Abstract: A device for controlling aircraft maneuvering units includes at least one control unit and a central computing unit. The control unit may be actuated by a pilot for issuing maneuvering commands. The central computing unit is capable of establishing control signals for at least one maneuvering unit from the maneuvering commands. Each central computing unit is being provided with its own failure detection system. The device further includes at least one backup electronic module respectively associated with a maneuvering unit and capable of also establishing control signals for this maneuvering unit from maneuvering commands. The electronic module lacks any failure detection system of its own, but it is connected to a central failure detection system.

Abstract: Device for controlling aircraft maneuvering units including:

Abstract: A method is provided for arranging the components and power connection points within an electromechanical braking system architecture in order to better maintain isolation of the power busses, and thereby improve overall integrity of the system, while still meeting system redundancy, performance and safety requirements as in the past. In addition, a method is provided for connecting and efficiently using available power in emergency braking and parking modes.