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1.
黄海风  梁甸农 《遥感学报》2006,10(2):221-226
针对主星带辅星群编队InSAR的双站、斜视、空间基线等特点,首先建立绝对测高误差与相对测高误差模型;重点分析了基线去相关对干涉相位误差的影响;对干涉车轮和钟摆编队的测高性能、对测高精度与基线矢量的关系进行仿真分析;其次与两种经典近似几何关系下的测高精度分析进行对比。仿真结果表明:干涉测高精度必须考虑基线去相关的影响;相对测高精度明显优于绝对测高精度;经典近似几何给分析测高精度带来很大误差。  相似文献   

2.
InSAR高程模型及其精度分析   总被引:3,自引:0,他引:3  
提出了一种改进的InSAR高程模型,建立了高程和干涉相位的直接关系,并对公式推导中一般采用的平行射线近似处理方法所引入的高程误差进行了量化分析。结果表明,对于星载雷达而言,平行射线近似误差不能忽略。给出了近似误差与基线参数的确定性关系及相应的误差传播曲线,有助于误差纠正和重建高精度DEM。另外,基于改进的高程模型,推导出了高程测量误差传播公式,明确了基线长度和方向对测高精度的影响,对合理选择干涉像对具有指导意义。  相似文献   

3.
星载GNSS-R干涉测高技术通过调制GNSS卫星信号的宽带混合码,可以实现高精度宽幅海面测高。为有效验证星载GNSS-R干涉测高性能,本文设计了基于岸基GNSS-R干涉测高结果,开展星载GNSS-R干涉测高精度等效评估的策略。评估结果表明,GNSS-R干涉测高与卫星导航系统信号体制及信号信噪比相关,星载GNSS-R干涉测高可实现分米级测高精度。本文的研究成果可为后续星载GNSS-R干涉测高工程实践提供技术参考和数据支持。  相似文献   

4.
王晓光  王治强  杨新 《测绘学报》2010,39(6):561-565
星载干涉合成孔径雷达(InSAR)基线的高精度测定是获取地面数字高程信息的关键技术。对双天线InSAR系统,采用光学相机和激光测距仪相结合实时动态测量基线。由于存在仪器误差和几何误差等,为满足干涉基线的确定精度,基于基线测量系统,构建状态方程和测量方程,并结合天线支撑臂模态分析,设计了Kalman滤波器,确定干涉基线的长度和指向。模拟仿真结果显示,该滤波器能够有效地估计干涉基线长度和指向,满足基线确定精度要求。  相似文献   

5.
干涉定标技术是机载InSAR获取高精度DEM的关键技术,根据GPS高精度定位数据支持下的机载SAR定标模型,通过一定数量的地面定标点校正干涉SAR系统参数,InSAR与高精度GPS/INS技术的结合进一步提高了InSAR测图的精度。文中对GPS支持下的干涉定标技术进行仿真试验,基于机载SAR正侧视模型的成像几何关系,建立关于干涉参数和地面定标点的定标模型,采用基于敏感度方程的干涉定标方法,对地面定标点的测量高程值上加入不同的随机误差,分析该测量误差对干涉定标结果的影响,结果表明,高精度的GPS定位数据提高了机载InSAR测图的精度。  相似文献   

6.
针对星载二号分布式干涉合成孔径雷达系统目标定位的问题,以双基成像模型为基础,推导了雷达发射信号时刻与接收回波时刻卫星平台位置及速度发生变化的三维目标定位方程,给出了解算过程中的数据处理策略。文中采用星载分布InSAR干涉影像进行的无控制点条件下的定位和精度检测实验,验证了模型和数据处理策略的有效性和准确性。  相似文献   

