Research Article
Fuzzy State Machine Energy Management Strategy for Hybrid Electric UAVs with PV/Fuel Cell/Battery Power System
Table 1
Comparison of the Aerosonde UAV and hybrid electric UAV.
| | Aerosonde UAV | Hybrid electric UAV |
| Configuration size | Length (m) | 1.74 | Length (m) | 1.74 | Wingspan (m) | 2.87 | Wingspan (m) | 2.87 | Wing area (m2) | 0.55 | Wing area (m2) | 0.55 |
| Weight distribution (kg) | Airframe | 3.6 | Airframe | 3.6 | Avionics/payload | 2.1 | Avionics/payload | 2.1 | Fuel and fuel tank | 5.6 | H2 and tank | 0.9 | Power plant | 2.2 | BLDC motor | 0.4 | Electric speed controller | 0.04 | Propeller | 0.06 | Fuel cell | 3 | Li battery | 0.9 | PV panel | 1 | DCDC converter | 1.2 | MPPT | 0.1 | Flight controller | 0.2 | Gross weight | 13.5 | Gross weight | 13.5 |
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