Multi-power-source series-connection type hybrid power unmanned aerial vehicle and control method thereof
A hybrid power and unmanned aerial vehicle technology, applied in the field of aviation aircraft, can solve the problems of low survivability and poor mobility
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[0081] In order to facilitate the understanding of those skilled in the art, the present invention will be further described below in conjunction with the embodiments and accompanying drawings, and the contents mentioned in the embodiments are not intended to limit the present invention.
[0082] refer to Figure 1-Figure 4 Shown, a kind of multi-power source tandem hybrid unmanned aerial vehicle of the present invention comprises: fuselage 22, left wing 18 (relative to nose), right wing 32, left aileron 19, right aileron 31 , left flap 20, right flap 30, empennage 34, left wing motor, left wing propeller, right wing motor, right wing propeller, spare propeller module, horizontal stabilizer 35, vertical stabilizer 37, elevator 39, rudder 36, engine 26, clutch 25. Inverter 10, generator / electric integrated machine 24, battery pack 8, super capacitor 9, fuel tank, temperature sensor 7, pressure sensor 11, state of charge (SOC) estimation module 28 and control module 23;
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