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捷联惯导系统/里程计自主式车载组合导航系统研究
引用本文:丁文娟,李岁劳,熊伟.捷联惯导系统/里程计自主式车载组合导航系统研究[J].航空计测技术,2006,26(1):14-16.
作者姓名:丁文娟  李岁劳  熊伟
作者单位:西北工业大学自动化学院,陕西西安710072
摘    要:利用里程计辅助捷联惯导系统构成一种完全自主式的车载组合导航系统.本文详细推导了里程计的速度误差方程.用捷联惯导系统解算出的速度量和里程计所测量的速度量之差作为组合导航系统卡尔曼滤波器的观测量,利用闭环卡尔曼滤波技术进行误差估计与校正,并给出了系统仿真结果.仿真结果表明该组合导航系统可有效地减小姿态、速度、经度和纬度等导航参数的误差累积.

关 键 词:捷联惯导系统  里程计  组合导航  卡尔曼滤波
文章编号:1002-6061(2006)01-0014-03
收稿时间:2005-06-01
修稿时间:2005年6月1日

Research on SINS/OD Independently Integrated Navigation System for Land Vehicles
DING Wen-juan,LI Sui-lao,XIONG Wei.Research on SINS/OD Independently Integrated Navigation System for Land Vehicles[J].Aviation Metrology & Measurement Technology,2006,26(1):14-16.
Authors:DING Wen-juan  LI Sui-lao  XIONG Wei
Abstract:An independently integrated navigation system using odometer(OD) to assist the strapdown inertial navigation system(SINS/OD) is discussed.In this paper,the OD error equations are proposed in detail.The observed quantity of the SINS/OD is the velocity's differences between SINS and OD,and the SINS/OD also adopts a closed kalman filter to estimate and correct the errors.The results of simulation indicate that the SINS/OD can effectively eliminate the following errors of navigation parameters:attitude,velocity,latitude and longitude etc.
Keywords:strapdown inertial navigation system  odometer  integrated navigation  kalman filter
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