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Design and analysis for an innovative scheme of SINS/GPS ultra-tight integration

机译:SINS / GPS超紧密集成创新方案的设计与分析

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摘要

Purpose - The purpose of this paper is to improve the tracking performance of the carrier phase lock loop (PLL) in the strapdown inertial navigation system/global positioning system (SINS/GPS) integrated system with an innovative scheme of ultra-tight integration. Design/methodology/approach - First, providing the Doppler frequency for PLL using SINS velocity could enlarge the loop equivalent bandwidth and reduce the dynamic effect on the carrier loop. Meanwhile, lowering the filter bandwidth could increase the immunity to noise. Second, the relationships between the PLL and SINS errors have been analyzed, and then the PLL error model is established to eliminate the correlation between the pseudo-range-rate error and SINS velocity error. Third, the carrier frequency is regulated to improve the tracking accuracy, according to the error estimations of Kalman filter. Findings - The innovative ultra-tightly integrated system could not only enhance the anti-jamming capability and the dynamic tracking performance of the tracking loops, but also improve the pseudo-range-rate measurements accuracy for the integrated filter. Originality/value - This paper provides further study on the method of enhancing the carrier-tracking performance and improving the integration mode in the ultra-tightly integrated system based on the software-defined GPS receiver.
机译:目的-本文的目的是通过一种创新的超紧密集成方案,提高捷联惯性导航系统/全球定位系统(SINS / GPS)集成系统中载波锁相环(PLL)的跟踪性能。设计/方法/方法-首先,使用SINS速度为PLL提供多普勒频率可能会增大环路等效带宽并降低对载波环路的动态影响。同时,降低滤波器带宽可以提高抗干扰能力。其次,分析了PLL和SINS误差之间的关系,然后建立了PLL误差模型以消除伪距率误差和SINS速度误差之间的相关性。第三,根据卡尔曼滤波器的误差估计,调节载波频率以提高跟踪精度。发现-创新的超紧密集成系统不仅可以增强跟踪环路的抗干扰能力和动态跟踪性能,而且还可以提高集成滤波器的伪距速率测量精度。原创性/价值-本文针对基于软件定义的GPS接收器的超紧密集成系统中提高载波跟踪性能和改进集成模式的方法进行了进一步研究。

著录项

  • 来源
    《Aircraft Engineering and Aerospace Technology》 |2010年第1期|p.1-12|共12页
  • 作者单位

    Yu Jie, School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing, China Wang Xinlong, School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing, China Ji Jiaxing, School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing, China;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

  • 入库时间 2022-08-17 23:18:13

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