公开(公告)号：WO2020081615A1

公开(公告)日：2020-04-23

申请号：PCT/US2019/056403

申请日：2019-10-15

Applicant: SAFE FLIGHT INSTRUMENT CORPORATION

Inventor： LAMBTON, Michael ,  SIMONS, Louis ,  GREENE, Randall A.

IPC: B64C13/00 ,  B64C13/04 ,  B64C13/38 ,  B64C13/50 ,  B64D31/00 ,  B64D31/04 ,  B64D31/14

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.