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低功耗BDS-SPP/INS融合定位系统的设计与试验

张天, 张智刚, 罗锡文, 彭铭达, 张国城, 黄海翔, 苑炳轩, 张闻宇

张天, 张智刚, 罗锡文, 等. 低功耗BDS-SPP/INS融合定位系统的设计与试验[J]. 华南农业大学学报, 2024, 45(3): 437-445. DOI: 10.7671/j.issn.1001-411X.202305028
引用本文: 张天, 张智刚, 罗锡文, 等. 低功耗BDS-SPP/INS融合定位系统的设计与试验[J]. 华南农业大学学报, 2024, 45(3): 437-445. DOI: 10.7671/j.issn.1001-411X.202305028
ZHANG Tian, ZHANG Zhigang, LUO Xiwen, et al. Design and experiment of low-power BDS-SPP/INS fusion positioning system[J]. Journal of South China Agricultural University, 2024, 45(3): 437-445. DOI: 10.7671/j.issn.1001-411X.202305028
Citation: ZHANG Tian, ZHANG Zhigang, LUO Xiwen, et al. Design and experiment of low-power BDS-SPP/INS fusion positioning system[J]. Journal of South China Agricultural University, 2024, 45(3): 437-445. DOI: 10.7671/j.issn.1001-411X.202305028

低功耗BDS-SPP/INS融合定位系统的设计与试验

基金项目: 国家重点研发计划(2022YFD2001601);国家糖料产业技术体系(CARS-170405)
详细信息
    作者简介:

    张 天,硕士,主要从事精准农业、智能农机控制研究,E-mail: 13298518970@163.com

    通讯作者:

    张闻宇,助理研究员,博士,主要从事研究方向为精准农业、无人化农场关键技术、智能农机控制研究,E-mail: zhangwenyu@scau.edu.cn

  • 中图分类号: TP273;V249.32

Design and experiment of low-power BDS-SPP/INS fusion positioning system

  • 摘要:
    目的 

    融合定位设备大多依赖于BDS-RTK,而BDS-RTK功耗大,在网络信号不佳的区域无法获取差分链路,只能使用标准单点定位(Standard point positioning,SPP),而SPP定位系统存在定位误差大、抗干扰能力弱的问题。本研究致力于解决这些问题。

    方法 

    提出一种惯性导航系统(Inertial navigation system,INS)和BDS-SPP传感器信息融合卡尔曼滤波方法,基于该方法开发了低功耗融合定位系统。采用BDS-RTK作为基准,测试了BDS-SPP的低功耗模块静态和动态的误差、航姿参考系统(Attitude and heading reference system,AHRS)零偏和噪声,同时进行滤波器融合定位试验,检测在单天线BDS受到干扰时AHRS的断点续航情况。

    结果 

    BDS定位的静态误差为0.4726 m,BDS-SPP/INS融合定位系统动态平均标准差小于1.9137 m,相较于融合前减少0.1652 m。断点续航试验结果表明,融合定位系统偏移距离平均标准差为3.6365 m,相较于融合前减少了2.5900 m。BDS-SPP/INS融合定位系统比BDS-RTK定位系统功率降低了33.3 W;融合后的输出频率较单独采用BDS-SPP情况提高了3倍。

    结论 

    本文的融合定位装置提高了BDS-SPP的抗干扰能力,减少了定位误差,可以在缺少RTK链路的情况下为农业机器人提供定位,可以为农业机器人导航研究提供了技术基础。

    Abstract:
    Objective 

    Most fusion positioning devices rely on BDS-RTK, which has high power consumption. In areas with poor network signals, differential links cannot be obtained, and only standard point positioning (SPP) can be used. SPP system has problems such as large positioning errors and weak anti-interference ability. This study is committed to addressing these issues.

    Method 

    This study proposed a low-power fusion positioning device that used inertial navigation system (INS) and BDS-SPP sensors based on the Kalman filter fusion method. The device was tested using BDS-RTK as a benchmark to evaluate the static and dynamic errors of the BDS-SPP low-power module, the attitude and heading reference system (AHRS) zero bias and noise. Additionally, filtering fusion positioning experiments were conducted to test the AHRS breakpoint continuation in the case of BDS interference with a single antenna.

    Result 

    The static error of BDS positioning was 0.4726 m, the average standard deviation of the dynamic BDS-SPP/INS fusion positioning system was less than 1.9137 m, and the average standard deviation reduced by 0.1652 m compared to before fusion. The breakpoint continuation experiment showed that the average standard deviation of the offset distance of the fusion positioning system was 3.6365 m, which decreased by 2.5900 m compared to before fusion. The BDS-SPP/INS fusion positioning system reduced the power consumption by 33.3 W compared to the BDS-RTK positioning system, and increased the output frequency by three times.

