公开(公告)号：EP4215437A1

公开(公告)日：2023-07-26

申请号：EP23152827.4

申请日：2023-01-23

申请人： Airbus Operations Limited

发明人： IZQUIERDO CIVERA, Fernando ,  PIDDOCK, Alex ,  JOHNSON, Mark

IPC分类号： B64C13/16 ,  B64C25/26 ,  B64C25/42 ,  B64C25/50

摘要： Disclosed is an aircraft control system 100 for controlling actuation of an aircraft component 700, the system comprising a control assembly 110 having control units, including a first control unit 130 for controlling actuation of the aircraft component during a first time period, using electrical resource 512 from a first electrical resource device 510, and a second control unit 140 for controlling actuation of the aircraft component during a second time period, and a switch mechanism 120 for switching control of the actuation of the aircraft component between the first and second control units, wherein the switch mechanism has a first electrical resource device status input 513 for indicating the status of the first electrical resource device 510 and wherein, the switch mechanism is configured to switch control between the first 130 and second 140 control units based on the first electrical resource device status input 513. Also disclosed is an aircraft 1000, aircraft assembly and a method of controlling an aircraft component of an aircraft.