Description: According to Newton s law of gravity in real-time calculation of satellite orbital position, get six orbital parameters of the satellite can be used for navigation and positioning
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轨道计算\Debug\MainFrm.obj
........\.....\sea1.obj
........\.....\StdAfx.obj
........\.....\vc60.idb
........\.....\vc60.pdb
........\.....\二体问题的轨道计算.exe
........\.....\二体问题的轨道计算.ilk
........\.....\二体问题的轨道计算.obj
........\.....\二体问题的轨道计算.pch
........\.....\二体问题的轨道计算.pdb
........\.....\二体问题的轨道计算.res
........\.....\二体问题的轨道计算Doc.obj
........\.....\二体问题的轨道计算View.obj
........\.....\新建 文本文档 (2).txt
........\MainFrm.cpp
........\MainFrm.h
........\ReadMe.txt
........\res\Toolbar.bmp
........\...\二体问题的轨道计算.ico
........\...\二体问题的轨道计算.rc2
........\...\二体问题的轨道计算Doc.ico
........\Resource.h
........\sea1.cpp
........\sea1.h
........\StdAfx.cpp
........\StdAfx.h
........\二体问题的轨道计算.aps
........\二体问题的轨道计算.clw
........\二体问题的轨道计算.cpp
........\二体问题的轨道计算.dsp
........\二体问题的轨道计算.dsw
........\二体问题的轨道计算.h
........\二体问题的轨道计算.ncb
........\二体问题的轨道计算.opt
........\二体问题的轨道计算.plg
........\二体问题的轨道计算.rc
........\二体问题的轨道计算Doc.cpp
........\二体问题的轨道计算Doc.h
........\二体问题的轨道计算View.cpp
........\二体问题的轨道计算View.h
........\Debug
........\res
轨道计算
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