首页 | 本学科首页   官方微博 | 高级检索  
     

激光陀螺单轴旋转惯导系统多位置对准技术研究
引用本文:于旭东,龙兴武,王宇,张鹏飞,汤建勋,魏国.激光陀螺单轴旋转惯导系统多位置对准技术研究[J].传感技术学报,2011,24(6):824-828.
作者姓名:于旭东  龙兴武  王宇  张鹏飞  汤建勋  魏国
作者单位:国防科技大学光电科学与工程学院,长沙,410073
摘    要:激光陀螺单轴旋转惯导系统初始对准精度受陀螺漂移和加速度计零位的限制,为了减少对准误差,对多位置对准技术进行了研究。给出了单轴旋转惯导系统误差方程,利用奇异值分解的方法,对多位置对准时的系统各状态变量的可观测性进行分析,利用卡尔曼滤波仿真研究了多位置对准过程中方位失准角估计误差收敛情况,系统地分析了卡尔曼滤波器参数P0、...

关 键 词:惯导系统  多位置对准  单轴旋转  卡尔曼滤波  可观测性分析

Research on Multi-position Alignment in Single-axial Rotation Inertial Navigation System with Ring Laser Gyroscope
YU Xudong,LONG Xingwu,WANG Yu,ZHANG Pengfei,TANG Jianxun,WEI Guo.Research on Multi-position Alignment in Single-axial Rotation Inertial Navigation System with Ring Laser Gyroscope[J].Journal of Transduction Technology,2011,24(6):824-828.
Authors:YU Xudong  LONG Xingwu  WANG Yu  ZHANG Pengfei  TANG Jianxun  WEI Guo
Abstract:The alignment accuracy of the single-axial rotation inertial navigation system is limited by the bias of the ring laser gyroscopes and accelerometers. The multi-position alignment is researched to reduce the error of the alignment. Firstly, the error model of the single-axial rotation inertial navigation system is given; and than the observability analysis of the multi-position alignment by the method of singular value decomposition is processed, and azimuth misalignment angle error of multi-position is simulated by kalman filter; Finally, the effects of the choice of the Kalman filter parameters (including P0, Q, R) on estimation errors and convergent speed during multi-position initial alignment are analyzed. The vehicle-borne test on moving base are carried through and the results show that the multi-position alignment can improve the estimation accuracy of the ring laser gyroscope and accelerometer bias and the alignment accuracy. The accuracy of the inertial navigation system in vehicle-borne test is better than 1 nautical mile per 72 hours.
Keywords:inertial navigation system  single-axial rotation  multi-position alignment  kalman filter  observability
本文献已被 万方数据 等数据库收录!
点击此处可从《传感技术学报》浏览原始摘要信息
点击此处可从《传感技术学报》下载全文
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