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Forward looking windshear detection apparatus and method

机译:前视风切变检测装置及方法

摘要

An integrated, remote sensing and reactive detection system is provided for detecting and confirming the presence of hazardous microbursts, macrobursts, and windshears in the general flight path of an aircraft. An infrared remote sensing system is used to seek out, detect, and provide advanced alerts of thermal gradients ahead of an aircraft which correlate with windshear conditions. The measurement of atmospheric temperature is accomplished by a scanning, multi-spectral radiometer that sweeps an approximate 60 degrees path in front of the aircraft at about a 5 hertz rate. The radiometer employs two rows of detectors that are slightly offset resulting in two simultaneous measurements of temperature that are about 7 degrees apart in elevation angle. This dual information allows the continuous measurement of the atmospheric vertical temperature gradient, or lapse rate, for use in determining the atmospheric stability, and hence the probability of microburst occurrence as well as the continuous measurement of atmospheric azimuth temperature gradient for use in detecting the existence of a negative gradient that correlates with a microburst.
机译:提供了一种集成的遥感和反应检测系统,用于检测和确认飞机的一般飞行路径中是否存在危险的微暴,大暴发和风切变。红外遥感系统用于在飞机前寻找,检测并提供与风切变条件相关的热梯度预警,并提供预警。大气温度的测量是通过扫描多光谱辐射计完成的,该辐射计以大约5赫兹的频率扫掠飞机前方大约60度的路径。辐射计采用两排检测器,它们略有偏移,导致两次同时测量仰角相差约7度的温度。该双重信息允许连续测量大气垂直温度梯度或流逝速率,以用于确定大气稳定性,因此可以进行微爆发生的概率,以及连续测量大气方位角温度梯度以用于检测是否存在与微爆发相关的负梯度

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