A Runway Overrun Risk Assessment Model for Civil Aircraft Based on Quick Access Recorder Data
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Published:2023-08-30
Issue:17
Volume:13
Page:9828
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ISSN:2076-3417
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Container-title:Applied Sciences
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language:en
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Short-container-title:Applied Sciences
Author:
Li Xiuyi1, Zhang Lin2ORCID, Shang Jiaxing34ORCID, Li Xiaoquan34, Qian Yu2ORCID, Zheng Linjiang34
Affiliation:
1. Guanghan Branch, Civil Aviation Flight University of China, Guanghan 618307, China 2. School of Flight Technology, Civil Aviation Flight University of China, Guanghan 618307, China 3. College of Computer Science, Chongqing University, Chongqing 400044, China 4. Key Laboratory of Dependable Service Computing in Cyber Physical Society, Ministry of Education, Chongqing University, Chongqing 400044, China
Abstract
The quick access recorder (QAR), as an airborne device used to monitor and record flight parameters, has been widely installed on various types of aircraft. Based on QAR data, research on runway overrun, a typical flight safety incident, has attracted widespread attention in recent years. However, existing runway overrun risk models generally suffer from oversimplified risk metrics or insufficient consideration of risk dynamics. In this paper, we propose a new dynamic runway overrun risk assessment model based on QAR data. We first consider the noise of aircraft trajectory data in the QAR parameters and present a landing trajectory correction method combining ground speed and runway position information. Second, to improve the accuracy of the risk assessment model, we design an algorithm to automatically recognize the aircraft autobrake level during the landing phase, based on which a new dynamic risk assessment model is developed. Finally, feature engineering is performed to extract the relevant contributing factors of runway overrun risk, based on which classification and regression models are applied to identify risky flights and predict the risk values. The proposed risk assessment model was evaluated using QAR data from an airline in China. The results show that the automatic deceleration rate, the way that the aircraft approaches the runway, the touchdown distance, and the kinetic energy at 50 ft are key factors in the risk of runway overrun during the landing phase.
Funder
National Key Research and Development Program of China National Natural Science Foundation of China Safety ability Foundation of Civil Aviation Administration of China Civil Aviation Flight Technology and Flight Safety Key Laboratory Foundation Open Fund of Key Laboratory of Flight Techniques and Flight Safety, and CAAC
Subject
Fluid Flow and Transfer Processes,Computer Science Applications,Process Chemistry and Technology,General Engineering,Instrumentation,General Materials Science
Reference38 articles.
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