首页 | 本学科首页   官方微博 | 高级检索  
     检索      

导航信号IQ正交性测试软件设计与实现CSCD
引用本文:崔小准,郑育红,付林春,聂欣,李懿.导航信号IQ正交性测试软件设计与实现CSCD[J].宇航计测技术,2015,35(2):67-71,75.
作者姓名:崔小准  郑育红  付林春  聂欣  李懿
作者单位:1、中国空间技术研究院总体部,北京 100094;; 2、中国空间技术研究院通信卫星事业部,北京 100094
摘    要: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°。

关 键 词:导航  信号  载波信噪比  正交性  测试软件

Design and Implementation of Test Software for IQ Orthogonality of Navigation Signal
CUI Xiao-zhun;ZHENG Yu-hong;FU Lin-chun;NIE Xin;LI Yi.Design and Implementation of Test Software for IQ Orthogonality of Navigation Signal[J].Journal of Astronautic Metrology and Measurement,2015,35(2):67-71,75.
Authors:CUI Xiao-zhun;ZHENG Yu-hong;FU Lin-chun;NIE Xin;LI Yi
Institution:1、Institude of Spacecraft System Engineering, China Academy of Space Technology, Beijing 100094;; 2、Institude of Telecommunication Satellite, China Academy of Space Technology, Beijing 100094
Abstract:As the general commercial instruments cannot satisfy the testing requirements for IQ orthogonality 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 dual-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 estimated, then the test result of IQ orthogonality is obtained. The software has characteristics of friendly interface, 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.
Keywords:Navigation                                                                                                                        Signal                                                                                                                        Carrier to noise ratio                                                                                                                        Orthogonality                                                                                                                        Test software
本文献已被 CNKI 维普 等数据库收录!
点击此处可从《宇航计测技术》浏览原始摘要信息
点击此处可从《宇航计测技术》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号