Aircraft electromagnetic attraction pedal disk device

The invention discloses an aircraft electromagnetic attraction pedal disk device which comprises a pedal disk body structure, an electromagnetic locking device, a metal antiskid cushion, a force sensor, a controller and a power supply. The force sensor is connected with the upper portion of the pedal disk body structure. A groove is formed in the bottom of the pedal disk body structure. The electromagnetic locking device is embedded in the groove. The metal antiskid cushion is detachably connected to the bottom of the pedal disk body structure. The electromagnetic attraction pedal disk deviceis installed at the lower end of a vertical aircraft takeoff and landing device or the lower end of a bionic aircraft limb, and an aircraft stops on a shaking horizontal landing surface or a verticalsurface under the action of electromagnetic attraction force and friction force. The aircraft electromagnetic attraction pedal disk device has the replaceability property and can be detached or replaced with other foot structu