Trajectory Prediction Module for Air Traffic Conflict Detection

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Solution Overview

Problem

Current air traffic control systems face challenges in maximizing aircraft throughput without increasing the risk of minimum separation loss, particularly due to the difficulty in monitoring and managing the positions and headings of multiple aircraft, leading to uncertainties that require human controllers to err on the side of caution.

Innovation Solution

A computerized system that includes a trajectory prediction module and a medium term conflict detector, which use radar data, flight plans, aircraft performance data, and meteorological information to calculate and display predicted aircraft trajectories with uncertainty regions, and classify interactions between aircraft as acceptable, uncertain, or unacceptable, aiding tactical controllers in maintaining safe separations.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If human controllers monitor and control multiple aircraft positions and headings, then safety is maintained through cautious control, but aircraft throughput is limited due to human capacity constraints

Engineering Contradiction:
ImprovesafetyVSAvoidaircraft throughput
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

The system introduces a computer-based intermediary that processes radar data, flight plans, and aircraft performance information to generate predicted trajectories and uncertainty regions. This intermediary assists controllers by automatically calculating separation risks and highlighting potential conflicts, allowing controllers to manage more aircraft while maintaining safety through enhanced situational awareness rather than increased human cognitive load.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Reliability

If controllers err on the side of caution to maintain minimum separation, then collision risk is minimized, but aircraft throughput is reduced due to overly conservative control

Engineering Contradiction:
Improvecollision avoidanceVSAvoidaircraft throughput
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

The system provides continuous feedback to controllers by displaying uncertainty regions around predicted aircraft trajectories and automatically classifying interactions as acceptable, uncertain, or unacceptable. This feedback mechanism allows controllers to make more informed decisions, maintaining caution where needed while confidently allowing closer spacing where the system predicts low risk, thereby increasing throughput without compromising collision avoidance.

Inventive Principle:
Principle #23Feedback

3Reliability

If more aircraft interactions are classified as uncertain to model generosity, then more potential conflicts are identified, but controller workload increases due to more puzzles to solve

Engineering Contradiction:
Improveconflict detectionVSAvoidcontroller workload
Core Design Contradiction:
ReliabilityVSEase of operation

Solution Approach 1:

The system performs self-service by automatically analyzing aircraft interactions and classifying them into three categories (acceptable, uncertain, unacceptable). This automated classification reduces controller workload by pre-processing the complex analysis of multiple aircraft trajectories and uncertainties, presenting controllers with organized information that requires interpretation rather than manual calculation, thus maintaining reliable conflict detection while easing operational burden.

Inventive Principle:
Principle #25Self-service

Data Source

PatentUS8255147B2Air traffic control
Publication Date: 2012.08.28 NATS & ROUTE
  • US8255147B2 patent drawing
  • US8255147B2 patent drawing
  • US8255147B2 patent drawing

AI summary

An air traffic control system includes a trajectory prediction module for calculating a trajectory for each aircraft, for inputting aircraft detected position data, and for recalculating the trajectories based on said position data, and a conflict detector for detecting, based on the trajectories, future circumstances under which pairs of aircraft violate predetermined proximity tests, and for causing a display on the display device indicating said circumstances. The systems uses a first proximity test and a second, more restrictive, proximity test; and displays a symbol representing pairs of aircraft which violate the second test in a first mode, and those which violate the first set but not the second set in a second mode.