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无人机飞行单光子动态成像中姿态补偿及重建方法

汪建民 赵浩冰 王轲 宋晓升 孙友文 胡晓敏 柳必恒 李大创

汪建民, 赵浩冰, 王轲, 宋晓升, 孙友文, 胡晓敏, 柳必恒, 李大创. 无人机飞行单光子动态成像中姿态补偿及重建方法[J]. 中国光学(中英文). doi: 10.37188/CO.2026-0004
引用本文: 汪建民, 赵浩冰, 王轲, 宋晓升, 孙友文, 胡晓敏, 柳必恒, 李大创. 无人机飞行单光子动态成像中姿态补偿及重建方法[J]. 中国光学(中英文). doi: 10.37188/CO.2026-0004
WANG Jian-min, ZHAO Hao-bing, WANG Ke, SONG Xiao-sheng, SUN You-wen, HU Xiao-min, LIU Bi-heng, LI Da-chuang. Attitude compensation and reconstruction methods for single-photon dynamic imaging during UAV flight[J]. Chinese Optics. doi: 10.37188/CO.2026-0004
Citation: WANG Jian-min, ZHAO Hao-bing, WANG Ke, SONG Xiao-sheng, SUN You-wen, HU Xiao-min, LIU Bi-heng, LI Da-chuang. Attitude compensation and reconstruction methods for single-photon dynamic imaging during UAV flight[J]. Chinese Optics. doi: 10.37188/CO.2026-0004

无人机飞行单光子动态成像中姿态补偿及重建方法

cstr: 32171.14.CO.2026-0004
基金项目: 航空科学基金(No. 2024Z075078003);安徽省重点研究与开发计划项目(No. 2022b13020002);安徽省高等学校省级自然科学研究重大项目(No. 2022AH040289);安徽省学术技术带头人及后备人选科研活动经费资助项目(No. 2019H208);合肥师范学院科研项目(No. 2025CGZH13);国家自然科学基金(No. 62322513)
详细信息
    作者简介:

    柳必恒(1980—),男,湖北武穴人,博士,研究员,博士生导师,2007年于中国科学技术大学获得博士学位,主要从事量子光学与量子信息研究。E-mail:bhliu@ustc.edu.cn

    李大创(1981—),男,安徽宿州人,博士,教授,硕士生导师,2009年于安徽大学获得博士学位,主要从事光电信息和量子信息技术研究。E-mail:dachuangli@ustc.edu.cn

  • 中图分类号: O436

Attitude compensation and reconstruction methods for single-photon dynamic imaging during UAV flight

Funds: Supported by Aeronautical Science Fund (No. 2024Z075078003); Anhui Provincial Key Research and Development Project (No. 2022b13020002); Anhui Provincial Major Natural Science Research Project of Higher Education Institutions (No. 2022AH040289); Anhui Provincial Academic and Technical Leaders and Reserve Personnel Research Activity Funding Project (No. 2019H208); the Hefei Normal University Research Project under Grant (No. 2025CGZH13); National Natural Science Foundation of China (No. 62322513)
More Information
  • 摘要:

    针对单光子深度成像中探测器受散粒噪声和背景噪声的干扰,以及无人机在飞行过程中姿态变化带来的单轴图像偏差问题,在经典的SPIRAL-TAP重建框架基础上,提出了一种融合多尺度图像特征与自适应阈值筛选的新型深度图重建方法,旨在提升深度图像在低信号背景噪声比(SBR)或高信号背景噪声比下的重建质量。该方法首先通过多尺度梯度与局部方差计算生成图像加权矩阵,以刻画图像纹理复杂度;随后结合基于 ROM(Rough Order Map)估计的尺度因子对阈值进行动态调整,以增强噪声鲁棒性;在阈值筛选阶段,提出自适应阈值策略,将尺度平滑与加权矩阵软调融合,限制阈值范围,使筛选更加稳定可靠。实验结果表明,在多种SBR和光子强度条件下,并考虑到无人机单轴姿态偏差影响下,本文方法均优于传统SPIRAL-TAP算法,具有更低的RMSE误差和更好的重建质量。在倾斜角为10°和15°时RMSE分别由0.32降至0.14和从0.43降至0.21。本文方法为无人机载单光子深度图像重建提供了有效的新思路,未来可用在机载高速单光子成像系统中。

     

