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1.
航空摄影测量的直接地理定位(direct georeferencing,DG)必须首先进行惯性测量单元(inertial measurement unit,IMU)和传感器间的视准轴偏差(boresight misalignment)检校。提出了一种简便的定位定向系统(position andorientation system,POS)辅助光束法平差检校模型,推导了其基础误差方程,并通过2个试验区验证该方法检校结果与商用软件CALQC的检校结果基本一致。通过直接地理定位互差和上下视差比较,证明用本文方法进行的视准轴偏差检校是正确有效的,检校后的外方位元素可直接用于1∶10 000比例尺的高山地区地形图测图。  相似文献   

2.
首先介绍了定向的定义、基准和应用背景,总结并比较了目前几种主要定向技术的特点。在此基础上分析了卫星定向技术的优势和改进需求;重点介绍了GNSS快速定位定向仪(臂长1.1 m)研制的基本情况、基本组成和特点。该仪器采用单接收机旋转方式定位定向。经过大量实验鉴定,通过3 min的连续测量可实现优于0.5个密位(108″)的定向精度和优于5 m的定位精度。  相似文献   

3.
研究了机载三线阵影像与POS位置、姿态同步测量数据联合平差的理论方法;设计了一种描述POS测量误差的数学模型,采用改进的定向片内插模型实现了机载三线阵影像的光束法平差,并利用ADS40影像进行了单航带和区域网平差的实验.结果表明,极少量地面控制点参与平差即可有效提高POS数据的定位精度;在测区3角布设控制点可得到稳定的平差结果,平面和高程精度均优于1.7个像素.高精度的POS数据可有效控制航带模型的旁向倾斜,使得单航带摄影测量作业成为可能.  相似文献   

4.
三维激光扫描定向标靶和连接标靶的工程测量系坐标和扫描坐标系坐标是后视定向的基础,两个坐标系坐标的精度直接影响点云定向和坐标转换的质量。而快速点云定向是指应用两球和一垂线实现点云定向。本文的主要内容包括标靶中心扫描坐标拟合,点云定向参数平差计算、点云定向精度统计分析等。通过对点云定向工作的精度评价来分析理论精度与实际精度的区别。事实证明,快速点云定向模型对于减少野外工作量,丰富定向方法有着重要的意义。  相似文献   

5.
针对近景视频摄影测量中椭圆标志点的中心定位精度影响后续的目标跟踪和三维重建精度的问题,该文为了保证获取椭圆亚像素的中心定位精度,提出了一种基于椭圆标志点亚像素边缘检测的中心定位方法。该方法首先利用Canny算子提取椭圆的轮廓,然后利用阈值分割、形态学边缘轮廓提取方法等方法对边缘进行约束,再利用形态学细化算法和空间矩提取椭圆的亚像素边缘,最后利用最小二乘拟合法实现椭圆中心的亚像素定位。实验结果表明:在模拟实验和真实影像的实验下,该方法与现有其他方法相比较,不仅能获取和定位高精度的椭圆中心(模拟实验下,椭圆中心定位精度高达0.02像素),而且具有高稳健性;能够满足近景摄影测量的精度和稳定性的需求。  相似文献   

6.
判断观测值粗差能否发现和定位的一种验前方法   总被引:5,自引:2,他引:5  
由于最小二乘(LS)残差统计相关,使得粗差发现和定位关系变得相当复杂,且至今未见有效的理论和方法。作者依据在LS平差前进行粗差发现和定位的思路,有意避开LS残差统计相关的难题,从条件平差模型推导出粗差判断方程(GEJE)Vr=JVt Wc建立起以上式判断矩阵J为基础的粗差发现和定位的判断准则:1.不能发现含有粗差的观测量;2.能发现含有粗差但不能定位粗差的观测量。通过算例的检验,证明了判断矩阵J与控制网中观测量数据结构的对应关系,同时说明粗差不能定位的观测量,再好的粗差检测方法也无法正确定位粗差。  相似文献   

7.
摄影测量技术已经成为一种有效的测量方法,并广泛应用。本文基于平差的理论模型,导出了由摄影测量所得地物特征点(广义点)的位置误差模型和误差传播模型,并进一步分析了观测值的质量特征(精度,可靠性,误差椭圆),通过以地物作为具体实例方案证明所得结论具有一定的参考价值。  相似文献   

8.
在分析加权总体最小二乘解与经典最小二乘解的区别和联系的基础上,将加权总体最小二乘平差理论首次应用于地面摄影测量的解析相对定向算法中,并给出了基于相对定向模型的加权总体最小二乘的算法步骤。同时,将Procrustes理论引入到解析绝对定向模型中,推导了基于Procrustes理论的加权总体最小二乘解。具体算例证明了加权总体最小二乘平差理论应用于地面摄影测量处理中能够获得精确稳定的解析参数。  相似文献   

