Wingtip Camera Reticule for Aircraft Clearance

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Solution Overview

Problem

Pilots often misjudge the clearance distance of aircraft wingtips when operating in tight or unfamiliar spaces, leading to collisions with ground facilities and other aircraft, due to the lack of reliable depth perception from two-dimensional camera displays.

Innovation Solution

A wingtip-mounted camera system that generates a video stream, transmits it to a processor for reticule generation, and displays it on a cockpit device, including a horizon line, distance lines, and an eye-safe laser beam to provide clear wingtip clearance information, allowing pilots to avoid obstacles.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If a two-dimensional camera display is used to show wingtip clearance, then the system complexity is low, but the depth perception and clearance information reliability are insufficient

Engineering Contradiction:
Improveclearance distance measurementVSAvoiddisplay system complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent transitions from a two-dimensional camera display to a three-dimensional virtual representation of the wingtip and its trajectory. The system generates a virtual model of the wingtip that moves through three-dimensional space, allowing pilots to perceive depth and clearance distances more accurately. This dimensional enhancement resolves the contradiction by providing reliable depth perception while maintaining reasonable system complexity through software-based virtual modeling rather than complex hardware additions.

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

2Reliability

If a wingtip-mounted camera system with reticule is implemented, then the clearance information reliability is improved, but the device complexity increases

Engineering Contradiction:
Improveclearance information reliabilityVSAvoidcamera and display system complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent introduces a virtual model of the wingtip as an intermediary between the physical camera system and the pilot's perception. This virtual representation, displayed on standard cockpit displays, mediates the information from the camera to the pilot, providing intuitive three-dimensional clearance information without requiring complex additional hardware. The virtual wingtip model acts as a mediator that translates camera data into reliable, easy-to-interpret visual information.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The system creates a virtual copy or replica of the actual wingtip and its trajectory. This virtual copy is generated by the processor based on camera input and aircraft movement data, then displayed to the pilot. The virtual copy provides accurate clearance information while avoiding the complexity of building physical models or using multiple complex sensors, as it relies on software-based replication of the wingtip's spatial position and movement.

Inventive Principle:
Principle #26Copying

3Object-affected harmful factors

If depth perception is enhanced for wingtip clearance, then collision avoidance capability is improved, but the information processing complexity increases

Engineering Contradiction:
Improvecollision riskVSAvoidinformation processing complexity
Core Design Contradiction:
Object-affected harmful factorsVSDevice complexity

Solution Approach 1:

The system uses the aircraft's existing navigation and flight control systems to provide the data needed for the virtual wingtip model. The processor leverages information already available in the aircraft's systems (position, velocity, orientation) to generate the three-dimensional representation. This self-service approach reduces information processing complexity by reusing existing data infrastructure rather than requiring separate complex sensing and processing systems.

Inventive Principle:
Principle #25Self-service

Data Source

PatentEP2856454B1Airport surface collision-avoidance system (ASCAS)
Publication Date: 2019.07.17 HONEYWELL INTERNATIONAL INC
  • EP2856454B1 patent drawingFigure 1
  • EP2856454B1 patent drawingFigure 2
  • EP2856454B1 patent drawingFigure 3

AI summary

Systems and methods for performing airport surface collision-avoidance. A wingtip-mounted camera allows the pilot to positively ascertain that the wingtip will clear objects located in the video. An exemplary system implemented on an aircraft includes a wingtip module having a camera that generates a video stream and a communication device that transmits the generated video stream. A processor receives the video stream and generates a reticule for the video stream. A display device simultaneously presents the video stream and the reticule. The reticule includes a horizon line and is based on a focal length of a lens of the camera and height of the camera above ground. The reticule includes curved and/or straight distance lines and curved or straight travel lines. The travel line(s) correspond to at least one aircraft component or a zone of importance and are based on location of the camera and trajectory of the aircraft.