IMPROVEMENT OF DIGITAL DEVICE FOR SUPPRESSION OF ERRONEOUS REQUEST BY LATERAL PETALS OF THE ANTENNA OF AIR TRAFFIC CONTROL SYSTEMS

T. Hovorushchenko, Alexander Yanovitskiy
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Abstract

This article considers the expansion of the capabilities of digital devices of three-pulse suppression of the request ofaircraft responders with side petals in terms of increasing the accuracy of measuring the azimuth of flight of aircraft. In existingdevices, the response of aircraft responders is carried out at the time of the boundary crossing by the aircraft of the frequencypattern of the antenna. The directional pattern of the radar systems of the main petal has an angle of 2o-4o in the horizontal planedepending on the type of radar system and the request period of terrestrial radar stations is 500 Hz, and the antenna rotationspeed is 10 rpm and the distance between pulses P1 and P3 is 14 μs. The time the aircraft is within the directional pattern of themain petal will be requested 17 times and the same number of responses, which in turn leads to ambiguity in fixing the definition ofthe aircraft in azimuth, especially over long distances. The response of the aircraft respondent to the request will be answeredwhen approaching the middle of the directional pattern of the antenna of the main lobe, where the highest power of the emittedsignal, which will significantly reduce the error of determining the aircraft by azimuth
空中交通管制系统天线侧瓣错误请求抑制数字装置的改进
本文从提高飞机飞行方位角测量精度的角度出发,考虑了扩展带有侧花瓣的飞机应答器请求的三脉冲数字抑制装置的能力。在现有的设备中,飞机应答者的响应是在飞机越过天线频率模式的边界时进行的。主瓣雷达系统的方向图根据雷达系统类型在水平面上的角度为20 ~ 40°,地面雷达站请求周期为500 Hz,天线转速为10 rpm,脉冲P1和P3之间的距离为14 μs。飞机在主花瓣的方向模式内的时间将被要求17次和相同数量的响应,这反过来导致飞机在方位角上的定义不明确,特别是在长距离上。应答飞行器对请求的响应将在接近发射信号功率最高的主瓣天线方向图的中间位置时得到应答,这将大大减少通过方位角确定飞行器的误差
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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