Aircraft Windshear Detection Using Turbulence-Adaptive Thresholds

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Solution Overview

Problem

Conventional aircraft windshear detection systems are susceptible to false alerts from normal atmospheric turbulence, leading to nuisance warnings and potential delays in detecting hazardous windshear conditions during takeoff and landing phases.

Innovation Solution

A system utilizing standard aircraft instrumentation, including accelerometers and air data computers, to calculate horizontal and vertical windshear components, with a signal processor that filters out turbulence effects by using predetermined thresholds and half-wave rectification to differentiate between hazardous windshear and normal turbulence, providing timely and reliable alerts to pilots.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If conventional windshear detection systems use fixed or variable thresholds to detect windshear, then windshear detection capability is improved, but false alerts from normal atmospheric turbulence increase

Engineering Contradiction:
Improvewindshear detection capabilityVSAvoidfalse alert rate
Core Design Contradiction:
Measurement precisionVSReliability

Solution Approach 1:

The system dynamically adjusts the windshear detection threshold based on real-time turbulence measurements. The threshold is no longer fixed or simply variable, but adapts continuously according to the measured turbulence level, allowing the system to maintain high detection sensitivity while automatically suppressing false alerts during turbulent conditions

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The detection threshold parameter is changed from a static or简单地 variable value to a turbulence-dependent value. The system measures turbulence characteristics and uses these measurements to modify the threshold parameter, effectively separating true windshear events from turbulence-induced false positives

Inventive Principle:
Principle #35Parameter changes

2Stability of the object's composition

If pilots reduce aircraft speed to maintain safe separation during landing, then aircraft spacing safety is improved, but windshear detection reliability deteriorates due to increased false alerts

Engineering Contradiction:
Improveaircraft spacing safetyVSAvoidwindshear detection reliability
Core Design Contradiction:
Stability of the object's compositionVSReliability

Solution Approach 1:

The system implements a feedback mechanism where turbulence measurements continuously inform the detection threshold adjustment. This feedback loop allows the system to recognize when reduced speed is causing turbulence-related false alerts and automatically compensates by raising the threshold, maintaining detection reliability throughout the landing approach

Inventive Principle:
Principle #23Feedback

Data Source

PatentUS8508387B2Systems and methods for aircraft windshear detection
Publication Date: 2013.08.13 AVIATION COMMUNICATION & SURVEILLANCE SYSTEMS LLC
  • US8508387B2 patent drawing
  • US8508387B2 patent drawing
  • US8508387B2 patent drawing

AI summary

The present invention allows quick detection of actual hazardous windshears while ignoring the effects of normal turbulence. A system according to one aspect of the present invention comprises a signal processor configured to determine a presence of hazardous windshear based on: (a) whether a measured windshear is beyond a first predetermined threshold, and (b) whether a measured turbulence level is beyond a second predetermined threshold.