Abstract: 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.
Type:
Application
Filed:
October 15, 2019
Publication date:
December 2, 2021
Applicant:
Safe Flight lnstrument Corporation
Inventors:
Michael LAMBTON, Louis SIMONS, Randall A. GREENE