文件名称:OrbitDynamics
- 所属分类：
- 交通/航空行业
- 资源属性：
- [Windows] [Visual.Net] [源码]
- 上传时间：
- 2013-08-27
- 文件大小：
- 4.02mb
- 下载次数：
- 0次
- 提 供 者：
- 李*
- 相关连接：
- 无
- 下载说明：
- 别用迅雷下载，失败请重下，重下不扣分！
介绍说明－－下载内容均来自于网络，请自行研究使用
卫星轨道动力学的解算，如轨道根数的求解，星历计算等。-Satellite orbital dynamics solver, such as orbital solving
(系统自动生成,下载前可以参看下载内容)
下载文件列表
OrbitDynamics\bin\OrbitDyn_debug.dll
.............\...\OrbitDyn_release.dll
.............\data\atmos.den
.............\....\EGM96.grv
.............\....\eigen-cg03c.gfc
.............\....\EOP.dat
.............\....\EOP_old.dat
.............\....\GLGM2.grv
.............\....\GMM1.grv
.............\....\GMM2B.grv
.............\....\JGM2.grv
.............\....\JGM3.grv
.............\....\LP165P.grv
.............\....\Mars50c.grv
.............\....\plteph.405
.............\....\tum2s.gfc
.............\....\WGS84.grv
.............\....\WGS84_EGM96.grv
.............\include\BaseException.h
.............\.......\CDatetime.h
.............\.......\CEngine.h
.............\.......\CentralBody.h
.............\.......\Config.h
.............\.......\Constant.h
.............\.......\Coordination.h
.............\.......\DE405.h
.............\.......\Euler.h
.............\.......\facility.h
.............\.......\Kepler.h
.............\.......\Maneuver.h
.............\.......\matrixtcl.h
.............\.......\Msise00.h
.............\.......\nrlmsise-00.h
.............\.......\OrbitDyn.h
.............\.......\PerfTimer.h
.............\.......\Quaternion.h
.............\.......\satellite.h
.............\.......\StopCondition.h
.............\.......\Utility.h
.............\.......\Vector.h
.............\m\a2t.m
.............\.\AU.m
.............\.\Avv.m
.............\.\Ayrp.m
.............\.\c2q.m
.............\.\cart2kepler.m
.............\.\Constant.m
.............\.\Contents.m
.............\.\date2mjd.m
.............\.\de405.m
.............\.\deg.m
.............\.\dfm2deg.m
.............\.\dnda.m
.............\.\drda.m
.............\.\duda.m
.............\.\Earth.m
.............\.\eci2ecf.m
.............\.\ecliptic_equator_angle.m
.............\.\eop.mat
.............\.\fm.m
.............\.\GEarth.m
.............\.\getcoi.m
.............\.\gha.m
.............\.\gham.m
.............\.\ghamj2000.m
.............\.\GMoon.m
.............\.\GSun.m
.............\.\h2n.m
.............\.\hms2deg.m
.............\.\hohmanntransfer.m
.............\.\hohmanntransfer_m.m
.............\.\J2.m
.............\.\J3.m
.............\.\J4.m
.............\.\kdeg.m
.............\.\kepler2cart.m
.............\.\keplerfunc.m
.............\.\kepleru.m
.............\.\krad.m
.............\.\limit360.m
.............\.\limitpi.m
.............\.\mexCreator\mexCreator.sln
.............\.\...DE405\mexde405.cpp
.............\.\........\mexDE405.def
.............\.\........\mexDE405.vcproj
.............\.\........\mexversion.rc
.............\.\mf.m
.............\.\mjd2000.m
.............\.\mjd2date.m
.............\.\nutation.m
.............\.\nutation_angle.m
.............\.\oblate.m
.............\.\OrbitDyn\mexversion.rc
.............\.\........\OrbitDyn.cpp
.............\.\........\OrbitDyn.def
.............\.\........\OrbitDyn.vcproj
.............\.\orbitdyn.m
.............\.\phaseplane.m
.............\.\phaseplanelogic.m
.............\.\phaseplanelogic_parabola.m