Volume 11 Issue 3
. 
Turn off MathJax
Article Contents
Article Navigation >  Journal of Traffic and Transportation Engineering  > 2011  >  11(3): 100-104
Next Previous
YANG Xiao-dong, DENG Tai-guang. Constant error analysis of two-point comprehensive calibration in gimbaled inertial navigation system[J]. Journal of Traffic and Transportation Engineering, 2011, 11(3): 100-104. doi: 10.19818/j.cnki.1671-1637.2011.03.017
Citation: YANG Xiao-dong, DENG Tai-guang. Constant error analysis of two-point comprehensive calibration in gimbaled inertial navigation system[J]. Journal of Traffic and Transportation Engineering, 2011, 11(3): 100-104. doi: 10.19818/j.cnki.1671-1637.2011.03.017
shu

Constant error analysis of two-point comprehensive calibration in gimbaled inertial navigation system

doi: 10.19818/j.cnki.1671-1637.2011.03.017
  • 1.

    Department of Navigational Instrument, Navy Submarine Academy, Qingdao 266042, Shandong, China

  • 2.

    No.3 Brigade of Graduate, Navy Submarine Academy, Qingdao 266042, Shandong, China

More Information
  • Author Bio:

    YANG Xiao-dong(1963-), male, professor, +86-532-51858653, yangxdqtxy@163.com

  • Received Date: 2011-01-16
  • Publish Date: 2011-06-25
    Abstract
  • In order to estimate and compensate the comprehensive calibration errors caused by various factors, the influences of exoteric measuring information error and inertial platform horizontal error angle in two-point comprehensive calibration of gimbaled inertial navigation system (INS) on the calibration effect of constant gyro drift were studied in theory. The relation between the maximum values of constant gyro drift error and calibration interval was deduced. Two-point calibration process affected by exoteric measuring information error was simulated. Analysis result shows that under current precision levels of exoteric measuring information error and platform horizontal error angle, the magnitudes of the maximum values induced by the two errors are both 0.001 (°) ·h-1 when the interval time of two adjustments is 10 h. The two kinds of errors are both linear with the estimation error of two-point calibration approach on constant gyro drift. In order to improve the precision of two-point calibration, it is important to increase exoteric measuring information precision and inertial platform horizontal precision efficiently.

     

    • FullText(HTML)
  • loading
    • References(13)
  • [1]
    WANG Guang-hui, ZHU Hai, MO Jun, et al. A kind of celestial navigation mode based on polarization of skylight[J]. Navigation of China, 2009, 32 (1): 14-16. (in Chinese) doi: 10.3969/j.issn.1000-4653.2009.01.004
    [2]
    YU Kun, LI Lin, LIU Wei-ren, et al. Correction of SINS based on undamped navigation mode[J]. Journal of Chinese Inertial Technology, 2008, 16 (6): 637-642. (in Chinese) https://www.cnki.com.cn/Article/CJFDTOTAL-ZGXJ200806003.htm
    [3]
    SINOPOLI B, SCHENATO L, FRANCESCHETTI M, et al. Kal man filtering with intermittent observations[J]. IEEE Transactions on Automatic Control, 2004, 49 (9): 1453-1464. doi: 10.1109/TAC.2004.834121
    [4]
    CHENG Jian-hua, HAO Yan-ling, SUN Feng, et al. Application of an auto-compensation technique in the comprehensive calibration of INS[J]. Journal of Harbin Engineering University, 2008, 29 (1): 40-44. (in Chinese) doi: 10.3969/j.issn.1006-7043.2008.01.008
    [5]
    GUAN Jin, CHENG Jian-hua, WU Lei, et al. The state switch technology of gi mbaled INS[J]. Ship Building of China, 2008, 49 (2): 75-80. (in Chinese) doi: 10.3969/j.issn.1000-4882.2008.02.010
    [6]
    QIAN Shan, LI Peng-kui, ZHANGShi-feng, et al. Study on modeling of MI MU/GPS navigation andti me delay synchronization method of GPS[J]. Systems Engineering and Electronics, 2009, 31 (6): 1432-1435. (in Chinese) doi: 10.3321/j.issn:1001-506X.2009.06.038
    [7]
    ZHANG Yuan, XU Jiang-ning, BIAN Hong-wei. Analysisfor capability of I NS error-correction based on GPS attitude determination system[J]. Information Command Control System & Simulation Technology, 2005, 27 (5): 96-100. (in Chinese) doi: 10.3969/j.issn.1673-3819.2005.05.023
    [8]
    HAN Lu, JING Zhan-rong, DUAN Zhe-min. Simulation of SINS/GPSintegrated navigation system[J]. Computer Simulation, 2009, 26 (9): 32-36. (in Chinese) doi: 10.3969/j.issn.1006-9348.2009.09.011
    [9]
    YANG Yan-juan, BIAN Hong-wei, TIAN Wei-feng, et al. A new INS/GPSintegrated navigation technique[J]. Journal of Chinese Inertial Technology, 2004, 12 (2): 23-26. (in Chinese) doi: 10.3969/j.issn.1005-6734.2004.02.006
    [10]
    HU Zhao-hui, WANG Jian-bo. Analysis on positioning accuracy of GPS/GLONASS integrated receiver[J]. Information Command Control System & Simulation Technology, 2002, 24 (9): 46-47. (in Chinese) doi: 10.3969/j.issn.1673-3819.2002.09.007
    [11]
    FENG Yue-qiang, WANG Bin, CAI Bai-gen. Investigation of GPS/GLONASS integrated location and navigation technology[J]. Journal of Beijing Jiaotong University, 2005, 29 (2): 91-93. (in Chinese) doi: 10.3969/j.issn.1673-0291.2005.02.023
    [12]
    YUE Ya-zhou, TIAN Yu, ZHANG Xiao-dong. Investigation on airborne inertial/celestial integrated navigation[J]. Optics and Optoelectronic Technology, 2008, 6 (2): 1-5. (in Chinese) doi: 10.3969/j.issn.1672-3392.2008.02.001
    [13]
    HE Ju. Survey of overseas celestial navigation technology development[J]. Ship Science And Technology, 2005, 27 (5): 91-96. (in Chinese) https://www.cnki.com.cn/Article/CJFDTOTAL-JCKX200505021.htm
    • Relative Articles
    • Supplements(0)
    • Cited By

Catalog

    Get Citation
    PDF
    XML

    Article Metrics

    Article views (721) PDF downloads(547) Cited by()
    Related

    Copyright《Journal of Traffic and Transportation Engineering》编辑部陕ICP备05001904号-1

    Address ：Editorial Department of Journal of Traffic and Transportation Engineering, Chang 'an University, Middle Section of South Second Ring Road, Xi 'an, Shaanxi（710064） Tel：029-82334388 Email：jygc@chd.edu.cn

    All visit:Today's visit:

    Supported by: Beijing Renhe Information Technology Co. Ltd    

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return