Wind-Aware Aircraft Progress Visualization for Approach Separation

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Solution Overview

Problem

Air traffic controllers face challenges in assessing and optimizing aircraft separation distances during landing approaches due to the lack of real-time wind direction and speed information, leading to suboptimal runway capacity utilization, especially at capacity-constrained airports.

Innovation Solution

A method and device that determine wind speed and direction within a predefined airspace, calculate reference distances along an aircraft's travel route, and visualize these distances on a display to help air traffic controllers anticipate and manage aircraft movements, incorporating wind effects and altitude profiles.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If air traffic controllers use traditional radar screens showing only current positions and speed vectors, then the system is simple to operate, but the controllers cannot accurately predict aircraft future progress during approach

Engineering Contradiction:
Improveprediction accuracy of aircraft progressVSAvoidcomplexity of display system
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The system performs preliminary calculations of aircraft future positions based on current wind conditions, airspeed, and flight path. By pre-computing and displaying predicted aircraft progress markers before the aircraft actually reaches those positions, the system enables controllers to anticipate future aircraft locations without adding complex real-time tracking mechanisms.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The patent introduces an intermediary computational layer that processes wind data, aircraft performance parameters, and flight plan information to generate predicted position markers. This intermediary system translates complex meteorological and operational data into simple visual markers on the radar display, bridging the gap between raw data and actionable information for controllers.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Reliability

If air traffic controllers increase separation distances between aircraft to compensate for uncertainty in wind effects, then safety is improved, but runway capacity utilization deteriorates

Engineering Contradiction:
Improvesafety of aircraft separationVSAvoidrunway capacity utilization
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

The system provides continuous feedback to controllers about predicted aircraft positions and ground speeds, enabling dynamic adjustment of separation standards. By showing real-time predictions of how wind will affect each aircraft's progress, controllers can make informed decisions about maintaining smaller, safer separations rather than applying blanket increased separations, thus optimizing both safety and capacity.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The patent dynamically changes the separation parameters based on actual wind conditions and aircraft-specific performance characteristics. Instead of using fixed separation distances, the system calculates variable separations that account for tailwinds increasing ground speed and headwinds decreasing it, allowing controllers to optimize separation margins to the minimum safe level rather than using conservative fixed values.

Inventive Principle:
Principle #35Parameter changes

3Ease of operation

If air traffic controllers rely on experience and observations of recent aircraft to assess approach progress, then no additional equipment is needed, but the ability to analyze current situation accurately deteriorates, especially when taking over from another controller

Engineering Contradiction:
Improveease of situation analysisVSAvoidloss of situational awareness
Core Design Contradiction:
Ease of operationVSLoss of information

Solution Approach 1:

The system pre-calculates and displays predicted position markers and ground speed information before the controller needs to make decisions. When a controller takes over, the predicted markers are already visible, providing immediate situational awareness without requiring the incoming controller to mentally process raw wind data and aircraft performance parameters.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The system automatically generates and updates predicted aircraft progress information based on data already being collected by the radar and meteorological systems. This self-service capability eliminates the need for controllers to manually calculate or estimate wind effects, providing accurate predictive information that assists rather than replaces controller expertise.

Inventive Principle:
Principle #25Self-service

Data Source

PatentUS11935418B2Method and device for visualizing an effect of wind on an aircraft travel
Publication Date: 2024.03.19 FREQUENTIS ORTHOGON GMBH
  • US11935418B2 patent drawing

AI summary

A method for visualizing an effect of wind on an aircraft travel comprising the steps determining at least one wind speed and wind direction for a predefined airspace, identifying a predefined travel route of at least one selected aircraft within the predefined airspace, calculating at least one reference distance flown by the selected aircraft along a route segment of the travel route in a predefined reference time interval, wherein the calculating uses at least one air speed of the selected aircraft at the route segment, the determined wind speed and the determined wind direction, and optionally at least one altitude, visualizing the predefined travel route or the route segment and indicating said reference distance on the visualized predefined travel route or route segment.