Satellite orbit computation in matlab

The following Matlab project contains the source code and Matlab examples used for satellite orbit computation. A modified version of the SGP4 code used for standard satellite orbit computation using two-line elements (TLE).

The source code and files included in this project are listed in the project files section, please make sure whether the listed source code meet your needs there.

Project Files: 

File NameSize
license.txt 1312
SatelliteOrbitPrediction_Readme.pdf 85643
GenerateSatelliteGeometry_DEMO.m 4812
SetPath4SGP4.m 411
SummarizeSatelliteGeometry.m 5313
angl.m 1258
constastro.m 2253
constmath.m 1171
days2mdh.m 2136
2009210.TLE 142
LCT-32765-SaoLuis.mat 30648
SCION-TLE.mat 2472
AIAA-2006-6753-Rev1.pdf 662029
dpper.m 6699
dscom.m 8536
dsinit.m 12042
dspace.m 7516
findIntercept.m 801
getgravc.m 2598
gstime.m 1439
initl.m 4219
invjday.m 2362
jday.m 1629
mag.m 994
newtonm.m 4575
newtonnu.m 3106
ReadTextFiles.m 457
RunSGP4.m 3725
rv2coe.m 7755
satGEOM.m 5924
sgp4.m 12224
sgp4init.m 14075
siderealtime.m 2702
spg4_ecf.m 864
testmat.m 5565
twoline2rv.m 10264
twoline2rvMOD.m 10007
alias.m 229
bold_fig.m 1556
boxcar_avg.m 267
colors.m 3847
computeSI.m 406
dB10.m 291
dB20.m 291
ellipse.m 1371
findIpeaks.m 2940
findPeaks.m 2603
freqs1.m 856
line12.m 218
line21.m 218
LinkZoom.m 1453
nicefftnum.m 218
pickfile.m 1137
pointsIncluded.m 865
polyrec.m 701
polyRegion_add.m 1981
position2index.m 245
showprogress.m 132
taylor.m 910
turbsim2.m 908

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