A system for controlling actuators in an aircraft. The system including at least a first actuator and a second actuator. Each of the actuators including a movement member, at least one measurement sensor, and a computing member internally connected to the movement member and configured to be connected to at least one electronic computer of the, aircraft. The computing member having a function for controlling the movement member, the measurement sensor of the first actuator being externally connected to the computing member of the second actuator, the computing member of the second actuator also having a monitoring function for monitoring the movement member of the first actuator.
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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