Method for selecting control instruction of flight control computer
By adding communication lines between adjacent secondary computers in the flight control system, the problem of rudder force oscillation caused by the secondary computer entering the downgrade mode is solved, and the stable control of the aircraft and the automatic landing capability of CAT IIIb are realized.
Patent Information
- Application Number
- CN202510466437.2
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2025-04-14
- Publication Date
- 2025-08-01
AI Technical Summary
After the computer enters the downgrade mode of the existing flight control system, the flight control system enters the hybrid mode, causing disputes in the rudder surface force oscillation, affecting the aircraft's handling performance and safety, and failing to meet the requirements of CAT IIIb automatic landing.
Increase communication lines between adjacent secondary computers, and pass the working mode status amounts between the secondary computers and select control instructions according to the working mode of the adjacent secondary computers to avoid the output of mixed mode instructions, ensuring that the back-end actuator is not actively controlled in the downgrade mode.
It avoids the flight control system entering hybrid working mode, improves the aircraft handling performance, supports CAT IIIb automatic landing function, and reduces the impact of the fatigue life of the rudder surface.