Integrated Modeling of Fatigue Impacts on C-17 Approach and Landing Performance

The current effort develops an initial integrated model of fatigue in the context of C-17 approach and landing operations. Specifically, we integrate a biomathematical fatigue model with a task network model to estimate pilot performance degradation. Fatigue risk management is a critical process in...

Full description

Saved in:
Bibliographic Details
Published inInternational journal of aerospace psychology Vol. 33; no. 1; pp. 61 - 78
Main Authors Veksler, Bella Z., Morris, Megan B., Krusmark, Michael A., Gunzelmann, Glenn
Format Journal Article
LanguageEnglish
Published Routledge 02.01.2023
Online AccessGet full text

Cover

Loading…
More Information
Summary:The current effort develops an initial integrated model of fatigue in the context of C-17 approach and landing operations. Specifically, we integrate a biomathematical fatigue model with a task network model to estimate pilot performance degradation. Fatigue risk management is a critical process in aviation and flight deck operations, given its dramatic impact on aviation safety and pilot health. Biomathematical fatigue models are useful tools in several aviation fatigue risk management programs that can be embedded in electronic device applications. However, these tools are limited in terms of identifying specific performance outcomes affected by fatigue, as well as individualizing fatigue estimates to individual pilots. Integrating computational cognitive models and biomathematical fatigue models can help address these issues. Forty-four aircrew members completed the study with 10 performing 33 landings with sets of corresponding actigraph data and C-17 performance metrics. We developed a task network model of C-17 approach and landing operations and integrated biomathematical fatigue model predictions based on actigraph data from the aircrew. We then compared predictions from this integrated model with C-17 performance metrics from the missions. We successfully predicted delays in setting flaps, landing gear, and engaging the speed brake. After further development and validation, this integrated model can be implemented within an application to provide real-time information on pilot fatigue and expected performance on specific aircraft operations.
ISSN:2472-1840
2472-1832
DOI:10.1080/24721840.2022.2149526