共查询到20条相似文献，搜索用时 500 毫秒
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针对可视化方法求取过程中受人眼观察比对的个体差异性以及多波束散点数据可视化显示形式的双重影响,两多波束条带人眼对齐误差较大,直接影响最终校正参数的计算精度问题,该文提出了基于两步法的多波束校正参数可视化精准计算方法,引入了多波束条带数据的自动对齐判断。首先依据两个多波束条带数据的几何关系,进行校正参数的粗校正计算;然后基于粗校正计算的估值,以抽样偏差最小为依据自动判断两条带数据是否对齐,实现校正参数的自动精确校正计算。实验结果表明,两步法计算多波束校正参数避免人眼视觉对齐带来的误差,有效地提高了校正参数可视化计算的自动化程度和计算精度。 相似文献
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平面随机线元等概率密度误差模型边界包络线 总被引：1，自引：0，他引：1
线状实体误差模型包络线既是GIS位置不确定性研究的重要内容,又是GIS可视化研究的关键指标.为了充分利用计算机技术求解符合GIS精度要求的误差模型包络线,基于文献[1,2]中探讨过的等概率密度误差模型建模机理和数值算法,研究了平面随机线元等概率密度误差模型边界包络线的确定原理和计算方法,并通过实例辅以可视化分析,验证了原理的正确性和可操作性. 相似文献
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电离层误差严重影响着GNSS的定位精度,GPS、BDS、Galileo、GLONASS有不同的电离层误差校正方法.全文概述了电离层误差校正方法,综述了单频电离层误差校正、双频电离层误差校正及多频电离层误差校正等技术的原理与发展现状.在单频电离层误差校正技术中总结了增强系统中的电离层误差校正技术、北斗全球电离层延迟修正模型(BeiDou global ionospheric delay correction model,BDGIM)、Klobuchar模型、单频电离层误差校正技术的优化—附加国际参考电离层(international reference ionosphere,IRI)约束模型和NeQuick-G模型;在双频电离层误差校正技术中重点总结了双频消电离层误差、无电离层组合模型及PPP-RTK技术中电离层误差校正方法;在多频电离层误差校正技术中介绍了高阶项改正和地磁场建模对电离层误差校正技术的优化与改进.最后,对电离层误差校正技术及其改进方法进行了分析,总结了其发展趋势与方向. 相似文献
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无人机遥感能够提供高时空分辨率的影像数据,拥有广泛的应用前景。辐射校正将传感器记录的数据转化为地表反射率,是无人机数据定量化应用的前提。然而无人机数据易受光照等因素的影响,导致影像间存在不同程度的辐射差异,为多张无人机影像的辐射校正带来困难。基于影像间重叠区域的信息,辐射区域网平差能够获得全局最优的辐射校正参数,降低影像间的辐射差异,因此在实现影像的辐射校正方面具有巨大潜力。但大量待求解未知参数降低了辐射校正模型的求解效率,特别是在数据量急剧增加时,该问题更为突出。基于影像重叠区辐射信息建立的最优路径很好地考虑了影像间的辐射转化关系,可有效控制误差累计,为减少辐射区域网平差中未知参数的数量提供了一种思路。因此,本文将最优路径与辐射区域网平差相结合,以降低待求解参数的数量,在保证辐射校正精度的同时提高辐射校正模型求解效率,进而提升辐射区域网平差在大数据集上的应用潜力。 相似文献
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利用轨道参数修正的无控制点星载SAR图像几何校正方法 总被引：1，自引：1，他引：0
使用距离多普勒模型进行SAR图像几何校正时,卫星轨道误差、系统成像参数误差和DEM高程的误差会影响几何校正精度。本文提出了一种基于轨道参数修正的星载SAR图像几何校正方法。首先利用多项式对卫星轨道进行参数化,然后使用模拟SAR图像与真实SAR图像进行匹配得到控制点来修正轨道参数,最后利用修正后的参数进行几何精校正,从而提高几何校正精度。该方法无需地面控制点,适用于不易于人工测量获取地面控制点地区的SAR图像几何校正,与基于模拟SAR图像匹配并使用多项式改正的几何校正方法相比,本文方法具有更高的精度。使用Radarsat-2图像进行试验,并使用地面实测GPS控制点验证了本方法的有效性。 相似文献
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基于神经网络模型的遥感影像几何校正研究 总被引：1，自引：0，他引：1
在遥感影像几何校正方法中,通常认为精度最高的是共线方程模型.针对共线方程模型定向参数解算过程中误差方程的病态问题,提出了利用基于控制点的神经网络方法进行高分辨率遥感影像几何校正方法,并从理论上进行了可行性分析.实验证明,在具有一定数量控制点作为训练样本的条件下,应用BP和RBF神经网络进行遥感影像几何校正,可以达到比共线方程模型更高的精度;神经网络模型能够自动抑制含较大误差控制点对模型纠正精度的影响,在实际应用中可以提高几何校正效率. 相似文献
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针对视觉测量系统中畸变校正过程烦琐、计算复杂等问题,提出了一种基于基本矩阵约束的镜头畸变自动校正及像主点坐标确定方法。基于对极几何的基本矩阵和一阶径向畸变模型构建了两视图同名点约束方程;为解决待求参数过多导致解不稳定的问题,采用分步求解策略分别求解基本矩阵及畸变参数和主点坐标,用RANSAC稳健估计方法求取基本矩阵,用迭代最小二乘优化求解畸变参数和主点坐标,两步交替进行。提出的算法仅使用两张图像即可获取径向畸变参数及主点坐标,可操作性强,且对噪声具有一定的鲁棒性,适用于自然场景图像的校正。 相似文献
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BRDF校正能消除Landsat-8遥感影像中由于太阳角、观测角与真实角度偏差引起的色差不一致,因此本文对多种体散射核与几何光学核的组合进行研究,在选用最佳核函数组合的基础上,采用改进的误差模型求解BRDF校正参数,最后完成Landsat-8影像的BRDF校正。实验结果表明:Ross Thick核和Li-Sparse核为BRDF模型的最佳核组合,并且利用改进的平差模型能提高解算精度,经过BRDF校正后,影像的"二向反射"现象得到明显改善。 相似文献
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介绍了卫星信号内部时延的定义以及在GPS导航电文NAV和CNAV中所给出的各种时延差参数,推导了采用不同的卫星信号测距时应采用的各种卫星钟差模型。 相似文献
