ICESat-2(Ice,Cloud and Land Elevation Satellite-2)是世界首颗采用光子计数模式的激光测高卫星,可快速获得高精度、大尺度地面三维数据。光子探测机制使得数据中除了地面信号外,还包含大气散射等背景信号,需要通过滤波才能获得地形...ICESat-2(Ice,Cloud and Land Elevation Satellite-2)是世界首颗采用光子计数模式的激光测高卫星,可快速获得高精度、大尺度地面三维数据。光子探测机制使得数据中除了地面信号外,还包含大气散射等背景信号,需要通过滤波才能获得地形等信息。为分析ICESat-2背景和信号光子的分布特点及点云滤波算法的效果和适用性,本文首先选取了六种地表覆盖类型(城市、海冰、沙漠、植被、海洋及冰盖/冰川)及不同观测条件的数据,对其背景光子率进行统计分析。分析结果表明:白天观测数据的背景光子率平均为106(点/秒)数量级,远高于夜晚观测数据的背景光子率——104(点/秒)数量级,弱波束的背景光子率与强波束背景光子率相当,六种地表覆盖类型中,冰盖/冰川的背景光子率最高。然后,根据统计结果筛选出21组测高数据,并选取七种具有代表性的点云滤波对其进行去噪实验,分析精度后得出结论:改进局部密度法的去噪效果最佳,算法召回率、精准度和F值均大于0.90,算法较为稳定。最后,对所选取各滤波算法的精度、特点与适用性等性质进行了总结与分析,可为后续该数据的使用和滤波算法的选择提供参考。展开更多
The geometric accuracy of topographic mapping with high-resolution remote sensing images is inevita-bly affected by the orbiter attitude jitter.Therefore,it is necessary to conduct preliminary research on the stereo m...The geometric accuracy of topographic mapping with high-resolution remote sensing images is inevita-bly affected by the orbiter attitude jitter.Therefore,it is necessary to conduct preliminary research on the stereo mapping camera equipped on lunar orbiter before launching.In this work,an imaging simulation method consid-ering the attitude jitter is presented.The impact analysis of different attitude jitter on terrain undulation is conduct-ed by simulating jitter at three attitude angles,respectively.The proposed simulation method is based on the rigor-ous sensor model,using the lunar digital elevation model(DEM)and orthoimage as reference data.The orbit and attitude of the lunar stereo mapping camera are simulated while considering the attitude jitter.Two-dimensional simulated stereo images are generated according to the position and attitude of the orbiter in a given orbit.Experi-mental analyses were conducted by the DEM with the simulated stereo image.The simulation imaging results demonstrate that the proposed method can ensure imaging efficiency without losing the accuracy of topographic mapping.The effect of attitude jitter on the stereo mapping accuracy of the simulated images was analyzed through a DEM comparison.展开更多
文摘ICESat-2(Ice,Cloud and Land Elevation Satellite-2)是世界首颗采用光子计数模式的激光测高卫星,可快速获得高精度、大尺度地面三维数据。光子探测机制使得数据中除了地面信号外,还包含大气散射等背景信号,需要通过滤波才能获得地形等信息。为分析ICESat-2背景和信号光子的分布特点及点云滤波算法的效果和适用性,本文首先选取了六种地表覆盖类型(城市、海冰、沙漠、植被、海洋及冰盖/冰川)及不同观测条件的数据,对其背景光子率进行统计分析。分析结果表明:白天观测数据的背景光子率平均为106(点/秒)数量级,远高于夜晚观测数据的背景光子率——104(点/秒)数量级,弱波束的背景光子率与强波束背景光子率相当,六种地表覆盖类型中,冰盖/冰川的背景光子率最高。然后,根据统计结果筛选出21组测高数据,并选取七种具有代表性的点云滤波对其进行去噪实验,分析精度后得出结论:改进局部密度法的去噪效果最佳,算法召回率、精准度和F值均大于0.90,算法较为稳定。最后,对所选取各滤波算法的精度、特点与适用性等性质进行了总结与分析,可为后续该数据的使用和滤波算法的选择提供参考。
文摘深空探测巡视任务中巡视器的高精度定位对于巡视器的自身安全与持续运行至关重要。巡视器定位主要包括相对定位和绝对定位两种方式,其中绝对定位方法主要是利用轨道器/着陆器的数据为基准确定巡视器在全局坐标系下的位置。美国Mars 2020任务携带的机智号无人机在火星环境下完成了飞行验证,它能够获得高分辨率的火星表面影像,从而为火星巡视器绝对定位提供了新思路。据此,本文提出了一种卫星-无人机-巡视器影像协同的多分辨率影像匹配绝对定位框架。首先,利用运动恢复结构(structure from motion, SFM)方法对无人机影像进行三维重建,获取局部高分辨率三维地图;然后,开展巡视器影像与无人机影像的多视角匹配,并基于匹配结果利用后方交会实现巡视器在无人机局部地图中的高精度定位;最后,通过局部无人机影像与卫星影像的配准,实现卫星影像全局坐标系下的巡视器绝对定位。为验证本文方法的可行性,开展了巡视器定位仿真试验,试验结果验证了本文方法的可行性,能够为后续我国开展类似工程任务提供参考。
基金Supported by the National Natural Science Foundation of China(42221002,42171432)Shanghai Municipal Science and Technology Major Project(2021SHZDZX0100)the Fundamental Research Funds for the Central Universities.
文摘The geometric accuracy of topographic mapping with high-resolution remote sensing images is inevita-bly affected by the orbiter attitude jitter.Therefore,it is necessary to conduct preliminary research on the stereo mapping camera equipped on lunar orbiter before launching.In this work,an imaging simulation method consid-ering the attitude jitter is presented.The impact analysis of different attitude jitter on terrain undulation is conduct-ed by simulating jitter at three attitude angles,respectively.The proposed simulation method is based on the rigor-ous sensor model,using the lunar digital elevation model(DEM)and orthoimage as reference data.The orbit and attitude of the lunar stereo mapping camera are simulated while considering the attitude jitter.Two-dimensional simulated stereo images are generated according to the position and attitude of the orbiter in a given orbit.Experi-mental analyses were conducted by the DEM with the simulated stereo image.The simulation imaging results demonstrate that the proposed method can ensure imaging efficiency without losing the accuracy of topographic mapping.The effect of attitude jitter on the stereo mapping accuracy of the simulated images was analyzed through a DEM comparison.