7.
星载分布式合成孔径雷达(SAR)系统用于干涉测绘,凭借其基线灵活、时间去相关很小的特点得到了快速发展。与传统模式相比,双频乒乓模式能够同时得到两种频率的多幅SAR图像,可以实现更高精度的高程测量。本文首先简单介绍了双频乒乓模式的工作原理,然后深入研究了该模式下SAR干涉对的相位比例关系和相关性,理论上分析了其干涉相位估计精度和对应的测高精度,从而为系统设计和干涉处理方法研究提供理论依据。最后仿真分析结果直观展示了双频乒乓模式相较于传统模式的优越性,由于该模式增加了不同频率的干涉相位数据,干涉相位估计精度和测高精度均显著提升。  相似文献   

8.
机载双天线InSAR(interferometric synthetic aperture Radar)是获取高精度数字高程模型(digital elevation model,DEM)的新技术。为了获取大面积高精度的DEM,在已有的应用机载InSAR数据生成DEM流程的基础上,引入精确干涉参数定标和区域网平差处理技术,提出了利用国产机载双天线InSAR数据生成丘陵地区大面积、高精度DEM的技术流程,主要包括干涉定标、干涉处理、区域网平差、相高转换、地理编码和影像镶嵌;基于VC++开发了InSAR地形制图处理系统。以四川江油试验区4个条带、76景高分辨率机载InSAR数据为基础进行试验研究,生成了覆盖超过500 km2的高精度DEM。利用野外布设的角反射器检查点进行精度检验的结果是点位中误差为±1.188 m,高程中误差为±0.508 m。该结果表明:应用上述技术流程生成的DEM能满足丘陵地区1∶1万比例尺一级高程中误差的精度要求;机载InSAR可作为复杂地区大面积地形测图制取的一种技术手段。  相似文献   

9.
从基线沿水平向分解的InSAR基本原理出发,推导出星载InSAR高程公式;然后根据斜距、基线、相位、基线倾角、入射角、高度等量之间的几何构形及存在的函数关系,推导出星载InSAR影响高度精度的误差公式,并定性和定量地分析斜距、基线、相位、基线倾角、入射角、水平基线及垂直基线等测高精度因子的相关性及与对高程误差的影响,明确基线长度和方向对测高精度的影响;最后,针对星载InSAR高程提取的特点,提出一些提高测量精度的参考和建议.  相似文献   

10.
董妍  董杰 《测绘科学》2014,39(12):8-10,32
文章研究了基于地基合成孔径雷达技术的两种DEM测高模型——近似测高模型和改进测高模型,根据星载雷达测高原理推导了这两种模型,并分析模型的精度.通过对近似测高模型中的平行射线近似处理方法进行量化分析,指出近似处理方法引入的高程误差不能被忽略.本文对改进测高模型中各参数的误差传播系数进行了仿真分析,结果表明改进测高模型提高了理论测高精度,并可采用增加基线长度和缩短斜距的方法提高测高精度.  相似文献   

11.
星载差分合成孔径雷达干涉测量(differential interferometric synthetic aperture radar,DInSAR)技术已经广泛应用于大范围的地表形变监测,但星载合成孔径雷达(synthetic aperture radar,SAR)数据获取的地表形变易受大气噪声的影响,且长时间的重访周期会导致像对之间的失相干。为了有效减弱这些影响,提出了利用零空间基线的车载合成孔径雷达干涉测量(interferometric synthetic aperture radar,InSAR)系统监测公路边坡形变的方法。在车载双天线系统采集不同时相的公路边坡SAR数据时,通过轨道控制使得异时相干涉对的空间基线接近零,从而使得利用DInSAR数据进行形变信息提取时可以减少去平地相位的过程,极大地简化了差分干涉处理的流程。以中国湖北省武汉市某区域获取的车载双天线InSAR数据为例,使用所提出的方法对7个布设的角反射器点进行形变精度分析,得到形变值均方根误差为2.206 mm。  相似文献   

