matlab
所属分类：matlab编程
开发工具：matlab
文件大小：430KB
下载次数：46
上传日期：2013-10-11 00:31:08
上 传 者：
johnnylc
说明： 使用SGP模型进行轨道计算的matlab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.)
文件列表:
Matlab\adbar2rv.m (1915, 2004-01-29)
Matlab\angl.m (1369, 2004-01-29)
Matlab\anglesdr.m (7603, 2011-12-30)
Matlab\anglesg.m (13583, 2013-02-08)
Matlab\anglesl.m (9945, 2012-01-12)
Matlab\azl2radc.m (689, 2007-03-09)
Matlab\biellip.m (4213, 2012-04-10)
Matlab\CeresHaccess.dat (3593, 2011-12-31)
Matlab\checkhit.m (2833, 2004-01-29)
Matlab\coe2rv.m (3826, 2012-04-10)
Matlab\combined.m (4944, 2012-05-30)
Matlab\constastro.m (2252, 2010-04-04)
Matlab\constmath.m (1168, 2011-10-11)
Matlab\convtime.m (10334, 2012-06-14)
Matlab\cubic.m (4807, 2013-09-12)
Matlab\cubicspl.m (1601, 2007-05-30)
Matlab\cubicspl1.m (3173, 2007-05-30)
Matlab\dayofwee.m (1114, 2007-03-15)
Matlab\days2mdh.m (2354, 2007-03-07)
Matlab\debug1.m (1587, 2006-08-12)
Matlab\debug2.m (3224, 2006-08-12)
Matlab\debug3.m (2703, 2006-08-12)
Matlab\debug4.m (1674, 2006-08-12)
Matlab\debug5.m (1064, 2005-08-23)
Matlab\debug6.m (4530, 2006-08-12)
Matlab\debug7.m (4676, 2006-08-12)
Matlab\dms2rad.m (1152, 2007-03-16)
Matlab\dolam.m (2680, 2007-01-04)
Matlab\doubler.m (4128, 2013-09-10)
Matlab\dpper.m (6697, 2008-07-04)
Matlab\dscom.m (8536, 2006-08-14)
Matlab\dsinit.m (12042, 2007-11-16)
Matlab\dspace.m (7516, 2008-08-27)
Matlab\ecef2eci.m (3287, 2011-12-30)
Matlab\ecef2mod.m (2876, 2011-05-06)
Matlab\ecef2pef.m (1496, 2011-04-18)
Matlab\ecef2teme.m (2636, 2012-05-24)
Matlab\ecef2tod.m (2862, 2011-04-18)
Matlab\eci2ecef.m (3270, 2005-02-15)
Matlab\eci2hill.m (2459, 2011-08-20)
... ...
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