Aircraft Type Identification Using Virtual Lidar Point Clouds

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Solution Overview

Problem

Existing aircraft identification systems at airports struggle to reliably distinguish between different aircraft types and sub-types, particularly due to the limitations of video detection and guidance systems, and the high cost and data processing demands of 3D Lidar sensors, which affect the efficiency and safety of airfield operations.

Innovation Solution

A computing device simulates virtual Lidar sensor data for 3D models of aircraft types and sub-types to generate point clouds, using a classification model to identify and track aircraft, and determine their pose and location, without the need for expensive 3D Lidar sensors.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of manufacture

If video detection and guidance systems are used for aircraft identification, then the system cost is reduced, but the ability to reliably distinguish between different aircraft types and sub-types deteriorates

Engineering Contradiction:
Improvesystem costVSAvoidaircraft type distinction ability
Core Design Contradiction:
Ease of manufactureVSMeasurement precision

Solution Approach 1:

The patent creates virtual 3D models of aircraft that replicate the geometric characteristics of real aircraft. These digital copies are used to generate synthetic Lidar point cloud data, enabling the system to identify aircraft types without requiring expensive physical Lidar sensors. The virtual models preserve the essential geometric features needed for classification while eliminating the need for costly hardware.

Inventive Principle:
Principle #26Copying

Solution Approach 2:

The patent replaces the mechanical/optical Lidar sensing system with a computational approach using virtual 3D models and synthetic data generation. Instead of using physical sensors to capture aircraft geometry, the system uses pre-created digital models and rendering techniques to generate equivalent measurement data, substituting hardware-based detection with software-based simulation.

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

2Measurement precision

If 3D Lidar sensors are used for aircraft identification, then the measurement precision of aircraft geometry is improved, but the device cost and data processing demands increase

Engineering Contradiction:
Improveaircraft geometry detection accuracyVSAvoidsensor cost and processing requirements
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent performs preliminary actions by pre-creating accurate 3D models of various aircraft types and generating their corresponding Lidar point cloud data in advance. This preparatory work allows the system to quickly compare real aircraft scans against pre-generated virtual data during actual identification operations, reducing real-time processing demands while maintaining high measurement precision.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The system creates virtual copies of Lidar point cloud data from 3D aircraft models. These synthetic point clouds serve as reference patterns for comparison with actual sensor data, enabling accurate aircraft identification without requiring the system to process complex raw Lidar data in real-time. The virtual copies preserve all geometric measurement precision while simplifying the identification process.

Inventive Principle:
Principle #26Copying

3Reliability

If virtual Lidar simulation and classification models are used, then the cost-effectiveness and reliability of aircraft identification is improved, but the computational complexity of the system increases

Engineering Contradiction:
Improveaircraft identification accuracyVSAvoidcomputational processing requirements
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The classification model and virtual 3D models are prepared in advance during an offline training phase. This preliminary action allows the system to learn aircraft characteristics and generate reference data before actual identification operations begin. During real-time operation, the system only needs to perform comparisons against pre-computed data, significantly reducing computational complexity while maintaining high identification reliability.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The system generates and stores comprehensive virtual Lidar data for multiple aircraft types and configurations in advance, creating an extensive database of reference patterns. This excessive preparation ensures that all possible aircraft variations are covered, improving identification reliability without increasing real-time computational demands, as the heavy processing occurs during the offline data generation phase.

Inventive Principle:
Principle #16Partial or excessive action

Data Source

PatentUS12372656B2Aircraft identification
Publication Date: 2025.07.29 HONEYWELL INTERNATIONAL INC
  • US12372656B2 patent drawing
  • US12372656B2 patent drawing
  • US12372656B2 patent drawing

AI summary

Methods, devices, and systems for aircraft identification are described herein. In some examples, one or more embodiments include a computing device comprising a memory and a processor to execute instructions stored in the memory to simulate virtual light detection and ranging (Lidar) sensor data for a three-dimensional (3D) model of an aircraft type to generate a first point cloud corresponding to the 3D model of the aircraft type, generate a classification model utilizing the simulated virtual Lidar sensor data of the 3D model of the aircraft type, and identify a type and/or sub-type of an incoming aircraft at an airport by receiving, from a Lidar sensor at the airport, Lidar sensor data for the incoming aircraft, generating a second point cloud corresponding to the incoming aircraft utilizing the Lidar sensor data for the incoming aircraft, and classifying the second point cloud corresponding to the incoming aircraft using the classification model.