搜索资源列表
SINS-MATLAB
- 一个捷联惯导系统的骨干程序，包括四元数计算，姿态更新，速度更新，经纬度计算等。-A main part SINS program, including quaternion calculation, attitude updates, update speed, latitude and longitude calculation.
Kalman_sins_alignment
- 一个捷连惯性导航系统的初始对准仿真程序，其设计依据详见《捷联惯导系统初始对准滤波技术研究》，该论文通过CK可以方便下载。-This is a simulation program of initial alignment of inertial navigation system, its design basis as described in SINS initial alignment filtering technology research , the paper can be ea
Strapdown
- 捷联惯性导航算法完整版（单子样姿态解算算法）-Strapdown inertial system
Matlab
- 捷联惯导数据计算的详细功能、包含内容说明，原始代码。-Detailed features SINS computing, including the content descr iption, source code is in these two a
666matlab.m
- 捷联惯导力学编排解算，很好的一段小程序，希望帮的到大家-SINS mechanical choreography solver
guandaojiesuan
- 捷联惯性导航解算程序，很有实用价值。对研究捷联惯性导航很有用。-SINS solver, very practical value. Inertial navigation is useful for the study of the Czech Republic.
Quaternion
- 应用四元数算法进行了捷联惯性导航的计算，并对比真值得到误差-Application quaternion algorithm SINS calculations and compare the true worth to the error
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
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.
dual_2
- 惯性导航系统误差仿真，针对捷联惯导系统的误差方程进行仿真，得到误差曲线-error simulation
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
SINS
- 严恭敏：基于matlab的捷联惯导算法设计与仿真-SINS algorithm design and simulation
mpu6050-program
- 陀螺仪姿态解算 四元数 捷联矩阵的初始值计算初始四元数值 用毕卡法求解四元数更新矩阵，即捷联矩阵-Gyro attitude solution
strapdown_kem
- 在导航应用上捷联惯导时对准中的卡尔曼滤波算法程序，是方差最小，无偏性的，实用性很强的估计算法-In the navigation application when SINS Alignment Kalman filter procedure is the minimum variance, unbiased, and very practical estimation algorithm
Kalman1
- 捷联惯性导航Kalman小失准角精对准程序-SINS Kalman small fine misalignment angle alignment procedure
INStoolSim
- 里面主要是捷联惯导算法程序，另外还有很多例子可供参考-strap inertial navigation systerm
imu
- 通过上位机经过串口对于捷联惯导系统的三个陀螺进行标定以及寻北运算。-Through the PC via the serial port for the three GFSINS system calibration and north-seeking operations.
instest
- 捷联惯导程序，十分实用，输出经纬度、高度以及姿态角信息。仿真效果不错，亲测可用，只需输入陀螺加速度计测量值即可-SINS program, very practical, simulation results are good, pro-test available, simply enter gyroscopic accelerometer measurements can be
DirectionCosin
- 载体的姿态解算算法是实现捷联式惯性导航系统精确导航的核心技术之一，采用了标准方向余弦法求解惯性导航的位置姿态-Carrier attitude algorithm of the algorithm is to achieve strapdown inertial navigation system is one of the core technology of accurate navigation, using the standard method of direction cosine
RotationVector
- 载体的姿态解算算法是实现捷联式惯性导航系统精确导航的核心技术之一，采用了标准旋转矢量法求解惯性导航的位置姿态-Carrier attitude algorithm of the algorithm is to achieve strapdown inertial navigation system is one of the core technology of accurate navigation, using the standard rotation vector method to s