INTEGRATING INFORMATION IN INTEGRATED NAVIGATION SYSTEM WITH LASER GYROS BASED ON EXTENDED KALMAN FILTER

机译：基于扩展卡尔曼滤波的激光陀螺综合导航系统信息集成

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Realization of algorithm for integrating the information in the integrated navigating system is offered. Together with an estimation of navigating parameters the sensors errors identification is carried out. Advantage of the used extended Kalman filter is more full account of object dynamics due to inclusion navigating parameters in a state vector. Features of practical realization of algorithm are listed. These features are connected with synchronization by the satellite and menial Information, and also division of the information processing on two channels with various speeds of calculations. Criteria of check of efficiency of the integrating the information in navigating system are formulated.

机译：提供了在集成导航系统中集成信息的算法的实现。连同导航参数的估计一起，进行传感器错误识别。由于在状态向量中包含导航参数，因此使用扩展卡尔曼滤波器的优势是可以更全面地考虑对象动力学。列出了算法的实际实现特点。这些功能与卫星和卫星信息的同步连接在一起，并且在两个通道上以不同的计算速度划分信息处理。制定了导航系统中信息集成效率的检验标准。

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来源
《Saint Petersburg International Conference on Integrated Navigation Systems; 20030526-28; St.Petersburg(RU)》|2003年|P.179-181|共3页
会议地点 St.Petersburg(RU)
作者
A.A.Fomitchev; V.B.Uspensky; K.Yu.Schastlyvets; Yu.Yu.Broslavets; A.B.Koltchev;
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作者单位

JSC 'Lasex', Institutsky per. 9, Dolgoprudny Moscow Area;

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会议组织
原文格式 PDF
正文语种 eng
中图分类导航设备;
关键词
extended filter; navigation; algorithm;

机译：扩展滤波器;导航;算法;

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1. Improved high-degree cubature Kalman filter based on resampling-free sigma-point update framework and its application for inertial navigation system-based integrated navigation [J] . Cui Bingbo, Wei Xinhua, Chen Xiyuan, Aerospace science and technology . 2021,第Octa期

机译：基于重采样的Sigma-Point更新框架改进的高度Cubature Kalman滤波器及其应用于基于惯性导航系统的集成导航
2. Extended Kalman filter synthesis for integrated global positioning/inertial navigation systems [J] . Faruqi FA., Turner KJ. Applied mathematics and computation . 2000,第2a3期

机译：扩展的卡尔曼滤波器综合，用于集成的全球定位/惯性导航系统
3. A Performance Comparison of Tightly Coupled GPS/INS Navigation Systems based on Extended and Sigma Point Kalman Filters [J] . J. WENDEL, J. METZGER, R. MOENIKES, Navigation . 2006,第1期

机译：基于扩展和西格玛点卡尔曼滤波器的紧耦合GPS / INS导航系统的性能比较
4. INTEGRATING INFORMATION IN INTEGRATED NAVIGATION SYSTEM WITH LASER GYROS BASED ON EXTENDED KALMAN FILTER [C] . A.A.Fomitchev, V.B.Uspensky, K.Yu.Schastlyvets, Saint Petersburg International Conference on Integrated Navigation Systems . 2003

机译：基于扩展卡尔曼滤波器的激光陀螺集成了集成导航系统信息
5. Using extended Kalman filtering (EKF) to fuse GPS and inertial navigation systems (INS) for land vehicle control. [D] . Zhang, Hao. 2004

机译：使用扩展的卡尔曼滤波（EKF）融合GPS和惯性导航系统（INS）进行陆地车辆控制。
6. A Modified Kalman Filter for Integrating the Different Rate Data of Gyros and Accelerometers Retrieved from Android Smartphones in the GNSS/IMU Coupled Navigation [O] . Wenlin Yan, Qiuzhao Zhang, Lijuan Wang, 2020

机译：用于集成从GNSS / IMU耦合导航中从Android智能手机检索的Gyros和加速度计的不同速率数据的修改后的Kalman滤波器
7. Design and Simulation of the Integrated Navigation System based on Extended Kalman Filter [O] . Zhou Weidong, Hou Jiaxin, Liu Lu, 2017

机译：基于扩展卡尔曼滤波的组合导航系统设计与仿真

INTEGRATING INFORMATION IN INTEGRATED NAVIGATION SYSTEM WITH LASER GYROS BASED ON EXTENDED KALMAN FILTER

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