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Improving the Performance of Tightly-Coupled GPS/INS Navigation by Using Time-Differenced GPS-Carrier-Phase Measurements and Low-Cost MEMS IMU

机译:通过使用时差GPS载波相位测量和低成本MEMS IMU改善紧密耦合的GPS / INS导航的性能

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摘要

To avoid the difficulties in fixing the carrier phase ambiguities, the time difference carrier phase approach is applied to a GPS/IMU tightly-coupled navigation system to eliminate the ambiguity between two successive GPS epochs, which can provide high velocity estimation accuracy. The carrier phases are carefully corrected before use. A modified method is proposed by using the system matrix in each time update to calculate the integration of the velocity errors in the measurement update equation. A Cubature Kalman Filter (CKF) is applied to the integrated navigation system to improve the attitude estimation accuracy. The navigation result and comparison show the accuracy improvement after applying the carrier phase corrections, modified measurement update method and the CKF.
机译:为了避免固定载波相位模糊度的困难,将时差载波相位方法应用于GPS / IMU紧密耦合的导航系统,以消除两个连续GPS历元之间的模糊度,从而可以提供较高的速度估计精度。使用前,请仔细校正载流子相。通过在每次更新中使用系统矩阵来计算测量更新方程中速度误差的积分,提出了一种改进的方法。 Cubature Kalman滤波器(CKF)被应用于集成导航系统,以提高姿态估计的准确性。导航结果和比较结果表明,在应用载波相位校正,改进的测量更新方法和CKF之后,可以提高精度。

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  • 来源
    《Gyroscopy and navigation》 |2015年第2期|133-142|共10页
  • 作者单位

    Physical and Satellite Geodesy, Institute of Geodesy, Technische Universitat Darmstadt, Darmstadt, Germany;

    Physical and Satellite Geodesy, Institute of Geodesy, Technische Universitat Darmstadt, Darmstadt, Germany;

    Physical and Satellite Geodesy, Institute of Geodesy, Technische Universitat Darmstadt, Darmstadt, Germany;

    Physical and Satellite Geodesy, Institute of Geodesy, Technische Universitat Darmstadt, Darmstadt, Germany;

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  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Times difference carrier phase; IMU; Cubature Kalman Filter; measurement update equation;

    机译:时差载波相位;IMU;Cubature卡尔曼滤波测量更新方程;
  • 入库时间 2022-08-18 02:23:17

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