共查询到20条相似文献，搜索用时 31 毫秒
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建筑物墙面、悬崖或危岩等目标物的立面信息对于地物精细化建模、地灾调查、分析、评估及防治等具有非常重要的作用。传统倾斜摄影测量获取影像的方式缺乏对地物立面信息的详细描述,在地形落差较大的地区也存在因影像重叠率不同而建模失败的情况。仿地飞行策略在一定程度上解决了上述问题,但其对于突然的高度变化,不能满足精细化建模的要求。本文提出了一种基于等高线构建无人机航线的新型仿地飞行策略,该方法基于目标区域的DSM生成等高线,经等高线简化、偏移等处理完成无人机航线的设计。通过试验将该方法构建的模型成果与传统仿地飞行方法建模成果相比较。结果表明,本文提出的方法可将悬崖上的危岩等刻画得更加真实,且相对于传统仿地飞行垂直于高度变化方向的航线设计为平行于等高线的航飞路线,避免了频繁的高度变化,有益于延长无人机执行飞行任务的时间,因此是一种有效、实用的航飞路线设计方法。 相似文献
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准确的空速和高度是进行飞行试验和确保飞行安全的基础,最新的民用运输类飞机适航标准要求在飞机全包线范围内都要进行空速系统校准。飞机在地面滑跑阶段和失速过程中速度是急剧变化的,而传统的空速校准方法只适用于飞机稳定平飞的状态。介绍了DGPS综合法的原理,利用DGPS高度差与飞机压力高度差之间的关系,获得了非稳态条件下空速系统的位置误差结果,并成功应用于国产支线飞机的合格审定试验。 相似文献
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针对TIN_DDM缓冲面构建与应用中存在的数据类型特殊、算法效率与模型精度不匹配的问题,本文将滚动球模型应用扩展至TIN_DDM缓冲面的构建过程。在分析滚动球模型构建精度局限的基础上,建立了滚动球半径关联的滚动球模型整体精度控制方法;结合大数据量TIN_DDM缓冲面多次构建的应用效率需求,阐明了关键采样点与滚动球半径对TIN_DDM缓冲面构建效率的影响规律;设计了TIN_DDM缓冲面构建关键采样点的判定准则,建立了关键采样点与滚动球半径的数值关联关系;提出了一种基于滚动球加速优化模型的TIN_DDM缓冲面快速构建算法,算法时间复杂度为O(n)。试验结果表明:本文算法可实现任意缓冲半径条件下TIN_DDM缓冲面的多次快速构建,且算法精度控制在2σ内。 相似文献
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A comparison of stable platform and strapdown airborne gravity 总被引：3，自引：1，他引：2
C. L. Glennie K. P. Schwarz A. M. Bruton R. Forsberg A. V. Olesen K. Keller 《Journal of Geodesy》2000,74(5):383-389
To date, operational airborne gravity results have been obtained using either a damped two-axis stable platform gravimeter
system such as the LaCoste and Romberg (LCR) S-model marine gravimeter or a strapdown inertial navigation system (INS), showing
comparable accuracies. In June 1998 three flight tests were undertaken which tested an LCR gravimeter and a strapdown INS
gravity system side by side. To the authors' knowledge, this was the first time such a comparison flight was undertaken. The
flights occurred in Disko Bay, off the west coast of Greenland. Several of the flight lines were partly flown along existing
shipborne gravity profiles to allow for an independent source of comparison of the results. The results and analysis of these
flight tests are presented. The measurement method and error models for both the stable platform and strapdown INS gravity
systems are presented and contrasted. An intercomparison of gravity estimates from both systems is given, along with a comparison
of the individual estimates with existing shipborne gravity profiles. The results of the flight tests show that the gravity
estimates from the two systems agree at the 2–3 mGal level, after the removal of a linear bias. This is near the combined
noise level of the two systems. It appears that a combination of both systems would provide an ideal airborne gravity survey
system, combining the excellent bias stability of the LCR gravimeter with the higher dynamic range and increased spatial resolution
of the strapdown INS.