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This paper examines the influence that certain omission and commission errors can have on the gravity field models estimated from the initial release of data (RL01) from the Gravity Recovery And Recovery Experiment (GRACE) satellite mission. The effects of omission errors were analyzed by limiting the degree and order to which the GPS and K-band range-rate (KBR) measurement partials were extended in the solution process. The commission error studies focused on the impact of an imperfect mean reference gravity field model on the solution. Combinations of both of these error sources were also explored. The nature of these errors makes them difficult to distinguish from the true gravity signal, so the exploration of these error sources was performed using simulations; however, comparisons to real-data solutions are provided. The results show how each of the specific error sources investigated influences the gravity field solution. The simulations also show how all of the errors examined can be sufficiently mitigated through the appropriate choice of processing parameters. 相似文献
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GOCE采用的高低卫-卫跟踪和卫星重力梯度测量技术在恢复重力场方面各有所长并互为补充,如何有效利用这两类观测数据最优确定地球重力场是GOCE重力场反演的关键问题。本文研究了联合高低卫-卫跟踪和卫星重力梯度数据恢复地球重力场的最小二乘谱组合法,基于球谐分析方法推导并建立了卫星轨道面扰动位T和径向重力梯度Tzz、以及扰动位T和重力梯度分量组合{Tzz-Txx-Tyy}的谱组合计算模型与误差估计公式。数值模拟结果表明,谱组合计算模型可以有效顾及各类数据的精度和频谱特性进行最优联合求解。采用61天GOCE实测数据反演的两个180阶次地球重力场模型WHU_GOCE_SC01S（扰动位和径向重力梯度数据求解）和WHU_GOCE_SC02S（扰动位和重力梯度分量组合数据求解）,结果显示后者精度优于前者,并且它们的整体精度优于GOCE时域解,而与GOCE空域解的精度接近,验证了谱组合法的可行性与有效性。 相似文献
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Fast GNSS ambiguity resolution as an ill-posed problem 总被引：4，自引：0，他引：4
A linear observational equation system for real-time GNSS carrier phase ambiguity resolution (AR) is often severely ill-posed
in the case of poor satellite geometry. An ill-posed system may result in unreliable or unsuccessful AR if no care is taken
to mitigate this situation. In this paper, the GNSS AR model as an ill-posed problem is solved by regularizing its baseline
and ambiguity parameters, respectively, with the threefold contributions: (i) The regularization parameter is reliably determined
in context of minimizing mean square error of regularized solution where the covariance matrix of initial values of unknowns
is used as an approximate smoothness term instead of the quadratic matrix of the true values of unknowns; (ii) The different
models for computing initial values of unknowns are systematically discussed in order to address the potential schemes in
real world applications; (iii) The superior performance of the regularized AR are demonstrated through the numerically random
simulations as well as the real GPS experiments. The results show that the proposed regularization strategies can effectively
mitigate the model’s ill-condition and improve the success AR probability of the observational system with a severely ill-posed
problem. 相似文献
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可见光-近红外波段大气上行与下行辐射分量参数化方法 总被引：1，自引：0，他引：1
可见光-近红外波段大气上行、下行辐射是辐射传输建模、成像模拟及大气校正关键的输入参数,根据四流辐射传输理论给出了与二者相关大气参量的数值模型及计算方法,针对Landsat 5 TM 6个波段建立了大气参量与水汽含量、能见度距离和太阳入射天顶角间的参数化模型,在此基础上对各参量间敏感性进行了分析,结果表明参数化模型具备较高精度。同时,计算了各波段大气上行、下行漫射辐射值,对二者在植被和裸土覆盖条件下的差异进行了定量分析。 相似文献
