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捷联式光纤陀螺罗经系统误差分析
引用本文:高亚楠,陈家斌,杨亭鹏.捷联式光纤陀螺罗经系统误差分析[J].北京理工大学学报,2005,25(5):423-426.
作者姓名:高亚楠  陈家斌  杨亭鹏
作者单位:北京理工大学,信息科学技术学院自动控制系,北京,100081
摘    要:对采用光纤陀螺的捷联式罗经系统进行了研究.提出了使用惯性组件旋转调制技术提高光纤陀螺捷联式罗经系统精度的方法,分析了罗经系统的误差特性.针对旋转组件的误差,在系统初始对准过程中,应用限定记忆的Kalman滤波进行状态估计,提高了对准精度.静止基座的初始对准仿真结果表明,航向失准角估计误差均方差为0.159°.

关 键 词:光纤陀螺  捷联惯性导航  旋转组件  限定记忆Kalman滤波  捷联式  光纤陀螺  罗经系统  误差分析  Compass  Gyro  Optic  Fiber  Analysis  差为  误差均方  状态估计  失准角  航向  仿真结果  基座  对准精度  滤波  Kalman  限定记忆  应用
文章编号:1001-0645(2005)05-0423-04
收稿时间:2004/6/11 0:00:00
修稿时间:2004年6月11日

Error Analysis of Strapdown Optic Fiber Gyro Compass
GAO Ya-nan,CHEN Jia-bin and YANG Ting-peng.Error Analysis of Strapdown Optic Fiber Gyro Compass[J].Journal of Beijing Institute of Technology(Natural Science Edition),2005,25(5):423-426.
Authors:GAO Ya-nan  CHEN Jia-bin and YANG Ting-peng
Institution:Department of Aoutmatic Control, School of Information Science and Technology, Beijing Institute of Technology, Beijing 100081, China;Department of Aoutmatic Control, School of Information Science and Technology, Beijing Institute of Technology, Beijing 100081, China;Department of Aoutmatic Control, School of Information Science and Technology, Beijing Institute of Technology, Beijing 100081, China
Abstract:The strapdown optic fiber gyro inertial navigation system is studied. A method to rotate the inertial measure unit is presented to improve the system accuracy. Error features of the gyro compass is analyzed. For the error of the rotation unit, a finite memory Kalman filter is applied to estimate the states during the initial alignment. It improves the accuracy of the alignment. Simulation results show that the mean square error of initial yaw alignment is about 0.159°.
Keywords:optic fiber gyro  strapdown inertial navigation system  rotation unit  finite memory Kalman filter
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