FIELD: aviation.
SUBSTANCE: aircraft actuating system comprising electromechanical actuator (25) comprising a nonvolatile memory (60) storing stored data (61) including configuration data (62) relating to said electromechanical actuator; control unit (22) using said configuration data in order to implement a servo control cycle, the output signal being a digital signal controlling the electric motor of said electromechanical actuator; at least one digital information transferring channel (50) connects the control unit and the electromechanical actuator.
EFFECT: complexity of the electric actuating system is reduced.
17 cl, 9 dwg
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Authors
Dates
2018-08-14—Published
2016-11-30—Filed