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XIA Wei-xing, YANG Xiao-dong, SHI Wen-ming, WANG Wang. Loose navigation state algorithm of INS two-point calibration in horizontal damping state[J]. Journal of Traffic and Transportation Engineering, 2013, 13(2): 99-105. doi: 10.19818/j.cnki.1671-1637.2013.02.015
Citation: XIA Wei-xing, YANG Xiao-dong, SHI Wen-ming, WANG Wang. Loose navigation state algorithm of INS two-point calibration in horizontal damping state[J]. Journal of Traffic and Transportation Engineering, 2013, 13(2): 99-105. doi: 10.19818/j.cnki.1671-1637.2013.02.015
shu

Loose navigation state algorithm of INS two-point calibration in horizontal damping state

doi: 10.19818/j.cnki.1671-1637.2013.02.015
  • 1.

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

  • 2.

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

More Information
  • Author Bio:

    XIA Wei-xing(1985-), male, doctoral student, +86-532-51858653, 596978805@qq.com

    YANG Xiac-dong(1963-), male, professor, PhD, +86-532-51858653, yangxd@163.com

  • Received Date: 2012-12-15
  • Publish Date: 2013-04-25
    Abstract
  • In order to satisfy high-accuracy navigation and improve comprehensive calibration accuracy, a INS two-point calibration loose navigation state algorithm in horizontal damping state was designed by using extended state observer(ESO).The principle of traditional two-point calibration, navigation state constraint and its shortage were analyzed.The platform horizontal misalignment angles of inertial navigation system were real-timely estimated by using ESO, and traditional two-point calibration was introduced.The algorithm was simulated and numerically verified.Verification result indicates that the estimation result of traditional two-point calibration considerably reduces and even diverges when navigation state constraint can not be satisfied, neverthelessly, loose navigation state algorithm has a stronger applicability not only to reduce restrictive navigation state, but also to improve comprehensive calibration accuracy.Gyro drifts for east, north and position in experiment 1 reduce from 33.5%, 51.2%, 17.9% to 8.0%, 1.8%, 3.1% respectively, and in experiment 2, the drifts reduce from 83.7%, 39.7%, 77.5% to 2.3%, 0.3%, 1.0% respectively.

     

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    • References(18)
  • [1]
    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. (in Chinese). doi: 10.3969/j.issn.1671-1637.2011.03.017
    [2]
    HARTMAN R, HAWKINSON W, SWEENEY K. Tactical underwater navigation system position[C]//IEEE. 2008 IEEE Position Location and Navigation Symposium. Monterey: IEEE, 2008: 898-911.
    [3]
    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
    [4]
    GUAN Jin, CHENG Jian-hua, WU Lei, et al. The state switch technology of gimbaled INS[J]. Shipbuilding of China, 2008, 49(2): 75-80. (in Chinese). doi: 10.3969/j.issn.1000-4882.2008.02.010
    [5]
    ZHANG Wei-ming, ZHANG Ji-wei, FAN Zi-jie, et al. Research on unscented Kalman filter in initial alignment of inertial navigation systems[J]. Systems Engineering and Electronics, 2007, 29(4): 589-592. (in Chinese). doi: 10.3321/j.issn:1001-506X.2007.04.023
    [6]
    LU Min, YIN Yong. Application of unscented particle filter in INS non-linear alignment[J]. Radar Science and Technology, 2008, 6(1): 44-47. (in Chinese). doi: 10.3969/j.issn.1672-2337.2008.01.008
    [7]
    SONG Jin-lai, HAN Jing-qing. Research on a fast initial alignment method for platform inertial navigation system[J]. Journal of Chinese Inertial Technology, 2002, 10(1): 25-29. (in Chinese). doi: 10.3969/j.issn.1005-6734.2002.01.006
    [8]
    WANG Chao, MA Lin-li. Application of the extend state observer on the initial alignment of the inertial navigationsystem[J]. Ship Science and Technology, 2009, 31(7): 85-88. (in Chinese). doi: 10.3404/j.issn.1672-7649.2009.07.018
    [9]
    NIU Li, LI Li, ZHAO Hui, et al. Application of active disturbance rejection control technique in initial alignment of SINS on moving base[J]. Journal of Chinese Inertial Technology, 2003, 11(6): 27-33. (in Chinese). doi: 10.3969/j.issn.1005-6734.2003.06.006
    [10]
    ZHAO Wang-yang, ZHUANG Liang-jie, YANG Gong-liu. Application of active disturbance rejection controller in initial alignment of INS on moving base[J]. Control and Decision, 2007, 22(2): 179-183. (in Chinese). doi: 10.3321/j.issn:1001-0920.2007.02.012
    [11]
    SONG Jin-lai, YANG Yu, XU Ke-kang, et al. Application of active disturbance rejection technique in initial alignment of inertial navigation system[J]. Journal of Chinese Inertial Technology, 2001, 9(4): 11-14, 27. (in Chinese). doi: 10.3969/j.issn.1005-6734.2001.04.003
    [12]
    YANG Chang-song, XU Xiao-su, WANG Li-yun, et al. Information fusion technology and its application in INS/GPS/DVL integrated navigation[J]. Journal of ChineseInertial Technology, 2006, 14(5): 39-43. (in Chinese). doi: 10.3969/j.issn.1005-6734.2006.05.011
    [13]
    LI Jia-qi, WANG Hong-wei, LIU Ai-dong, et al. A CNS/INS combined navigation system[J]. Control Theory and Applications, 2005, 24(4): 13-15. (in Chinese). https://www.cnki.com.cn/Article/CJFDTOTAL-ZDHJ200504004.htm
    [14]
    FANG Jiang-cheng, WAN De-jun. A fast initial alignment method for strapdown inertial navigation system on stationary base[J]. IEEE Transactions on Aerospace and Electronic Systems, 1996, 32(4): 1501-1505. doi: 10.1109/7.543871
    [15]
    HUANG Yi, HAN Jing-qing. Disturbace rejection and tracting design via the SSR aproach for second order uncertionsystems[J]. System Sciences and Mathematical Sciences, 1999, 12(3): 238-245.
    [16]
    ZHAO Wang-yang, WU Jun-jie, ZHUANG Liang-jie, et al. Initial alignments of inertial navigation system on static base with ESO technique[J]. Journal of Data Acquisition and Processing, 2007, 22(1): 105-109. (in Chinese). doi: 10.3969/j.issn.1004-9037.2007.01.018
    [17]
    HUANG Yi, HAN Jing-qing. Analysis and design for the second order nonlinear continuous extended state observer[J]. Chinese Science Bulletin, 2000, 45(21): 1938-1944. doi: 10.1007/BF02909682
    [18]
    NIU Li, LI Li, ZHUANG Liang-jie. Active disturbance rejection control of stabilizing circuits for inertial platform[J]. Journal of Chinese Inertial Technology, 2004, 12(6): 48-51, 64. (in Chinese). doi: 10.3969/j.issn.1005-6734.2004.06.011
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