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Passive acoustic method for aircraft states estimation based on the Doppler effect

机译:基于多普勒效应的飞机状态估计的无源声学方法

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摘要

A passive acoustic method to locate moving sound sources is applied to maneuvering aircraft. The advantages of the method are that it is suitable for all kinds of aircraft, not only propeller-driven, and is not restricted to low height above the ground. Its applicability could be, for instance, to supplement aircraft noise monitoring systems or to supervise small airports' activities. The method is based on the relation between the relative Doppler effect observed from a set of at least seven microphone receivers, distributed in the airport surroundings, and the aircraft position and speed. The method requires knowledge of the position of the aircraft at the start of takeoff. The ambiguity function is used to calculate the relative Doppler stretch of the spectrum of the sound between pairs of microphones. The results of applying the ambiguity function are the inputs to a system of equations that relates the aircraft position and speed to the relative Doppler frequency stretches. This system of equations is solved using a genetic algorithm. The performance of the method was tested by computer simulation. The results showed that the location errors are of the same order of magnitude as the size of an average aircraft, even if the takeoff position is not accurately known.
机译:用于定位移动声源的无源声学方法被应用于机动飞机。该方法的优点在于它不仅适用于螺旋桨驱动,而且适用于所有类型的飞机,并且不限于地上高度低。它的适用性可以是,例如,补充飞机噪声监测系统或监督小型机场的活动。该方法基于从分布在机场环境中的一组至少七个麦克风接收器中观察到的相对多普勒效应与飞机位置和速度之间的关系。该方法需要知道起飞开始时飞机的位置。模糊函数用于计算麦克风对之间的声音频谱的相对多普勒拉伸。应用歧义函数的结果是方程系统的输入,该方程系统将飞机的位置和速度与相对多普勒频率范围相关。使用遗传算法求解方程组。通过计算机仿真测试了该方法的性能。结果表明,即使无法准确知道起飞位置,位置误差也与普通飞机的大小相同。

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