Received: 3 June 1999 / Accepted: 30 November 1999 相似文献
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小型消费级无人机地形数据精度验证 总被引：5，自引：0，他引：5
低空遥感是近几年快速发展、应用非常广泛的新兴技术。小型消费级无人机集成可见光传感器,具有快速、灵活、高性价比等优势,受到广泛关注。然而目前有关该类无人机综合测量精度的研究不足,影响其进一步的推广应用。为此,本文开展了针对大疆(Phantom 3 professional)小型消费级无人机地形测量数据精度验证工作,设定6种航高(50 m、60 m、70 m、80 m、90 m和100 m)获取研究区的立体像对,生成影像点云(point cloud)、数字表面模型(DSM)以及数字正射影像图(DOM)等结果。在测量精度验证中,首先,在标准实验场均匀布设地面控制点(GCP),利用差分GPS测出GCP的高精度3维坐标;然后,通过GCP对立体像对进行绝对定位;最后,利用误差统计方法分析上述结果的测量精度。验证表明,在50—100m航高时,无人机影像结果的分辨率为2.22—4.23 cm,水平方向平均误差为±0.51 cm,垂直方向平均误差为±4.39 cm,相对均方根误差(RMSE)水平方向为±2.79 cm,垂直方向为±9.98 cm。研究结果表明,小型消费级无人机在飞控系统下的测量精度可达厘米级,这不仅为野外地理和生态调查工作者提供一种低成本、快速、灵活与精确获取地形信息的新型测量手段,同时还对使用此类无人机做航测应用及飞行参数设置提供一定参考。 相似文献
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配准作为干涉处理过程中的重要一步,其精度直接影响后续的处理。机载重复轨道干涉数据,由于飞行的姿态不一致,导致影像间产生较大的相对变形,常规的方法无法对整幅影像进行配准。本文结合SIFT匹配算法的稳健性和解析搜索配准算法高精度的优点,利用飞行轨道间的关系和统计分析剔除错误的匹配,提出了一种针对机载重复轨道干涉数据的配准方法,有效解决了机载重复轨道干涉数据的配准问题。首先利用SIFT匹配算法提取一定数量的匹配点,然后利用飞行轨道之间的关系和对匹配点偏移量的统计分析,剔除误匹配的点,完成粗配准,最后使用解析搜索算法完成精配准。本文利用国产CASMSAR系统获取的机载P波段重复轨道干涉数据进行实验,取得了良好的效果。 相似文献
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在分析空中目标飞行的特点及对其进行高精度测量的必要性基础上,基于GPS载波相位差分技术,设计了一套空中目标飞行测量系统,提出了该系统在地面控制系统中的应用方法,并通过构建事后差分系统进行了静态精度验证和机载动态验证。 相似文献
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针对现有的LiDAR航线设计软件绝大多数针对大中型无人机,主要依靠飞行人员根据实际经验敷设航线,少数采用传统摄影测量改变基线长度的方式实现复杂地势下LiDAR航线自动敷设,但高地势地区航线较密,飞行成本高,有局限性,目前能实现轻小型无人机载LiDAR航线自主敷设的软件很少等问题,参照轻小型机载LiDAR的特点,该文提出一种复杂地势下基于DEM改变航高的航线设计方法。以延庆某山区进行试验。结果表明:该方法适当放宽分区高差限制,综合考虑地形信息、飞机性能等要素,使得单条航带点云密度得到保证,提高航线规划效率,节约飞行时间。将考虑DEM与未考虑DEM两种方式对比,确保重叠度,满足工程点云密度,便于后期数据处理。 相似文献
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智能飞行器在军用和民用领域发挥着越来越重要的作用. 在飞行过程中经常会出现累积的定位误差并且飞行到达应用场景时有定位精度要求,故需要对飞行轨迹进行适当的位置校正. 为此,提出了一种在复杂条件下的智能飞行器航迹规划方法,利用基于线性矩阵不等式(LMI)的优化方法实现最少校正次数和最短飞行距离的双重目标. 根据可用校正点数量以及它们对飞行器位置的不同影响,首先生成一个0~1三角变量矩阵来表示从点A开始的飞行航迹,以面向目标的方式不重复的遍历一系列校正点,并最终到达目标点;然后对航迹相关矩阵的变量项施加强制性的约束条件,将所有的约束作为一个整体转换和施加到之前定义的变量矩阵中,最后利用基于LMI的优化方法实现双重优化. 通过仿真结果验证了所提出的航迹规划方法在计算资源和优化结果方面比线性规划等其他优化方法更优越. 相似文献
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For the high-resolution airborne synthetic aperture radar (SAR) stereo geolocation application, the final geolocation accuracy
is influenced by various error parameter sources. In this paper, an airborne SAR stereo geolocation parameter error model,
involving the parameter errors derived from the navigation system on the flight platform, has been put forward. Moreover,
a kind of near-direct method for modeling and sensitivity analysis of navigation parameter errors is also given. This method
directly uses the ground reference to calculate the covariance matrix relationship between the parameter errors and the eventual
geolocation errors for ground target points. In addition, utilizing true flight track parameters’ errors, this paper gave
a verification of the method and a corresponding sensitivity analysis for airborne SAR stereo geolocation model and proved
its efficiency. 相似文献
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利用Landsat8数据,以成都市为研究对象,采用光谱混合分解模型研究估算成都市的不透水面分布信息。通过MNF变换和PPI指数运算,确定高、低反照率,植被及土壤四类光谱端元,并利用Landsat8新增的卷云波段去除云、土壤、沙地等噪声和MNDWI指数去除水体。修正后的高、低反照率组分含量之和即为不透水面含量的估计值。通过将不透水面信息与利用TIRS11波段反演的地表温度进行回归分析,发现两者呈正相关。 相似文献
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陈捷 《测绘与空间地理信息》2015,(4):88-91
当前大多数测绘生产单位航摄飞行质量检查基本上依靠传统的人工方法,速度慢、效率低,无法快速形成质量检查报告,不能适应信息化测绘生产的要求。本文从生产实际出发,结合当前数字摄影测量的特点,总结了一套基于数字航空影像自动化快速镶嵌的航摄飞行质量检查方法,并研发原型系统。最后,利用浙江省东南沿海摄区103张航摄影像共3个航带进行验证,试验结果表明,该方法能实现航摄飞行质量的快速检查,并自动输出飞行质量评定报告,基本可以取代传统的人工检查方法。 相似文献
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仿地飞行对于无人机航测至关重要,能否相对地面保持稳定的航高直接关系到无人机在复杂地形区域的安全性和数据质量问题。本文提出一种基于单目视觉的无人机航高估计方法,通过光流法对无人机实时获取的视频进行跟踪和分析,提取运动信息以估算实时航高。试验结果表明,该方法能够快速、准确地估算无人机实时航高,在没有地表高程信息的情况下实现了自动仿地飞行。 相似文献
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Alexander V. Parshin Vladimir A. Morozov Anton V. Blinov Alexey N. Kosterev Alexander E. Budyak 《地球空间信息科学学报》2018,21(1):67-74
