An aircraft control of the rudder bar type, which includes a box-shaped pedal, a support, a first rotation shaft connecting the pedal to the support with a first rotation axis, a first pivot connection configured to allow the pedal to pivot about the first rotation axis relative to the support, a rod, a second rotation shaft, distinct from the first rotation shaft and connecting the pedal to the rod with a second rotation axis, and a second pivot connection configured so as to allow the pedal and/or the rod to pivot about the second rotation axis.