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

惯导速度辅助下GPS接收机码环的噪声响应和动态跟踪性能分析
引用本文:秦永元,俞济祥.惯导速度辅助下GPS接收机码环的噪声响应和动态跟踪性能分析[J].航空学报,1990,11(12):564-569.
作者姓名:秦永元  俞济祥
作者单位:西北工业大学 (秦永元),西北工业大学(俞济祥)
摘    要: 本文推导了C/A码信号相干和非相干接收的GPS接收机码环的动力学方程,分析了码环的噪声响应和动态跟踪性能对码环带宽的矛盾要求,并提出了解决矛盾的方法:惯导速度辅助。分析结果表明:窄带宽码环经精度为1nmile/h的惯导系统速度辅助后,动态跟踪误差为无辅助时的1/1000,接收机将兼有抗强干扰和跟踪高动态的性能。

关 键 词:惯性导航  卫星导航  锁相环路  信噪比  跟踪  误差  

NOISE RESPONSE AND MANOEUVRE TRACKING PERFORMANCE ANALYSIS FOR THE GPS RECEIVER CODF LOOP AIDED BY THE INS VELOCITY
Northwestern Pol ytechnical University Qin Yongyuan and Yu Jixiang.NOISE RESPONSE AND MANOEUVRE TRACKING PERFORMANCE ANALYSIS FOR THE GPS RECEIVER CODF LOOP AIDED BY THE INS VELOCITY[J].Acta Aeronautica et Astronautica Sinica,1990,11(12):564-569.
Authors:Northwestern Pol ytechnical University Qin Yongyuan and Yu Jixiang
Institution:Northwestern Pol ytechnical University Qin Yongyuan and Yu Jixiang
Abstract:This paper has deduced dynamic equations of the code loop of the GPS receiver which operates in coherent and noncnherent' manner when C/A code signal is considered. The contradictory requirements imposed on the code loop bandwidth by the noise response and manoeuvre tracking are analysed in detail as well. It is proposed that the contradiction can be solved by the velocity aiding from the inertial navigation system. The results show that if a narrow bandwidth code loop is aided by the inertial navigation system of 1nm/h accuracy, the manoeuvre tracking error will be 1/1000 as large 3.s that of without aiding, and thus both high anti-jamming and manoeuvre tracking performances can be achieved.
Keywords:inertial navigation  satellite navigation  phase-locked loop  signal-to-noise ratio  tracking  error  
本文献已被 CNKI 等数据库收录!
点击此处可从《航空学报》浏览原始摘要信息
点击此处可从《航空学报》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