SATELLITE NAVIGATION SYSTEM ESTIMATION ALGORITHM USING LINEAR KALMAN FILTERING

机译：线性卡尔曼滤波的卫星导航系统估计算法

获取原文

获取原文并翻译 | 示例

页面导航

摘要
著录项
相似文献
相关主题

摘要

A recursive Kalman filter which estimates the user coordinates has been designed, when satellite radio navigation system is used. This filter also makes finding the distance measuring errors (clock bias) resulted from the time differences between user and satellite, possible. Results of performed simulation revealed that the designed filter has worked with high accuracy and has considered both user coordinates and clock bias in real time.

机译：当使用卫星无线电导航系统时，已经设计了一种估计用户坐标的递归卡尔曼滤波器。该滤波器还可以查找由于用户和卫星之间的时间差而导致的距离测量误差（时钟偏差）。进行的仿真结果表明，所设计的滤波器具有很高的精度，并且实时考虑了用户坐标和时钟偏差。

著录项

来源
《Saint Petersburg International Conference on Integrated Navigation Systems; 20030526-28; St.Petersburg(RU)》|2003年|P.167-168|共2页
会议地点 St.Petersburg(RU)
作者
Ch.M.Hajiyev; U.K.Hajiyeva;
展开▼
作者单位

Istanbul Technical University, Faculty of Aeronautics and Astronautics, Istanbul, Turkey;

展开▼
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
satellite radio navigation; kalman filter; linear regression;

机译：卫星无线电导航；卡尔曼滤波；线性回归;

相似文献

外文文献
中文文献
专利

1. Integrated Navigation System Design for Micro Planetary Rovers: Comparison of Absolute Heading Estimation Algorithms and Nonlinear Filtering [J] . Muhammad Ilyas, Beomjin Hong, Kuk Cho, Sensors . 2016,第5期

机译：微型行星漫游器的集成导航系统设计：绝对航向估计算法与非线性滤波的比较
2. Research on Nonlinear Comprehensive Calibration Algorithm for the Single-Axis Rotation Inertial Navigation System Based on Modified Unscented Kalman Filter [J] . Cheng Jianhua, Li Meiling, Guan Dongxue, Journal of computational and theoretical nanoscience . 2017,第3期

机译：基于修改的Unscented Kalman滤波器的单轴旋转惯性导航系统非线性综合校准算法研究
3. Quasi-Optimal Algorithms for Detection, Identification, and Adaptive Estimation for Information Processing in Navigation Systems of Mobile Ground Objects Based on Satellite Radio Navigation Systems [J] . Ivanov A. V., Surkov V. O., Komrakov D. V. Journal of Communications Technology and Electronics . 2020,第6期

机译：基于卫星无线电导航系统的移动地对象导航系统中的检测，识别和自适应估计的准优化算法
4. SATELLITE NAVIGATION SYSTEM ESTIMATION ALGORITHM USING LINEAR KALMAN FILTERING [C] . Ch.M.Hajiyev, U.K.Hajiyeva Saint Petersburg International Conference on Integrated Navigation Systems . 2003

机译：卫星导航系统估算算法使用线性卡尔曼滤波
5. Kinematic Localization for Global Navigation Satellite Systems: A Kalman Filtering Approach [D] . Tabatabaee, Mohammad Hadi. 2017

机译：全球导航卫星系统的运动学定位：一种卡尔曼滤波方法
6. Integrated Navigation System Design for Micro Planetary Rovers: Comparison of Absolute Heading Estimation Algorithms and Nonlinear Filtering [O] . Muhammad Ilyas, Beomjin Hong, Kuk Cho, 2016

机译：微型行星漫游车综合导航系统设计：绝对航向估计算法与非线性滤波的比较
7. Kalman filtering method and its application to air pollution episode forecasting. Kalmanifilters are a class of linear minimum-error-variance sequential state estimation algorithms [O] . P Switzer, P Zannetti 1979

机译：卡尔曼滤波方法及其在空气污染集预测中的应用。 Kalmanifilters是一类线性最小误差 - 方差顺序状态估计算法

SATELLITE NAVIGATION SYSTEM ESTIMATION ALGORITHM USING LINEAR KALMAN FILTERING

摘要

著录项

相似文献

相关主题

期刊订阅