Automated Aircraft Collision Avoidance via Separation Perimeter

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Solution Overview

Problem

Current aircraft collision avoidance systems rely on human intervention, which can lead to errors due to factors like fatigue and stress, and are inadequate in high-traffic conditions, as they require pilots to exchange and perform escape maneuvers, potentially leading to further collision risks.

Innovation Solution

An automated vehicle-centric collision avoidance system that predicts the closest point of approach between aircraft and alters flight trajectories to maintain a predefined separation perimeter, reducing the need for human intervention and minimizing the risk of collisions.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If human air traffic controllers and pilots are used for collision avoidance, then the system can operate with existing technology and procedures, but human errors due to fatigue, stress, or lack of experience reduce reliability

Engineering Contradiction:
Improvecollision avoidance reliabilityVSAvoidautomation level
Core Design Contradiction:
ReliabilityVSExtent of automation

Solution Approach 1:

The aircraft collision avoidance system performs collision detection and escape maneuver selection autonomously without requiring human intervention. The system monitors its own flight path, detects potential collisions with other aircraft, and automatically executes escape maneuvers, enabling the aircraft to serve its own safety needs

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The patent replaces the mechanical human decision-making process with an automated electronic system that calculates closest point of approach, determines collision risk, and selects escape maneuvers based on pre-programmed logic and algorithms, eliminating human factors such as fatigue and stress from the collision avoidance process

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

2Productivity

If pilots rely on situational awareness and air traffic controller instructions for collision avoidance, then the system can function with current operational procedures, but the ability to avoid collisions is limited by human capacity and communication delays

Engineering Contradiction:
Improveaircraft separation management capacityVSAvoidresponse time
Core Design Contradiction:
ProductivityVSLoss of time

Solution Approach 1:

The automated collision avoidance system continuously monitors the flight path and positions of surrounding aircraft without interruption, maintaining constant awareness of potential collision risks rather than relying on periodic updates or human attention, enabling uninterrupted safety monitoring

Inventive Principle:
Principle #20Continuity of useful action

Solution Approach 2:

The system receives real-time position and trajectory data from other aircraft via transponders, processes this feedback information to calculate closest point of approach and collision risk, and continuously adjusts escape maneuver selections based on the evolving situational data, creating a closed-loop safety system

Inventive Principle:
Principle #23Feedback

3Reliability

If TCAS alerts pilots of potential flight path conflicts, then collision awareness is improved, but effective avoidance depends on pilot exchange of escape maneuver intentions and execution, which may be incompatible with other air traffic

Engineering Contradiction:
Improvecollision avoidance effectivenessVSAvoidescape maneuver coordination complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The aircraft's collision avoidance system autonomously determines and executes escape maneuvers without requiring pilot action or coordination with other pilots, with the system serving its own collision avoidance needs by automatically selecting and implementing the appropriate escape direction based on real-time conflict analysis

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The system pre-calculates multiple potential escape maneuvers and their compatibility with other air traffic before a collision becomes imminent, selecting the optimal escape path in advance rather than requiring last-minute pilot decisions, thereby reducing coordination complexity and response time

Inventive Principle:
Principle #10Preliminary action

4Reliability

If ground-based air traffic control systems direct aircraft separations, then collision avoidance is achieved through centralized control, but the workload of air traffic controllers increases in heavy air traffic conditions

Engineering Contradiction:
Improveaircraft separation controlVSAvoidcontroller workload
Core Design Contradiction:
ReliabilityVSEase of operation

Solution Approach 1:

Each aircraft's collision avoidance system independently monitors and manages its own separation from other aircraft, eliminating the need for continuous ground controller intervention in separation decisions, thereby reducing controller workload while maintaining reliable separation control

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The centralized air traffic control function is segmented and distributed to individual aircraft, with each aircraft's collision avoidance system handling its own separation responsibilities rather than relying on a single ground-based controller to manage all separations, thereby distributing the operational burden

Inventive Principle:
Principle #1Segmentation

Data Source

PatentUS9243930B2Vehicle-based automatic traffic conflict and collision avoidance
Publication Date: 2016.01.26 THE BOEING CO
  • US9243930B2 patent drawing
  • US9243930B2 patent drawing
  • US9243930B2 patent drawing

AI summary

Systems and methods for providing vehicle-centric collision avoidance are disclosed. An example method includes determining a first flight trajectory for a first aircraft, determining a second flight trajectory for a second aircraft, predicting a distance between the first aircraft and the second aircraft at a predicted closest point of approach based on the first and second flight trajectories, comparing the distance to a separation perimeter layer, the separation perimeter layer configured to provide a minimum separation distance from the first aircraft to the second aircraft, and altering the first flight trajectory when the distance breaches the separation perimeter layer.