首页 | 本学科首页   官方微博 | 高级检索  
     检索      

星载SAR轨道及姿态误差模型分析
引用本文:韩中生,黄惠明,龙方.星载SAR轨道及姿态误差模型分析[J].飞行器测控学报,2005,24(5):38-43.
作者姓名:韩中生  黄惠明  龙方
作者单位:北京跟踪与通信技术研究所,北京100094
摘    要:平台轨道及姿态误差模型是星载SAR数据模拟及相应的模拟系统的关键组成部分。简要分析了机载SAR和星载SAR的差异,重点对星载SAR的平台轨道及姿态模型进行了分析,最后对星载SAR回波信号仿真方法进行了分析。

关 键 词:星载SAR  卫星椭圆轨道模型  平台姿态误差模型
收稿时间:2005-03-29
修稿时间:2005-05-31

Analysis of the Orbit and Attitude Error Model of Space-borne SAR
HAN Zhong-sheng, HUANG Hui-ming, LONG Fang.Analysis of the Orbit and Attitude Error Model of Space-borne SAR[J].Journal of Spacecraft TT&C Technology,2005,24(5):38-43.
Authors:HAN Zhong-sheng  HUANG Hui-ming  LONG Fang
Institution:Beijing Institute of Tracking and Telecommunications Technology, Beijing 100094
Abstract:Accurate orbit and attitude model is of great importance to data and system simulation of space-borne SAR. Following a brief analysis of the difference between air-borne and space-borne SAR, the paper analyzes the simulated orbit and attitude model of space-borne SAR. Finally, analysis is given on the simulation method on the echo of space-borne SAR.
Keywords:Space-borne SAR  Elliptical Orbit Model of Satellite  Platform Attitude Error Model
本文献已被 CNKI 维普 等数据库收录!
点击此处可从《飞行器测控学报》浏览原始摘要信息
点击此处可从《飞行器测控学报》下载免费的PDF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