Fault detection and isolation for GNSS/SINS integrated navigation system based on MSS and PNN

被引：0
|
作者：
Li, Peiran [1 ]
Liu, Haiying [1 ]
Wen, Xin [1 ]
Lu, Yuping [1 ]
机构：
[1] Nanjing Univ Aeronaut & Astronaut, Nanjing 210016, Peoples R China
来源：
2018 IEEE CSAA GUIDANCE, NAVIGATION AND CONTROL CONFERENCE (CGNCC) | 2018年
关键词：
Fault detection and isolation; Probabilistic Neural Network; Multiple Solution Separation; GNSS; SINS; MODELS;
D O I：
暂无
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
This paper present a fault detection and isolation method for GNSS/SINS integrated navigation system based on MSS (Multiple Solution Separation) and PNN (Probability Neural Network). The method can also be well applied in the field of general aviation aircraft. Firstly the GNSS/SINS tightly integrated navigation system is designed. Based on the model, the principles and methods of MSS used for fault detection are deduced. Then the fault isolation method using PNN are analyzed too. Lastly, by establishing a simulation system, the analysis and availability for the method are verified.
引用
收藏
页数：6
相关论文
共 50 条
  • [1] Fault Tolerant Design of Integrated Navigation Computer Based on SINS/CNS/GNSS
    Zhang, Ruimin
    Wang, Xusheng
    Fan, Shigang
    PROCEEDINGS OF THE 2017 2ND INTERNATIONAL CONFERENCE ON MODERN MANAGEMENT, EDUCATION TECHNOLOGY, AND SOCIAL SCIENCE (MMETSS 2017), 2017, 146 : 259 - 264
  • [2] SINS/GNSS integrated navigation system based on maximum versoria filter
    Chunhui ZHAO
    Zhenyu YANG
    Xiaoran CHENG
    Jinwen HU
    Xiaolei Hou
    Chinese Journal of Aeronautics, 2022, 35 (08) : 168 - 178
  • [3] SINS/GNSS integrated navigation system based on maximum versoria filter
    Chunhui ZHAO
    Zhenyu YANG
    Xiaoran CHENG
    Jinwen HU
    Xiaolei Hou
    Chinese Journal of Aeronautics , 2022, (08) : 168 - 178
  • [4] SINS/GNSS integrated navigation system based on maximum versoria filter
    Zhao, Chunhui
    Yang, Zhenyu
    Cheng, Xiaoran
    Hu, Jinwen
    Hou, Xiaolei
    CHINESE JOURNAL OF AERONAUTICS, 2022, 35 (08) : 168 - 178
  • [5] A Fault Detection Method for GNSS/INS Integrated Navigation System Based on GARCH Model
    Cong, Li
    Li, Xin
    Yang, Xingguang
    Huang, Xiaoyang
    Xue, Rui
    Tsai, Yung-Fu
    PROCEEDINGS OF THE ION 2015 PACIFIC PNT MEETING, 2015, : 713 - 718
  • [6] Research on GNSS/SINS Tightly Coupled Integrated Navigation System
    Chang, Yaowei
    Chen, Shuai
    MODERN TECHNOLOGIES IN MATERIALS, MECHANICS AND INTELLIGENT SYSTEMS, 2014, 1049 : 1832 - 1835
  • [7] GNSS/SST/SINS integrated navigation system for ballistic missile
    Navigation Research Center, Nanjing University of Aeronautics and Astronautics, 29 Yudao Street, Nanjing 210016, China
    Wuhan Daxue Xuebao (Xinxi Kexue Ban), 2006, 2 (176-179):
  • [8] An Outlier Detection Method of GNSS/SINS Integrated Navigation Based on Accelerometer Bias Stability
    Tao X.
    Zhang X.
    Zhu F.
    Xiao J.
    Wuhan Daxue Xuebao (Xinxi Kexue Ban)/Geomatics and Information Science of Wuhan University, 2018, 43 (07): : 1078 - 1084
  • [9] A method for fault detection and isolation in the integrated navigation system for UAV
    Yang Bo
    Qin Yongyuan
    Chai Yan
    MEASUREMENT SCIENCE AND TECHNOLOGY, 2006, 17 (06) : 1522 - 1528
  • [10] Design of marine-based miniature tightly integrated SINS/GNSS navigation system
    Yan, Jie
    Xu, Xiao-Su
    Zhang, Tao
    Liu, Yi-Ting
    Wu, Liang
    Zhongguo Guanxing Jishu Xuebao/Journal of Chinese Inertial Technology, 2013, 21 (06): : 775 - 780
12345