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Approximation of pilot operational behavior affecting noise footprint in steep approaches

机译:在陡峭方法中影响噪声占地面积的导频操作行为的近似值

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摘要

Landing aircraft create noise that disturbs residents living close to airports. One method to reduce such noise is to fly the final approach at a steeper glide slope than the normal 3.0 degrees glide slope, thus increasing the distance between the source of the noise and the ground. If this is performed, there is a risk that the operational behavior of the pilot counteracts the noise reduction possible to achieve, due to the fact that the pilot must manage the aircraft's speed on a steeper glide slope. For practical reasons, there are few live trials and studies on pilot behavior during steeper approaches. In this project, a method to approximate pilot operational behavior during slightly steeper approaches, using flight data recorder data from standard approaches, was developed. The method exploits the fact that flying an approach in tailwind conditions creates the same operational challenges for a pilot as flying a steeper than normal approach does. The method was applied to 1159 flights. The results indicate that the pilots' operational behavior will change when glide slope angle increases. Extension of final flap and landing gear in steeper approaches will take place at a greater height but closer to the airport than for standard 3.0 degrees ILS approaches. The result can be a reduction of the noise from arriving aircraft by up to 2 dB in some areas beneath the approach path if a 3.5 degrees glide slope angle is used. (C) 2020 Institute of Noise Control Engineering.
机译:着陆飞机产生噪音,距离机场附近的居民。减少这种噪声的一种方法是在陡峭的滑动斜率下飞行最终的方法,而不是正常的3.0触发斜率,从而增加了噪声源与地之间的距离。如果执行这一点,则由于飞行员必须在陡峭的滑动斜坡上管理飞机的速度,因此导航飞行员的操作行为抵消了可以实现的降噪,因此可能存在可能的风险。出于实际原因,较少的实时试验和陡峭方法中的试验行为研究。在该项目中,开发了一种使用来自标准方法的飞行数据记录数据在稍陡的方法期间近似飞行员操作行为的方法。该方法利用了在尾风条件下飞行方法的事实为飞行员创造了与飞行器比正常方法更陡的飞行员的操作挑战。该方法应用于1159个飞行。结果表明,当滑动斜率角度增加时,导频的操作行为将改变。最终襟翼和较陡的挡板的延伸将在更大的高度但更接近机场而不是标准的3.0度ILS方法。如果使用3.5度滑动斜率角度,则结果可以减少到到达飞机的噪声高达2 dB,如果使用3.5度滑动斜率角度,则在接近路径下方的某些区域。 (c)2020噪声控制工程研究所。

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