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Tian‐Xiang Yue Na Zhao Hai Yang Yin‐Jun Song Zheng‐Ping Du Ze‐Meng Fan Dun‐Jiang Song 《Transactions in GIS》2013,17(6):943-952
A method of high accuracy surface modeling (HASM) has been constructed to find a solution for error problems that had long troubled surface modeling in geographical information systems (GIS). It is found that when a preconditioned conjugate gradient (PCG) algorithm is used to solve the large sparse linear system, which HASM can be transferred into, HASM performs best in terms of simulation compared with all other algorithms. But its computing speed is not fast enough for all applications. A multi‐grid method is introduced into HASM to try to shorten its computing time. Both numerical and real‐world tests demonstrate that there is a range of stop error (SE). The multi‐grid method of HASM (HASM‐MG) greatly increases computing speed when SEs are within this range, compared with the PCG algorithm of HASM (HASM‐PCG). HASM‐MG is suitable for applications with a need for less accuracy and a shorter computing time. HASM‐PCG is appropriate for issues needing higher accuracy. HASM‐MG performs better than HASM‐PCG in flat areas, while HASM‐PCG does better in complex terrainm in terms of accuracy and computing time. 相似文献
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海洋磁力测量误差补偿技术研究 总被引：2，自引：1，他引：2
在分析海洋磁力测量主要误差来源的基础上，分阶段建立了能够反映海洋磁力测量误差变化规律的误差模型及相应的误差补偿模型，提出了误差补偿模型的解算方法，讨论了求解过程的稳定性和误差补偿效果的显著性检验等一系列应用中的具体问题，并使用一个实际观测网数据验证了各种补偿方法的有效性和可靠性。 相似文献
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The combination of GPS measurements and high-fidelity dynamic models via a Kalman filter/smoother, known as the reduced dynamic technique, allows 3D positioning of Low Earth Orbiters to the sub-decimeter level. Such accuracies can only be achieved if the GPS data are nearly continuous, post-processed and a dual-frequency receiver is utilized. The focus of this study is to quantitatively analyze the degradations in position accuracy in the presence of various limitations or constraints, which can be brought on by mission hardware limitations, for example, on micro- or nanosatellites. The constraints explored in this study are as follows: the use of single-frequency data only; real-time processing; limited dynamic modeling due to computing capabilities; and non-continuous GPS receiver operation due to power limits. The experiments are conducted with 6-h data arcs for 7 separate days using data from the CHAllenging Mini-Satellite Payload. A 3D root mean square (rms) error of 15 cm is observed in the best-case solution, in which dual-frequency data are post-processed with all available data. Various levels of accuracy degradations are observed as constraints are placed on this best-case solution. The 3D rms error of the post-processed, single-frequency solution is 68 cm and 1.3 m for the real-time, dual-frequency solution. In very challenging environments, for example, with the receiver on for only 10 min of a 90-min orbit, the 3D rms increases to 350 m. 相似文献