9.
一种适合于数字近景影像的绝对定向方法   总被引:1,自引:0,他引:1  
数字近景影像的绝对定向同经典的航空摄影测量有很大的不同,为提高数字近景影像的绝对定向精度,提出了一种基于逐次相关条件平差模型的近景影像绝对定向方法。首先给出计算绝对定向参数初始值的严密公式。然后利用绝对定向方程的严密线性化形式进行逐次相关条件平差。同传统的基于经典间接平差的绝对定向方法相比,该方法可有效提高绝对定向的精度,非常适合于数字近景影像的绝对定向。  相似文献   

10.
基于已知定向参数影像的光束法区域网平差   总被引:1,自引:1,他引:1  
从自检校光束法区域网平差模型出发,建立了利用同一地区已知定向参数的影像解求新获取影像外方位元素并进行目标定位的数学模型。以此为基础,对来自某地区相隔两年的三期不同摄影比例尺航空影像两两组合地进行联合光束法区域网平差。结果表明,当两期影像比例尺相近时,所解求的新影像外方位元素和加密点坐标精度基本达到常规光束法区域网平差的精度;当两期影像比例尺不同时,利用已知定向参数的大比例尺影像解求出的小比例尺影像的外方位元素和加密点坐标可满足现行规范精度要求,利用已知定向参数的小比例尺影像去解求大比例尺影像的外方位元素和加密点坐标精度明显下降且不可用。本文的研究证实,就同一地区的多时相航摄影像而言,利用已知定向参数的影像进行新影像的定向方法是可行的。  相似文献   

11.
Lidar (laser scanning) technology has been proven as a prominent technique for the acquisition of high-density and accurate topographic information. Because of systematic errors in the lidar measurements (drifts in the position and orientation information and biases in the mirror angles and ranges) and/or in the parameters relating the system components (mounting parameters), adjacent lidar strips may exhibit discrepancies. Although position and orientation drifts can have a more significant impact, these errors and their impact do not come as a surprise if the quality of the GPS/INS integration process is carefully examined. Therefore, the mounting errors are singled out in this work. The ideal solution for improving the compatibility of neighbouring strips in the presence of errors in the mounting parameters is the implementation of a rigorous calibration procedure. However, such a calibration requires the original observations, which may not be usually available. In this paper, a strip adjustment procedure to improve the compatibility between parallel lidar strips with moderate flight dynamics (for example, acquired by a fixed-wing aircraft) over an area with moderately varying elevation is proposed. The proposed method is similar to the photogrammetric block adjustment of independent models. Instead of point features, planar patches and linear features, which are represented by sets of non-conjugate points, are used for the strip adjustment. The feasibility and the performance of the proposed procedure together with its impact on subsequent activities are illustrated using experimental results from real data.  相似文献   

12.
In digital photogrammetry, corresponding points have been widely used as the basic source of information to determine the relative orientation parameters among adjacent images. Sometimes, though, the conventional relative orientation process cannot be precisely implemented due to the accumulation of random errors or in the case of inadequate corresponding points. A new relative orientation approach with multiple types of corresponding features, including points, straight lines, and circular curves, is proposed in this paper. The origin of the model coordinate system is set at the projection center of the first image of a strip, and all of the exterior orientation parameters, except φ and ω of the first image, are set at zero. The basic models of relative orientation with corresponding points, straight lines, and circular curves are discussed, and the general form of a least squares adjustment model for relative orientation based on multi-features is established. Our experimental results show that the proposed approach is feasible and can achieve more reliable relative orientation results than the conventional approach based on corresponding points only.  相似文献   

13.
This paper deals with the orientation of three-line imagery which has been taken during the MOMS-02/D2 experiment in spring 1993, and during the MOMS-2P/PRIRODA mission since April 1996. The reconstruction of the image orientation is based on a combined adjustment of the complete image, ground control, orbit and attitude information. The combined adjustment makes use of the orientation point approach or the orbital constraints approach. In the second case, the bundle adjustment algorithm is supplemented by a rigorous dynamical modeling of the spacecraft motion. The results of the combined adjustment using MOMS-02/D2 imagery and control information of orbit #75b are presented. Based on the orientation point approach an empirical height accuracy of up to 4 m (0.3 pixel) is obtained. In planimetry the empirical accuracy is limited to about 10 m (0.7 pixel), since the ground control points (GCP) and check points could not be identified in the imagery with the required accuracy. Computer simulations on MOMS-2P/PRIRODA image orientation based on realistic input information have shown that good accuracies of the estimated exterior orientation parameters and object point coordinates can be obtained either with a single strip and a few precise GCP or even without ground control information, if a block of several overlapping and crossing strips with high geometric strength (q≈60%) is adjusted.  相似文献   

