文件名称:cpp
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- 上传时间：2013-10-11
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使用SGP模型进行轨道计算的C源码 使用两行星历TLE-Simplified perturbations models are a set of five mathematical models (SGP, SGP4, SDP4, SGP8 and SDP8) used to calculate orbital state vectors of satellites and space debris relative to the Earth-centered inertial coordinate system. This set of models is often referred to collectively as SGP4 due to the frequency of use of that model particularly with two-line element sets produced by NORAD and NASA.
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下载文件列表
Cpp/ast2body.cpp
Cpp/ast2body.h
Cpp/astiod.cpp
Cpp/astiod.h
Cpp/astmath.cpp
Cpp/astmath.h
Cpp/asttime.cpp
Cpp/asttime.h
Cpp/coordfk5.cpp
Cpp/coordfk5.h
Cpp/debug1.cpp
Cpp/debug2.cpp
Cpp/debug3.cpp
Cpp/debug4.cpp
Cpp/debug5.cpp
Cpp/debug6.cpp
Cpp/debug7.cpp
Cpp/eoppn1.txt
Cpp/eopspw.cpp
Cpp/eopspw.h
Cpp/msis00.cpp
Cpp/msis00.h
Cpp/msiscom.cpp
Cpp/msiscom.h
Cpp/nut80.dat
Cpp/sgp4-ver.tle
Cpp/sgp4dc.cpp
Cpp/sgp4dc.h
Cpp/sgp4ext.cpp
Cpp/sgp4ext.h
Cpp/sgp4io.cpp
Cpp/sgp4io.h
Cpp/sgp4unit.cpp
Cpp/sgp4unit.h
Cpp/tcppver.out
Cpp/tcppvera.out
Cpp/testcpp.cpp
Cpp/testcpp.exe
Cpp/testdc.cpp
Cpp/TWOLINE.TXT
Cpp/ast2body.h
Cpp/astiod.cpp
Cpp/astiod.h
Cpp/astmath.cpp
Cpp/astmath.h
Cpp/asttime.cpp
Cpp/asttime.h
Cpp/coordfk5.cpp
Cpp/coordfk5.h
Cpp/debug1.cpp
Cpp/debug2.cpp
Cpp/debug3.cpp
Cpp/debug4.cpp
Cpp/debug5.cpp
Cpp/debug6.cpp
Cpp/debug7.cpp
Cpp/eoppn1.txt
Cpp/eopspw.cpp
Cpp/eopspw.h
Cpp/msis00.cpp
Cpp/msis00.h
Cpp/msiscom.cpp
Cpp/msiscom.h
Cpp/nut80.dat
Cpp/sgp4-ver.tle
Cpp/sgp4dc.cpp
Cpp/sgp4dc.h
Cpp/sgp4ext.cpp
Cpp/sgp4ext.h
Cpp/sgp4io.cpp
Cpp/sgp4io.h
Cpp/sgp4unit.cpp
Cpp/sgp4unit.h
Cpp/tcppver.out
Cpp/tcppvera.out
Cpp/testcpp.cpp
Cpp/testcpp.exe
Cpp/testdc.cpp
Cpp/TWOLINE.TXT
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