The invention belongs to the technical field of
hybrid power supply, and discloses a start and power generation integrated unmanned aerial vehicle miniature
hybrid power
system and a start method. Thesystem comprises a two-
stroke piston engine, a start and power generation integrated motor, a
position sensor, a
motor controller, and a power source, a rotor shaft of the start and power generationintegrated motor is coupled to a
crankshaft of the two-
stroke piston engine, the
motor controller includes a
driving circuit, a rectifying circuit, a charge-
discharge circuit, a first
diode, a seconddiode and a two-way
relay, the
driving circuit comprises a driving
chip, one end of the rectifying circuit is connected with the power source, and the other end of the rectifying circuit is grounded,the output end of the rectifying circuit is connected with the start and power generation integrated motor, the charge-
discharge circuit comprises a first super
capacitor and a second super
capacitor,the first super
capacitor is connected with the first
diode in series to form a first series circuit, the second super capacitor and the second
diode are connected in series to form a second series circuit, and the first series circuit and the second series circuit are connected with the rectifying circuit in parallel. The
system has the
advantage of reducing start resistance and resistance moment fluctuation.