宇航计测技术
宇航計測技術
우항계측기술
JOURNAL OF ASTRONAUTIC METROLOGY AND MEASUREMENT
2015年
2期
67-71,75
,共6页
崔小准%郑育红%付林春%聂欣%李懿
崔小準%鄭育紅%付林春%聶訢%李懿
최소준%정육홍%부림춘%섭흔%리의
导航%信号%载波信噪比%正交性%测试软件
導航%信號%載波信譟比%正交性%測試軟件
도항%신호%재파신조비%정교성%측시연건
Navigation%Signal%Carrier to noise ratio%Orthogonality%Test software
针对通用的商用仪器不能适用现代导航信号 IQ 正交性的测试要求,开发一种基于 Matlab GUI 环境的导航信号 IQ 正交性测试软件。该软件通过网络接口控制高速数字示波器,对导航信号源的秒脉冲信号和导航信号进行双通道高速数据采样,根据秒脉冲信号确定导航信号起始点,截取导航信号数据,采用本地数字波形对导航信号进行匹配滤波和伪随机码同步等数字信号处理,精密估计 I 和 Q 支路载波初始相位,从而得到 IQ 正交性测试结果。软件具有界面友好,操作简单,显示直观等特点。仿真测试结果表明,在典型载噪比情况下,测试软件所得到的测试结果随机误差小于0.5°。
針對通用的商用儀器不能適用現代導航信號 IQ 正交性的測試要求,開髮一種基于 Matlab GUI 環境的導航信號 IQ 正交性測試軟件。該軟件通過網絡接口控製高速數字示波器,對導航信號源的秒脈遲信號和導航信號進行雙通道高速數據採樣,根據秒脈遲信號確定導航信號起始點,截取導航信號數據,採用本地數字波形對導航信號進行匹配濾波和偽隨機碼同步等數字信號處理,精密估計 I 和 Q 支路載波初始相位,從而得到 IQ 正交性測試結果。軟件具有界麵友好,操作簡單,顯示直觀等特點。倣真測試結果錶明,在典型載譟比情況下,測試軟件所得到的測試結果隨機誤差小于0.5°。
침대통용적상용의기불능괄용현대도항신호 IQ 정교성적측시요구,개발일충기우 Matlab GUI 배경적도항신호 IQ 정교성측시연건。해연건통과망락접구공제고속수자시파기,대도항신호원적초맥충신호화도항신호진행쌍통도고속수거채양,근거초맥충신호학정도항신호기시점,절취도항신호수거,채용본지수자파형대도항신호진행필배려파화위수궤마동보등수자신호처리,정밀고계 I 화 Q 지로재파초시상위,종이득도 IQ 정교성측시결과。연건구유계면우호,조작간단,현시직관등특점。방진측시결과표명,재전형재조비정황하,측시연건소득도적측시결과수궤오차소우0.5°。
As the general commercial instruments cannot satisfy the testing requirements for IQ or-thogonality testing of modern navigation signal, a testing software for IQ orthogonality has been developed based on Matlab GUI. The software controls high-speed digital oscilloscope via the network interface and samples the PPS (Pulse Per second)and navigation signals of navigation signals source respectively in du-al-channel. The navigation signal data is extracted according to the starting point of the navigation signal determined by the PPS. After digital waveform-matching of navigation signal has been done with the local pseudo-random code modulation wave, the carrier initial phase of I and Q branch can be precisely esti-mated, then the test result of IQ orthogonality is obtained. The software has characteristics of friendly in-terface, easy operation, intuitive display. The simulation results show that random error of the test result is less than 0. 5 degrees in the case of typical carrier to noise ratio.