Abstract
This paper proposes a novel Hybrid Electric Propulsion System (HEPS) architecture based on adaptive droop control, comprising a Permanent Magnet Synchronous Generator (PMSG), a Fuel Cell (FC), and a Lithium-ion (Li-ion) battery. The system employs a voltage-compensated adaptive droop control strategy integrated with a state machine energy management strategy (SMEMS), enabling the three energy sources to coordinate effectively and meet the power demands of the aircraft efficiently under various operating conditions. The paper includes a detailed analysis and modeling of each energy source and develops corresponding PI control strategies. The feasibility of the proposed topology is confirmed by the simulation results, demonstrating the coordinated performance and stability of the system.
Original language | English |
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Title of host publication | CSAA/IET International Conference on Aircraft Utility Systems, AUS 2024 |
Publisher | Institution of Engineering and Technology |
Pages | 1171-1177 |
Number of pages | 7 |
Volume | 2024 |
Edition | 13 |
ISBN (Electronic) | 9781837240852, 9781837241217, 9781837241224, 9781837241484, 9781837241521, 9781837241552, 9781837241842, 9781837241880, 9781837241910, 9781837241927, 9781837241958, 9781837241989, 9781837242108, 9781837242115, 9781837242139, 9781837242153, 9781837242160, 9781837242177, 9781837242252, 9781837242405, 9781837242412, 9781837242535, 9781837242672 |
DOIs | |
State | Published - 2024 |
Event | 2024 CSAA/IET International Conference on Aircraft Utility Systems, AUS 2024 - Xi�an, China Duration: 16 Aug 2024 → 19 Aug 2024 |
Conference
Conference | 2024 CSAA/IET International Conference on Aircraft Utility Systems, AUS 2024 |
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Country/Territory | China |
City | Xi�an |
Period | 16/08/24 → 19/08/24 |
Keywords
- ADAPTIVE DROOP CONTROL
- HYBRID PROPULSION AIRCRAFT SYSTEM
- PI CONTROL
- STATE MACHINE