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sins_alignment
- 这是本人编写的一个接联惯性导航系统解析粗对准的仿真程序，其中分别采用了传统和改进的解析对准算法。-This is the one I prepared received Inertial Navigation System Analysis rough at the simulation program, which were used to the traditional and improved analytical alignment algorithm.
INS_GPS_integrated_navigation_system
- 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
GPSSINS
- GPS与惯性导航系统组成的组合导航系统仿真程序-GPS and inertial navigation system consisting of integrated navigation system simulation program
aUKF_align_10state
- 大失准角初始对准。应用UKF进行初始对准； 用于惯性导航初始对准-alignment navigation inertial
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
导航程序
- 惯性导航程序，四元素方法，欧拉角法等。粗对准，精对准，卡尔曼滤波算法
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)
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)
integrated navigation
- 以捷联惯性导航系统为主，添加里程计、卫星成为组合导航的半实物仿真程序(integrated navigation)
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)
67506272integrated_navigation_systems
- 《GNSS惯性导航组合第3版》随书光盘，包括Matlab各章节例程和数据(Integrated GNSS inertial navigation assembly 3rd edition portable CD - ROM)
INSNEW
- 根据给定的数据进行惯性导航的解算，从而确定姿态，速度和位置的更新(The calculation of inertial navigation based on the given data to determine the update of attitude, speed and position)
PDRExperiment
- 惯性走路姿势测步数，以及姿态估计侧姿势，预支手机姿态和惯性感应，手机灵活感应(The step number of the inertial walking posture, and the posture of the attitude estimation side, the mobile phone attitude and the inertial induction, the flexible induction of the mobile phone)
矩阵论例题
- 惯性导航MATLAB程序，里面涉及到四元数算法(Inertial navigation MATLAB program)
2011_inertial-navigation_second
- 2011年秋季 北京航空航天大学惯性导航原理第二次大作业(2011 inertial navigation the second homework of beihang university )
tra011
- 惯性导航解算，得出飞行器的经度纬度高度，陀螺仪和加速度计的值(Inertial Navigation Solution, the longitude, latitude, altitude, gyroscope and accelerometer of the aircraft are obtained.)
daohangthree
- 西工大研一惯性测量实验的粗对准程序以及图示，参考《捷联惯导算法与组合导航原理讲义》(Coarse alignment procedure and graphics for the INS experiment of Xigong University of Technology, refer to the Lecture on Strapdown Inertial Navigation Algorithms and Integrated Navigation Principles.)
exp3
- 车载惯性/卫星组合导航实验，起始时刻车辆停止不动，但车身有一定干扰晃动，10分钟后车辆行驶，采集惯导系统IMU数据、车辆里程计数据、GPS数据等。采用前2分钟数据进行粗对准，后8分钟数据进行精对准，分别得到惯性导航、惯性/GPS组合导航、惯性/里程计组合导航的导航结果。(Vehicle-mounted inertial/satellite integrated navigation experiment: the vehicle stops at the initial moment, but
惯性测量装置IMU的仿真模型
- 惯性测量装置IMU的matlab仿真模型。(Matlab simulation model of IMU.)