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基于EKF的多MEMS传感器姿态测量系统.caj
- 摘 要: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
GPS.rar
- GPS时差数据卡尔曼滤波器 的设计与应用,The time difference between GPS data Kalman filter design and application of
Matlab-Kalman-Filter
- Matlab Kalman Filter 全世界下载次数最多的Matlab程序-Matlab Kalman Filter in Matlab the world' s most downloaded program
Kalman2D
- Simulate GPS tracking Object 2D and smooth its obits by Kalman filter.
GPS数据的卡尔曼滤波处理及其在飞行试验中的应用
- GPS数据的卡尔曼滤波处理及其在飞行试验中的应用。-GPS data, Kalman filtering and its application in flight test.
Gpsins-integration-using-kalman-filter
- Gps/ins integration using kalman filter
An-Integrated-DGPS_IMUh
- 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
Attitude-estimation-
- 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
An-Integration-of-GPS-
- 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
GPS_INS-integration
- 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
Data-Fusion-Approach-for-Altitude-Location-Error.
- 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
MEMS-IMU
- This thesis is to investigate the integration of Precise Point Positioning GPS and low cost MEMS IMU. Both loosely and tightly coupled Kalman filters are developed to derive the optimal navigation solution.Global Positioning System (GPS) and lo
GPS-Global-Positioning-Systems---Inertial-Navigat
- this is signal processig and kalman ffilter
Analysis-Ultra-Tightly-
- 很好的GPS/INS超紧组合导航的文章，关键词：GPS,INS，超紧组合导航，抗干扰-The performance of an Ultra-Tightly Coupled (UTC) Global Positioning System/Inertial Navigation System (GPS/INS) is evaluated using a system simulation of the GPS receiver and navigation processing.
-dynamic-positioning-
- GPS动态定位中卡尔曼滤波模型的建立及其强跟踪算法研究-Establishment of dynamic positioning GPS Kalman filter model and its strong tracking algorithm
KalmanFilter
- 卡尔曼滤波器在GPS导航中的一些应用，包括滤波算法和一些误差分析-Kalman filter in GPS navigation in a number of applications, including filtering algorithms and error analysis of some
RTK GPS
- Many manufacturers of Real-Time Kinematic (RTK) Global Positioning System (GPS) positioning software ignore the temporal correlations found in GPS measurement errors. To understand the statistical value of GPS positions, temporal correlations must be
10.20317_MillerC
- Many manufacturers of Real-Time Kinematic (RTK) Global Positioning System (GPS) positioning software ignore the temporal correlations found in GPS measurement errors. To understand the statistical value of GPS positions, temporal correlations must be