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基于自適應濾波的民航導航通信干擾檢測系統設計
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交通運輸部北海第一救助飛行隊

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Design of civil aviation navigation communication interference detection system based on adaptive filtering
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    摘要:

    針對目前使用的民航導航通信干擾檢測系統受到背景噪聲與電磁干擾信號重疊影響,導致干擾檢測結果不精準的問(wèn)題,提出了基于自適應濾波的民航導航通信干擾檢測系統設計。使用多信道檢測接收機,將接收結果經(jīng)過(guò)PCI接口傳送給上位機。使用測向天線(xiàn)陣,捕獲來(lái)自其他天線(xiàn)陣元的信號幅值、相位。使用由三個(gè)垂直磁阻傳感器組成的電子羅盤(pán),測量X、Y、Z方向的電磁干擾,經(jīng)過(guò)A/D轉換器放大處理和主機檢測后,完成硬件結構設計。計算系統輸出結果,結合自適應濾波處理技術(shù),整理自適應濾波的加權矢量,徹底分離開(kāi)噪聲信號與電磁信號,避免噪聲干擾。計算相位差,并對其進(jìn)行矢量化處理,獲取多組載波相位差,確定干擾信號的數值和方向,完成通信干擾檢測。由實(shí)驗結果可知,該系統在同頻干擾、臨頻干擾情況下,信號波動(dòng)的-0.2-0.4和-0.8-0.7幅值均與實(shí)際干擾信號波動(dòng)幅值一致,具有精準檢測結果。

    Abstract:

    Aiming at the problem that the currently used civil aviation navigation communication interference detection system is affected by the overlapping of background noise and electromagnetic interference signals, resulting in inaccurate interference detection results, a design of civil aviation navigation communication interference detection system based on adaptive filtering is proposed. The multi-channel detection receiver is used, and the received result is transmitted to the upper computer through the PCI interface. Use direction finding antenna arrays to capture the amplitude and phase of signals from other antenna array elements. The electronic compass composed of three vertical magnetoresistive sensors is used to measure the electromagnetic interference in the X, Y and Z directions, and the hardware structure design is completed after A/D converter amplification processing and host detection. Calculate the output result of the system, combine the adaptive filtering processing technology, sort out the weighted vector of the adaptive filtering, completely separate the noise signal from the electromagnetic signal, and avoid noise interference. Calculate the phase difference, perform vectorization processing on it, obtain multiple groups of carrier phase differences, determine the value and direction of the interference signal, and complete the communication interference detection. It can be seen from the experimental results that in the case of co-frequency interference and adjacent frequency interference, the amplitudes of -0.2-0.4 and -0.8-0.7 of the signal fluctuation are consistent with the fluctuation amplitude of the actual interference signal, and the detection results are accurate.

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任萍.基于自適應濾波的民航導航通信干擾檢測系統設計計算機測量與控制[J].,2022,30(7):78-83.

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歷史
  • 收稿日期:2022-01-20
  • 最后修改日期:2022-02-25
  • 錄用日期:2022-02-28
  • 在線(xiàn)發(fā)布日期: 2022-07-19
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