Aircraft Heading Estimation with Incremental ALS Feature Updates

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Solution Overview

Problem

Aircraft struggle to accurately estimate heading in low visibility conditions due to insufficient detection of approach lighting system (ALS) lights or known objects, leading to increased risk of heading errors during landing.

Innovation Solution

An aircraft heading estimation system using sensors to detect features, compare with expected patterns, and incrementally update heading estimates as resolution improves, combining long-range sensors with image processing to enhance accuracy.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Length of stationary object

If long-range sensors are used to detect features in low visibility conditions, then the detection range is improved, but the measurement precision of heading estimation deteriorates

Engineering Contradiction:
Improvedetection rangeVSAvoidheading estimation accuracy
Core Design Contradiction:
Length of stationary objectVSMeasurement precision

Solution Approach 1:

The system initiates heading estimation early in the approach using long-range sensor data, even when visibility is poor and features are distant. By starting the estimation process beforehand and continuously refining it as the aircraft approaches, the system overcomes the limitation of low precision at long ranges.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The system incrementally updates the heading estimation by comparing newly detected features with expected features and refining the estimate based on the difference. This feedback loop allows continuous improvement of heading accuracy as more features are detected and as the aircraft gets closer to the airport.

Inventive Principle:
Principle #23Feedback

2Measurement precision

If high resolution sensors are used to detect features, then the measurement precision is improved, but the detection range deteriorates

Engineering Contradiction:
Improvefeature detection resolutionVSAvoiddetection range
Core Design Contradiction:
Measurement precisionVSLength of stationary object

Solution Approach 1:

The system uses long-range sensors to initiate heading estimation early in the approach, accepting lower resolution at long distances. As the aircraft approaches and resolution improves, the system refines the heading estimate, combining the benefits of early detection with later precision.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The system dynamically adapts its operation based on the aircraft's distance from the airport and current visibility conditions. It transitions from using long-range detection capabilities to relying more on high-resolution feature detection as the aircraft approaches, optimizing the balance between range and precision throughout the approach.

Inventive Principle:
Principle #15Dynamics

3Reliability

If multiple verification procedures are implemented to improve heading accuracy, then the reliability is improved, but the device complexity increases

Engineering Contradiction:
Improveheading estimation reliabilityVSAvoidsystem complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The system employs a feedback mechanism where detected features are compared with expected features, and the heading estimation is incrementally updated based on the comparison results. This continuous refinement process provides multiple verifications of the heading estimate without requiring complex additional hardware or procedures.

Inventive Principle:
Principle #23Feedback

Data Source

PatentEP4711712A1Flight heading estimation
Publication Date: 2026.03.18 ROCKWELL COLLINS INC
  • EP4711712A1 patent drawingFigure 1~2
  • EP4711712A1 patent drawing
  • EP4711712A1 patent drawing

AI summary

An aircraft heading estimation system comprising: one or more sensors arranged on the aircraft to detect features in a viewing region and provide feature signals indicative of the detected features; an image processor storing predetermined image information of one or more expected features, being features that might be expected to be present in the viewing region, the image processor configured to compare the features indicated by the feature signals with the one or more expected features to generate an estimated observed image and to derive an estimated heading for the aircraft based on the estimate observed image; wherein the image processor is further configured to incrementally update the estimated observed image with new feature signals generated by the sensors as their distance to the viewing region changes, and to incrementally updated the estimated heading based on the updated estimate observed image.