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国外关于GPS与INS组合导航的一篇新文章,涉及到GPS数据与INS数据的融合,卡尔曼滤波器设计和仿真思路-abroad on GPS and INS navigation combination of a new article, relate to the GPS data with the INS data fusion, Kalman filter design and simulation ideas
Update : 2025-04-04 Size : 280kb Publisher : 阳文

读取TXT文档里的GPS数据卡尔曼滤波程序,对于初学者很有帮助-TXT file to read GPS data in the Kalman filter procedure, very helpful for beginners
Update : 2025-04-04 Size : 1kb Publisher : 姜玉林

本压缩文件包含GPS量测数据仿真和惯性导航解算以及卡尔曼滤波在导航解算中的应用-The compressed file contains the GPS measurement data simulation and inertial navigation and Kalman filter solver solver in the navigation application
Update : 2025-04-04 Size : 11kb Publisher : neargdd

捷连惯导和GPS组合导航,利用kalman滤波进行数据融合并输出-Jie Lian INS and GPS navigation, the use of kalman filter for data fusion and output
Update : 2025-04-04 Size : 1kb Publisher : 爱爱

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
Update : 2025-04-04 Size : 361kb Publisher : 张明

通过卡尔曼滤波并采用开环控制方式实现惯性导航和GPS的数据融合-Through the Kalman filter and use the open-loop control method to achieve inertial navigation and GPS, data fusion
Update : 2025-04-04 Size : 4kb Publisher : dj

本文主要介绍了用模糊自适应卡尔曼滤波技术实现惯导和GPS的数据融合。-This paper presents a fuzzy adaptive Kalman filter technology for inertial navigation and GPS-data fusion.
Update : 2025-04-04 Size : 348kb Publisher : dj

kalman滤波用于GPS数据处理,本人已用过,非常好的源码-calman filter for GPS data processing,I have used, very good source
Update : 2025-04-04 Size : 11kb Publisher : 吴哥

GPS的MATLAB仿真程序,仿真了读取导航电文信息、卡尔曼滤波、解算定位等功能。-GPS for MATLAB simulation, emulation of the read navigation data information, Kalman filter, calculate the positioning function.
Update : 2025-04-04 Size : 47kb Publisher : wushumin

通过卡尔曼滤波算法对INS和GPS数据进行联合解算,获取解算数据 -Kalman filter algorithm by INS and GPS data for the United Solution, solving the data access
Update : 2025-04-04 Size : 300kb Publisher : 向华强

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了比较,二者在静态情况下非常吻合,在动态情况下基本吻合。 - The attitude information is one of the most important parameters in flight control systems. This paper describes an attitude measurement system based on a MEMS multi-sensor. The data from 3-axis MEMS accelerators and 3-axis MEMS gyros is used to determine the pitch angle and the roll angle of the air vehicle using an extended Kalman filter (EKF) equation deduced from the direction cosine matrix. An expert system was designed to estimate the vehicle motion to adjust the measurement noise matrix of the extended Kalman filter equation so that the system can be used in dynamic as well as static environments. The measured airspeed and altitude are also used to revise the pitch angle. The heading is determined from GPS information. Test results compare well with an imported commercial autopilot in a static test with less accurate results in a dynamic test.
Update : 2025-04-04 Size : 49kb Publisher : cisca

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.
Update : 2025-04-04 Size : 956kb Publisher : 刘桂辛

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
Update : 2025-04-04 Size : 57kb Publisher : abc

研究GPS与INS数据融合编程卡尔曼滤波算法-Study of GPS and INS data fusion programming Kalman filter algorithm
Update : 2025-04-04 Size : 622kb Publisher : 孙冬凯

Altitude location for UAV by using federated filter is discussed, the fourth structure is selected, because its two sub-filters involving altitude sensor and the difference Global Positioning System (d-GPS) respectively are fully isolated from each other and thus make the federated filter more fault-tolerant and better in real-time performance. Data fusion based on this federated filter was simulated. When the d-GPS is working normally and simulation results show that values estimated by data fusion base on federated filter are very close to real values and the variance of federated filter converges to 10m. When the electromagnetic environment is very bad, as is usually the case in war zone, the d-GPS is silent for a long time, variance based on federated filter converges to 13m, bigger than the 10m. Compared with previous paper variance based on Kalman converges to 15m, higher than the 13m. Federated filter can give much more accurate estimation than Kalman filter.
Update : 2025-04-04 Size : 321kb Publisher : Clovis

DL : 0
星历仿真,数据读取,定位,kalman及自适应kalman滤波-Ephemeris simulation, data reading, positioning, Kalman and adaptive Kalman filter
Update : 2025-04-04 Size : 47kb Publisher : Kevin Lucas

卡尔曼滤波GPS静动态滤波实验的实验程序和数据-The kalman filter for GPS static and dynamic experimental program and data filtering experiment
Update : 2025-04-04 Size : 64kb Publisher : s

GPS/INS组合导航位置校正仿真程序,能够仿真减少位置误差(His finishing some classic papers about kalman filtering, data and programs, for beginners of kalman filter has a lot of help.)
Update : 2025-04-04 Size : 620kb Publisher : 007amw

对于组合导航的学习,需要先了解kalman滤波算法,ins/gps组合导航运用的最多的数据融合算法就是kalman(For integrated navigation learning, need to understand the kalman filter algorithm, ins/GPS integrated navigation using most of the data fusion algorithm is kalman)
Update : 2025-04-04 Size : 3kb Publisher : eloquent

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 algorithm of GPS/INS based on position loosening combination. It is divided into two parts. GPS_INS.m is the main file of the combined algorithm, inputs the measured data of the strapdown inertial navigation platform, sets the measurement noise parameters, and carries out data fusion correction by calling the Kalman filter function, and finally realizes the drawing. Function; kalman_GPS_INS.m is Kalman filter program, input measurement error and noise parameters can be estimated position and velocity.)
Update : 2025-04-04 Size : 619kb Publisher : 不知晓
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