搜索资源列表
SINS_Kalman
- 卡尔曼滤波程序 GPS/INS 组合导航例子-the Kalman filter GPS/INS integration algorithm of GPS/INS
pose_estimator_6dof.tar
- This is an Adaptation of Stergios Roumeliotis 6 DOF Extended Kalman Filter. Includes classes for incorporating odometers, motors, GPS, accelerometers and gyroscopes. These classes were used to control the NASA Mars Rover-This is an Adaptation of Ster
GPS_INS_navigation
- GPS/INS Integration 未使用Kalman Filter -GPS/INS Integration unused Kalman Filter
High-Dynamic-Carrier-Tracking-Using-Kalman-Filter.
- GPS信号的基带处理在IEEE发表的文章有关信号捕获和跟踪的-GPS baseband signal in the IEEE published articles related to signal acquisition and tracking of
GLOBK_Ref_10.3
- 对地观测数据的卡尔曼滤波器，详细叙述了数学模型和软件操作过程，GPS编程进阶材料-Earth observation data, Kalman filter, the mathematical model described in detail the process and software, GPS Programming Advanced Materials
INSGPS
- 本文介绍了GPS和工NS的基本原理和组成，建立了组合导航系统误差模型，推导了 惯性导航系统误差方程，主要研究了INS/GPs组合导航中卡尔曼滤波技术的应用问题。-This thesis introduces basic principle and composition of GPS and INS， infers the system error equations，getstheerrormode，studiesaPPlicationof Kalman filtering in
KALMAN_GPS
- 利用卡尔曼滤波实现的GPS动态定位的程序，可以获得速度和位置-Using the GPS Kalman filter is the dynamic positioning of the program, get the speed and position
EKF_MEMS
- 姿态信息是飞行控制中最关键的参数之一,因此姿态测量成为飞行控制系统首要解决的问题。利用多MEMS传感器研制了一种微型姿态测量系统。利用三轴MEMS加速度计和三轴MEMS陀螺数据,由方向余弦矩阵的姿态表示形式推导了扩展Kalman滤波方程,解算出飞行器的俯仰角和横滚角 设计专家系统判断飞行器的运动状态,并根据该状态调整滤波算法中的测量噪声矩阵,使系统可同时满足静态情况和动态情况的使用 利用空速和高度数据对俯仰角进行修正,利用GPS解算航向角。将实验结果与国外最新 的商用自动驾驶仪的姿态结果进行
GPSandINS
- 基于卡尔曼滤波的无人驾驶飞机GPS和INS导航系统模拟机仿真程序。-Kalman filter-based unmanned aircraft GPS and INS navigation system simulator emulator.
Loosecombination
- 组合导航中INS与GPS松组合的程序 Kalman滤波器-INS and GPS navigation in the loose combination of the Kalman filter procedure
binary_orbit
- kalman filter for gps
A-Kalman-filter-updating-method-
- 利用kalman滤波实现GPS定位精度的提高-GPS positioning using kalman filter to improve the accuracy achieved
Adaptive-Kalman-Filtering-for-INS-and-GPS.pdf
- Adaptive Kalman Filtering for INS and GPS
GPS
- Integration of Inertial Navigation System and Global Positioning System Using Kalman Filtering
Kalman-_ltering-for-GPS-navigation
- 用卡尔曼滤波器处理GPS航迹的导航系统的数据。-Kalman filter to deal with the navigation system of GPS track data.
kalman
- GPS变形监测动态数据处理中卡尔曼滤波的应用-gps monitor kalman filter data process application dynamic
Tracking-of-Weak-GPS-Signals
- 针对全球定位系统( GPS) 的微弱信号跟踪容易失锁问题, 提出一种新的跟踪方法. 利用平方根卡尔曼滤波算法, 在运算过程中运用误差协方差矩阵的平方根形式进行迭代, 有效减小了舍入误差带来的影响. 提出了一种新的GPS 信号跟踪测量模型, 在连续积分的基础上, 加入了非连续积分过程, 通过有效处理, 避免了导航信息位翻转对信号相关运算产生的影响-Weak signal tracking for the Global Positioning System (GPS), easy to loss o
gps_kalman
- GPS接收机中的采用卡尔曼滤波实现定位解算的MATLAB代码-Kalman filter is used to achieve the positioning solver MATLAB code GPS receiver
GPS_SINS
- 几个用C++编写的关于GPS捷联惯性组合导航的程序，采用kalman滤波(Several programs written in C++ about GPS strapdown inertial integrated navigation, using Kalman filtering)
KalmanFilter_GPS_INS
- 该程序基于MATLAB平台编写，实现了GPS/INS基于位置松组合的卡拉曼滤波算法，分为两部分，GPS_INS.m为组合算法主文件，输入捷联惯导平台实测数据，设置各量测噪声参数，在调用卡尔曼滤波函数进行数据融合校正，最后实现绘图功能；kalman_GPS_INS.m 为卡拉曼滤波程序，输入量测误差以及各噪声参数可得位置和速度估计值。(The program is based on MATLAB platform, and realizes the Kalman filtering algori