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AbstractPilots’ operation has an important effect on flight safety and performance, particularly in the final landing stage when pilots need to deal with complicated operations. This study aims to determine the potential value of flight data and develop a method of evaluating a pilot’s performance during landing phase based on flight quick access recorder (QAR) data from the perspective of risk assessment. First, a Landing Operation Performance Evaluation Model was developed based on risk evaluation principles. Three landing parameters, which are touchdown distance, touchdown vertical acceleration and touchdown pitch angle, were selected as indicators to evaluate the pilots’ landing operation performance in this model. Second, the flight landing operation performance evaluation system (FLOPES) was set up based on the evaluation model. Test results showed that FLOPES can accomplish all calculation flow of operation performance evaluation. Finally, it concluded that this method is a more accurate and effective way for evaluating the landing operation performance of a flight. It could be as a practical tool for airlines to manage landing risk quantitatively and to provide a more practical support for improving training and design in aviation.Practitioner summary: This study aims to determine the potential value of flight data and to develop a method of evaluating pilot’s landing operation performance from the risk evaluation perspective. Test results showed that this method is effective and could be as a practical tool for airlines to manage landing risk and improve training.Abbreviations:QAR: Quick Access Recorder; FLOPES: Flight Landing Operation Performance Evaluation System; ICAO: International Civil Aviation Organization; IATA: International Air Transport Association; SMS: Safety Management System; CAAC: Civil Aviation Administration of China; FOQA: Flight Operations Quality Assurance; VBA: Visual Basic for Applications 相似文献
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Spam网页主要通过链接作弊手段达到提高搜索排名而获利的目的,根据链接作弊的特征,引入链接相似度和作弊系数两个指标来判定网页作弊的可能性。借鉴BadRank算法思想,从Spam网页种子集合通过迭代计算链接相似度和作弊系数,并根据与种子集合的链接指向关系设置权重,将待判定的网页进行度量。最后选取Anti-Trust Rank等算法作对比实验,结果验证了本文算法在准确率和适应性方面优于对比算法。 相似文献
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This study aimed to investigate the effects of brand anthropomorphism on consumer-brand relationships in a social media marketing context. We hypothesized that anthropomorphism on a brand’s Facebook fan page can strengthen the relationships between brands and consumers by yielding both social presence and a positive inference regarding the brand’s quality as a relationship partner. Our longitudinal experiment confirmed the effects of brand anthropomorphism on consumer-brand relationships on social media and the mediating role of social presence. The results suggest that when the anthropomorphized brand had relationships with consumers, a favorable attitude was shown toward the brand. Further, the participants perceived the anthropomorphized brand as a trustworthy relationship partner, giving more “Likes” for the posts from the anthropomorphized brand than those from the non-anthropomorphized brand. Further, the results confirmed that these favorable relationships were maintained even after the participants became aware of a brand transgression. 相似文献
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着陆缓冲机构是着陆器实现行星探测软着陆的关键部位之一,它的缓冲性能直接关系到着陆器是否能安全地在行星表面实现软着陆。根据某院提供的火星着陆器模型,在三维建模软件中建立着陆器的合理简化模型,为了提高分析着陆器软着陆过程冲击响应的准确性,采用MSC公司的Patran/Dytran有限元软件,用瞬态动力学的方法对着陆器的缓冲性能进行分析。仿真结果与试验数据十分吻合,着陆器的缓冲和传力性能良好。因此,采用拉杆缓冲的桁架式火星着陆器是可行的,仿真结果与试验数据也为今后的火星探测提供了参考。 相似文献
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Now, effectively searching web page becomesmore and more critical as the online information con-tinues to overload the web. Asolution is to make areasonable web page clustering analysis . But there isanother problem,because we must find out the webstructure and page hyperlinks , especially si milarityamongthe pages . At the same ti me ,there are someother very i mportant information such as the i mpor-tance of each page ,page content and so on[1 -3].Hyperlink analysis has already been applied … 相似文献
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:针对舰尾气流和甲板运动影响着舰精度的问题,提出一种基于自适应动态逆的纵向着舰控制律设计方法。
建立舰载机模型、舰尾流和甲板运动模型,基于自适应动态逆控制设计纵向自动驾驶仪,并在Lyapunov 稳定意义下
证明了控制器的稳定性;设计着舰导引律和迎角恒定的动力补偿器;采用Monte Carlo 模拟方法对建立的自动着舰控
制系统进行仿真验证。仿真结果表明:该自动着舰控制律具有更好鲁棒性,能够削弱舰尾流和甲板运动的影响,提
高了着舰的精度。 相似文献
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深孔及深孔型腔的加工一直是飞机起落架产品加工的难点和瓶颈,随着航空飞机总体性能的不断提高,对飞机各主承力结构件所受载荷的要求越来越高,传统的起落架结构件采用焊接技术以及普通钢材已经不适用。针对起落架目前采用高强度钢和整体结构设计后,涉及到典型深孔及型腔的加工技术成为了难题,通过对大型结构件深孔及型腔的加工技术研究,实现起落架重要结构件整体加工技术的革新。 相似文献
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