基于激光雷达的飞机尾涡反演方法改进研究
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国家自然科学基金项目(No.U2133210);中央高校基本科研业务费项目(No.3122017067);天津市科技计划项目(No.23JCZDJC00580)资助。


Improved LiDAR based aircraft wakevortex retrieval methods
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    摘要:

    针对激光雷达径向分辨率偏大、致使尾涡反演精度偏低的问题。通过三次插值和三次样条插值在激光雷达距离门之间按照密度1、2、4、8m对尾涡径向风场进行插值,并使用梯度法反演涡核位置;然后对梯度法进行改进,在各个距离门的梯度绝对值最大值之间使用三次插值和三次样条插值按照密度1、2、4、8m进行插值。最后提出了基于三次样条插值的分辨率提升方法,通过改进梯度法提高了涡核识别准确度。研究表明,三次样条插值较三次插值对尾涡数据吻合程度更高;在算例中,三次插值涡核位置最高修正率为20~35,三次样条插值涡核位置最高修正率为39~71;比较尾涡径向风场插值算法和改进梯度法识别涡核的效率,改进梯度法较尾涡径向风场插值算法所用时间提高了82。

    Abstract:

    To address the issue of low wake vortex retrieval accuracy caused by the large radial resolution of lidar,cubic interpolation and cubic spline interpolation are applied to interpolate the radial wind field of wake vortices between lidar range gates at densities of 1,2,4,and 8 meters.And the gradient method is then used to invert the vortex core positions.Subsequently,the gradient method is improved by applying cubic interpolation and cubic spline interpolation between the maximum absolute gradient values across range gates at the same densities (1,2,4,8 meters).Finally,a resolution enhancement method based on cubic spline interpolation is proposed to improve vortex core identification accuracy through the enhanced gradient method.Studies demonstrate that cubic spline interpolation achieves better consistency with wake vortex data compared to cubic interpolation.In numerical cases,the maximum correction rates for vortex core positions reach 20%~35% using cubic interpolation and 39%~71% using cubic spline interpolation.When comparing the efficiency of the wake vortex radial wind field interpolation algorithm and the improved gradient method in identifying vortex cores,the time consumption of the improved gradient method is reduced by 82% compared to the interpolation algorithm.

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魏志强,杨宪康.基于激光雷达的飞机尾涡反演方法改进研究[J].激光与红外,2026,56(2):211~219
WEI Zhi-qiang, YANG Xian-kang. Improved LiDAR based aircraft wakevortex retrieval methods[J]. LASER & INFRARED,2026,56(2):211~219

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  • 在线发布日期: 2026-02-10
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