The invention relates to a system (9) for controlling actuators in an aircraft, the system comprising at least a first actuator (2-a) and a second actuator (2-b) each comprising: - a movement member (3-a, 3-b); - at least one measurement sensor (4-a, 4-b); and - a computing member (5-a, 5-b) internally connected to the movement member (3-a, 3-b) and configured to be connected to at least one electronic computer (1) of the aircraft, the computing member (5-a, 5-b) having a function (COM) for controlling the movement member (3-a, 3-b), the measurement sensor (4-a) of the first actuator (2-a) being externally connected to the computing member (5-b) of the second actuator (2-b), the computing member (5-b) of the second actuator (2-b) also having a function (MON) for monitoring the movement member (3-a) of the first actuator (2-a).
SYSTÈME ET PROCÉDÉ DE PILOTAGE D'ACTIONNEURS DANS UN AÉRONEF
SYSTEM AND METHOD FOR CONTROLLING ACTUATORS IN AN AIRCRAFT
SYSTEM UND VERFAHREN ZUR STEUERUNG VON AKTUATOREN IN EINEM FLUGZEUG
2025-02-19
Patent
Electronic Resource
French
IPC: | B64C AEROPLANES , Flugzeuge |
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