A hybrid information fusion method for SINS/GNSS integrated navigation system utilizing GRU-aided AKF during GNSS outages

被引:0
|
作者
Xu, Chuan [1 ]
Chen, Shuai [1 ]
Hou, Zhikuan [1 ]
机构
[1] Nanjing Univ Sci & Technol, Sch Automat, Nanjing 210094, Peoples R China
关键词
GNSS outage; GRU neural network; adaptive Kalman filter; error correction; BRIDGING GPS OUTAGES; ALGORITHM;
D O I
10.1088/1361-6501/ad57e2
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
To enhance the performance of integrated inertial navigation system (INS) and global navigation satellite system (GNSS) during GNSS outages, this paper proposed a fusion positioning method based on predictive observation information and adaptive filter parameter. Combined with an adaptive Kalman filter (AKF) and a Gated Recurrent Unit neural network (NN) that directly relates the inertial measurement unit (IMU) output sequence to the error estimation, the hybrid information fusion system can provide effective corrections to compensate for horizontal position errors under the constraints of complex and dynamic vehicle movement data during GNSS outages. Meanwhile, the designed adaptive parameter of the integrated navigation filter can adjust the credibility of the state prediction section when the GNSS is reconnected, ensuring the system can switch rapidly between the INS/GNSS and INS/NN integrated modes. The performance of the proposed information fusion method has been experimentally validated using IMU and GNSS data collected in a vehicle navigation test conducted on a stretch of expressway. The comparison results indicate that the proposed algorithm has error suppression capabilities under various experimental constraints and demonstrates a degree of extendibility and reusability.
引用
收藏
页数:13
相关论文
共 50 条
  • [41] Design of SINS/GNSS integrated navigation system for aerial time-critical guided bomb
    School of Automation, Nanjing University of Science and Technology, Nanjing 210094, China
    Zhongguo Guanxing Jishu Xuebao, 2 (195-199):
  • [42] Implementation and Performance Evaluation of a Distributed GNSS/SINS Ultra-Tightly Integrated Navigation System
    Jiang, Changhui
    Chen, Shuai
    Liu, Yaling
    Han, Xiao
    Chen, Shuai
    Liu, Yaling
    Han, Xiao
    2016 IEEE INTERNATIONAL INSTRUMENTATION AND MEASUREMENT TECHNOLOGY CONFERENCE PROCEEDINGS, 2016, : 923 - 926
  • [43] Design of Missile-Borne GNSS/SINS Tightly-coupled Integrated Navigation System
    Bai Hongyang
    Xiong Kai
    Duan Jiangfeng
    Xu Huiling
    2015 34TH CHINESE CONTROL CONFERENCE (CCC), 2015, : 5348 - 5353
  • [44] Design and Algorithm Research of a GNSS/FOG-SINS Integrated Navigation System for Unmanned Vehicles
    Wang, Han
    Wang, Maosong
    Wen, Kun
    Wu, Wenqi
    PROCEEDINGS OF THE 36TH CHINESE CONTROL CONFERENCE (CCC 2017), 2017, : 6157 - 6162
  • [45] UKF filtering algorithm for SINS/CNS/GNSS integrated navigation in launch inertial coordinate system
    Qiao Yuxin
    Lin Xueyuan
    Zhang Jisong
    Chen Xiangguang
    CHINESE SPACE SCIENCE AND TECHNOLOGY, 2021, 41 (05) : 103 - 109
  • [46] An integrated navigation algorithm assisted by CNN-Informer during short-time GNSS outages
    Hu, Yuan
    Fan, Zhe
    Liu, Wei
    Wu, Linjin
    MEASUREMENT SCIENCE AND TECHNOLOGY, 2024, 35 (09)
  • [47] POS error estimation method based on hybrid prediction model during GNSS outages
    Chen L.
    Liu Z.
    Zhongguo Guanxing Jishu Xuebao/Journal of Chinese Inertial Technology, 2022, 30 (01): : 74 - 80
  • [48] High-precision vehicle GNSS/INS integrated navigation system aided by odometer
    Liu P.-F.
    Guangxue Jingmi Gongcheng/Optics and Precision Engineering, 2020, 28 (04): : 979 - 987
  • [49] Radar and Visual Odometry Integrated System Aided Navigation for UAVS in GNSS Denied Environment
    Mostafa, Mostafa
    Zahran, Shady
    Moussa, Adel
    El-Sheimy, Naser
    Sesay, Abu
    SENSORS, 2018, 18 (09)
  • [50] Integrity monitoring method for GNSS/IMU integrated navigation system of UAV
    Zhao J.
    Song D.
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2024, 45 (07):