Head-Tracking System Drift Error Correction via Sensor Fusion

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Solution Overview

Problem

Existing head-tracking systems for aircraft and ground vehicles face challenges in accuracy, update rate, latency, and jitter due to the accumulation of errors and time delays from multiple sources, which degrades the performance of georeferenced head-tracking functions.

Innovation Solution

A head-tracking system that combines a georeferenced head tracker (GHT) with a platform-referenced head-tracker (PRHT) and an avionic system, using a controller to access and compare drift errors, generating update data based on platform-referenced head and aircraft position data to maintain accurate georeferenced head position data.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If a two-step approach using platform-referenced head-tracking system is used to compute georeferenced head position, then the system can provide georeferenced head position data, but error accumulation and time delay from multiple sources degrade accuracy and responsiveness

Engineering Contradiction:
Improvegeoreferenced head position accuracyVSAvoidresponsiveness
Core Design Contradiction:
Measurement precisionVSReliability

Solution Approach 1:

The system segments the head-tracking function into two independent parallel subsystems: a platform-referenced head-tracking subsystem and a georeferenced head-tracking subsystem. Each subsystem operates independently to perform its specific function, avoiding the sequential error accumulation of traditional two-step approaches while maintaining the ability to compute georeferenced head position data.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The system changes the operational parameters of the head-tracking system by enabling simultaneous operation of multiple tracker subsystems at full capacity. The georeferenced head tracker and platform-referenced head tracker both operate continuously and independently, with their outputs combined through sensor fusion algorithms to produce accurate georeferenced head position data without the time delays inherent in sequential processing.

Inventive Principle:
Principle #35Parameter changes

2Measurement precision

If multiple tracker subsystems are combined to meet accuracy and update rate requirements, then measurement precision improves, but device complexity increases

Engineering Contradiction:
Improvehead-tracking accuracyVSAvoidsystem complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The system divides the complex head-tracking function into distinct modular subsystems: a georeferenced head tracker (using inertial sensors), a platform-referenced head tracker (using optical or magnetic sensors), and a sensor fusion processor. Each module has a specific, well-defined function, making the overall complex system manageable through clear separation of concerns and independent optimization of each component.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The system employs universal sensor fusion algorithms that can process and integrate data from multiple different types of tracker subsystems (inertial, optical, magnetic). This multi-functional processing approach allows the same core algorithmic framework to handle various sensor inputs, reducing the need for separate specialized processing paths and thereby managing complexity while maintaining high measurement precision.

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

3Reliability

If existing combinations of magnetic, optical and inertial tracker subsystems are used, then various performance requirements are attempted to be met, but performance is still in need of improvement

Engineering Contradiction:
Improveperformance consistencyVSAvoidgeoreferenced head position accuracy
Core Design Contradiction:
ReliabilityVSMeasurement precision

Solution Approach 1:

The system segments the tracking function so that inertial sensors handle georeferenced orientation measurement while optical or magnetic sensors handle platform-referenced position measurement. This functional segmentation allows each sensor type to operate in its optimal performance range, with the sensor fusion processor combining these specialized measurements to achieve both consistent reliability and high measurement precision.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The system implements feedback through sensor fusion algorithms that continuously monitor and integrate data from multiple tracker subsystems. The fusion processor compares measurements from different sensors, detects inconsistencies or drift, and applies correction algorithms in real-time, providing feedback that maintains both performance consistency and measurement precision throughout operation.

Inventive Principle:
Principle #23Feedback

Data Source

PatentUS9874931B1Head-tracking system and method
Publication Date: 2018.01.23 ROCKWELL COLLINS INC
  • US9874931B1 patent drawing
  • US9874931B1 patent drawing
  • US9874931B1 patent drawing

AI summary

A head-tracking system includes a georeferenced head tracker (GHT) configured to provide georeferenced head position data, and a platform-referenced head-tracker (PRHT) configured to provide platform-referenced head position data. A controller is coupled with the GHT and the PRHT, and configured to be coupled with an avionic system configured to provide georeferenced aircraft position data. The controller includes a processor configured to access the georeferenced head position data, compare a current drift error of the GHT with a predetermined error threshold. When the current drift error is below the threshold, the processor transmits a signal indicative of the georeferenced head position data being a current georeferenced head position data. When the current drift exceeds the threshold, the processor access the georeferenced aircraft position-data, generates update data based on the platform-referenced head position data and the georeferenced aircraft position data, and updates the GHT at a known instant in time.