角速度与加速度仿真

说明：  惯性导航系统是以陀螺和加速度计为敏感器件的导航参数解算系统，该系统根据陀螺的输出建立起导航坐标系，根据加速度计输出解算出运载体的速度和位置。本程序依据比力坐标变换和姿态阵解算的方法，利用MATLAB仿真捷联式惯导系统中陀螺和加速度计的输出，得到角速度和加速度仿真数据。 本仿真可作为课程学习的参考例程，也可作为撰写期刊论文的基础例程，“main_model.m”是主程序，各子模块均有注释。(Inertial navigation system (INS) is a navigation parameter calculation system with gyroscope and accelerometer as sensitive devices. The navigation coordinate system is established according to the output of gyroscope, and the speed and position of carrier are calculated according to the output of accelerometer. According to the method of specific force coordinate transformation and attitude matrix calculation, the output of gyro and accelerometer in strapdown inertial navigation system is simulated by MATLAB, and the simulation data of angular velocity and acceleration are obtained. This simulation can be used as a reference routine for course learning and basic routine for writing journal papers_ Model. M "is the main program, and each sub module is annotated.)

AttitudeAngle2Cbn.m, 619 , 2018-04-08
Data_fb_Wibb.mat, 17135252 , 2018-04-08
diffAtt2Wnbb.m, 706 , 2018-04-08
get_fb_Wibb.m, 3060 , 2018-04-08
main_model.m, 952 , 2018-04-08
update_geoinf.m, 962 , 2018-04-08
Wnbb2Wibb.m, 675 , 2018-04-08