中文说明：《导航原理》课程中的捷联惯导程序，依据加表和陀螺仪的输出数据来求解飞行器的姿态，已经完成调试，可进行计算
English Description：
Strapdown inertial navigation principle in the course of proceedings, according to add tables and output data to solve the aircraft attitude gyros, have finished debugging, and can be calculated