The utility model relates to the field of unmanned aerial vehicles, and provides a converter for a fuel
cell of an unmanned aerial vehicle, which comprises a
boost chopper circuit and a half-bridge resonant circuit, the
boost chopper circuit is connected with the half-bridge resonant circuit in parallel, and the
boost chopper circuit comprises a
direct current power supply a, a fly-wheel
diode a, a full-control device a, an
inductor a, a
capacitor a and a
resistor a, the positive
electrode of the direct-current power supply a is connected with the
inductor a, the
inductor a is respectively connected with the fly-wheel
diode a and the full-control device a, the fly-wheel
diode a is respectively connected with the
capacitor a and the
resistor a, and the full-control device a, the
capacitor a and the
resistor a are connected with the negative
electrode of the direct-current power supply a. When in use, the unmanned aerial vehicle has the advantages of high efficiency, stability, small size,
energy conservation,
environmental protection and the like, the space and the weight of the unmanned aerial vehicle are saved, the stability and the control precision of the unmanned aerial vehicle are enhanced, and stable flight of the unmanned aerial vehicle and normal operation of equipment are ensured.