机载差分干涉SAR的误差分析

钟雪莲; 向茂生; 岳焕印; 郭华东

doi:10.3724/SP.J.1146.2009.00377

机载差分干涉SAR的误差分析

doi: 10.3724/SP.J.1146.2009.00377

钟雪莲^{①②;向茂生,},
向茂生,
岳焕印,
郭华东

计量
- 文章访问数: 3717
- HTML全文浏览量: 84
- PDF下载量: 914
- 被引次数: 0
出版历程
- 收稿日期: 2009-03-23
- 修回日期: 2009-10-09
- 刊出日期: 2010-04-19

Error Analysis for Airborne Differential SAR Interferometry

摘要

摘要: 该文就机载差分干涉中影响精度的几个重要因素进行了详细的分析，为开展机载差分干涉应用提供理论基础。首先考虑机载差分干涉算法流程中引入的误差，指出必须利用外部DEM(Digital Elevation Model)计算本地视角才能实现高精度的形变反演。随后，重点讨论了影响差分干涉SAR (Synthetic Aperture Radar) 的几个重要影响因素：系统参数误差、相干性和大气效应。系统参数中基线和基线角的误差对差分干涉的精度影响最大，由此对机载残余运动的补偿提出了很高的要求。相干性分析又对机载差分干涉中形变像对的基线长度提出了严格的限制条件。和星载SAR一样，机载SAR同样受到大气的影响。通过计算这些因素的对机载差分干涉精度的影响，给出了机载差分干涉精度的表达式。
- 机载SAR差分干涉; 精度; 大气效应; 相干性
Abstract: This paper mainly analyzes the important factors that influence the accuracy of airborne differential SAR interferometry. The error induced by the processing procedure of differential SAR interferometry is first considered, and it is point out that external DEM is indispensable to achieve high accuracy in detecting and monitoring deformations of the earths surface. Then several factors, i.e. system parameters, coherence and atmosphere, are discussed in detail. Among these factors, baseline length and orientation play a much more crucial role, and that means high quality of motion compensations are necessary. By connecting the coherence with the accuracy of airborne SAR differential interferometry, the flight path for repeat-pass interferomtery have to be precisely controlled to meet the baseline requirement. Similar to spaceborne SAR, Airborne SAR also suffers atmosphere effect. After discussing all these factors, the mathematical expressions of the accuracy are presented for airborne differential SAR interferometry.

HTML全文

参考文献(1)

Cumming I G and Wong F H. Digital Processing of SyntheticAperture, Radar Data: Algorithms and Implementation.America, Artech House Inc, 2005: 322-331.[2]Zhang Yun-hua and Zhai Wen-shuai. A new method forDoppler cenrtoid estimation for spaceborne SAR based onchirp scaling algorithm. Geoscience and Remote SensingSymposium, 2007, IGARSS2007, Barcelona Spain, July23-28, 2007: 543-546.[3]Dukhopelnikova I V. New difference Doppler centroidestimation method with high space resolution. Microwaves.[J].Radar and Remote Sensing Symposium, MRRS2008, KievUkraine, September 22-2.2008,:-[4]魏钟铨. 合成孔径雷达. 北京：科学出版社, 2001: 132-152.Wei Zhong-quan. Synthetic Aperture Radar Satellite. Beijing:Publishing House of Science, 2001: 132-152.[5]Raney R K. Doppler properties of radars in circular orbits[J].International Journal of Remote Sensing.1986, 7(9):1153-1162[6]Fiedler H and Boerner E. Total zero Doppler steeringAnew method for minimizing the Doppler centroid[J].Geoscienceand Sensing Letters.2005, 2(2):141-145[7]Boerner E and Fiedler H. A new method for total zeroDoppler steering. Geoscience and Remote SensingSymposium.[J].IGARSS2004, Anchorage Alaska, September20-2.2004,:-[8]Fiedler H.[J].Fritz T, and Kahle R. Verification of the total zeroDoppler steering. Radar2008 International Conference,Rome Italy, September 2-.2008,:-[9]郗晓宁, 王威. 近地航天器轨道基础. 长沙: 国防科技大学出版社, 2003, 4, 第7章, 第8章.Xi Xiao-ning and Wang Wei. Fundamentals of Near-earthSpacecraft Orbit. Changsha: Publishing House of NationalUniversity of Defence Technology, 2003, 4, Chapter7,Chapter8.[10]孟云鹤, 尹秋岩, 戴金海. SAR卫星多普勒频移偏航导引补偿效果分析. 中国空间科学技术, 2004, 24(1): 45-48.Meng Yun-he, Yin Qiu-yan, and Dai Jin-hai. Dopplerfrequency shift compensation analysis of SAR satellite yawsteering. Chinese Space Science and Technology, 2004, 24(1):45-48.

施引文献

资源附件(0)

访问统计