Description: Six degrees of freedom trajectory simulation, using fixed step Changlong Kutta method, consider the control system and rudder bias.
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File list (Check if you may need any files):
Guidance_Missile\debug\Guidance_Missile.exe
................\.....\Guidance_Missile.ilk
................\.....\Guidance_Missile.pdb
................\Guidance_Missile\Debug\BuildLog.htm
................\................\.....\Guidance_Missile.exe.embed.manifest
................\................\.....\Guidance_Missile.exe.embed.manifest.res
................\................\.....\Guidance_Missile.exe.intermediate.manifest
................\................\.....\Guidance_Missile.obj
................\................\.....\Guidance_Missile.pch
................\................\.....\mt.dep
................\................\.....\stdafx.obj
................\................\.....\vc80.idb
................\................\.....\vc80.pdb
................\................\Guidance_Missile.cpp
................\................\Guidance_Missile.vcproj
................\................\Guidance_Missile.vcproj.PC-201012221215.Administrator.user
................\................\ReadMe.txt
................\................\stdafx.cpp
................\................\stdafx.h
................\Guidance_Missile.ncb
................\Guidance_Missile.sln
................\Guidance_Missile.suo
................\................\Debug
................\debug
................\Guidance_Missile
Guidance_Missile
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