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

光纤陀螺/GPS组合导航系统中的信息融合技术
引用本文:张小跃,张春熹.光纤陀螺/GPS组合导航系统中的信息融合技术[J].北京航空航天大学学报,2008,34(4):422-425.
作者姓名:张小跃  张春熹
作者单位:北京航空航天大学仪器科学与光电工程学院,北京,100083;北京航空航天大学仪器科学与光电工程学院,北京,100083
摘    要:光纤陀螺捷联惯导系统用于导航定位具有自主性的优点,但系统误差随时间累积.全球定位系统(GPS,Global Position System)用于导航定位精度很高,误差不随时间积累,但抗干扰性能很差,没有自主性.运用信息融合技术将光纤陀螺捷联系统和GPS进行组合,将GPS的高度信息引入惯导高度反馈通道,设定反馈系数,抑制高度发散,将GPS经度、纬度、地速信息作为系统卡尔曼滤波器量测信息,消除惯导积累误差.提出的信息融合方案运用于某中精度光纤陀螺/GPS组合导航系统并进行路试,导航系统输出3个方向位置数据与定位基准相比,误差不随时间积累,路试结果表明此信息融合方案的有效性及工程的实用性.

关 键 词:光纤陀螺  全球定位系统  信息融合  卡尔曼滤波
文章编号:1001-5965(2008)04-0422-04
收稿时间:2007-04-02
修稿时间:2007年4月2日

Information fusion technology in FOG/GPS integrated navigation system
Zhang Xiaoyue,Zhang Chunxi.Information fusion technology in FOG/GPS integrated navigation system[J].Journal of Beijing University of Aeronautics and Astronautics,2008,34(4):422-425.
Authors:Zhang Xiaoyue  Zhang Chunxi
Institution:School of Instrument Science and Opto-electronics Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100083, China
Abstract:Fiber optic gyro(FOG) strapdown inertial navigation system used in orientation has an advantage of independence,but its system error accumulates with time;Global position system(GPS) can provide more accurate information,but it is interfered easily.FOG and GPS was integrated using information fusion technology.GPS height information was introduced into vertical channel to restrain error increasing basing on setting feedback coefficients.GPS latitude,longitude and horizontal velocity was introduced as Kalman filter observation to remove accumulating error.Information fusion means presented here was applied in a medium-precision FOG/GPS navigation system,and tested in a vehicle. Error of system output positioning parameters was not increased along with time.The testing results are presented to validate the availability and engineering utility of the information fusion means.
Keywords:fiber optic gyro  global position system  information fusion  Kalman filter
本文献已被 CNKI 维普 万方数据 等数据库收录!
点击此处可从《北京航空航天大学学报》浏览原始摘要信息
点击此处可从《北京航空航天大学学报》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