JIN Jihang, BIAN Shaofeng. Analysis of Inertial Navigation System Positioning Error Caused by Gravity Disturbance[J]. Geomatics and Information Science of Wuhan University, 2010, 35(1): 30-32.
Citation: JIN Jihang, BIAN Shaofeng. Analysis of Inertial Navigation System Positioning Error Caused by Gravity Disturbance[J]. Geomatics and Information Science of Wuhan University, 2010, 35(1): 30-32.

Analysis of Inertial Navigation System Positioning Error Caused by Gravity Disturbance

Funds: 国家杰出青年科学基金资助项目(40125013);国家自然科学基金资助项目(40774002)
More Information
  • Received Date: October 27, 2009
  • Revised Date: October 27, 2009
  • Published Date: January 04, 2010
  • The error of high-accuracy inertial navigation system(INS) caused by the gravity disturbance can't be neglected.Starting from the physical geodesy and Newton's second law,an error dynamics equation of INS,including the influence of gavity disturbance,is firstly presented in this paper.Then,taking single-axis INS as an example,the position error caused by the deflection of vertical and corresponding characteristics of error propagation in three situation were analyzed.Finally,simulation was done on 1′×1′ deflection of vertical database,and from the simulation result we can see that the horizontal error of INS caused by deflections of the vertical on the sailing course can reach as large as 3 km.
  • Related Articles

    [1]Fu Shuaizhi, Chen Wei, Wu Di, Kong Haiyang, Zheng Hongjiang, Du Luyao. A GNSS/INS Vehicle Integrated Navigation System Based on LSTM-EKF[J]. Geomatics and Information Science of Wuhan University. DOI: 10.13203/j.whugis20200115
    [2]GUAN Bin, SUN Zhongmiao, WU Fumei, LIU Xiaogang. Influence of Horizontal Disturbing Gravity on Position Error in Inertial Navigation Systems[J]. Geomatics and Information Science of Wuhan University, 2017, 42(10): 1474-1481. DOI: 10.13203/j.whugis20160006
    [3]ZHANG Qiuzhao, ZHANG Shubi, LIU Zhiping, ZHENG Nanshan. Tightly-coupled GPS/SINS Integrated System Measurement Model Based on Double-difference Pseudo-range/Pseudo-range Rate[J]. Geomatics and Information Science of Wuhan University, 2015, 40(12): 1690-1694,1700. DOI: 10.13203/j.whugis20130349
    [4]LI Zengke, WANG Jian, GAO Jingxiang. The Apply of Precise Point Positioning in GPS/INS Integrated Navigation[J]. Geomatics and Information Science of Wuhan University, 2013, 38(1): 48-51.
    [5]REN Kai, SONG Xiaoyong, JIA Xiaolin, OUYANG Guichong. A Type of Navigation Strategy of Regional Navigation Satellite System[J]. Geomatics and Information Science of Wuhan University, 2012, 37(11): 1356-1359.
    [6]QIN Fangjun, XU Jiangning, LI An. A New Calculative Method for Gyro-Free Inertial Navigation System Using 9Accelerometers[J]. Geomatics and Information Science of Wuhan University, 2012, 37(3): 278-281.
    [7]QIN Zheng, BIAN Xinqian, SHI Xiaocheng, LI Juan. Simulation Platform of Gravity Aided Inertial Navigation System for Underwater Vehicle[J]. Geomatics and Information Science of Wuhan University, 2008, 33(7): 755-758.
    [8]ZHANG Ka, SHENG Yehua, YE Chun, LIANG Cheng. Absolute Calibration and Precision Analysis for Vehicle-Borne 3D Data Acquiring System Integrated with GPS,INS and CCD-Camera[J]. Geomatics and Information Science of Wuhan University, 2008, 33(1): 55-59.
    [9]YANG Jun, CAO Chong. Market Forecast and Benefit Analysis of Application of Beidou Navigation Satellite System in China[J]. Geomatics and Information Science of Wuhan University, 2004, 29(9): 775-778.
    [10]ZHANG Feizhou, SI Wenfang, YAN Lei, GE Yuansheng. Simulation Research on Matching Algorithm of Autonomous Underwater Navigation System[J]. Geomatics and Information Science of Wuhan University, 2003, 28(2): 153-157.

Catalog

    Article views (1194) PDF downloads (591) Cited by()
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return