GNSS World of China

Volume 47 Issue 4
Sep.  2022
Turn off MathJax
Article Contents
LIU Chunke, XU Gong, SHI Zhimin, ZHANG Yingqi, WANG Chenchen. Research on attitude determination method based on GNSS antenna array[J]. GNSS World of China, 2022, 47(4): 113-121. doi: 10.12265/j.gnss.2022025
Citation: LIU Chunke, XU Gong, SHI Zhimin, ZHANG Yingqi, WANG Chenchen. Research on attitude determination method based on GNSS antenna array[J]. GNSS World of China, 2022, 47(4): 113-121. doi: 10.12265/j.gnss.2022025

Research on attitude determination method based on GNSS antenna array

doi: 10.12265/j.gnss.2022025
  • Received Date: 2022-02-21
  • Accepted Date: 2022-02-21
  • Available Online: 2022-07-20
  • Aiming at the determination of the attitude of the moving carrier by the vehicle-mounted mobile measurement system, the attitude determination method of the vehicle-mounted Global Navigation Satellite System (GNSS) antenna array is studied, the attitude calculation formula of the direct method and the least square method is analyzed, and the GNSS is carried out. Antenna array vehicle experiment. In order to obtain the accuracy of the two attitude determination methods, the direct method and the least square method are used to calculate the attitude on the basis of different software positioning modes. The experimental and analysis results show that the accuracy of the four-antenna array least squares attitude determination is better than the three-antenna array direct method, and the reliability is higher; among all the combinations, the four-antenna array least squares attitude determination accuracy based on the moving-base positioning mode is the highest, its heading angle, pitch angle and roll angle accuracy can reach 0.066 0°, 0.168 4° and 0.267 8° respectively.

     

  • loading
  • [1]
    李征航. GPS测量与数据处理[M]. 武汉: 武汉大学出版社, 2013: 219-226.
    [2]
    秦永元. 惯性导航[M]. 北京: 科学出版社, 2014: 112-125.
    [3]
    CAI X B, HSU H, CHAI H, et al. Multi-antenna GNSS and INS integrated position and attitude determination without base station for land vehicles[J]. Journal of navigation, 2018, 72(2): 342-358. DOI: 10.1017/S0373463318000681
    [4]
    ALESHECHKIN A. Algorithm of GNSS-based attitude determination[J]. Gyroscopy and navigation, 2011, 2(4): 269-276. DOI: 10.1134/s207510871104002x
    [5]
    刘根友, 欧吉坤. GPS单历元定向和测姿算法及其精度分析[J]. 武汉大学学报(信息科学版), 2003, 28(6): 732-735.
    [6]
    张方照, 柴艳菊, 柴华, 等. 两种多天线GNSS定姿方法的精度分析[J]. 中国惯性技术学报, 2016, 24(1): 30-35.
    [7]
    蔡小波, 许厚泽, 柴华, 等. 两种多天线GNSS动态定姿方法的比较[J]. 导航与控制, 2017, 16(6): 14-18. DOI: 10.3969/j.issn.1674-5558.2017.06.004
    [8]
    肖凯. 多频GNSS/INS组合精密定位定姿理论与方法研究[D]. 郑州: 战略支援部队信息工程大学, 2018.
    [9]
    王冰, 隋立芬, 张清华, 等. 利用GPS解算载体测姿的算法研究[J]. 武汉大学学报(信息科学版), 2013, 38(12): 1392-1395.
    [10]
    杨鸿毅, 王潜心, 胡超, 等. GPS/BDS组合多天线定姿与精度分析[J]. 合肥工业大学学报(自然科学版), 2020, 43(6): 818-822,854.
    [11]
    韦永僧, 贺凯飞, 邱立杰, 等. 陆地导航中GNSS单天线姿态测量的误差及精度分析[J]. 大地测量与地球动力学, 2021, 41(10): 1014-1017,1050.
    [12]
    王立红, 郝继平, 汤云. 基于最小二乘法的GPS多天线测姿及精度分析[J]. 测试技术学报, 2007, 21(1): 1-5. DOI: 10.3969/j.issn.1671-7449.2007.01.001
    [13]
    陈杨, 唐艳, 周伟, 等. 三天线GPS姿态解算误差分析[J]. 全球定位系统, 2012, 37(3): 16-18. DOI: 10.3969/j.issn.1008-9268.2012.03.006
    [14]
    杨洁, 王新龙, 陈鼎, 等. GNSS定姿技术发展综述[J]. 航空兵器, 2018(6): 16-25.
    [15]
    蔡小波, 许厚泽, 王勇, 等. 车载三天线GNSS的直接法定姿及精度评估[J]. 武汉大学学报(信息科学版), 2018, 43(6): 820-825.
    [16]
    蔡小波. 多天线GNSS/INS组合定位定姿方法研究[D]. 武汉: 中国科学院测量与地球物理研究所, 2016.
  • 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

    Figures(15)  / Tables(5)

    Article Metrics

    Article views (348) PDF downloads(39) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return