《捷联式惯导系统动静基座初始对准》共分13章。第1章简述了捷联式惯导系统的基本原理和初始对准的要求与特点；第2章论述了捷联式惯导系统的误差方程、可观测性和可观测度分析方法以及最优估计理论；第3章讲述了捷联式惯导系统静基座初始对准的实现方法；第4章讲述了捷联式惯导系统静基座多位置初始对准方法；第5章讲述了捷联式惯导系统晃动基座的初始对准方法；第6章讲述了捷联式惯导系统动基座传递对准理论与方法等。

捷联式惯导系统的算法是指从惯性器件的输出到给出需要的导航和控制信息所必进行的全部计算问题的计算方法，在本程序中使用四元数法和旋转矢量法。

sins，初始对准，捷联惯导，matlab，程序，精对准；粗对准；

捷联惯导matlab程序求解飞行器姿态，依据加速度计和陀螺仪的输出数据来求解飞行器的姿态，可以输出速度，经纬度

捷联惯导的解算程序，是MATLAB编程的源代码，分享给大家看看

捷联惯导系统静基座初始对准 MATLAB

用IMU的数据进行机器人位置和姿态的估计，比如acc或者gyro积分每个sample怎么进行坐标变换，怎么由rawdata得到位置和姿态信息的计算细节等。 In recent years, microelectromechanical system (MEMS) inertial sensors (3D accelerometers and 3D gyroscopes) have become widely available due to their small size and low cost. Inertial sensor measurements are obtained at high sampling rates and can be integrated to obtain position and orientation information. These estimates are accurate on a short time scale, but suer from integration drift over longer time scales. To overcome this issue, inertial sensors are typically combined with additional sensors and models. In this tutorial we focus on the signal processing aspects of position and orientation estimation using inertial sensors. We discuss dierent modeling choices and a selected number of important algorithms. The algorithms include optimization-based smoothing and ltering as well as computationally cheaper extended Kalman lter and complementary lter implementations. The quality of their estimates is illustrated using both experimental and simulated data.

高精度捷联惯性导航系统Matlab工具箱

用四元数法进行姿态解算的matlab程序。

捷联惯性导航系统的一个仿真实现，基于MATLAB的，仿真出一个捷联系统的跟踪轨迹，是三维的，同时生成了经度误差，维度误差和高度误差，可以直接运行，不行 我退积分