Multiple Detection Zones for Runway Collision Avoidance

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Solution Overview

Problem

Existing collision avoidance systems for runway safety use a single region of interest for all aircraft, which is a compromise due to varying navigation accuracy levels, leading to either false alarms or delayed alerts.

Innovation Solution

Implementing multiple detection zones based on individual aircraft navigation accuracy levels, with zone size determined by accuracy, ensuring a nominal certainty level before declaring an aircraft on the runway, thereby managing nuisance alerts and optimizing alert timing.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If a single region of interest is used for all aircraft, then the system is simple to operate, but position measurement precision deteriorates due to varying navigation accuracy levels

Engineering Contradiction:
Improvesystem operation simplicityVSAvoidaircraft position detection accuracy
Core Design Contradiction:
Ease of operationVSMeasurement precision

Solution Approach 1:

The single region of interest is divided into multiple detection zones with different sizes, each corresponding to a specific navigation accuracy level. Aircraft are assigned to appropriate detection zones based on their reported navigation accuracy, enabling precise position detection tailored to each aircraft's capabilities while maintaining simple system operation.

Inventive Principle:
Principle #1Segmentation

2Device complexity

If a single region of interest is used for all aircraft, then device complexity is reduced, but reliability deteriorates due to false alarms or delayed alerts

Engineering Contradiction:
Improvesystem structure complexityVSAvoidrunway presence detection reliability
Core Design Contradiction:
Device complexityVSReliability

Solution Approach 1:

The detection system is segmented into multiple zones with different buffer distances from the runway centerline. Each zone corresponds to a navigation accuracy level, allowing the system to provide reliable detection for each aircraft type without requiring complex adaptive algorithms. The segmented structure maintains simplicity while improving reliability.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Different detection zones have different spatial characteristics (sizes and positions) matched to the local navigation accuracy requirements of specific aircraft. This local optimization ensures that each aircraft is evaluated against appropriate detection criteria, enhancing overall system reliability without increasing global complexity.

Inventive Principle:
Principle #3Local quality

3Measurement precision

If a larger detection zone is used to account for position inaccuracies, then measurement precision is improved, but the system generates more nuisance alerts

Engineering Contradiction:
Improveaircraft position detection accuracyVSAvoidnuisance alert rate
Core Design Contradiction:
Measurement precisionVSObject-generated harmful factors

Solution Approach 1:

The detection region is segmented into multiple zones with progressively larger buffer distances from the runway centerline. Each zone corresponds to a navigation accuracy level, with smaller zones for high-accuracy aircraft and larger zones for low-accuracy aircraft. This segmentation allows the system to achieve necessary detection precision while minimizing nuisance alerts by not using unnecessarily large detection zones for all aircraft.

Inventive Principle:
Principle #1Segmentation

4Object-generated harmful factors

If a smaller detection zone is used to reduce nuisance alerts, then false alarms are reduced, but detection reliability deteriorates for aircraft with lower navigation accuracy

Engineering Contradiction:
Improvefalse alarm rateVSAvoiddetection reliability for low-accuracy aircraft
Core Design Contradiction:
Object-generated harmful factorsVSReliability

Solution Approach 1:

The detection system is segmented into multiple zones, with each zone's size matched to the navigation accuracy of aircraft using that zone. Aircraft with lower navigation accuracy are assigned to larger detection zones that account for their position uncertainties, ensuring reliable detection without generating false alarms from using uniformly small zones.

Inventive Principle:
Principle #1Segmentation

Data Source

PatentUS8847793B2Systems and methods using multiple zones of detection as a function of accuracy
Publication Date: 2014.09.30 AVIATION COMMUNICATION & SURVEILLANCE SYSTEMS LLC
  • US8847793B2 patent drawing
  • US8847793B2 patent drawing
  • US8847793B2 patent drawing

AI summary

Embodiments of the present invention relate to avionics systems, and more particularly, to collision avoidance systems. In one embodiment, a system is delineated comprising a plurality of detection zones for a plurality of aircraft and means for issuing a report based on one or more of the plurality of detection zones.