Aircraft Sensor Image Field of View Adjustment for Low Visibility

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Solution Overview

Problem

Conventional Enhanced Flight Vision Systems (EFVS) struggle to provide useful information during low visibility conditions, as sensor-based images can be noisy and distracting, hindering pilot performance during approach and landing operations.

Innovation Solution

A control module that adjusts the Field Of View (FOV) of sensor-based images on aircraft flight deck displays based on received visibility information, reducing the FOV when low visibility conditions are detected to minimize noise and enhance relevant information display.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Area of stationary object

If the FOV of sensor images is increased to provide broader situational awareness, then the area of displayed information is improved, but the noise and distraction level increases during low visibility conditions

Engineering Contradiction:
Improvedisplayed image areaVSAvoidnoise and distraction
Core Design Contradiction:
Area of stationary objectVSObject-generated harmful factors

Solution Approach 1:

The system dynamically adjusts the FOV of sensor images based on detected visibility conditions. During low visibility conditions, the FOV is automatically reduced to minimize noise and distraction, while during good visibility conditions, the FOV is expanded to provide broader situational awareness. This dynamic adaptation resolves the contradiction by making the displayed area variable rather than fixed.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The system changes the FOV parameter of sensor images based on visibility conditions. By adjusting this key parameter, the system optimizes the balance between providing sufficient displayed area for situational awareness and limiting noise/distraction during low visibility operations.

Inventive Principle:
Principle #35Parameter changes

2Object-generated harmful factors

If the FOV of sensor images is reduced to minimize noise during low visibility, then the harmful distraction effect is reduced, but the situational awareness capability deteriorates

Engineering Contradiction:
ImprovedistractionVSAvoidsituational awareness
Core Design Contradiction:
Object-generated harmful factorsVSLoss of information

Solution Approach 1:

The system dynamically adjusts the FOV based on real-time visibility detection. When visibility is good, a larger FOV provides comprehensive situational awareness. When visibility deteriorates, the system automatically reduces FOV to minimize distraction while maintaining essential awareness, thus resolving the information loss concern through context-appropriate display adaptation.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The FOV parameter is adjusted based on visibility conditions to optimize the balance between minimizing distraction and maintaining situational awareness. This parameter change ensures that the display provides appropriate information levels matched to current operational conditions.

Inventive Principle:
Principle #35Parameter changes

3Adaptability or versatility

If the FOV is dynamically adjusted based on visibility conditions, then the adaptability to different operating environments is improved, but the device complexity increases

Engineering Contradiction:
Improvevisibility condition adaptationVSAvoidcontrol module complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The control module is segmented into distinct functional components: a visibility detection subsystem that monitors environmental conditions, and a FOV adjustment subsystem that modifies sensor image display parameters. This segmentation allows the complex adaptability function to be implemented through modular, manageable components, reducing overall system complexity while maintaining high adaptability.

Inventive Principle:
Principle #1Segmentation

Data Source

PatentEP3438614B1Aircraft systems and methods for adjusting a displayed sensor image field of view
Publication Date: 2020.10.28 HONEYWELL INTERNATIONAL INC
  • EP3438614B1 patent drawingFigure 1
  • EP3438614B1 patent drawingFigure 2
  • EP3438614B1 patent drawingFigure 3

AI summary

A vehicle system and method are provided. The system includes a control module coupled to an imaging system and a display system. The control module receives position and location information of the aircraft, and processes that with map features to identify a landing location. The control module commands the display system to render on display system a landing image having thereon a sensor based visually enhanced area defined by a field of view (FOV) of first dimensions. The control module continually receives and processes visibility reports to determine the visibility at the landing location. When there is low visibility at the landing location, the control module reduces the FOV dimensions.