Aircraft Vision System Gain Scheduling for Low Visibility

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Solution Overview

Problem

Pilots face challenges during aircraft landing maneuvers, especially in low visibility conditions, as existing vision systems may not provide sufficient or clear vision information to ensure safe landing.

Innovation Solution

An enhanced vision system for aircraft that combines data from infrared and millimeter wave sensors, with automatic gain adjustments based on aircraft position relative to the runway, to merge images and reduce distortions, providing enhanced vision information to the pilot.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a single vision system is used during landing, then the system complexity is low, but the vision information is insufficient in low visibility conditions

Engineering Contradiction:
Improvevision information qualityVSAvoidsystem complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent combines multiple vision systems (infrared and millimeter wave sensors) into a single integrated enhanced vision system. The processor merges images from both sensors to provide comprehensive vision information that overcomes the limitations of individual systems, particularly in low visibility conditions while maintaining manageable system complexity through unified processing.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The enhanced vision system performs multiple functions by integrating different sensing modalities. The system can operate effectively across various visibility conditions by switching between and combining infrared and millimeter wave sensing, making it universally applicable for landing operations regardless of environmental conditions.

Inventive Principle:
Principle #6Universality (Multi-functionality)

2Reliability

If multiple vision systems are combined, then the vision information quality improves, but the image distortion increases

Engineering Contradiction:
Improvevision information qualityVSAvoidimage distortion
Core Design Contradiction:
ReliabilityVSLoss of information

Solution Approach 1:

The processor uses gain scheduling based on aircraft position relative to the runway to dynamically adjust the contribution of each sensor. This feedback mechanism optimizes the merged image quality by reducing distortions while maintaining the benefits of multi-sensor integration throughout the landing approach.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The system dynamically adjusts the gain of individual sensors based on real-time aircraft position. As the aircraft approaches the runway, the processor modifies the weighting of infrared and millimeter wave images to account for their different effective ranges, thereby minimizing distortion and maintaining optimal vision information quality.

Inventive Principle:
Principle #15Dynamics

3Adaptability or versatility

If manual gain adjustment is required, then the system adaptability is high, but the ease of operation decreases

Engineering Contradiction:
Improvesystem adaptabilityVSAvoidease of operation
Core Design Contradiction:
Adaptability or versatilityVSEase of operation

Solution Approach 1:

The system performs automatic gain scheduling based on aircraft position relative to the runway, eliminating the need for manual pilot intervention. The processor autonomously adjusts sensor gains and merges images according to the aircraft's approach phase, maintaining high adaptability while significantly improving ease of operation.

Inventive Principle:
Principle #25Self-service

Data Source

PatentEP3143468B1Advanced aircraft vision system utilizing multi-sensor gain scheduling
Publication Date: 2019.04.10 GULFSTREAM AEROSPACE CORP
  • EP3143468B1 patent drawingFigure 1
  • EP3143468B1 patent drawingFigure 2
  • EP3143468B1 patent drawingFigure 3

AI summary

An enhanced vision system is provided for an aircraft performing a landing maneuver. Accordingly to non-limiting embodiments, a processor onboard the aircraft receives data from sensors or systems onboard the aircraft and determines a position of the aircraft relative to a runway using the data. Responsive to this determination, the processor adjusts the gain of a first vision system and a second vision system. Images from the first vision system and the second vision system are merged and displayed to the pilot until the completion of the landing maneuver.