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

航空遥感中基于高阶INS误差模型的GPS/INS组合定位定向方法
引用本文:孙红星,袁修孝,付建红.航空遥感中基于高阶INS误差模型的GPS/INS组合定位定向方法[J].测绘学报,2010,39(1):28-33.
作者姓名:孙红星  袁修孝  付建红
作者单位:武汉大学遥感信息工程学院,湖北,武汉,430079;Department of Civil and Environmental Engineering and Geodetic Science,The Ohio State University,Columbus 43210,USA;武汉大学遥感信息工程学院,湖北,武汉,430079
基金项目:国家自然科学基金(40501060,40771176)
摘    要:基于随机常数、随机游走和一阶马尔可夫过程组合的高阶IMU误差模型,建立36阶卡尔曼滤波器。通过松散组合模式,最终实现位置标准差±5cm、俯仰/横滚角标准差±0.002°、航向角标准差±0.008°的定位定向精度。

关 键 词:直接地理参考  直接平台定向  航空三角测量  GPS/INS集成  卡尔曼滤波

The GPS/INS Integrated Positioning and Orientation in the Aerial Remote Sensing Based on the High-order INS Stochastic Error Model
SUN Hongxing,YUAN Xiuxiao,FU Jianhong.The GPS/INS Integrated Positioning and Orientation in the Aerial Remote Sensing Based on the High-order INS Stochastic Error Model[J].Acta Geodaetica et Cartographica Sinica,2010,39(1):28-33.
Authors:SUN Hongxing  YUAN Xiuxiao  FU Jianhong
Institution:SUN Hongxing1,2,YUAN Xiuxiao1,FU Jianhong11. School of Remote Sensing , Engineering,Wuhan University,Wuhan 430079,China,2. Department of Civil , Environmental Engineering , Geodetic Science,The Ohio State University,Columbus 43210,USA
Abstract:Despite significant progress in GSP/INS-based direct georeferencing technology in the last decade,there is still room for improvement in terms of better accuracy. The main objective of this paper is the stochastic modeling of Inertial Measurement Unit (IMU) errors,which determines significantly the final performance of the GPS/INS integrated system. With the random constants,random walks and first-order Markov process models to characterize the stochastic errors of IMU,one Kalman Filter with 36 orders was m...
Keywords:direct georeferencing  aerial triangulation  direct platform orientation  GPS/INS integration  Kalman filter  
本文献已被 CNKI 万方数据 等数据库收录!
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