红外与激光工程
紅外與激光工程
홍외여격광공정
INFRARED AND LASER ENGINEERING
2014年
9期
2986-2991
,共6页
卫星导航接收机%大角域%多状态联合校准%灰色关联分析%场景映射
衛星導航接收機%大角域%多狀態聯閤校準%灰色關聯分析%場景映射
위성도항접수궤%대각역%다상태연합교준%회색관련분석%장경영사
satellite navigation receiver%wide angle%multi-state joint calibration%gray relational analysis%scene mapping
提出了一种基于微波暗室的大角域测试场景构建方法,该方法利用已有42°射频面阵,采用多状态联合校准方法对面阵天线单元到接收机的信号幅度和相位进行校准,以及采用灰色关联分析方法将外界环境下的卫星星座、动态干扰在微波暗室内实现逼真映射,构造最大视场角为160°的半实物抗干扰测试场景。仿真测试结果表明:暗室天线单元与实际场景下的卫星星座在角域关系下最大误差在高增益3 dB波束宽度内,暗室模拟的动态干扰与实际环境下到达接收机的功率基本一致;最后实现了对多波束抗干扰接收机的测试,并通过干信比与有效载噪比的关系曲线说明了该方法能够在室内实现导航接收机测试环境的逼近模拟,并准确地测试出多波束接收机的抗干扰性能。
提齣瞭一種基于微波暗室的大角域測試場景構建方法,該方法利用已有42°射頻麵陣,採用多狀態聯閤校準方法對麵陣天線單元到接收機的信號幅度和相位進行校準,以及採用灰色關聯分析方法將外界環境下的衛星星座、動態榦擾在微波暗室內實現逼真映射,構造最大視場角為160°的半實物抗榦擾測試場景。倣真測試結果錶明:暗室天線單元與實際場景下的衛星星座在角域關繫下最大誤差在高增益3 dB波束寬度內,暗室模擬的動態榦擾與實際環境下到達接收機的功率基本一緻;最後實現瞭對多波束抗榦擾接收機的測試,併通過榦信比與有效載譟比的關繫麯線說明瞭該方法能夠在室內實現導航接收機測試環境的逼近模擬,併準確地測試齣多波束接收機的抗榦擾性能。
제출료일충기우미파암실적대각역측시장경구건방법,해방법이용이유42°사빈면진,채용다상태연합교준방법대면진천선단원도접수궤적신호폭도화상위진행교준,이급채용회색관련분석방법장외계배경하적위성성좌、동태간우재미파암실내실현핍진영사,구조최대시장각위160°적반실물항간우측시장경。방진측시결과표명:암실천선단원여실제장경하적위성성좌재각역관계하최대오차재고증익3 dB파속관도내,암실모의적동태간우여실제배경하도체접수궤적공솔기본일치;최후실현료대다파속항간우접수궤적측시,병통과간신비여유효재조비적관계곡선설명료해방법능구재실내실현도항접수궤측시배경적핍근모의,병준학지측시출다파속접수궤적항간우성능。
A construction method of wide angle test scenario based on the anechoic chamber was proposed. Utilizing the existing 42° RF array, the amplitude and phase of signals arriving at the receiver from array antenna units were calibrated by multi-state joint calibration. And by gray relational analysis principles, the proposed method achieved the approximately true mapping satellite constellation and dynamic interference in the anechoic chamber. So the semi-physical anti-jamming test environment whose largest field angle was 160° was constructed. Simulation and test results show that the maximal deviation between antenna units in the anechoic chamber and the angular domain of the satellite constellations in the real scene is within high gain 3 dB beam width, and the power needed for dynamic interference to arrive at the receiver is approximately the same whether at actual scene or under simulation in anechoic chamber. Lastly, the anti-jamming test of multi-beam receiver was completed, the relation curves of J/S and C/N0 were given, indicating that the proposed method can not only effectively simulate the outfield test scenario of satellite navigation receiver indoors, but also accurately test the performance of multi-beam anti-jamming receiver.