RUDDER PEDAL CONTROL DEVICE AND CONTROL METHOD FOR AIRPLANE

摘要

Disclosed is a rudder pedal control device for an airplane, wherein a brake pedal connecting rod thereof can be shortened and is provided with a first sensor, and a brake sensing signal is generated by the first sensor when the brake pedal connecting rod is compressed because there is no rotation of a brake pedal crank relative to a rudder pedal control rocking arm. The rudder pedal control device comprises a second sensor for sensing the relative rotation between the brake pedal crank and the rudder pedal control rocking arm; a speed comparator for comparing the current speed of the airplane with a predetermined speed; and a controller for electrically connecting the first sensor, the second sensor and the speed comparator, and shielding the brake sensing signal generated by the first sensor when the second sensor senses that there is no rotation of the brake pedal crank relative to the rudder pedal control rocking arm and the current speed compared by the speed comparator is greater than the predetermined speed.