Application of the spherical harmonic gravity model in high precision inertial navigation systems

被引:19
|
作者
Wang, Jing [1 ,2 ]
Yang, Gongliu [1 ,2 ]
Li, Xiangyun [3 ]
Zhou, Xiao [1 ,2 ]
机构
[1] Beihang Univ, Sch Instrument Sci & Optoelect Engn, Beijing 100191, Peoples R China
[2] Beihang Univ, Sci & Technol Inertial Lab, Beijing 100191, Peoples R China
[3] Dongying Vocat Coll, Sch Elect Informat & Media, Dongying 257091, Peoples R China
基金
中国国家自然科学基金;
关键词
spherical harmonic gravity model; computational complexity; appropriate degree; high precision INS; APPROXIMATION; COMPENSATION;
D O I
10.1088/0957-0233/27/9/095103
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The spherical harmonic gravity model (SHM) may, in general, be considered as a suitable alternative to the normal gravity model (NGM), because it represents the Earth's gravitational field more accurately. However, the high-resolution SHM has never been used in current inertial navigation systems (INSs) due to its extremely complex expression. In this paper, the feasibility and accuracy of a truncated SHM are discussed for application in a real-time free-INS with a precision demand better than 0.8 nm h(-1). In particular, the time and space complexity are analyzed mathematically to verify the feasibility of the SHM. Also, a test on a typical navigation computer shows a storable range of cut-off degrees. To further evaluate the appropriate degree and accuracy of the truncated SHM, analyses of covariance and truncation error are proposed. Finally, a SHM of degree 12 is demonstrated to be the appropriate model for routine INSs in the precision range of 0.4-0.75 nm h(-1). Flight simulations and road tests show its outstanding performance over the traditional NGM.
引用
收藏
页数:10
相关论文
共 50 条
  • [41] Spherical harmonic analysis and synthesis using FFT: Application to temporal gravity variation
    Hwang, C
    Kao, YC
    COMPUTERS & GEOSCIENCES, 2006, 32 (04) : 442 - 451
  • [42] Trends in inertial systems technology for high accuracy AUV navigation
    Huddle, JR
    PROCEEDINGS OF THE 1998 WORKSHOP ON AUTONOMOUS UNDERWATER VEHICLES, (AUV '98), 1998, : 63 - 73
  • [43] Stochastic Modeling of Gravity Compensation Error in GNSS-aided Inertial Navigation Systems
    Needham, Timothy G.
    Braasch, Michael S.
    2020 IEEE/ION POSITION, LOCATION AND NAVIGATION SYMPOSIUM (PLANS), 2020, : 770 - 780
  • [44] High-Precision Simulator for Strapdown Inertial Navigation Systems Based on Real Dynamics from GNSS and IMU Integration
    Yan, Gongmin
    Wang, Jinling
    Zhou, Xinyi
    CHINA SATELLITE NAVIGATION CONFERENCE (CSNC) 2015 PROCEEDINGS, VOL III, 2015, 342 : 789 - 799
  • [45] An Analysis of the Effect of Gravity Anomaly to Height Estimation in High-Precision INS/GNSS Integrated Navigation Systems
    Xiong, Hao
    Zhao, Yingwei
    Wang, Xingshu
    Dai, Dongkai
    Zheng, Jiaxing
    Zhan, Dejun
    IEEE SENSORS JOURNAL, 2019, 19 (07) : 2713 - 2721
  • [46] Achieving High Navigation Accuracy Using Inertial Navigation Systems in Autonomous Underwater Vehicles
    Panish, Robert
    Taylor, Mikell
    2011 IEEE - OCEANS SPAIN, 2011,
  • [47] Application of H∞ filtering to fast ground alignment of inertial navigation systems
    Wang, Yandong
    Fan, Yuezu
    Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics, 2000, 26 (05): : 516 - 518
  • [48] KALMAN FILTER, BASIC OBSERVATIONS AND POSSIBLE APPLICATION IN INERTIAL NAVIGATION SYSTEMS
    KROGMANN, U
    ZEITSCHRIFT FUR FLUGWISSENSCHAFTEN, 1972, 20 (04): : 155 - +
  • [49] Application of covariance analysis method in design of modulated inertial navigation systems
    Guan B.
    Hu W.
    Li S.
    Yang X.
    Li C.
    Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University, 2023, 41 (06): : 1146 - 1154
  • [50] APPLICATION OF OPTIMAL SMOOTHING TO TESTING AND EVALUATION OF INERTIAL NAVIGATION SYSTEMS AND COMPONENTS
    NASH, RA
    KASPER, JF
    CRAWFORD, BS
    LEVINE, SA
    IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1971, AC16 (06) : 806 - +