Power-assisted control system for a rotorcraft

摘要: An assisted control system for controlling the attitude of a rotorcraft comprises flight device; at least one member configured to act on an aerodynamic element rotorcraft; mechanical connection connecting device member, including rod moveable in translation, crank pivotably disposed about stationary support shaft passing through device, and motor drive rotor stator facilitate pivoting movement support; rotation relative stator; sensor measure information representative operation performed by under pilot deliver signal device.