Volume 11 Issue 3
. 
Turn off MathJax
Article Contents
Article Navigation >  Journal of Traffic and Transportation Engineering  > 2011  >  11(3): 100-104
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]
    王光辉, 朱海, 莫军, 等. 一种基于天空光偏振特性的天文导航方式[J]. 中国航海, 2009, 32 (1): 14-16. doi: 10.3969/j.issn.1000-4653.2009.01.004

    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]
    于堃, 李琳, 刘为任, 等. 舰船惯性导航系统海上无阻尼状态的校准[J]. 中国惯性技术学报, 2008, 16 (6): 637-642. https://www.cnki.com.cn/Article/CJFDTOTAL-ZGXJ200806003.htm

    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]
    程建华, 郝燕玲, 孙枫, 等. 自动补偿技术在平台式惯导系统综合校正中的应用研究[J]. 哈尔滨工程大学学报, 2008, 29 (1): 40-44. doi: 10.3969/j.issn.1006-7043.2008.01.008

    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]
    关劲, 程建华, 吴磊, 等. 船用平台式惯导系统状态转换技术的应用[J]. 中国造船, 2008, 49 (2): 75-80. doi: 10.3969/j.issn.1000-4882.2008.02.010

    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]
    钱山, 李鹏奎, 张士峰, 等. MI MU/GPS组合导航建模及GPS时间延迟补偿算法研究[J]. 系统工程与电子技术, 2009, 31 (6): 1432-1435. doi: 10.3321/j.issn:1001-506X.2009.06.038

    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]
    张源, 许江宁, 卞鸿巍. GPS姿态测量系统对惯性导航系统误差修正能力分析[J]. 情报指挥控制系统与仿真技术, 2005, 27 (5): 96-100. doi: 10.3969/j.issn.1673-3819.2005.05.023

    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]
    韩璐, 景占荣, 段哲民. SINS/GPS组合导航系统仿真研究[J]. 计算机仿真, 2009, 26 (9): 32-36. doi: 10.3969/j.issn.1006-9348.2009.09.011

    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]
    杨艳娟, 卞鸿巍, 田蔚风, 等. 一种新的I NS/GPS组合导航技术[J]. 中国惯性技术学报, 2004, 12 (2): 23-26. doi: 10.3969/j.issn.1005-6734.2004.02.006

    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]
    胡朝晖, 王建波. GPS/GLONASS集成接收机定位精度分析[J]. 情报指挥控制系统与仿真技术, 2002, 24 (9): 46-47. doi: 10.3969/j.issn.1673-3819.2002.09.007

    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]
    冯跃强, 王彬, 蔡伯根. GPS/GLONASS组合定位导航技术的测试[J]. 北京交通大学学报, 2005, 29 (2): 91-93. doi: 10.3969/j.issn.1673-0291.2005.02.023

    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]
    岳亚洲, 田宇, 张晓冬. 机载惯性/天文组合导航研究[J]. 光学与光电技术, 2008, 6 (2): 1-5. doi: 10.3969/j.issn.1672-3392.2008.02.001

    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]
    何炬. 国外天文导航技术发展综述[J]. 舰船科学技术, 2005, 27 (5): 91-96. https://www.cnki.com.cn/Article/CJFDTOTAL-JCKX200505021.htm

    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
  • 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
    Get Citation
    PDF
    XML

    Article Metrics

    Article views (623) PDF downloads(544) Cited by()
    Proportional views
    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