Dynamic Approach Speed Threshold for Landing Alerts
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Solution Overview
Problem
The SmartLanding algorithm has a limitation where the 'Too Fast' threshold cannot be less than 30 knots above a reference speed, leading to aircraft needing to fly at high speeds to trigger alerts, especially in conditions with little or no wind/gust information, resulting in delayed or missed alerts.
Innovation Solution
A system that adjusts the target approach speed based on predefined wind settings and pilot-inputted bug speeds, using a processing device to compare aircraft speed to a dynamically set target speed, triggering alerts when the aircraft exceeds this speed by a predefined error value near a landing point.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Reliability
If the 'Too Fast' threshold is set at least 30 knots above reference speed (V REF), then the system maintains a safe margin above reference speed, but the aircraft must fly at very high speed to trigger the alert, resulting in delayed or missed alerts in calm wind conditions
Solution Approach 1:
The patent applies dynamics by making the 'Too Fast' threshold dynamic rather than fixed. The threshold is adjusted based on real-time wind and gust conditions detected by the system. When strong winds or gusts are present, the threshold increases accordingly, allowing alerts to trigger at lower speed deviations. This resolves the contradiction by enabling timely alerts in calm conditions while maintaining appropriate safety margins in windy conditions.
Solution Approach 2:
The patent changes the parameter of the speed threshold based on environmental conditions. Instead of using a fixed 30-knot offset from V REF, the system modifies the threshold parameter dynamically according to wind speed and gust intensity. This allows the alert mechanism to adapt to varying operational conditions, triggering alerts at appropriate speed deviations regardless of wind conditions.
2Reliability
If the system adds 20 knots to V REF plus 10 knots technical error value to account for wind/gust conditions, then the system attempts to compensate for unknown wind conditions, but the aircraft still needs to fly at excessively high speeds (e.g., 154 kts when V REF is 124 kts) to trigger alerts
Solution Approach 1:
The patent implements feedback by continuously monitoring actual wind conditions and using this information to adjust the 'Too Fast' threshold in real-time. The system receives feedback from wind sensors and gust detection mechanisms, then dynamically modifies the alert threshold accordingly. This eliminates the need for fixed conservative additions to V REF, as the threshold automatically adapts to actual environmental conditions.
Solution Approach 2:
The system performs self-service by autonomously detecting wind and gust conditions and automatically adjusting its own alert threshold without requiring manual intervention or fixed conservative margins. The system serves itself by using its own sensor data to configure its monitoring parameters, eliminating the need for arbitrary additions like 20 knots to V REF.
Data Source
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AI summary
Systems and methods for adjusting target approach speed for use in a "Too Fast" approach to landing condition. An exemplary system (22) stores predefined maximum wind setting and a predefined reference speed and a pilot set bug speed value. A processing device (24) sets a target speed equal to the bug speed, if the bug speed is less than the reference speed plus a value associated with a predefined maximum wind setting, and sets the target speed equal to the reference speed plus the max wind added value, if the manual bug speed is not less than the reference speed plus the max wind added value. An output device (36,37) outputs an alert if the received aircraft speed is greater than the set target speed plus a predefined error value when the received aircraft location is within a threshold value of a touchdown point.