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1)  Unscented Kalman Filte(UKF) algorithm
无迹卡尔曼滤波算法
2)  Unscented kalman filter(UKF)
无迹卡尔曼滤波
1.
The unscented Kalman filter(UKF) model for the system is built up,and a numerical simulation is performed with the software Matlab.
设计了一种采用陀螺罗经和多普勒速度仪组合加GPS间歇校正的水下航行器组合导航系统,建立了该组合导航系统的无迹卡尔曼滤波模型,并利用MATLAB软件对其进行了数学仿真验证。
2.
We aim to eliminate these shortcomings as much as possible with a different and we believe better method by using the unscented Kalman filter(UKF) based SLAM(simultaneous localization and mapping) technique.
针对应答器未校准情况下的水下长基线定位问题,提出了基于无迹卡尔曼滤波的同步定位与地图创建方法。
3.
Its core consists of:(1) we design a variable structure sliding-mode speed controller and a variable structure sliding -mode current controller to replace the traditional speed PI controller and two current PI controllers;(2) we design the unscented Kalman filter(UKF) observer to estimate direct-axis current,quadrature-axis current,load torque,rotor position and speed simultaneously.
针对电机控制中采用的PI调节器对电机参数变化及外加干扰时鲁棒差和无位置传感器控制实现困难等问题,在研究常规永磁同步电机矢量控制策略的基础上,将滑模变结构控制(VSSMC)和无迹卡尔曼滤波(UKF)引入该策略中,用VSSMC分别替代策略中速度PI控制器和2个PI电流控制器,同时利用UKF对电机定子直轴电流、交轴电流、负载转矩、转子位置和转速进行实时估计,提出了一种新颖的基于VSSMC和UKF的永磁同步电机无传感器矢量控制方案。
3)  UKF
无迹卡尔曼滤波
1.
In view of the problem that determination of relative attitude between formation satellites is difficult,a modified Unscented Kalman Filter(UKF)was adopted to design the Filter of system in the paper.
针对编队卫星相对姿态确定问题,采用一种改进的无迹卡尔曼滤波UKF进行了系统滤波器设计,根据UKF滤波器的性质,推导出了适用于编队卫星相对姿态确定的UKF滤波算法。
2.
The Standard Kalman Filter can not solve the nonlinear mathematic model,and the Extending Kalman Filter(EKF) will consume much more calculation,so Unscented Kalman Filter(UKF) is adopted in this system.
由于标准卡尔曼滤波不能处理非线性模型,而扩展卡尔曼滤波有计算量大等缺点,故采用无迹卡尔曼滤波(UKF)进行处理。
4)  unscented Kalman filter
无迹卡尔曼滤波
1.
Application of unscented Kalman filter to novel terrain passive integrated navigation system;
无迹卡尔曼滤波在新型地形无源组合导航系统中的应用(英文)
2.
Based on combination of sampling importance resampling(SIR) and unscented Kalman filter(UKF),a novel particle filter is proposed,possessing the merits of high utility efficiency of particles in unscented particle filter(UPF) and of simple operation in SIR,and overcoming the drawback of the rate of increase of computational cost being faster than that of state dimension in UPF.
将采样重要再采样(SIR)方法与无迹卡尔曼滤波(UKF)相结合,提出一种新的粒子滤波算法。
3.
This paper introduces the newly proposed unscented Kalman filter (UKF).
无迹卡尔曼滤波算法(UFK)以少量的采样点表示随机变量的分布,通过非线性系统传播,能以三阶精度获得非线性变换的均值和协方差的估计。
5)  Unscented Kalman filtering
无迹卡尔曼滤波
1.
In view of the influence of non-linear measurement equation on precision and stability of filtering in target tracking application,this paper especially analyzes the basic principle,characteristics and adaptive conditions of model-linearization filtering algorithm,unscented Kalman filtering(UKF)algorithm and particle filtering(PF)algorithm.
针对目标跟踪实际应用中量测方程非线性对滤波精度和稳定性的影响,重点分析了模型线性化的滤波算法、无迹卡尔曼滤波(UKF)和粒子滤波算法(PF)的基本原理和特点以及适应的条件。
6)  Kalman filter algorithm
卡尔曼滤波算法
1.
Therefore,we transform the rotational velocity of propeller to the speed of AUV,use the method of data fuse and presents a Kalman filter algorithm of AUV/SINS integrated navigation to reduce navigation error.
针对由于复杂海洋环境导致的DVL失效,使整个导航精度急剧下降的情况,该文将螺旋桨转速变换成AUV航速,利用航速惯导组合系统信息融合方法,提出了一种通过航速惯导组合导航的卡尔曼滤波算法,可以减小导航误差。
2.
Kalman filter algorithms for bearing-only target tracking are discussed.
本文介绍了纯方位目标运动分析的卡尔曼滤波算法,利用Lyapunov稳定性理论,通过计算算法的稳定性度量值,对三种卡尔曼滤波算法的稳定性进行了分析讨论,并通过仿真计算对各方法的估计性能进行了比较。
3.
Adaptive α-β filter algorithm was introduced,and then it was compared to LSR filter algorithm and Kalman filter algorithm,the mean square deviation of distance,position,speed and direction of these algorithms on the flight line was analyzed to discuss the specific use of the three filters in straight-line flight and about-sh.
介绍了一种改进的α-β滤波算法,然后将它和最小二乘滤波算法、卡尔曼滤波算法进行比较,对三种算法跟踪空中目标的直线飞行、改变航向的直线飞行两种情况的距离、方位、速度和航向等参数的均方差加以分析,证明了改进的α-β滤波算法在直线飞行模型下有着很好的综合效果,且计算量小,更有利于系统建模与仿真。
补充资料:卡尔曼滤波
      见波形估计。
  

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