Radar Pulse Width Optimization for Runway Centerline Detection

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Solution Overview

Problem

Conventional enhanced flight vision systems (EFVS) face challenges in low visibility conditions, such as CAT III fog and heavy precipitation, as infrared-based systems struggle to detect and display runways effectively, while RF-based systems deliver lower resolution images, and the use of additional equipment for integrity monitoring increases aircraft cost and weight.

Innovation Solution

A radar system with a radar antenna emitting pulses less than 6 microseconds, processing radar data to identify centroids of runway lights or infrastructure, and using best fit analysis to determine the runway centerline, which is then displayed on an electronic display, leveraging weather radar data to provide a clear representation of the runway centerline in all weather conditions.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If infrared-based enhanced vision systems are used, then the system can provide enhanced flight visibility, but the system fails to detect and display runways in low visibility conditions (RVR under 300 feet)

Engineering Contradiction:
Improverunway detection capabilityVSAvoidlow visibility conditions
Core Design Contradiction:
ReliabilityVSObject-affected harmful factors

Solution Approach 1:

The patent changes the operational parameters of the radar system by using pulse widths less than 6 microseconds, which improves range resolution and enables accurate detection of runway features in low visibility conditions where infrared systems fail

Inventive Principle:
Principle #35Parameter changes

2Object-affected harmful factors

If RF signals (millimeter wave radar) are used, then the system can penetrate challenging weather conditions, but the system delivers images of lower resolution compared to infrared cameras

Engineering Contradiction:
Improveweather penetration capabilityVSAvoidimage resolution
Core Design Contradiction:
Object-affected harmful factorsVSMeasurement precision

Solution Approach 1:

The patent changes the pulse width parameter to less than 6 microseconds, which significantly improves the range resolution of the radar system while maintaining its ability to penetrate challenging weather conditions like fog and heavy precipitation

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent replaces infrared optical detection with radar electromagnetic wave detection, substituting a system that works in clear weather but fails in low visibility with a system that can operate in all weather conditions while achieving sufficient resolution through optimized pulse parameters

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

3Reliability

If additional equipment (integrity monitor) is added to provide monitored SVS, then the system can allow lower landing minimums, but the aircraft cost and weight increase

Engineering Contradiction:
Improvelanding minimum authorizationVSAvoidaircraft weight
Core Design Contradiction:
ReliabilityVSWeight of moving object

Solution Approach 1:

The patent makes the radar system perform multiple functions: it provides both the primary enhanced flight visibility function and serves as its own integrity monitor by detecting runway features and generating the extended centerline, eliminating the need for separate integrity monitoring equipment

Inventive Principle:
Principle #6Universality (Multi-functionality)

Solution Approach 2:

The radar system performs self-integrity monitoring by independently detecting runway lights and infrastructure to generate the extended centerline display, making the system self-sufficient and eliminating dependence on additional external monitoring equipment

Inventive Principle:
Principle #25Self-service

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

This solution enables accurate detection and display of runway centerlines in challenging weather, enhancing pilot visibility and allowing for lower landing minimums by providing a reliable and cost-effective means of situational awareness, integrating with existing aircraft systems for improved system integrity.

Implementation Method 1

processing electronics configured to cause the radar antenna to emit radar pulses and configured to receive radar data associated with signals associated with the radar antenna

Methodology Applied
Scientific EffectRadar: Radar

Data Source

PatentUS10928510B1System for and method of image processing for low visibility landing applications
Publication Date: 2021.02.23 ROCKWELL COLLINS INC
  • US10928510B1 patent drawing
  • US10928510B1 patent drawing
  • US10928510B1 patent drawing

AI summary

An apparatus is for use with an aircraft radar system having a radar antenna. The apparatus includes processing electronics configured to cause the radar antenna to emit radar pulses having a pulse width less than 6 microseconds and configured to receive radar data associated with signals associated with the radar antenna. The radar data is processed to identify centroids associated with indications of the runway lights for a runway in the radar data. A best fit analysis of the centroids is used to identify a runway centerline associated with the runway.