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Linear Mixed-Effects Models for Human-in-the-Loop Tracking Experiment DataLinear mixed-effects models provide several benefits over more traditional statistical inference tests that are particularly useful for most human-in-the-loop tracking experiment data. However, surprisingly, mixed models are virtually not used for the analysis of tracking experiment data. This paper uses of linear mixed-effects models to analyze combined tracking data from two previous human-in-the-loop roll tracking experiments that compared control behavior metrics collected in both a research aircraft and a motion-base simulator. In the experiments, pilots' behavior under 10 different motion configurations with varying motion filter gains and break frequencies was evaluated and compared to that in the real aircraft. The linear mixed-effects model analysis on the combined dataset confirmed the main statistical outcomes of the individual experiments. The main benefits of mixed models for this type of data were demonstrated by successfully combining data from two experiments that used different experimental conditions and of which one had an additional apparatus and the other a missing participant. Finally, the mixed-model analysis was able to explicitly test for scientifically relevant statistical differences in the dependent measures between the aircraft and simulator, as well as both experiments.
Document ID
20205010928
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Peter M. T. Zaal
(Metis Technology Solutions, Inc. Albuquerque, NM)
Daan M. Pool
(Delft University of Technology Delft, Zuid-Holland, Netherlands)
Max Mulder
(Delft University of Technology Delft, Zuid-Holland, Netherlands)
Date Acquired
December 2, 2020
Subject Category
Air Transportation And Safety
Meeting Information
Meeting: AIAA SciTech Forum
Location: Online
Country: US
Start Date: January 11, 2021
End Date: January 21, 2021
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNX17AE07A
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
NASA Technical Management
Keywords
manual control
linear mixed-effects models
simulator motion
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