14.
利用数字模拟方法,进一步探讨了类似MOMS-02参数的卫星三线阵CCD影像单航线、航线首末4角隅设一个控制点(以下简写为单航线4控点)的空中三角测量高程精度低的问题。研究得出,宽高比特别小(1:9)只是原因之一,更主要的因素还在于平差整过程数学关系带有近似性(包括EFP法和定向片法)。提出了改善精度的措施,并拟订了提高卫星三线阵CCD影像空中三角测量精度及摄影测量覆盖效能的系统。模拟计算表明,航线长度可以≥2B,在有外方位元素或无外方位元素少量控制点条件下,不论二线交会区,还是三线交会区均可达到高程精度为6m的摄影测量成果。  相似文献   

15.
目前导线网平差多采用相关平差法。按该法在网(结点)平差时计算未知数的协因数阵,可以评定结点的点位精度。文献[2]等均未曾论及各个导线点的精度评定问题。实际上,导线网中的最弱点不一定出现在结点内,为此需全面评定导线点的精度。本文将专门论述导线网相关平差中导线点的精度评定问题。  相似文献   

16.
卫星摄影三线阵CCD影像的EEP法空中三角测量(三)   总被引:1,自引:1,他引:0  
4 平差方案及模拟数据平差实验4.1 自由网+控制点空中三角测量由前方交会(2.1)式,后方交会(2.2)式以及外方位元素平滑制约条件(2.3)式,可以构成类似经典的光束法空中三角测量,但由于EFP像点坐标是推算出来的,所以控制点不宜直接参与平差过程.于是平差要分成自由网平差及利用控制点作三维线性变换两个步骤.另一方面,卫星摄影中起始角元素大约在±0.5°左右,对于经典空中三角测量,角元素起始近似值均可按零处理.但在EFP平差中,φ角起始值φ0对空中三角测量,像元素起始近似值均可按零处理.在EFP平差中,φ角起始值φ0对整条航线的几何状态影响很大,必须采用特殊的程序预先加以确定.我们采用不断步进φ角值,比较由前方交会及(1.2)式计算的Y视差的均方根值最小者,即作为φ的最佳起始值.平差框图见图4.  相似文献   

17.
关于卫星网的位置基准及其对联合平差的影响   总被引:1,自引:0,他引:1  
周忠谟  晁定波 《测绘学报》1991,20(4):269-275
  相似文献   

18.
The determination of the attitude, the position and the intrinsic geometric characteristics of the camera is recognised as the fundamental photogrammetric problem. It can be summarised as the determination of camera interior and exterior orientation parameters, as well as the determination of 3D coordinates of object points. The term "exterior orientation"of an image refers to its position and orientation related to an exterior (object space) coordinate system. Several methods can be applied to determine the parameters of the orientation of one, two or more photos. The orientation can be processed in steps (as relative and absolute orientation) but simultaneous methods (such as bundle adjustments) are now available in many software packages. Several methods have also been developed for the orientation of single images. They are based in general on geometric and topological characteristics of imaged objects.
This paper presents a survey of classical and modern methods for the determination of the exterior parameters in photogrammetry, some of which are available as software packages (with practical examples) on the Internet. The methods presented are classified in three principal groups. In the first, a selection of approximate methods for applications that do not require great accuracy is presented. Such methods are also used to calculate values required for iterative processes. In the second group, standard point–based methods derived from collinearity, coplanarity or coangularity conditions are briefly reviewed, followed by line–based approaches. The third group represents orientation methods based on constraints and on concepts of projective geometry, which are becoming of increasing interest for photogrammetrists. In the last section, the paper gives a summary of existing strategies for automatic exterior orientation in aerial photogrammetry.  相似文献   

19.
卫星摄影三线阵CCD影像的EFP法空中三角测量(一)   总被引:10,自引:2,他引:8  
系统地介绍了EFP法空中三角测量的基本思想、EFP像点坐标计算、平差的数学模型和卫生摄影测量的数字模拟,并以模拟数据进行了自由网+控制点平差、外方位元素量测值参与平差、外方位元素量测值常差的分离以及区域平差等实验计算和实验结果分析。通过研究分析得出结论:(1)三条基线的航线可以保证三线阵CCD影像光束法平差的几何强度;(2)控制点可以布设在航线首末端,二线交会区的高程精度比三线交会区仅低约1.4因子;(3)外方位元素观测值是三线阵CCD影像光束法平差不可缺少的数据,经过平差可以不同程度地提高平差的高程精度。即使外方位元素观测值达到现代的精度,光束法平差的高程精度仍比直接前方交会高,所以三线阵CCD相机比单线阵、双线阵相机在全球性无控制卫星摄影测量或外星球摄影测量方面有更大的优势。  相似文献   

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