An aircraft control system includes: a motor with a rotating shaft; a pilot control input; a linear actuator connecting the pilot control input to the rotating shaft; a sensor identifying a position of the pilot control input; and a transmitter transmitting the pilot control input position to a controller, the controller adjusting an aircraft performance device based on the received pilot control input position.
AIRCRAFT TORQUE CONTROL DEVICE
2021-12-02
Patent
Electronic Resource
English
European Patent Office | 2018
|European Patent Office | 2018
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