GNSS World of China

Volume 44 Issue 4
Aug.  2019
Turn off MathJax
Article Contents
ZHANG Xuanxuan, YANG Cheng. Performance analysis of IMU fine alignment  based on wavelet de-noising[J]. GNSS World of China, 2019, 44(4): 16-24. doi: DOI:10.13442/j.gnss.1008-9268.2019.04.003
Citation: ZHANG Xuanxuan, YANG Cheng. Performance analysis of IMU fine alignment  based on wavelet de-noising[J]. GNSS World of China, 2019, 44(4): 16-24. doi: DOI:10.13442/j.gnss.1008-9268.2019.04.003

Performance analysis of IMU fine alignment  based on wavelet de-noising

doi: DOI:10.13442/j.gnss.1008-9268.2019.04.003
  • Publish Date: 2019-08-15
  • Precision alignment performance is an essential condition to ensure the accuracy of inertial navigation. This paper summarizes the research status of precision alignment at home and abroad, and finds that precision alignment is usually achieved by Kalman filter and linear error equation of small misalignment angle of inertial sensor. Based on this, Kalman filter and wavelet analysis are used in this paper. The precision alignment performance of three kinds of inertial sensors with different performances is analyzed. It is found that the high precision inertial sensors have better alignment accuracy, while the low precision sensors have lower alignment accuracy due to noise deviation and non-linear reasons, even the situation of filter divergence.

     

  • loading
  • [1]
    韩继韬. 高精度光纤捷联惯性导航系统初始对准[D].哈尔滨: 哈尔滨工程大学, 2015.
    [2]
    BRITTING K R. Inertial navigation systems analysis[J]. 1971.DOI: http://dx.doi,org/.
    [3]
    DEYST J, SUTHERLAND A A. Strapdown [JP]inertial system alignment using statistical filtersA simplified formulation[J]. AIAA Journal, 1973, 11(4): 452-456.DOI: 10.2514/3.6773.
    [4]
    JIANG C F, WAN D J. A fast initial alignment method for strapdown inertial navigation system on stationary base[J]. IEEE Transactions on aerospace and electronic systems, 1996, 32(4): 1501-1504.
    [5]
    牟玉涛, 方海涛. 大摇摆情形的自对准方法[J]. 中国科学(信息科学), 2012, 42(11): 1364-1378.
    [6]
    ELSHEIMY N, NASSAR S, NOURELDIN A. Wavelet denoising for IMU alignment[J]. IEEE Aerospace and Electronic Systems Magazine, 2004, 19(10): 32-39.Doi: 10.1109/MAES.2004.1365016.
    [7]
    柴华, 王勇, 许大欣, 等. 地固系下四元数和卡尔曼滤波方法的惯导初始精对准研究[J]. 武汉大学学报(信息科学版), 2012, 37(1): 68-72.
    [8]
    严恭敏. 车载自主定位定向系统研究[D].西安:西北工业大学, 2006.
    [9]
    秦永元. 惯性导航[M].2版. 北京:科学出版社, 2014.
    [10]
    TITTERTON D, WESTON J . [JP]Strapdown inertial navigation technology[M]. IEEE Aerospace and Electronic Systems Magazine, 2005,20(7):33-34. DOI: 10.1109/MAES.2005.1499250.
    [11]
    QUINCHIA A G, FALCO G, FALLETTI E, et al. A comparison between different error modeling of MEMS applied to GPS/INS integrated systems[J]. Sensors, 2013, 13(8): 9549-9588. DOI: 10.3390/S130809549.
    [12]
    周雪梅. 基于多尺度估计理论的组合导航系统研究[D]. 哈尔滨: 哈尔滨工程大学, 2006.
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Article Metrics

    Article views (390) PDF downloads(100) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return