搜索资源列表
CALMAN
- 卡尔曼滤波初始对准,静基座和动基座初始对准-Kalman filter initial alignment, stationary base and moving base initial alignment
sins
- 惯导仿真部分模块化,标准化,分为IMU模块,初始对准模块,SINS解算模块,SINS性能评价模块,SINS解算的输出为地理坐标系内速度、经纬高、姿态角,运行INS_perforEva.m可以得到惯导仿真结果。-INS simulation part modular, standardized, divided IMU module, the initial alignment module, SINS solver module, SINS performance uation module,
kalman_filter2
- 北航研究生课程卡尔曼滤波与组合导航第2题,静基座初始对准-Buaa graduate course kalman filtering and integrated navigation second question, the static base initial alignment
SINS-Alignment-C
- 捷联惯导系统的初始对准的程序,加入了算法描述,方便大家使用。-SINS Alignment programmer
Liru_1_DynamicAlignment_Coarse
- 我们卫星定位导航课中导航中双历元GNSS辅助SINS动态初始对准方法的m文件,只要有测量数据应该就可以实现,大家可以参考一下-Our lesson navigation satellite positioning and navigation double epoch dynamic GNSS assistance SINS initial alignment method m file, as long as the measurement data should be able to ach
KF
- 初始对准是捷联惯导系统进行导航的前提,初始对准的好坏将直接影响到系统的导航精度。捷联惯导系统(SINS)初始对准的本质是确定载体的初始姿态。-The initial alignment of strapdown inertial navigation system is the premise for navigation, initial alignment will directly affect the quality of the navigation system precision.
Kalman
- 捷联惯性导航,利用卡尔曼滤波,matlab程序,关于初始对准-SINS initial alignment procedure Kalman
KF_SINS
- 用于初始对准的卡尔曼滤波程序,包含10个状态量-Kalman filter for initial alignment of programs, with 10 States
ZJY_KF_SINS
- 用于初始对准的卡尔曼滤波程序,包含10个状态量-Kalman filter for initial alignment of programs, with 10 States
Inertial-Navigation-System-program
- 严恭敏老师编写的SINS的Matlab仿真程序,包括大方位误差角扩展卡尔曼(EKF),滤波初始对准仿真,静态惯导/星敏感器组合,大姿态误差角非线性状态模型,UKF滤波。-Yan Gong Min teacher preparation SINS of Matlab simulation program, including large azimuth error extended Kalman (EKF), filtering initial alignment simulation, stat
sins-alignment
- 严恭敏的惯导系统工具箱,有初始对准的相关程序。-Yan Gong Min Inertial Navigation System Toolbox, an initial alignment procedures.
chushiduizhunchengxu
- 实现平台的初始对准,实验中使用非常有效果,并且给出了不同的滤波方法-Achieve initial alignment platform, used in the experiments is very effective, and gives a different filtering methods
PSINS
- 工具箱主要功能: 1) 姿态向量、四元数、矩阵、滤波算法等各类子程序 2) 圆锥运动仿真 划船运动仿真 惯性器件随机误差仿真 3) Kalman滤波初始对准 基于惯性系初始对准 罗经法初始对准 大方位失准角EKF初始对准 大失准角UKF初始对准 速度+姿态传递对准 4) 纯惯性导航SINS仿真 航位推算、SINS/DR仿真 SINS/GPS组合仿真 GPS/BD/GLONASS单点伪距定位 SINS/GPS松/紧组合
KF
- 卡尔曼滤波用于导航解算初始对准过程中的精对准-Kalman filtering
psins151009
- MATLAB 工具箱,可用于惯性导航的常用模拟,包括器件误差、平台误差、纯惯导解算、惯导与GPS融合、惯导与DR融合、初始对准等滤波算法-Filtering algorithm MATLAB toolbox can be used to simulate conventional inertial navigation, including device error, error platform, Inertial Navigation solver, INS and GPS integrat
stukf
- 此程序是运用强跟踪UKF滤波实现捷联惯导实现初始对准,可以仿真数据,如果有实验数据也可以用!效果还可以。-This procedure is the use of strong tracking UKF SINS to achieve the initial alignment, simulation data, if the experimental data can be used! Effect can also be.
duizhun
- 初始对准程序从别人那儿看来的,觉得同不错 -SINS dasdasd
SINS
- 捷联惯导初始对准的C源码 -SINS initial alignment of the C source, including
aim-at
- 捷联惯导初始对准程序matlab,精对准-Strapdown inertia initial alignment program matlab, fine alignment
捷联惯导及其组合导航研究
- 本文对捷联惯导系统(sINS)及其与全球定位系统(GPS)的组合导航系统进行 了研究。首先对实现S取S的初始对准及姿态矩阵计算等关键技术进行了系统研究。 在仿真的基础上进行了实际捷联惯导系统的系统研制,针对陀螺漂移补偿等关键算法 开展深入研究,实验结果表明经过补偿解算后,整个捷联惯导系统导航参数的解算精 度大大提高。在实现SINS的基础土,研究了SINS与GPS(The strapdown inertial navigation system (sINS) and global posi