MULTIPLE DEGREES OF TRANSLATIONAL ADJUSTMENT PEDALS

摘要

A pedal system for an aircraft comprising a pedal and a pedal mounting mechanism is provided. The pedal is configured for manipulation through at least one operational degree of freedom by a pilot to provide control inputs to the aircraft. The pedal mounting mechanism is configured for supporting the pedal within a cockpit of the aircraft for manipulation by the pilot. The pedal mounting mechanism provides at least two adjustment degrees of freedom for adjusting the position of the pedal within the cockpit.