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INS辅助的GPS接收机跟踪环结构和性能分析
引用本文:赵剡,易骁骁,张晓明.INS辅助的GPS接收机跟踪环结构和性能分析[J].宇航计测技术,2007,27(6):45-48,64.
作者姓名:赵剡  易骁骁  张晓明
作者单位:北京航空航天大学仪器科学与光电工程学院,北京,100083
摘    要:分析了GPS/INS的不同组合方式,研究了GPS接收机跟踪环的结构,给出了多普勒频移和时钟误差频率的外部估计方法,提出了一种使用低成本惯性器件信息辅助GPS接收机跟踪环的深组合(deepintegration)结构,建立了这种结构的前馈模型,并对其进行了仿真分析。仿真结果表明,这种结构可以使得接收机具有较宽的跟踪带宽和较好的抑制噪声能力,能显著提高GPS接收机的性能。

关 键 词:全球定位系统  接收机  惯性导航    跟踪环  模拟
文章编号:1000-7202(2007)06-0045-04
修稿时间:2007年1月15日

Performance and Architectures Analysis for INS-Aided GPS Tracking Loops
ZHAO Yan,YI Xiao-xiao,ZHANG Xiao-ming.Performance and Architectures Analysis for INS-Aided GPS Tracking Loops[J].Journal of Astronautic Metrology and Measurement,2007,27(6):45-48,64.
Authors:ZHAO Yan  YI Xiao-xiao  ZHANG Xiao-ming
Abstract:Global positioning system(GPS) and inertial sensors have complementary characteristics,which have been exploited in the design of integrated GPS inertial navigation systems(INS).A scheme of integration can be used,in which the inertial sensors are used to aid the GPS phase/frequency tracking loops directly.This level of coupling is referred to as ultra-tight integration.It offers potential improvements to GPS performance,such as higher phase-tracking bandwidth,and more resistance to frequency noise.We propose a simple architecture for GPS-INS with ultra-tight integration and present the analysis for the performance of such systems.It is proved that this integration scheme can reduce the carrier tracking loop-filter bandwidth for improved signal-to-noise ratio.
Keywords:Global positioning system Receiver Inertial navigation Tracking loop Simulation
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