  • 图 1  单光子激光雷达成像系统示意图

    Figure 1.  Schematic diagram of the single-photon counting LiDAR imaging system

    图 2  极少回波光子情形下典型光子到达时间直方图。(a)单个像素的光子到达时间直方图,在低光子计数条件下呈现稀疏分布;(b) 所有像素的光子时间分布聚合图,整体仍表现出高稀疏性与背景噪声的均匀性

    Figure 2.  Typical photon arrival time histograms under extremely few echo photon conditions. (a) Photon arrival time histogram of a single pixel, exhibiting sparse distribution under low photon counts; (b) aggregated photon temporal distribution of all pixels, illustrating persistent high sparsity and uniform background noise

    图 3  算法流程图

    Figure 3.  Algorithm flowchart

    图 4  仿真数据流程图

    Figure 4.  Simulation data flow diagram

    图 5  无人机飞行姿态偏差模拟图

    Figure 5.  Simulation model of UAV flight attitude deviation and its geometric impact

    图 6  加权矩阵$ {\boldsymbol{W}}_{i,j} $生成流程图

    Figure 6.  Flowchart of weighted matrix $ {\boldsymbol{W}}_{i,j} $ generation

    图 7  结构中像素相似性及边权分布示意图

    Figure 7.  Schematic of pixel similarity and edge weight distribution within the graph-based structure

    图 8  信噪比为10、SPPP分别为1、2、5、10时算法优化前后仿真卧室的重建效果

    Figure 8.  Reconstruction results of the simulated bedroom with SPPP of 1, 2, 5, and 10 before and after algorithm optimization when the signal-to-noise ratio is 10

    图 9  信噪比为0.8、SPPP分别为1、2、5、10时算法优化前后仿真卧室的重建效果

    Figure 9.  Reconstruction results of the simulated bedroom with SPPP of 1, 2, 5, and 10 before and after algorithm optimization when the signal-to-noise ratio is 0.8

    图 10  无人机飞行速度为4m/s时的俯仰角度实时变化

    Figure 10.  Real-time changes in the pitch angle when the flight speed of the unmanned aerial vehicle is 4 m/s

    图 11  无人机飞行速度为8 m/s时的俯仰角度实时变化

    Figure 11.  Real-time changes in the pitch angle when the flight speed of the unmanned aerial vehicle is 8 m/s

    图 12  无人机有无姿态偏差的深度bin值对比

    Figure 12.  Comparison of depth bin values with and without UAV attitude deviation

    表  1  信噪比为10和0.8,对于算法优化前后为RMSE量化结果

    Table  1.   Comparison of RMSE before and after algorithm optimization with SNR of 10 and 0.8

    Methods SPPP=1 SPPP=2 SPPP=5 SPPP=10
    RMSE/m (SNR=10) Shin 0.44 0.37 0.13 0.07
    proposed 0.23 0.16 0.07 0.06
    Methods SPPP=1 SPPP=2 SPPP=5 SPPP=10
    RMSE/m (SNR=0.8) Shin 1.40 1.10 0.43 0.19
    proposed 0.76 0.43 0.23 0.09
    下载: 导出CSV

    表  2  不同俯仰倾角下的重建误差(RMSE)对比(SBR=10, SPPP=5)

    Table  2.   Comparison of reconstruction error (RMSE) at different pitch angles (SBR = 10, SPPP = 5)

    俯仰角度($ \phi $)Shin方法+
    (未补偿)
    Proposed+
    (姿态补偿)
    误差降低
    比例
    RMSE/m0°(平飞)0.120.120%
    0.180.1327.8%
    10°0.320.1456.2%
    15°0.430.2151.1%
    20°0.650.2266.1%
    25°0.880.2373.8%
    下载: 导出CSV

    表  3  算法模块消融实验对比(SBR=10, SPPP=5, ϕ = 15°)

    Table  3.   Comparison of ablation experiments on algorithm modules (SBR = 10, SPPP = 5, ϕ = 15°)

    实验
    方案
    姿态
    补偿
    多尺度
    加权
    自适应
    阈值
    RMSE 提升贡献
    A - - - 0.43 基准
    B - - 0.31 解决了系统性几何畸变
    C - 0.25 抑制了空间随机噪声
    D 0.21 找回了微弱信号特征
    下载: 导出CSV
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  • 收稿日期:  2026-01-08
  • 修回日期:  2026-01-28
  • 录用日期:  2026-03-11
  • 网络出版日期:  2026-04-29

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