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光纤陀螺捷联惯导系统艇上系泊状态自标定方法 被引量:4

Calibration method for mooring state of ship borne FOG SINS
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摘要 从实际工程使用角度出发,提出了一种在系泊状态下的系统级自标定方案,避免了惯导系统在艇上的反复拆装。提出的系统级标定方法设计了15位置转位方案,可以通过Kalman滤波对陀螺仪和加速度计的零次项误差,标度因数误差,安装误差进行精确估计,除了对以上误差参数的估计外,对影响导航精度的内杆臂参数和加速度计正负通道非对称误差也可以进行估计。并根据系泊状态的特殊晃动环境,设计了零相位延迟的低通滤波器从惯导系统的速度解算中得到速度误差,保证了惯导系统在不依赖外界输入条件下完成自标定任务。仿真及实验结果表明,该方法能在系泊状态下准确估计出全部误差变量,且与静基座标定结果相符,具有实际应用价值。 From the practical engineering point of view,a new systematic calibration method of SINS in mooring state is presented,which avoids the repeated assembling of SINS on the ship.The proposed systematic calibration method designs a 15-position scheme,which can accurately estimate the gyros and accelerometers bias errors,scale errors and installation angle errors.In addition to the above error parameters,the inner lever arm parameters and accelerometer asymmetric error that affect the navigation accuracy can also be estimated.According to the special sloshing environment of the mooring state,a filtering with zero-phase error is designed to obtain the velocity error from the calculation of the SINS,to ensure the self-calibration of the SINS without relying on external input.Simulation and experiment results indicate that the method can accurately estimate all errors in mooring state,and is consistent with the calibration results of the static base,which has practical application value.
作者 刘凯 万少巍 王激扬 于峰 LIU Kai;WAN Shao-wei;WANG Ji-yang;YU Feng(Beijing Institute of Aerospace Control Device,Beijing 100039,China;Ordance Equipment Bureau of Naval Equipment Department,Beijing 100163,China;No.91550 Troops of PLA,Dalian 116023,China)
出处 《激光与红外》 CAS CSCD 北大核心 2020年第3期344-349,共6页 Laser & Infrared
关键词 系泊状态自标定 光纤陀螺捷联惯导系统 KALMAN滤波 内杆臂参数 mooring state calibration FOG SINS Kalman filtering inner lever arm parameters
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  • 1方广有,张忠治.探地雷达最优工作信号与脉冲波形畸变的整形技术[J].电波科学学报,1994,9(1):12-17. 被引量:7
  • 2陆志东,王磊.捷联惯导系统的空中标定方法[J].中国惯性技术学报,2007,15(2):136-138. 被引量:31
  • 3Simon Haykin.自适应滤波器原理[M].北京:电子工业出版社,1998:1-56.
  • 4余济祥.卡尔曼滤波及其在惯性导航中的应用[M].西安:西北工业大学出版,1984:1-22.
  • 5王宇.机抖激光陀螺捷联惯导系统的初步探索[D].中国优秀博硕士学位论文全文数据库,2005,(11):69-76.
  • 6Grewal M S, Henderson V D, Miyasako R S. Appli- action of Kalman filtering to the calibration and align- ment of inertial navigation systemiCS. Proceedings of tKZXhe 29th Conference on Decision and Control. Hono- lulu, Hawaii, 1990, 12: 3325-3334.
  • 7Saab S S, Gunnasson K T. Automatic aligment and calibration of an inertial navigation system[C]. IEEE PLANS'94, 1994: 845-852.
  • 8Camberlein L. Calibration technique for laser gyro strap-down inertial navigation system[C]. Symposi-um Gyro Technology, 1985.
  • 9杨小霞,黄一.激光陀螺捷联惯导系统的系统级标定方法研究[J].Proceedings of the 26 Chinese Con-trol Conference, 2007.
  • 10Bekkeng,Jan K.Calibration of a novel MEMS inertial reference unit. IEEE Transactions on Instrumentation and Measurement . 2009

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