Aircraft Collision Risk Assessment with Lateral Maneuverability

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Solution Overview

Problem

Existing aircraft collision avoidance systems only consider vertical maneuverability and a narrow flight path, ignoring lateral maneuverability and dynamic hazards, providing limited information for pilots or autopilots in situations requiring significant deviations and failing to account for dynamic obstacles.

Innovation Solution

A method and apparatus that determine an aircraft's risk of collision by considering its maneuverability, initial trajectory, and candidate positions, incorporating Gaussian probability distributions to assess the likelihood of occupying these positions and the presence of hazards, including dynamic obstacles, to provide a continuous or categorized risk indicator.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If existing collision avoidance systems only consider vertical maneuverability and narrow flight path, then the system complexity is reduced, but the collision avoidance capability and information availability for pilots are insufficient

Engineering Contradiction:
Improvecollision avoidance capabilityVSAvoidsystem complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent extends the traditional vertical maneuverability consideration to include lateral maneuverability dimensions. The system calculates probability of occupancy in three-dimensional space by considering both vertical and lateral movements, providing comprehensive collision risk assessment that accounts for all possible aircraft maneuvers within a time period.

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

Solution Approach 2:

The system segments the collision risk assessment into multiple independent components: probability of occupancy calculation, hazard presence determination, and risk computation. This modular approach allows complex risk assessment to be broken down into manageable calculations while maintaining overall system reliability.

Inventive Principle:
Principle #1Segmentation

2Loss of information

If existing systems provide binary risk indicators, then the system complexity is reduced, but the information availability and decision-making support for pilots are limited

Engineering Contradiction:
Improveinformation availabilityVSAvoidsystem complexity
Core Design Contradiction:
Loss of informationVSDevice complexity

Solution Approach 1:

The system transforms the binary risk indicator into a continuous probability-based risk assessment. By calculating the probability of occupancy at candidate positions and combining it with hazard presence, the system provides graded risk information that enables more nuanced decision-making while maintaining computational feasibility through standardized probability calculations.

Inventive Principle:
Principle #35Parameter changes

3Adaptability or versatility

If existing systems only consider narrow window along planned flight path, then the calculation time is reduced, but the maneuvering options and safe alternatives available to pilots are limited

Engineering Contradiction:
Improvemaneuvering optionsVSAvoidcalculation time
Core Design Contradiction:
Adaptability or versatilityVSLoss of time

Solution Approach 1:

The system performs preliminary calculations of candidate positions and probability distributions before actual collision risk assessment. By pre-calculating the probability of occupancy across multiple candidate trajectories and positions within a time period, the system prepares comprehensive maneuvering options in advance, enabling rapid decision-making when collisions are detected.

Inventive Principle:
Principle #10Preliminary action

Data Source

PatentUS20250308396A1Aircraft collision risk determination
Publication Date: 2025.10.02 ROCKWELL COLLINS FRANCE SAS
  • US20250308396A1 patent drawing
  • US20250308396A1 patent drawing
  • US20250308396A1 patent drawing

AI summary

A method of determining an aircraft's risk of collision at a candidate position includes determining the candidate position which the aircraft is capable of traversing to within a time period, based on the aircraft's: i) initial position; ii) initial trajectory; and iii) maneuverability. The method also includes determining a probability that the aircraft will traverse to the candidate position, and determining a presence of any collision hazards at the candidate position. A risk of collision is determined based on the determined probability that the aircraft will occupy the candidate position, and the determined presence of any collision hazards.