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光纤SINS/GPS组合导航系统分析
引用本文:霍庚,杜军波,丁宏升,隋振.光纤SINS/GPS组合导航系统分析[J].吉林大学学报(信息科学版),2012,30(2):144-150.
作者姓名:霍庚  杜军波  丁宏升  隋振
作者单位:1.中国人民解放军92941部队95分队,辽宁 葫芦岛 125001;2.吉林大学 通信工程学院,长春130025
摘    要:为提高光纤陀螺捷联惯导系统的精度,以光纤陀螺捷联惯导系统与全球定位系统(GPS Globle Position System)为研究对象,采用联邦卡尔曼滤波算法,构成了SINS/GPS(Strap-down Inertial Navigation Systerm/ Globle PositionSystem)组合导航系统。仿真结果表明,该算法能及时修正子滤波器的偏差,大大降低子滤波器的模型误差,进而提高整个滤波器的精度,并有效克服了滤波发散现象。

关 键 词:光纤陀螺  捷联惯导  组合导航  联邦卡尔曼滤波  
收稿时间:2011-08-19

Analysis and Study of Optical SINS/GPS Integrated Navigation System
HUO Geng , DU Jun-bo , DING Hong-sheng , SUI Zhen.Analysis and Study of Optical SINS/GPS Integrated Navigation System[J].Journal of Jilin University:Information Sci Ed,2012,30(2):144-150.
Authors:HUO Geng  DU Jun-bo  DING Hong-sheng  SUI Zhen
Institution:1.Element 95,Unit 92941 of Pepole’s Liberation Army,Huludao 125001,China;2.College of Communication and Engineening,Jilin University,Changchun 130025,China
Abstract:In order to improve the accuracy of SINS(Strap-down Inertial Navigation Systerm).The optical SINS and the GPS(Globle Position System) have been the objects of the study,and adopt the kalman filtering algorithm,constituting of the integrated system.The simulation shows that the integrated navigation system improves the precision of navigation system by correcting the subfilter offset timely and reducing the subfilter model error.especially overcoming filter diverging problem.
Keywords:fiber optic gyroscope  strap-down inertial navigation systerm(SINS)  integrated navigation  kalman filter
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