Weather Radar Hazard Identification via Spatial Frequency Analysis

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Solution Overview

Problem

Current weather radar systems cannot effectively differentiate between hazardous and non-hazardous weather conditions, leading to inefficient flight paths and increased difficulty in routing aircraft through safe portions of weather systems, particularly in regions like the tropical convergence zone.

Innovation Solution

A weather radar system that utilizes spatial frequency and reflectivity gradient parameters derived from Fourier transforms of radar return levels to detect non-hazardous weather regions, allowing for the differentiation of hazardous and non-hazardous weather conditions by adjusting display intensities and providing symbolic indicators on the radar display.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If weather radar systems use traditional reflectivity-based hazard curves to identify hazardous weather, then they can detect precipitation intensity, but they cannot differentiate between hazardous and non-hazardous weather conditions

Engineering Contradiction:
Improveweather hazard identification accuracyVSAvoidweather type differentiation capability
Core Design Contradiction:
Measurement precisionVSLoss of information

Solution Approach 1:

The patent segments weather systems into hazardous and non-hazardous regions by analyzing spatial variations in reflectivity. It divides the weather system into discrete cells and evaluates each cell's characteristics (spatial frequency, reflectivity gradient) to classify it as either hazardous or non-hazardous, enabling differentiated identification rather than treating all precipitation equally

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent transitions from traditional one-dimensional reflectivity analysis to multi-dimensional analysis by incorporating spatial frequency and reflectivity gradient parameters. This dimensional expansion allows the system to characterize weather structure and differentiate between convective and stratiform patterns, providing enhanced hazard identification capability

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

2Reliability

If pilots avoid all yellow and red encoded weather regions, then they can ensure safety, but they create inefficient flight paths and increased flight time

Engineering Contradiction:
Improveflight safetyVSAvoidflight time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The patent applies local quality by providing spatially differentiated hazard information within weather systems. Instead of treating entire weather regions uniformly, it identifies specific hazardous cells versus non-hazardous cells within the same weather system, allowing pilots to navigate through non-hazardous areas while avoiding only the dangerous portions

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The system provides feedback to pilots through enhanced radar display that shows differentiated hazard levels. This feedback enables informed decision-making about route selection, allowing pilots to confidently penetrate non-hazardous regions while maintaining safety margins around hazardous areas

Inventive Principle:
Principle #23Feedback

3Reliability

If air traffic control implements conservative routing around weather systems, then aircraft safety is maintained, but routing efficiency and airspace utilization decrease

Engineering Contradiction:
Improveaircraft safetyVSAvoidrouting efficiency
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

The patent segments weather systems into hazardous and non-hazardous regions, providing air traffic control with granular information about where weather threats actually exist. This enables controllers to route aircraft through non-hazardous portions of weather systems rather than implementing blanket avoidance of entire weather regions

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The system dynamically identifies hazardous versus non-hazardous regions within weather systems, allowing for flexible and adaptive routing decisions. Controllers can adjust routes in real-time based on the spatial distribution of hazards, optimizing both safety and efficiency

Inventive Principle:
Principle #15Dynamics

4Ease of operation

If weather radar systems display all precipitation as potential hazards using traditional color coding, then they maintain simplicity, but they cause pilots to make unnecessary flight deviations

Engineering Contradiction:
Improveradar display simplicityVSAvoidflight deviation time
Core Design Contradiction:
Ease of operationVSLoss of time

Solution Approach 1:

The patent applies local quality to the radar display by providing spatially differentiated information about hazard levels. Non-hazardous regions are displayed with indicators that distinguish them from hazardous areas, allowing pilots to quickly identify which regions are safe to penetrate without complicating the overall display

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The system uses color changes and symbolic indicators to differentiate hazardous from non-hazardous weather regions on the radar display. This visual differentiation maintains ease of operation by using intuitive color coding while providing the critical information needed to avoid unnecessary deviations

Inventive Principle:
Principle #32Color changes

Data Source

PatentUS7307576B1Hazardous and non-hazardous weather identification system and method
Publication Date: 2007.12.11 ROCKWELL COLLINS INC
  • US7307576B1 patent drawing
  • US7307576B1 patent drawing
  • US7307576B1 patent drawing

AI summary

A weather radar system or method can be utilized to determine non-hazardous weather region for an aircraft. The weather radar system can utilize processing electronics coupled to an antenna. The processing electronics can determine presence of the non-hazardous weather region in response to data related to returns received by the weather radar antenna. The data can include a spatial frequency parameter or reflectivity gradient.