首页 | 本学科首页   官方微博 | 高级检索  
     

柔性基线抖动对机载干涉SAR 性能影响分析
引用本文:刘忠胜,汪丙南,向茂生,陈龙永.柔性基线抖动对机载干涉SAR 性能影响分析[J].雷达学报,2014,3(2):183-191.
作者姓名:刘忠胜  汪丙南  向茂生  陈龙永
作者单位:1.(中国科学院电子学研究所微波成像技术重点实验室 北京 100190)2.(中国科学院大学 北京 100049)
基金项目:国家部委基金;中国科学院科研装备研制项目—多模式脉冲散射测量及微波天线测试设备(YZ201107)资助课题
摘    要:机载干涉SAR 平台在飞行过程中通常会受气流、机械振动等因素的影响,造成柔性基线抖动,从而严重影响干涉SAR 系统的性能。该文针对柔性基线机载干涉SAR 系统中的基线抖动问题,首先推导了基线抖动下的斜距误差模型,然后从1 次、2 次和一般斜距误差建立了SAR 复图像信号模型和双通道相关系数模型,并理论分析了基线抖动对SAR 成像和干涉性能的影响。最后通过回波仿真实验验证了理论分析的正确性。 

关 键 词:柔性基线抖动    干涉SAR    相关系数    干涉性能
收稿时间:2014-01-22

Performance Analysis for Airborne Interferometric SAR Affected by Flexible Baseline Oscillation
Liu Zhong-sheng,Wang Bing-nan,Xiang Mao-sheng,Chen Long-yong.Performance Analysis for Airborne Interferometric SAR Affected by Flexible Baseline Oscillation[J].Journal of Radars,2014,3(2):183-191.
Authors:Liu Zhong-sheng  Wang Bing-nan  Xiang Mao-sheng  Chen Long-yong
Affiliation:1.(Science and Technology on Microwave Imaging Laboratory, Institute of Electronics, Chinese Academy of Sciences, Beijing 100190, China)2.(University of Chinese Academy of Sciences, Beijing 100049, China)
Abstract:The airborne interferometric SAR platform suffers from instability factors, such as air turbulence and mechanical vibrations during flight. Such factors cause the oscillation of the flexible baseline, which leads to significant degradation of the performance of the interferometric SAR system. This study is concerned with the baseline oscillation. First, the error of the slant range model under baseline oscillation conditions is formulated. Then, the SAR complex image signal and dual-channel correlation coefficient are modeled based on the first-order, second-order, and generic slant range error. Subsequently, the impact of the baseline oscillation on the imaging and interferometric performance of the SAR system is analyzed. Finally, simulations of the echo data are used to validate the theoretical analysis of the baseline oscillation in the airborne interferometric SAR. 
Keywords:
本文献已被 CNKI 等数据库收录!
点击此处可从《雷达学报》浏览原始摘要信息
点击此处可从《雷达学报》下载全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号