A simulation system for civil aircraft flight control
By designing automatic flight control simulation subsystem, flight control simulation subsystem and flight simulation subsystem for civil aircraft, the problem of difficulty in effectively simulating and controlling the flight performance of civil aircraft in the prior art is solved, and the simulation of multiple controls and flight states of the aircraft is realized, and the efficiency of simulation testing is improved.
Patent Information
- Application Number
- CN202210716656.8
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Filing Date
- 2022-06-22
- Publication Date
- 2025-03-28
- Estimated Expiration
- 2042-06-22
AI Technical Summary
The prior art is difficult to effectively simulate and control the flight performance of civil aircraft, especially during automatic flight, flight control, takeoff and landing.
A simulation system including an automatic flight control simulation subsystem, a flight control simulation subsystem and a flight simulation subsystem are designed. Through the simulation of the aircraft's redundant flight control digital computer, actuator electronic control device and remote control electronic device, the full authority of the aircraft is realized in real-time operation and automatic flight functions.
The simulation of the pitch, roll, yaw and trim control of the aircraft is realized, and the lift and drag control during takeoff and landing is controlled, reducing the cost of simulation testing of the flight control system and improving the efficiency of simulation testing.