Flight control assembly and unmanned aerial vehicle

The invention provides a flight control assembly. The flight control assembly comprises a flight control board, and further comprises damping structures connected to the flight control assembly; the flight control assembly is connected with a supporting body through the damping structures; the damping structures are used for damping vibration of the flight control assembly from the supporting body to realize overall damping of the flight control assembly. The invention further relates to an unmanned aerial vehicle employing the flight control assembly.