惯性导航误差分析，附带数据，是word文档，需要自行复制成m文件-Inertial navigation error analysis, ancillary data, word documents, need their own copy into m file

通过matlab调用xfoil程序，对翼型升阻力力矩进行计算，并将计算结果生成结果文件，程序中对三种翼型进行了计算，用户可根据需要删减或复制程序的相同部分即可-Xfoil by calling the same part of matlab procedures, the airfoil lift and drag torque is calculated, and the calculated results file is generated, the program for the thr