TY - GEN
T1 - Modeling and Control of a Hybrid Power System for Electric Propulsion Aircraft
AU - Liang, Siyang
AU - Zhao, Hongwei
AU - Yang, Tao
AU - Wang, Xin
AU - Qi, Yang
AU - Li, Weilin
N1 - Publisher Copyright:
© 2024 The Institute of Electrical Engineers of Japan.
PY - 2024
Y1 - 2024
N2 - This paper proposes a novel Hybrid Electric Propulsion System (HEPS) architecture for electric propulsion aircraft, containing a Fuel Cell (FC), a Permanent Magnet Synchronous Generator (PMSG), and a Li-ion battery. Through the coordination of these three sources, the system can meet the requirements of high-power discharge and efficient energy storage, thereby satisfying the aircraft's power demands across a range of operating conditions. All power sources are connected to a DC bus in parallel through the corresponding converters to supply the load. This paper presents modeling and analysis of each power source and converter in the system separately. By simulating the system under different control strategies, the results validate the feasibility of the modeling, the load-sharing performance of the HEPS, and the system stability.
AB - This paper proposes a novel Hybrid Electric Propulsion System (HEPS) architecture for electric propulsion aircraft, containing a Fuel Cell (FC), a Permanent Magnet Synchronous Generator (PMSG), and a Li-ion battery. Through the coordination of these three sources, the system can meet the requirements of high-power discharge and efficient energy storage, thereby satisfying the aircraft's power demands across a range of operating conditions. All power sources are connected to a DC bus in parallel through the corresponding converters to supply the load. This paper presents modeling and analysis of each power source and converter in the system separately. By simulating the system under different control strategies, the results validate the feasibility of the modeling, the load-sharing performance of the HEPS, and the system stability.
KW - equivalent Hydrogen Consumption Strategy
KW - hybrid propulsion aircraft system
KW - PI control
KW - state machine
UR - http://www.scopus.com/inward/record.url?scp=105002373314&partnerID=8YFLogxK
U2 - 10.23919/ICEMS60997.2024.10921202
DO - 10.23919/ICEMS60997.2024.10921202
M3 - 会议稿件
AN - SCOPUS:105002373314
T3 - 2024 27th International Conference on Electrical Machines and Systems, ICEMS 2024
SP - 1590
EP - 1595
BT - 2024 27th International Conference on Electrical Machines and Systems, ICEMS 2024
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 27th International Conference on Electrical Machines and Systems, ICEMS 2024
Y2 - 26 November 2024 through 29 November 2024
ER -