12.
An adaptive contoured window filter is proposed to filter off the noise from phase images of interferometric synthetic aperture radar (InSAR) in this letter. The contoured windows can best satisfy the requirement that constrains the phase signal constant inside windows on which low-pass filtering can remove the noise well while the fringe phases are well preserved. The contoured windows are determined by tracing along the local fringe orientation. An algorithm for determining window sizes adaptive to the fringe density is also proposed. The theoretical analysis and experiments prove that the proposed filter can greatly remove decorrelation noise while preserving the fringe phase well, even for those fringes with strong curvatures for InSAR processing  相似文献   

13.
Abstract

Information of snow cover (SC) over Himalayan regions is very important for regional climatological and hydrological studies. Precise monitoring of SC in the Himalayan region is essential for water supply to hydropower stations, irrigation requirements, and flood forecasting. Microwave remote sensing has all weather, day and night earth observation capability unlike optical remote sensing. In this study, spaceborne synthetic aperture radar interferometric (InSAR) coherence analysis is used to monitor SC over Himalayan rugged terrain. The feasibility of monitoring SC using synthetic aperture radar (SAR) interferometry depends on the ability to maintain coherence over InSAR pair acquisition time interval. ERS-1/2 InSAR coherence and ENVISAT ASAR InSAR coherence images are analyzed for SC mapping. Data sets of winter and of snow free months of the Himalayan region are taken for interferogram generation. Coherence images of the available data sets show maximum decorrelation in most of the area which indicates massive snowfall in the region in the winter season and melting in the summer. Area showing coherence loss due to decorrelation is mapped as a snow-covered area. The result is validated with field observations of snow depth and it is found that standing snow is inversely related to coherence in the Himalayan region.  相似文献   

14.
三维相位解缠是时序干涉合成孔径雷达(interferometric synthetic aperture radar,InSAR)技术的关键环节之一,解缠结果直接影响时序InSAR地面沉降监测的精度。针对地面沉降严重、地形坡度变化较大的区域,因相位欠采样引起的整周期解缠误差问题,提出了一种基于频域置信度的加权最小二乘相位解缠算法,并以此替代时空三维相位解缠中空间维以相位梯度为权重的加权最小二乘相位解缠算法。通过提高相位坡度变化估计的准确性,进而提高时空三维相位解缠的精度和稳定性。以北京地区地面沉降监测为例进行了验证,结果表明,与经典的时空三维相位解缠算法相比,改进算法得到的沉降监测结果精度更高,特别是对于坡度变化较大、失相干现象明显的沉降漏斗区,其沉降监测精度有明显改善。  相似文献   

15.
汪丙南  张帆  向茂生 《遥感学报》2010,14(6):1176-1188
提出并分析了基线抖动造成的干涉SAR 相位误差模型。基于干涉SAR 基线抖动模型, 分为水平抖动和 垂直抖动, 推导了存在基线抖动情况下辅天线复图像信号模型及基线抖动带来的干涉相位误差公式, 分析了基线 抖动对成像质量和干涉相位的影响, 针对SRTM 系统进行了计算机仿真。通过基于基线抖动的干涉SAR 原始回波 数据计算, 仿真了点目标和面目标场景的回波信号, 并进行成像得到了复图像和干涉条纹, 仿真结果验证了理论分 析的正确性。  相似文献   

16.
介绍了COSMO-SkyMed对地观测系统,分析了高分辨率SAR传感器和Tandem观测星座与相干性之间的关系,并利用间隔1 d的COSMO-SkyMed Tandem数据生成了祁连山区的DEM。提出通过对无地形变化的差分干涉相位进行滤波来提取大气和轨道误差引起的测量偏差,探讨了实验干涉数据去相干的因素,并将生成的DEM与ASTER GDEM进行了对比。  相似文献   