    Conclusion 

    The fusion positioning device in this article improves the anti-interference capability of BDS-SPP and reduces positioning errors. It can provide positioning for agricultural robots in the absence of an RTK link, and provide a technical basis for agricultural robot navigation research.

  • 图  1   机器人运行学模型图

    XY是质点运动方程的坐标系,(xy)是此瞬时质点在坐标轴的投影,θ是此瞬时运动轨迹与X轴的夹角

    Figure  1.   Model diagram of robot operationology

    X and Y are the coordinate system of the motion equation of the particle, (x, y) is the instantaneous projection of the particle on the coordinate axis, and θ is the angle between the instantaneous motion trajectory and X axis

    图  2   AHRS与BDS结构图

    Figure  2.   Structure diagram of AHRS and BDS

    图  3   低功耗的BDS-SPP/INS融合定位系统结构示意图

    Figure  3.   Structure diagram of BDS-SPP/INS fusion positioning system with low power

    图  4   低功耗的BDS-SPP/INS融合定位系统实物示意图

    1:RTK-GNNS 定位系统;2:接收卫星信号天线;3:4G天线;4:AHRS系统;5:低功耗MCU测试系统

    Figure  4.   Physical diagram of BDS-SPP/INS fusion positioning system with low power

    1: RTK-GNNS positioning system; 2: Antenna to receive satellite signal; 3: 4G antenna; 4: AHRS system; 5: Low-power MCU test system

    图  6   BDS-SPP (A)和BDS-RTK (B)定位的静态误差图

    Figure  6.   Static error diagrams of BDS-SPP (A) and BDS-RTK (B) positioning

    图  7   BDS-SPP定位以高精度BDS-RTK定位作为参照圆心的圆概率误差

    Figure  7.   Probability error of BDS-SPP positioning using high-precision BDS-RTK positioning as the reference center for the circle

    图  8   融合前、后的系统动态定位散点图(A)和偏移距离图(B)

    图A中,上方和下方的短平行线是对箭头指向位置的定位轨迹的放大

    Figure  8.   Dynamic positioning scatter plot (A) and offset distance plot (B) of the system before and after fusion

    In Figure A, the short parallel lines above and below magnify the positioning trajectories of the positions pointed by arrows

    图  9   抗干扰第1号试验的系统动态定位散点图(A)和偏移距离图(B)

    Figure  9.   Dynamic positioning scatter plot (A) and offset distance plot (B) of the system for anti-interference test No. 1

    表  1   BDS-SPP定位系统的静态误差

    Table  1   Static error of BDS-SPP positioning system

    t/s标准差/m
    Standard deviation
    圆概率误差/m
    Circular probable error
    平均误差/m
    Mean error
    北纬/(°)
    North latitude
    东经/(°)
    East longitude
    21000.60050.49820.462723.1626113.3399
    18000.68270.55640.540123.1560113.3584
    9000.26310.21810.240423.2423113.6378
    22800.73810.60680.647123.2432113.6380
    平均值 Avearage0.57110.46990.4726
    下载: 导出CSV

    表  2   不同定位系统的动态性能

    Table  2   Dynamic performance of different positioning systems

    t/s速度/(m·s−1)
    Speed
    行驶距离/m
    Distance traveled
    偏移距离的标准差/m Standard deviation of offset distance
    BDS-SPPBDS-SPP/INS
    4505.7726001.76351.7445
    3964.5518001.80431.5160
    4415.2123002.79382.7251
    4795.2225001.15141.1415
    4565.1523501.77261.4454
    4105.9125003.22403.0516
    平均值 Average2.07891.9137
    下载: 导出CSV

    表  3   抗干扰试验的不同定位系统动态性能

    Table  3   Dynamic performance for different positioning systems in anti-interference test

    t/s速度/(m·s−1)
    Speed
    行驶距离/m
    Distance traveled
    偏移距离的标准差/m Standard deviation of offset distance
    BDS-SPPBDS-SPP/INS
    10804.7825005.71194.4576
    10205.3323508.72694.6847
    10205.6723005.24082.7674
    平均值 Average6.22653.6365
    下载: 导出CSV
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出版历程
  • 收稿日期:  2023-05-23
  • 网络出版日期:  2024-03-24
  • 发布日期:  2024-03-14
  • 刊出日期:  2024-05-09

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