搜索资源列表
SINS_Kalman
- 捷联惯性导航系统、GPS/SINS组合导航系统仿真程序-Strapdown inertial navigation systems, GPS/SINS Integrated Navigation System Simulation Program
toolofINS
- 惯性导航系统工具箱 能有效帮助仿真惯性导航系统-Inertial navigation system simulation toolbox can be effective in helping inertial navigation system
navigation
- 一本很不错的关于惯性导航的书籍，对惯性基本方程以及算法编程，都有很好的说明。-A very good book on the inertial navigation, the basic equation of the inertia and the algorithm programming, have a good explanation.
EKFsins
- 捷联惯性导航系统的卡尔曼滤波对准程序，非常有用-alignment sins
EKF_5order
- EKF在捷联惯性导航系统初始对准中的应用？在方位角为大失准角的情况下，如何进行初始对准-EKF in SINS Initial Alignment? In the azimuth misalignment angle for the big cases, how to initial alignment
navi_test
- 惯性导航的MATLAB算法，根据陀螺与加表的值计算姿态-MATLAB inertial navigation algorithm, based on gyro and attitude add value table
NEW
- 基于四元数法的捷联惯性导航系统姿态解算及正弦输入函数的生成-Quaternion-based strapdown inertial navigation system attitude solution and the generation of sinusoidal input function
simulation
- MATLAB_Simulink的捷联惯性导航系统仿真-MATLAB_Simulink of strapdown inertial navigation system simulation
progen
- 惯性导航轨迹生成器，用于生成惯性导航轨迹-INS trajectory generator, used to generate the inertial navigation path
dazuoye2
- 惯性导航误差方程的建立，系统误差传播特性分析(Establishment of inertial navigation error equation and analysis of system error propagation characteristics)
51622443trace_generate
- c语言编写的惯性导航系统轨迹发生器，用于结算惯性导航系统(inertial navigation system)
strapdown
- 捷联惯性导航数据分析，很基础的程序代码，有助于初学者理解(Strapdown inertial navigation data analysis)
四旋翼PID-科特斯积分
- 利用科特斯积分计算高精度惯性导航 stm32f407单片机 四旋翼飞行器(High precision inertial navigation using integral Cortez)
新建文件夹
- 捷联惯性导航的简单程序，可以直接使用的代码，希望可以帮到大家(Strapdown inertial navigation of simple procedures, you can directly use the code, I hope you can help everyone)
psins151009
- 惯性导航分析工具箱 matlab工具箱 组合导航 卡尔曼滤波(this toolbox can be used to analysis the navigation system and assist to do some simulation on navigation system.)
GPS_ins_mag_int_sim
- 惯性导航，磁罗盘，卫星导航相互组合，采用联邦滤波算法。(Inertial navigation, magnetic compass and satellite navigation are combined, and federated filter algorithm is adopted.)
fyanggundonghenggunjisuan
- 主功能就是解算惯性导航中的姿态角，通过解算四元数来求解横滚角，航向角，俯仰角(The main function is to calculate the attitude angle in inertial navigation)
惯性导航四元数法
- 主要利用四元数来解算姿态角，并实时更新四元数，然后实时更新姿态角。(The attitude angle is calculated by four variables, and the four variables are updated in real time, and then the attitude angle is updated in real time.)
惯性导航中加速度计和陀螺仪性能研究_徐东升
- 通过利用陀螺仪数据来解算和更新四元数，进而来计算姿态角。(The attitude angle is calculated by using the gyro data to solve and update the number of four variables.)
Factor Graph in Inertial Navigation Systems
- 利用因子图和积算法设计的无人机惯性导航系统算法，利用matlab仿真实现(An algorithm of unmanned aerial vehicle (UAV) inertial navigation system designed by factor diagram and calculation method is realized by MATLAB simulation)