AbstractThe prospects for expanding the mineral resource base in many countries are linked with the exploration of stranded sites localized at unexplored areas with complex natural and landscape conditions that make any ground survey, including magnetic prospecting, difficult and expensive. The current level of geology requires high-precision and large-scale data at the first stages of geological exploration. Since 2012, technologies of aeromagnetic surveying with unmanned aircraft vehicles (UAV) enter the market, but most of them are based on big fixed-wing UAV and do not allow to substantially increase the level of survey granularity compared with traditional aerial methods. To increase the scale of survey, it is necessary to reduce the altitude and speed of flight, for which the authors develop the methodical and technical solutions described in this article. To obtain data at altitudes of 5 m above the terrain even in a rugged relief, we created heavy multirotor UAVs that are stable in flight and may be used in a wide range of environmental conditions (even a moderate snowfall), and develop a special software to generate flight missions on the basis of digital elevation models. A UAV has special design to reduce magnetic interference of the flight platform; the magnetic sensor is hung below the aircraft. This technology was conducted in a considerable amount of magnetic surveys in the mountainous regions of East Siberia between 2014 and 2016. The results of the comparison between airborne and ground surveys are presented, which show that the sensitivity of the developed system in conjunction with low-altitude measurements can cover any geologically significant anomalies of the magnetic field. An unmanned survey is cheaper and more productive; the multirotor-based technologies may largely replace traditional ground magnetic exploration in scales of 1:10,000?1:1000. 相似文献
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Signs of long-term glaciological processes and past ice-sheet structure are preserved in the internal layer manifestations of the Greenland ice sheet. Internal layer data have been collected over a substantial portion of the Greenland ice sheet using the University of Kansas ice-sounding radar. In this letter, these layers are traced along thousands of kilometers of flight lines from the ice divide toward Jakobshavn, which is the most active glacier in Greenland. The authors determine the traced radar layers' age at the Greenland Ice Core Project (GRIP) site using the GRIP core age-depth relationship. Inasmuch as the depth varies spatially for a layer of a specific dated age, an age-depth relationship for each location along the flight lines of this letter can be found using the traced layers. Thirty-one points where flight lines cross over one another were analyzed. From the flight line crossover analysis, a 9-m maximum difference (< 1%) was found 相似文献
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Estimation of the polarization orientation angle shifts induced by terrain azimuth slope variations is a recently developed application in radar polarimetry. In general, without any prior knowledge on the terrain, two polarimetric SAR (POLSAR) flight passes are required to derive terrain slopes in perpendicular directions for digital elevation model (DEM) generation. Moreover, we note that SAR intensity is a strong indicator of the range component of the terrain slopes. In this letter, we developed a method for DEM generation requiring only one POLSAR flight pass, by combining orientation angle estimation and a shape-from-shading technique. In particular, when limited POLSAR data are available, this POLSAR technique provides an alternative way for DEM generation. National Aeronautics and Space Administration Jet Propulsion Laboratory (NASA/JPL) AIRSAR L-band POLSAR data over Camp Roberts, California, is used to demonstrate the results of the method proposed in this letter, and a DEM derived from simultaneously measured C-band interferometric SAR from NASA/JPL topographic SAR instrument is selected as the comparative ground truth to validate the effectiveness of this single POLSAR method. Analyses and discussions are also included in this letter. 相似文献