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Development and Validation of a UAV Based System for Air Pollution Measurements

机译:基于无人机的空气污染测量系统的开发和验证

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摘要

Air quality data collection near pollution sources is difficult, particularly when sites are complex, have physical barriers, or are themselves moving. Small Unmanned Aerial Vehicles (UAVs) offer new approaches to air pollution and atmospheric studies. However, there are a number of critical design decisions which need to be made to enable representative data collection, in particular the location of the air sampler or air sensor intake. The aim of this research was to establish the best mounting point for four gas sensors and a Particle Number Concentration (PNC) monitor, onboard a hexacopter, so to develop a UAV system capable of measuring point source emissions. The research included two different tests: (1) evaluate the air flow behavior of a hexacopter, its downwash and upwash effect, by measuring air speed along three axes to determine the location where the sensors should be mounted; (2) evaluate the use of gas sensors for CO2, CO, NO2 and NO, and the PNC monitor (DISCmini) to assess the efficiency and performance of the UAV based system by measuring emissions from a diesel engine. The air speed behavior map produced by test 1 shows the best mounting point for the sensors to be alongside the UAV. This position is less affected by the propeller downwash effect. Test 2 results demonstrated that the UAV propellers cause a dispersion effect shown by the decrease of gas and PN concentration measured in real time. A Linear Regression model was used to estimate how the sensor position, relative to the UAV center, affects pollutant concentration measurements when the propellers are turned on. This research establishes guidelines on how to develop a UAV system to measure point source emissions. Such research should be undertaken before any UAV system is developed for real world data collection.
机译:在污染源附近收集空气质量数据非常困难,尤其是当站点很复杂,有物理障碍或正在移动时。小型无人机(UAV)为空气污染和大气研究提供了新方法。但是,需要做出许多关键的设计决策,以实现代表性的数据收集,尤其是空气采样器或空气传感器进气口的位置。这项研究的目的是在六旋翼飞机上为四个气体传感器和一个粒子数浓度(PNC)监视器建立最佳安装点,从而开发一种能够测量点源排放的无人机系统。该研究包括两个不同的测试:(1)通过测量沿三个轴的空气速度来确定应安装传感器的位置,从而评估六轴飞行器的气流行为,其下冲和上冲效果。 (2)评估使用CO2,CO,NO2和NO的气体传感器,以及PNC监测器(DISCmini),通过测量柴油机的排放来评估基于无人机的系统的效率和性能。测试1产生的空速行为图显示了传感器与无人机一起安装的最佳位置。该位置受螺旋桨冲洗效果的影响较小。试验2的结果表明,无人机螺旋桨会产生分散效应,这通过实时测量的气体和PN浓度的降低来体现。线性回归模型用于估算螺旋桨开启时传感器相对于无人机中心的位置如何影响污染物浓度的测量。这项研究建立了有关如何开发用于测量点源排放的无人机系统的指南。在开发用于实际数据收集的任何无人机系统之前,应进行此类研究。

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