Advanced Search
Volume 39 Issue 11
Nov.  2013
Turn off MathJax
Article Contents
Journal of Beijing University of Aeronautics and Astronautics  > 2013  >  39(11): 1525-1528,1541.
Wang Kedong, Hu Zheng, Hou Shaodonget al. Simulated GPS IF and IMU signals and verification[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(11): 1525-1528,1541. (in Chinese)
Citation: Wang Kedong, Hu Zheng, Hou Shaodonget al. Simulated GPS IF and IMU signals and verification[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(11): 1525-1528,1541. (in Chinese)
shu

Simulated GPS IF and IMU signals and verification

  • School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • Received Date: 19 Dec 2012
  • Publish Date: 30 Nov 2013
    Abstract
  • A software simulator to simulate GPS IF signal and inertial measurement unit(IMU) signal was developed for the research on the GPS/INS integration algorithm. The vehicle trajectory was modeled in kinematics. The method to simulate the signal was put forward. The IMU signal was modeled based on the typical vehicle motions, such as the level motion, the rolling, the pitching, and the yawing. The typical interference signals, including the spoofing signal and the blocking signal (the narrow-band noise interference, the wide-band noise interference, the continuous-wave interference, and the sawtooth frequency modulated continuous wave interference), were modeled and generated to simulate the interference scenarios. The data generated by the simulator were calculated by the GPS/INS integration algorithm. The results prove that the algorithm of the signal simulation is correct and the IF signal and IMU signal provided by the simulator are effective preliminarily.

     

    • FullText(HTML)
  • loading
    • References(17)
  • [1]
    Brenner M.Integrated GPS/inertial fault detection availability[J].Journal of the Institute of Navigation, 1996, 43 (2):111-130
    [2]
    Noureldin A, Karamat T B, Eberts M D, et al.Performance enhancement of MEMS-based INS/GPS integration for low-cost navigation applications[J].IEEE Transactions on Vehicle Technology, 2009, 58 (3):1077-1096
    [3]
    Knight D T.Rapid development of tightly coupled GPS/INS systems[J].IEEE Aerospace and Electronic Systems Magazine, 1999, 12 (2):14-18
    [4]
    Soloviev A, Gunawardena S, Graas F V.Deeply integrated GPS/low-cost IMU for low CNR signal processing:concept description and in-flight demonstration[J].Journal of the Institute of Navigation, 2008, 55 (1):1-13
    [5]
    Gebre E.What is the difference between 'loose', 'tight', 'ultra-tight' and 'deep' integration strategies for INS and GNSS[J].Inside GNSS, 2007, 2 (1):28-33
    [6]
    Fedora N, Ford C, Boulton P.A versatile solution for testing GPS/inertial navigation systems[C]//Proceedings of the 21st International Technical Meeting of the Satellite Division of the Institute of Navigation.New York:Curran Associates Inc, 2008:992-1001
    [7]
    东方联星公司.NS800多系统导航卫星信号模拟器[EB/OL].[2013-08-02].http://www.olinkstar.com/products/ls-0852812500633.aspx OlinkStar Co., Ltd.NS800 Multi-system navigation satellite signal simulator[EB/OL].[2013-08-02].http://www.olinkstar.com/products/ls-0852812500633.aspx (in Chinese)
    [8]
    Dong L.IF GPS signal simulator development and verification[D].Alberta:Calgary University, 2003
    [9]
    侯博, 谢杰, 刘光斌.卫星信号模拟器的发展现状与趋势[J].电讯技术, 2011, 51 (5):127-132 Hou Bo, Xie Jie, Liu Guangbin.Navigation satellite signal simulator:current states and developing trend[J].Telecommunication Engineering, 2011, 51 (5):127-132 (in Chinese)
    [10]
    郑晓冬.卫星导航系统复杂干扰信号模拟源设计[D].成都:电子科技大学, 2012 Zheng Xiaodong.The design for complex interference signal simulator of satellite navigation systems[D].Chengdu:University of Electronic Science and Technology of China, 2012 (in Chinese)
    [11]
    谢钢.GPS原理与接收机设计[M].北京:电子工业出版社, 2009:74-75 Xie Gang.Principles of GPS and receiver design[M].Beijing:Publishing House of Electronics Industry, 2009:74-75 (in Chinese)
    [12]
    赵军详, 张其善, 常青, 等.高动态GPS卫星信号模拟器关键技术分析及应用[J].电讯技术, 2003, 46 (4) , 49-54 Zhao Junxiang, Zhang Qishan, Chang Qing, et al.The key technique analysis and applications of high dynamic GPS signal simulato[J].Telecommunication Engineering, 2003, 46 (4) , 49-54 (in Chinese)
    [13]
    于波, 陈云相, 郭秀中.惯性技术[M].北京:北京理工大学出版社, 1994:13-14 Yu Bo, Chen Yunxiang, Guo Xiuzhong.Inertial technology[M].Beijing:Beijing Institute of Technology Press, 1994:13-14 (in Chinese)
    [14]
    以光衢.惯性导航原理[M].北京:航空工业出版社, 1987:84-85 Yi Guangqu.Inertial navigation principle[M].Beijing:Aviation Industry Press, 1987:84-85 (in Chinese)
    [15]
    解晶, 刘畅.转发式GPS干扰技术及其仿真[J].仪器仪表用户, 2011, 18 (5):71-73 Xie Jing, Liu Chang.GPS repeater-jamming and performances simulation[J].Instrumentation Customer, 2011, 18 (5):71-73 (in Chinese)
    [16]
    Chang Chungliang, Juang Jyh Ching.Performance analysis of narrowband interference mitigation and near-far resistance scheme for GNSS receivers[J].Signal Processing, 2010 (90):2676-2685
    [17]
    郭伟荣, 粟苹, 陈慧敏, 等.锯齿调频连续波建模与数值仿真[J].红外与激光工程, 2009, 38 (6):977-980 Guo Weirong, Su Ping, Chen Huimin, et al.Modeling and numerical simulation of sawtooth FMCW[J].Infrared and Laser Engineering, 2009, 38 (6):977-980 (in Chinese)
    • Relative Articles
    • Supplements(0)
    • Cited By
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索
    Get Citation
    PDF
    XML

    Article Metrics

    Article views(1499) PDF downloads(599) Cited by()
    Proportional views
    Related

    Copyright © Journal of Beijing University of Aeronautics and Astronautics

    Address: Editorial Department of Journal of Beijing University of Aeronautics and Astronautics, 37 Xueyuan Road, Haidian District, Beijing Post Code: 100191 Email: jbuaa@buaa.edu.cn

    Supported by: Beijing Renhe Information Technology Co., Ltd.    

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return