一种基于下滑道偏差生成过载指令的方法和设备
By generating deviation vertical velocity and distance estimates, and processing sensor data using complementary filtering and low-pass filtering, normal overload commands are generated. This solves the problem of insufficient accuracy and robustness in glide slope approach control, and improves the accuracy of aircraft smooth landing and overload control.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- COMMERCIAL AIRCRAFT CORP OF CHINA LTD
- Filing Date
- 2026-04-27
- Publication Date
- 2026-07-17
AI Technical Summary
Existing glide slope approach control methods are greatly affected by interception distance, have poor sensor robustness, are easily affected by altitude, terrain and weather factors, and rely on the accuracy of ILS models, resulting in low control precision.
By generating deviation vertical velocity and distance estimates, sensor data is processed using complementary filtering and low-pass filters with different time constants. Combined with gain coefficients to generate normal overload commands, the weights are dynamically adjusted to improve accuracy.
It improves the accuracy and robustness of glide slope approach control, ensuring that the aircraft lands smoothly along the correct trajectory, reducing overload variations, and enhancing passenger comfort.
Smart Images
Figure CN122131792B_ABST