首页> 外国专利> METHOD FOR OPERATION OF A PULSE-DOPPLER ON-BOARD RADAR STATION WITH RECOGNITION OF THE EFFECT OF INTERFERENCE FROM A REMOTE POINT OF SPACE WHEN AN AIR TARGET IS DETECTED, COVERED BY A NOISE PRODUCER

METHOD FOR OPERATION OF A PULSE-DOPPLER ON-BOARD RADAR STATION WITH RECOGNITION OF THE EFFECT OF INTERFERENCE FROM A REMOTE POINT OF SPACE WHEN AN AIR TARGET IS DETECTED, COVERED BY A NOISE PRODUCER

机译:识别噪声目标,确定空间目标时从空间远程点产生干扰的脉冲多普勒车载雷达站的工作方法

摘要

FIELD: radar ranging and radio navigation.;SUBSTANCE: invention relates to radar ranging and can be used to expand functional capabilities of pulse-Doppler on-board radar station (BRS). Method consists in scanning the space with the main beam of the beam pattern of the antenna (BPA) with the compensation channel on the side lobes when the aerial target (AT) is detected by means of the pulse-Doppler BRS, setting the gain in the main channel smaller and commensurate with the signal gain in the compensation channel, converting the signals in the main and compensation channels into corresponding amplitude-frequency spectra, at that, when the AT is irradiated of the pulse-Doppler radar BRS BPA main beam amplitudes A1 and A2 spectral components of the signal in the main and compensation channels, respectively, are located at the frequency position f1, caused by Doppler shift of carrier frequency of BRS due to mutual movement of its carrier and irradiated AT, when the production aircraft is irradiated to noise of DRFM type – digital radio-frequency memory equipped with a radio reconnaissance station (RRS), main beam BPA of pulse-Doppler BRS amplitudes A3 and A4 spectral components of the signal in the main and compensation channels, respectively, are located at the frequency position f2, caused by Doppler shift of carrier frequency of BRS due to mutual movement of its carrier and irradiated aircraft-producer of noise type DRFM, when the AT is irradiated to the main beam of the BPA and the jamming by the aircraft-producer is hitting the sighting point on the frequency position f2 previously explored using the RRS, type DRFM interference on BPA side lobes of amplitudes A1 and A2 spectral components of the signal in the main and compensation channels, respectively, are located at the frequency position f1, amplitudes An1 and An2 spectral components of the interference signal in the main and compensation channels, respectively, are located at the frequency position f2, analysis of the spectral components of the signal and their amplitudes is carried out, depending on the result, only the useful BRS signal is processed or the useful BRS signal is processed in the radar antenna with simultaneous rejection of the DRFM type interference at the frequency position f2.;EFFECT: broader functional capabilities of the BRS due to recognition of the action on the side lobes of the BPA from the outermost point of the space of the frequency-targeted noise of the DRFM type when detecting the AT, covered by the noise producer aircraft, and, in case of its effect, treatment of useful signal in BRS with simultaneous rejection of DRFM type interference.;1 cl, 3 dwg
机译:雷达测距和无线电导航技术领域本发明涉及雷达测距,并且可以用于扩展脉冲多普勒车载雷达站(BRS)的功能。该方法包括:当通过脉冲多普勒BRS检测到空中目标(AT)时,以天线(BPA)波束方向图的主波束和旁瓣上的补偿信道扫描空间,将增益设置为主信道较小且与补偿信道中的信号增益相对应,从而在对脉冲多普勒雷达BRS BPA主波束幅度进行AT辐射时,将主信道和补偿信道中的信号转换为相应的幅度频谱主和补偿通道中信号的A 1 和A 2 频谱分量分别位于频率位置f 1 当生产飞机受到DRFM类型的噪声照射时,由于BRS的载波和被照射的AT的相互运动而引起的BRS载波频率的多普勒频移–配备有无线电侦察站(RRS)的主射频BPA脉冲多普勒BRS a主信道和补偿信道中信号的幅度A 3 和A 4 频谱分量分别位于频率位置f 2 ,当AT辐射到BPA的主光束上并且飞机生产者的干扰正在瞄准时先前使用RRS探索的频率位置f 2 上的点,在幅度A 1 和A 2 频谱分量的BPA旁瓣上键入DRFM干扰主通道和补偿通道中的信号分别位于频率位置f 1 ,幅度A n1 和A n2 的频谱分量主信道和补偿信道中的干扰信号分别位于频率位置f 2 ,分析信号的频谱分量并根据其结果执行幅度,在雷达天线中仅处理有用的BRS信号或处理有用的BRS信号,同时抑制频率位置f 2 .;效果:由于在检测到AT时从DRFM类型的以频率为目标的噪声的空间的最外点识别了BPA旁瓣的作用,因此BRS的功能更广泛,被噪声覆盖生产机,并在其影响的情况下,在同时抑制DRFM类型干扰的情况下处理BRS中的有用信号。; 1 cl,3 dwg

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