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Airport Noise Computational Models - Using Aircraft Trajectory Data to Assess Approach Profiles Including New Generation Continuous Descent Approach

机译:机场噪声计算模型 - 使用飞机轨迹数据评估方法轮廓,包括新一代连续血液方法

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Approach operations have historically received less attention than departures in community noise model systems. However, recent attention to the study of Continuous Descent Approaches both in the US and Europe have re-focused the research community on the approach noise modeling assumptions in the assessment tools available to the airport planner. These include the source noise definition as well as the general relationship between noise and aircraft performance that is central to modeling systems. Modeling approach noise performance is much more difficult than departure due to the uncertainty in approach trajectory resulting from air traffic control procedures and pilot technique. Existing noise model guidance does not provide a method to make the assessment tractable for the general user. Inaccuracies in the size of aircraft noise contours due to the uncertainties listed above will make the assessment of CDA's error prone for the decision planners who balance CDA's across a broad array of noise mitigation alternatives. In this paper we analyze radar data from two major airports in the US to determine the trajectory variation that is typical in operation, gain insight into the procedural constraints that drive this variation, and develop trajectory clusters that are representative of nominal operations. Results of the analysis indicate that there is a tendency to have average glide slopes slightly higher than the nominal 3 degrees, and that downwind approaches tend to have a higher glide slope than straight-in approaches. It is the intent that the result of this research be made available to the general user through input into guidance given in international noise modeling documents such as SAE-AIR-1845, European Civil Aviation Conference Document 29 and ICAO Circular 205.
机译:接近操作历史上收到的关注而不是社区噪声模型系统的偏离。然而,最近对美国和欧洲的连续下降方法的研究重新关注了研究界对机场规划师可用的评估工具中的方法噪声建模假设。这些包括源噪声定义以及噪声和飞行器性能之间的一般关系,这是建模系统的核心。由于空中交通管制程序和试验技术产生的方法轨迹的不确定性,建模方法噪声性能远远困难。现有的噪声模型引导不提供对普通用户进行评估的方法。由于上面列出的不确定性,飞机噪声轮廓的不准确性将使CDA的评估易于倾向于平衡CDA在广泛的噪音缓解替代方案中的决策计划。在本文中,我们分析了来自美国的两个主要机场的雷达数据来确定典型的操作中的轨迹变化,深入了解驱动这种变化的程序约束,以及开发代表名义操作的轨迹集群。分析结果表明存在平均滑动斜率略高于标称3度的趋势,并且顺风方法倾向于具有比直接接近更高的滑动斜率。意图是通过在国际噪声建模文件中的指导下,如SAE-AIR-1845,欧洲民航会议文件29和ICAO通告等,通过输入来向一般用户提供本研究的结果。

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