Abstract: In an electric power steering system, an electric motor generates output power for power-assisting steering operation of a steering wheel, a torque sensor generates a plurality of electric output signals corresponding to a torque applied to the steering wheel, and a control unit controls the steering operation of the electric motor in accordance with at least one of the electric output signals of the torque sensor. The control unit detects a difference between rotation speeds of left and right steered wheels, checks whether any one of the plurality of output generating parts is in failure, and specify a failing-device based on the rotation speed difference and the plurality of output signals.

Abstract: Disclosed is a method of detecting at least one oscillatory fault in at least one positional slaving chain for at least one airfoil of an aircraft. The method involves estimating a reference position of the airfoil in the absence of a fault, and calculating a residual value based on the difference between the estimated reference position and the actual position measured by at least one sensor. The calculated residual value is compared with at least one predetermined threshold value to determine the number of successive and alternating overshoots of the predetermined threshold value by the residual value, and oscillatory fault is determined based on the determined number.

Abstract: The fields of the invention are vehicle on-board security and vehicle piloting safety. The invention relates to a method and device for aiding the restoral of command of a vehicle by an operator of the vehicle. The command of the vehicle by the operator is ensured through vehicle piloting controls, when the operator has lost command of the vehicle in favor of a device for disabling piloting controls. The device disables the action of the piloting controls on the piloting means during the loss of command. According to the invention, the method includes emitting a restoral of command request; a vehicle motion phase is determined; a reference state of the piloting control is determined as a function of the motion phase; a current state of the piloting control is determined; the current state with the reference state is compared so as to identify a deviation ? between the current state and the reference state. When no deviation ? is identified, the command of the vehicle by the operator is restored.