present study introduced the fuzzy logic control-equivalent consumption minimum strategy (FLC-ECMS), a fuzzy-based composite energy management strategy that incorporates the robustness and adaptability of fuzzy logic control. Through simulation tests under general aviation cruise flight and cargo transport flight scenarios, the results indicated that hybrid UAV equipped with the HEPS can decrease fuel consumption and CO2 emissions by at least 18.6% and NO ������ emissions by 10.1% in the first profile and by 23.6% and 11.2% in the second profile, compared to conventional oil-powered UAV. The FLC-ECMS method not only reduces fuel consumption and emissions, but also maintains the battery SOC within permitted range and minimizes the difference between front and back SOC. This study provides new insights into the optimal energy management of HEPS for complex profiles in UAVs, highlighting the significance of UAVs in reducing environmental impacts, and has the potential for broader application in other electric propulsion systems.

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