A
rudder pedal
input control device (100, 200, 300, 400A, 400B, 500, 600) is described that utilizes a linear mechanism and a rotary joint to achieve
linear motion within a compact volume. The apparatus includes a lever linkage (106, 108, 206, 208, 306, 308, 506, 606) that converts forward movement of the pedals (110, 112, 210, 212, 310, 312, 510, 610) into rotational movement of the common shaft (102, 202, 302, 502, 602) such that forward movement of one pedal (110, 112, 210, 212, 310, 312, 510, 610) causes retraction of the other pedal (110, 112, 210, 212, 310, 312, 510, 610) while allowing
yaw movement control of the aircraft.