GPS/IMU Integrated Navigation System Case Study with Unscented Kalman Filtering

被引:0
|
作者
Guo, Hang [1 ]
Wang, Lixun [1 ]
Yu, Min [2 ]
机构
[1] Nanchang Univ, Jiangxi 330031, Peoples R China
[2] Jiangxi Normal Univ, Dept Comp Sci, Digital Signal Proc, Nanchang, Jiangxi, Peoples R China
关键词
D O I
暂无
中图分类号
TP18 [人工智能理论];
学科分类号
081104 ; 0812 ; 0835 ; 1405 ;
摘要
The Unscented Kalman Filtering (UKF), which is a new nonlinear filtering method, avoids the linearization for nonlinear system state equations. Compared with the extended Kalman Filtering (EKF), the UKF has the characteristics of overcoming calculation divergence (such as linearization error), easy realization and higher state estimation accuracy as well. In the case study, the UKF is applied to an airplane GPS/IMU integrated navigation system including NovAtel, Trimble GPS receivers for the base station and rover, Litton LN 200 IMU on the aircraft. Differential GPS processing results are used for the observation values of the integrated system, the initial values of the airplane positions, velocities, and attitudes are approximately determined by GPS positions and velocities, and a modified observation equation has been developed. The field GPS/IMU data sets was collected in Alps mountain area flight test, 1999. The UKF, EKF, and IEKF position, velocity, and attitude parameters were obtained. The processing results showed that UKF has effectively solved nonlinearity problem of system state equation in this case study. And the UKF has position accuracy RMS of 0.018, 0.025, 0.041 meters in East, North, and Up directions, velocity accuracy RMS of 0.004, 0.005, 0.006 m/s in East, North, and Up directions, attitude error angle of 1.5, 15, 14 arcseconds in East, North, and Up directions, while EKF has position accuracy RMS of 0.018, 0.025, 0.041 meters in East, North, and Up directions, velocity accuracy RMS of 0.013, 0.017, 0.027 m/s in East, North, and Up directions, attitude error angle of 60, 61, 74 arcseconds in East, North, and Up directions,. Comparing with EKF, GPS/IMU integrated navigation parameters predicted by UKF have higher accuracy. In addition, EKF has experienced an attitude divergence for a time period of 450 seconds due to its linearization problem, but UKF with the modified observation equation didn't. It's also verified that the UKF is superior to the EKF.
引用
收藏
页码:698 / 705
页数:8
相关论文
共 50 条
  • [41] An integrated GPS/MEMS-IMU navigation system for an autonomous helicopter
    Wendel, Jan
    Meister, Oliver
    Schlaile, Christian
    Trommer, Gert F.
    [J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2006, 10 (06) : 527 - 533
  • [42] Realization of low-cost IMU/GPS integrated navigation system
    Yu, Min
    Guo, Hang
    Gao, Weiguang
    [J]. FCST 2006: JAPAN-CHINA JOINT WORKSHOP ON FRONTIER OF COMPUTER SCIENCE AND TECHNOLOGY, PROCEEDINGS, 2006, : 189 - +
  • [43] An Adaptive Dual Kalman Filtering Algorithm for Locata/GPS/INS Integrated Navigation
    Zhou, Zebo
    Yang, Ling
    Li, Yong
    [J]. CHINA SATELLITE NAVIGATION CONFERENCE (CSNC) 2013 PROCEEDINGS: PRECISE ORBIT DETERMINATION & POSITIONING, ATOMIC CLOCK TECHNIQUE & TIME-FREQUENCY SYSTEM, INTEGRATED NAVIGATION & NEW METHODS, 2013, 245 : 527 - 541
  • [44] Multipath Mitigation using GPS/INS Integrated Navigation with Adaptive Kalman Filtering
    Kim, Younsil
    Kim, Jungbeom
    Yu, Sunkyoung
    Kee, Changdon
    Park, Byungwoon
    [J]. PROCEEDINGS OF THE 2016 INTERNATIONAL TECHNICAL MEETING OF THE INSTITUTE OF NAVIGATION, 2016, : 893 - 901
  • [45] Correlational inference-based adaptive unscented Kalman filter with application in GNSS/IMU-integrated navigation
    Yang, Cheng
    Shi, Wenzhong
    Chen, Wu
    [J]. GPS SOLUTIONS, 2018, 22 (04)
  • [46] A new two-step adaptive robust Kalman filtering in GPS/INS integrated navigation system
    Wu, Fumei
    Yang, Yuanxi
    [J]. Cehui Xuebao/Acta Geodaetica et Cartographica Sinica, 2010, 39 (05): : 522 - 527
  • [47] Correlational inference-based adaptive unscented Kalman filter with application in GNSS/IMU-integrated navigation
    Cheng Yang
    Wenzhong Shi
    Wu Chen
    [J]. GPS Solutions, 2018, 22
  • [48] Unscented Kalman Filtering on Manifolds for AUV Navigation - Experimental Results
    Krauss, Stephen T.
    Stilwell, Daniel J.
    [J]. 2022 OCEANS HAMPTON ROADS, 2022,
  • [49] Research on Adaptive Unscented Kalman Filter for Integrated Navigation
    Xu, Tianlai
    [J]. MATERIALS PROCESSING AND MANUFACTURING III, PTS 1-4, 2013, 753-755 : 2582 - 2585
  • [50] A Matching-Unscented Kalman Filtering for Gravity Aided Navigation
    Wu, Lin
    Tian, Xin
    Ma, Hong
    Tian, Jinwen
    [J]. MIPPR 2011: AUTOMATIC TARGET RECOGNITION AND IMAGE ANALYSIS, 2011, 8003