The invention relates to a switching circuit for an unmanned aerial vehicle. The switching circuit comprises a first switching unit, a
current limiting unit, a second switching unit and a
delay unit,wherein the input end, control end and output end of the first switching unit are correspondingly connected with an external power supply, a conduction unit and one end of the
current limiting unit, the other end of the
current limiting unit is connected with a load, the input end, control end and output end of the second switching unit are correspondingly connected with the external power supply,the conduction unit and the input end of the
delay unit, and the output end of the
delay unit is connected with the load. When the external power supply is required to supply power to the load, the conduction unit is switched on to provide a conduction
voltage for the first switching unit and the second switching unit to connect the first switching unit and the second switching unit, the currentlimiting unit exists in a
branch circuit where the first switching unit is located to limit a surge current generated immediately when the external power supply is turned on and, meanwhile, the delayunit exists in a
branch circuit where the second switching unit is located, connected in parallel with the
branch circuit to switch on the branch circuit where the second switching unit is located after a delay. Therefore, an input current is provided for the load after current and
voltage stabilization.