Autonomous Runway Centerline Alignment Under Poor Visibility

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Solution Overview

Problem

Existing aircraft ground navigation at airports relies heavily on pilot skills and airport markings, lacking autonomous or semi-autonomous systems to ensure safe and precise navigation, especially in challenging conditions.

Innovation Solution

A system utilizing sensors and a computing system to process environmental data, providing control instructions for semi-autonomous or fully autonomous aircraft navigation, aligning with airport markings and avoiding obstacles, using cameras, radar, and LIDAR for environment mapping and obstacle detection.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If pilot-controlled navigation with airport markings is used, then navigation guidance is provided, but navigation precision and safety deteriorate in challenging conditions such as poor visibility or missing markings

Engineering Contradiction:
Improvenavigation safetyVSAvoidadaptability to challenging conditions
Core Design Contradiction:
ReliabilityVSAdaptability or versatility

Solution Approach 1:

The patent replaces the mechanical/pilot-dependent navigation system with an autonomous computer vision system. The system uses cameras to capture images of airport markings, processes these images through algorithms to detect centerlines and boundaries, and automatically generates navigation guidance without requiring pilot interpretation of visual markings.

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

Solution Approach 2:

The patent introduces an intermediary processing system between the airport markings and the aircraft navigation. This system includes image capture devices, processing units that analyze marking patterns, and guidance generation modules that translate detected markings into actionable navigation instructions, bridging the gap between static markings and dynamic navigation needs.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Measurement precision

If autonomous navigation systems are implemented, then navigation precision improves, but system complexity increases

Engineering Contradiction:
Improvenavigation precisionVSAvoidsystem complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent divides the autonomous navigation system into distinct functional modules: image capture subsystem, image processing subsystem, marking detection subsystem, and guidance generation subsystem. Each module performs a specific function, making the overall complex system manageable through modular architecture where each segment can be independently developed, tested, and maintained.

Inventive Principle:
Principle #1Segmentation

3Measurement precision

If multiple sensors are used for environment mapping, then obstacle detection accuracy improves, but device complexity and cost increase

Engineering Contradiction:
Improveobstacle detection accuracyVSAvoidsensor system complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent combines multiple sensor types (cameras, radar, LIDAR) into an integrated sensing system that shares common processing infrastructure. The sensors work synergistically, with each sensor type compensating for the weaknesses of others, while the system uses unified processing algorithms to fuse data from all sensors, reducing overall system complexity compared to separate independent systems.

Inventive Principle:
Principle #5Merging (Combining)

Data Source

PatentEP3598418B1System, method, and computer readable medium for autonomous airport runway navigation
Publication Date: 2025.09.17 THE BOEING CO
  • EP3598418B1 patent drawingFigure 1
  • EP3598418B1 patent drawingFigure 2~3
  • EP3598418B1 patent drawingFigure 4~5

AI summary

Example implementations relate to autonomous airport runway navigation. An example system includes a first sensor and a second sensor coupled to an aircraft at a first location and a second location, respectively, and a computing system configured to receive sensor data from one or both of the first sensor and the second sensor to detect airport markings positioned proximate a runway. The computing system is further configured to identify a centerline of the runway based on the airport markings and receive sensor data from both of the first sensor and the second sensor to determine a lateral displacement that represents a distance between a reference point of the aircraft and the centerline of the runway. The computing system is further configured to control instructions that indicate adjustments for aligning the reference point of the aircraft with the centerline of the runway during subsequent navigation of the aircraft.