A flight control system (100, 200) for a flight control surface (102) includes a first actuator control electronics (ACE) (202), a second ACE (204), a third ACE (206), a first remote electronics unit (REU) (208), and a second REU (210). The first ACE (202) is configured to generate a first control signal for the flight control surface (102). The second ACE (204) is configured to generate a second control signal for the flight control surface (102). The third ACE (206) is configured to generate a third control signal for the flight control surface (102). The first REU (208) is coupled to the first ACE (202) and the second ACE (204), and configured to operate, based on the first control signal and the second control signal, an actuator (216, 220) coupled to the flight control surface (102). The second REU (210) is coupled to the second ACE (204) and the third ACE (206), and configured to operate, based on the second control signal and the third control signal, the actuator (216, 220).
СИСТЕМА УПРАВЛЕНИЯ ПОЛЕТОМ И СПОСОБ ИСПОЛЬЗОВАНИЯ
05.03.2020
Patent
Elektronische Ressource
Russisch
IPC: | G08G Anlagen zur Steuerung, Regelung oder Überwachung des Verkehrs , TRAFFIC CONTROL SYSTEMS |
Способ управления воздушным судном, система управления и воздушное судно
Europäisches Patentamt | 2018