Analysis of the influence of HUD brightness adjustment on pilots' information perception
Abstract
In order to study the visual effects of the external visual environment and HUD character brightness design on HUD information recognition, a 2×2 within-subject experimental design with two factors of character display brightness and environmental illumination was used, and the subjects were required to operate under experimental conditions. Complete the complete flight simulation process. The experiment collected subjects' performance data, SART scale data and physiological data. The experimental results show that the brightness factor is significant for the accuracy rate, and the environmental illumination factor is significant for the reaction time; among them, the environmental illumination factor is significant for the heart rate variability index SDNN, CV, and is borderline significant for the breathing index.
Keywords: HUD, situation awareness, display brightness, ambient illuminance
DOI: 10.54941/ahfe1005203
Cite this paper
More from this volume
- Scientific Evaluation of the Impact of an Increase in the Retirement Age on the Cognitive Functions and Well-Being of Air Traffic Controllers (ATCOs)
- Vigilant Air Traffic Control: Gaze-based Recognition of Detection Failures to Visual Warnings
- Hidden Dangers on the Flight Deck: A Stakeholder Analysis of the Issues Surrounding Commercial Pilot Mental Health
- Making Sense of Culture in the Cockpit: The Crash of Japan Airlines Flight 1045
- Remote Digital Tower to support Air Traffic Control Systems
- The Impact of Delayed Communication on NASA’s Human-Systems Operations: Preliminary Results of a Systematic Review
- The Challenges of the Implementation of Artificial Intelligence (AI) in Transportation.
- Should I board this Advanced Air Mobility vehicle? A systemic risk assessment of eVTOL in a vertiport
- Show the Way: Accelerating General Aviation Accident Investigations through LLMs and HFACS
- Patterning Risk: An Innovative Task Design Method for Simulating Incidents in Transportation Studies
- Reduction and Modification for Aero Engine Rotor Model Considering Contact Stiffness
- Improved One-Step Block Precise Integration Method For Rotor Nonlinear Response Calculation


AHFE Open Access