Please wait a minute...
img

官方微信

遥感技术与应用  2004, Vol. 19 Issue (6): 498-503    DOI: 10.11873/j.issn.1004-0323.2004.6.498
技术方法     
星载雷达高度计幅度和相位误差分析与估算
 徐曦煜,刘和光,许 可
(1.中国科学院空间科学与应用研究中心,北京 100080;2.中国科学院研究生院,北京 100039)
The Analysis and Estimate of the Bias due to the Amplitudeand Phase Ripples in Spaceborne Radar Altimeter
XU Xi-yu, LIU He-guang, XU Ke
1.Center for Space Science and Applied Research,Chinese Academy of Sciences,NationalMicrowave Remote Sensing Laboratory,Beijing100080,China; 2.The GraduateSchool of Chinese Academy of Sciences,Beijing100039,China)
 全文: PDF 
摘要:

在星载雷达高度计中,误差分析是其核心内容之一。而其中幅度和相位误差一直是设备误差中相当重要的一项。利用成对回波理论推导了幅度和相位误差带来的距离旁瓣,并将旁瓣与测高误差对应起来,结合具体参数进行了定量分析,对系统的幅度及相位误差进行了估算。

关键词: 雷达高度计幅度和相位起伏成对回波理论距离旁瓣测高误差    
Abstract:

Radar altimeter has become one of the most useful microwave sensing instruments for observing theearth in the past three decades, and the results from several successful missions, such as Geosat、ERS1+2 andTopex,has been widely used in many geodesy field, particularly in ocean topography. Error analysis is one ofthe core techniques in the design of Spaceborne Radar Altimeter, because the altimeter data may be impracticalfor some application cases without adequate precision. Amplitude and phase ripples of the RF system are impor-tant error sources in height measurement. This paper deals with the error issue with the help of the well-estab-lished tool——“paired-echo theory”. Firstly, we consider that the ripples have the sinusoid forms, and then wecan convert these ripples into range side lobes. On the other hand, we establish the form of the side lobe andderive the relationship between side lobes and height bias. In this way we can establish the relationship betweenamplitude (phase) ripples and height bias. And finally, applying this method to a practical system, we can getsome quantitative requirements for the amplitude and phase ripples. These requirements are very critical inradar altimeter design.

收稿日期: 2004-10-22 出版日期: 2011-12-26
:  TP 75   
作者简介: 徐曦煜(1979-),男,研究生,主要从事雷达高度计等微波遥感器的研究工作。
服务  
把本文推荐给朋友
加入引用管理器
E-mail Alert
RSS
作者相关文章  

引用本文:

徐曦煜,刘和光,许 可. 星载雷达高度计幅度和相位误差分析与估算[J]. 遥感技术与应用, 2004, 19(6): 498-503.

XU Xi-yu, LIU He-guang, XU Ke. The Analysis and Estimate of the Bias due to the Amplitudeand Phase Ripples in Spaceborne Radar Altimeter. Remote Sensing Technology and Application, 2004, 19(6): 498-503.

链接本文:

http://www.rsta.ac.cn/CN/10.11873/j.issn.1004-0323.2004.6.498        http://www.rsta.ac.cn/CN/Y2004/V19/I6/498

〔1〕 Mcmorgan J T. The S-193 Radar Altimeter Experiment〔J〕.Proc IEEE, 1974, 62: 793~803.〔2〕 许可.高分辨率星载雷达高度计系统研究〔D〕.中国科学院博士学位研究生学位论文,2001.〔3〕 姜景山.空间科学与应用〔M〕.北京:科学出版社,2001.279~312.〔4〕 班守正.星载雷达高度计设备误差对测高精度影响的分析和验证〔R〕.国家863计划微波遥感实验室技术报告,2002.〔5〕 Klauder J R. The Theory and Design of Chirp Radars〔J〕. TheBell System Technical Journal, 1960, 4: 745~804.〔6〕 Brooks L W, Dooley R P. Technical Guidance and AnalyticServices in Support of Seasat-A (Final Report)〔R〕. NASACR-141399. APR.1975.〔7〕 Brown G S. The Average Impulse Response of a Rough SeaSurface and Its Applications〔J〕. IEEE Trans Antennas Propa-gation,1977,AP-25(1):67~74.〔8〕 Chelton D B. Pulse Compression and Sea Level Tracking inSatellite Altimetry〔J〕. Journal of Atmos. Oceanic Technical,1989, 6(3): 407~438.〔9〕 Seasat Special Issue Part 1〔J〕. J G R, 1982, 87(C5): 3173~3438.〔10〕 British Aerospace Dynamic Group. Radar Altimeter Test andCalibration Study(Final Report)〔R〕.ESA-SOS N83-20942,1982.119~150.〔11〕 Technology Service Corporation, Sliver Spring, MD. Study ofRadar Pulse Compression for High-resolution Satellite Altimetry(Final Report)〔R〕. NASA CR-137474,1974. 88~134.

[1] 杨双宝,翟振和,许可,王志森,史灵卫,王磊,崔海英,徐曦煜. 合成孔径雷达高度计数据处理方法[J]. 遥感技术与应用, 2017, 32(6): 1083-1092.
[2] 徐永生,高乐,张云华. 美国新一代测高卫星SWOT—评述我国宽刈幅干涉卫星的发展借鉴[J]. 遥感技术与应用, 2017, 32(1): 84-94.
[3] 张国首,苗洪利,王桂忠,郭迎婷,荆玉洁,张杰. 雷达高度计海况偏差估计不同纬度区间参数模型研究[J]. 遥感技术与应用, 2016, 31(6): 1054-1058.
[4] 高 阳,刘和光. 基于MATLAB/SIMULINK的海面回波模拟器仿真与分析[J]. 遥感技术与应用, 2007, 22(4): 565-569.
[5] 张 婷,许 可. 一种提高海洋雷达高度计重跟踪估值精度的处理方法[J]. 遥感技术与应用, 2007, 22(3): 422-427.
[6] 徐曦煜,刘和光,许 可. 基于海洋二号高度计内定标方案的工程设计和误差分析[J]. 遥感技术与应用, 2007, 22(2): 141-146.
[7] 刘保有,许 可. 雷达高度计误指向角的估计与补偿[J]. 遥感技术与应用, 2007, 22(1): 101-104.
[8] 许 可, 董晓龙, 张德海, 刘和光, 姜景山. HY-2 雷达高度计和微波散射计[J]. 遥感技术与应用, 2005, 20(1): 89-93.
[9] 许 可,刘和光,姜景山. 神舟4号雷达高度计在轨工作模式及实时数据处理[J]. 遥感技术与应用, 2005, 20(1): 162-165.
[10] 郭 伟,张晓辉. 回波模拟器在雷达高度计地面测试和定标中的应用[J]. 遥感技术与应用, 2005, 20(1): 178-181.
[11] 许 可,姜景山. 基于最大似然估计的雷达高度计跟踪处理[J]. 遥感技术与应用, 2000, 15(2): 104-107.
[12] 张云华, 许可, 李茂堂, 李靖, 刘和光, 王新中 . 星载三维成像雷达高度计研究[J]. 遥感技术与应用, 1999, 14(1): 11-14.
[13] 许可, 周宁, 李茂堂. 星载海洋雷达高度计信号处理实时仿真 [J]. 遥感技术与应用, 1999, 14(1): 20-24.
[14] 张俊荣. 我国微波遥感现状及前景[J]. 遥感技术与应用, 1997, 12(3): 58-64.
[15] 张升伟 ,张俊荣, 郭伟. 星载雷达高度计设计方案[J]. 遥感技术与应用, 1996, 11(2): 15-19.