Description: Aerodynamic coefficients calculated by missile missile equations of motion of the heart, and using MATLAB graphics, including trajectory, velocity-time curve
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第2题\importfile.m
.....\main2.m
.....\outputdata.txt
daodanfeixinglixue_2\daodanfeixinglixue_2.dsp
....................\daodanfeixinglixue_2.dsw
....................\daodanfeixinglixue_2.ncb
....................\daodanfeixinglixue_2.opt
....................\daodanfeixinglixue_2.plg
....................\Debug\daodanfeixinglixue_2.exe
....................\.....\daodanfeixinglixue_2.ilk
....................\.....\daodanfeixinglixue_2.pch
....................\.....\daodanfeixinglixue_2.pdb
....................\.....\main.obj
....................\.....\vc60.idb
....................\.....\vc60.pdb
....................\main.c
....................\outputdata.txt
....................\Debug
第2题
daodanfeixinglixue_2
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