METHOD FOR SETTING AIRCRAFT CONTROLS
DE602023002477T2Active Publication Date: 2025-03-19AIRBUS OPERATIONS (SAS)
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Patent Information
- Application Number
- DE602023002477
- Authority / Receiving Office
- DE · DE
- Patent Type
- Patents
- Current Assignee / Owner
- Priority Date
- 2022-08-29
- Filing Date
- 2023-08-28
- Publication Date
- 2025-03-19
- Estimated Expiration
- 2043-08-28
AI Technical Summary
Technical Problem
Aircraft trajectory deviations due to wind, particularly turbulence, cause issues with angular speed, aircraft plate, and structural fatigue, which existing digital flight control systems struggle to mitigate effectively.
Method used
An aircraft supervisory control process that estimates three-dimensional wind using aircraft measurements, adjusts the control law for the ailerons by adding a compensation term proportional to the wind derivative, and applies this adjusted control law to reduce wind impact.
Benefits of technology
This solution automatically and digitally reduces the impact of wind on aircraft trajectory and structural fatigue, enhancing flight stability and safety.
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