17.
Voids caused by shadow, layover, and decorrelation usually occur in digital elevation models (DEMs) of mountainous areas that are derived from interferometric synthetic aperture radar (InSAR) datasets. The presence of voids degrades the quality and usability of the DEMs. Thus, void removal is considered as an integral part of the DEM production using InSAR data. The fusion of multiple DEMs has been widely recognized as a promising way for the void removal. Because the vertical accuracy of multiple DEMs can be different, the selection of optimum weights becomes a key problem in the fusion and is studied in this article. As a showcase, two high-resolution InSAR DEMs near Mt. Qilian in northwest China are created and then merged. The two pairs of InSAR data were acquired by TerraSAR-X from an ascending orbit and COSMO-SkyMed from a descending orbit. A maximum likelihood fusion scheme with the weights optimally determined by the height of ambiguity and the variance of phase noise is adopted to syncretize the two DEMs in our study. The fused DEM has a fine spatial resolution of 10 m and depicts the landform of the study area well. The percentage of void cells in the fused DEM is only 0.13 %, while 6.9 and 5.7 % of the cells in the COSMO-SkyMed DEM and the TerraSAR-X DEM are originally voids. Using the ICESat/GLAS elevation data and the Chinese national DEM of scale 1:50,000 as references, we evaluate vertical accuracy levels of the fused DEM as well as the original InSAR DEMs. The results show that substantial improvements could be achieved by DEM fusion after atmospheric phase screen removal. The quality of fused DEM can even meet the high-resolution terrain information (HRTI) standard.  相似文献   

18.
基于卫星编队InSAR空间同步对系统性能影响的分析   总被引:2,自引:0,他引:2  
根据卫星编队条件下InSAR高程测量的要求,对空间同步的要求进行了研究。在此基础上,分析了空间同步对InSAR系统的高程测量精度和分辨率的影响。  相似文献   

19.
Recent studies have demonstrated the usefulness of global positioning system (GPS) receivers for relative positioning of formation-flying satellites using dual-frequency carrier-phase observations. The accurate determination of distances or baselines between satellites flying in formation can provide significant benefits to a wide area of geodetic studies. For spaceborne radar interferometry in particular, such measurements will improve the accuracy of interferometric products such as digital elevation models (DEM) or surface deformation maps. The aim of this study is to analyze the impact of relative position errors on the interferometric baseline performance of multistatic synthetic aperture radar (SAR) satellites flying in such a formation. Based on accuracy results obtained from differential GPS (DGPS) observations between the twin gravity recovery and climate experiment (GRACE) satellites, baseline uncertainties are derived for three interferometric scenarios of a dedicated SAR mission. For cross-track interferometry in a bistatic operational mode, a mean 2D baseline error (1σ) of 1.4 mm is derived, whereas baseline estimates necessary for a monostatic acquisition mode with a 50 km along-track separation reveal a 2D uncertainty of approximately 1.7 mm. Absolute orbit solutions based on reduced dynamic orbit determination techniques using GRACE GPS code and carrier-phase data allows a repeat-pass baseline estimation with an accuracy down to 4 cm (2D 1σ). To assess the accuracy with respect to quality requirements of high-resolution DEMs, topographic height errors are derived from the estimated baseline uncertainties. Taking the monostatic pursuit flight configuration as the worst case for baseline performance, the analysis reveals that the induced low-frequency modulation (height bias) fulfills the relative vertical accuracy requirement (σ<1 m linear point-to-point error) according to the digital terrain elevation data level 3 (DTED-3) specifications for most of the baseline constellations. The use of a GPS-based reduced dynamic orbit determination technique improves the baseline performance for repeat-pass interferometry. The problem of fulfilling the DTED-3 horizontal accuracy requirements is still an issue to be investigated. DGPS can be used as an operational navigation tool for high-precision baseline estimation if a geodetic-grade dual-frequency spaceborne GPS receiver is assumed to be the primary instrument onboard the SAR satellites. The possibility of using only single-frequency receivers, however, requires further research effort.Deutsche Forschungsgemeinschaft (DFG) research fellow until Sept. 2004 at the Microwaves and Radar Institute, Deutsche Zentrum für Luft- und Raumfahrt (DLR) e.V., 82234 Weßling, Germany  相似文献   

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