Acta Aeronautica et Astronautica Sinica ›› 2024, Vol. 45 ›› Issue (17): 530032-530032.doi: 10.7527/S1000-6893.2023.30032
• Articles • Previous Articles
Shuhao DENG1(), Tao LEI1,2, Xianqiu JIN1, Junxiang CHEN3, Daiwen HUANG3, Xiaobin ZHANG1,2
Received:
2023-12-27
Revised:
2024-02-21
Accepted:
2024-03-25
Online:
2024-04-19
Published:
2024-04-19
Contact:
Shuhao DENG
E-mail:shuhao_d@163.com
Supported by:
CLC Number:
Shuhao DENG, Tao LEI, Xianqiu JIN, Junxiang CHEN, Daiwen HUANG, Xiaobin ZHANG. Stability and power control method of hybrid power system for fuel cell UAVs[J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(17): 530032-530032.
Table 2
Rule-based energy management strategies
约束条件 | 状态 | PFC计算值 |
---|---|---|
If SOC High & PCPL<PFCmin | State 1 | PFC=PFCmin |
If SOC High & PCPL∈[PFCmin, PFCmax] | State 2 | PFC=PCPL |
If SOC High & PCPL>PFCmax | State 3 | PFC=PFCmax |
If SOC Normal & PCPL<PFCmin | State 4 | PFC=PFCmin |
If SOC Normal & PCPL∈[PFCmin,PFCopt] | State 5 | PFC=PFCopt |
If SOC Normal & PCPL∈[PFCopt,PFCmax] | State6 | PFC=PCPL |
If SOC Normal & PCPL>PFCmax | State 7 | PFC=PFCmax |
If SOC Low & PCPL<PFCmin | State 8 | PFC= PFCmin |
If SOC Low & PCPL∈[PFCmin,PFCopt] | State 9 | PFC=max(PCPL+Pbatchar, PFCopt) |
If SOC Low & PCPL∈[PFCopt,PFCmax] | State10 | PFC= PCPL+Pbatchar |
If SOC Low & PCPL>PFCmax | State11 | PFC=PFCmax |
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