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System dynamics modeling of the safety evolution of blended-wing-body subscale demonstrator flight testing

机译:混合机翼子秤演示飞行测试安全演变的系统动力学建模

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摘要

Between 2008 and 2010, three blended-wing-body (BWB) aircraft configuration subscale demonstrators developed by our research team encountered frequent accidents in flight tests. After the crash of the third demonstrator in March 2010, we initialized a systematic safety control approach and achieved improved safety records on the fourth demonstrator in 2012. This paper aims to develop a system dynamics model to represent such safety evolution process and to reveal the organizational mechanism involving complex dynamic interactions of accident causal factors (technical, organizational and human). Using VENSIM (R) software as a modeling tool, a qualitative system dynamic simulation is performed to model the feedback relationships of safety-related variables that affect the accident rate of demonstrator flight testing across time. This paper gives an innovative example to apply system dynamics methodology on accident causation analysis in the area of aviation. (C) 2016 Elsevier Ltd. All rights reserved.
机译:在2008年至2010年之间,我们的研究团队开发了3架混合机翼身(BWB)飞机配置规模演示器,在飞行测试中屡屡发生事故。在2010年3月第三个示威者坠机后,我们初始化了系统安全控制方法,并在2012年对第四个示威者进行了改进的安全记录。本文旨在建立一个系统动力学模型来表示这种安全演化过程并揭示组织涉及事故因果(技术,组织和人)的复杂动态相互作用的机制。使用VENSIM(R)软件作为建模工具,进行了定性系统动态仿真,以对与安全相关的变量的反馈关系进行建模,这些变量影响整个演示飞行器测试的事故率。本文给出了一个创新的例子,将系统动力学方法应用于航空领域的事故原因分析。 (C)2016 Elsevier Ltd.保留所有权利。

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