ELECTRIC FLIGHT CONTROL SYSTEM FOR AN AIRCRAFT HAVING A DETECTION OF OSCILLATORY PILOTAGE COUPLINGS AND A PILOTAGE MEMBER FOR SUCH A SYSTEM

摘要

P - Electric flight control system for aircraft comprising a detection of oscillatory piloting couplings and piloting member for such a system. According to the invention, provision is made for damping the tilting of said piloting member (2) by controllable damping means (15, 16), controlled by means (7) detecting the oscillations corresponding to said oscillatory pilot couplings. /P