Gravity assist trajectory design and analysis in matlab

The following Matlab project contains the source code and Matlab examples used for gravity assist trajectory design and analysis. PDF document and a MATLAB script called flyby_matlab that can be used to design and optimize interplanetary trajectories that include a single gravity assist maneuver.

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
atan3.m 534
bplane.m 1924
eci2orb1.m 2248
fbhyper.m 2136
fbyfunc.m 3192
flyby_matlab.eps 111834
flyby_matlab.m 23045
flyby_matlab.out 4171
flyby_matlab.pdf 530374
flyby_matlab.sum 12900
flyby_matlab_64bit.m 23213
flyby_specs.txt 194
fpa_event.m 426
gdate.m 903
getdate.m 731
glambert.m 13753
heqm.m 509
jd2str.m 548
jplephem.m 15643
julian.m 1151
kepler1.m 2072
keycheck.m 122
lambert.m 8921
lambfunc.m 7078
license.txt 1311
modulo.m 289
oeprint2.m 1691
orb2eci.m 1621
p2000.m 639
peqm.m 1282
rv2bp.m 2591
rv2bp2.m 2722
soi_event.m 593
svprint.m 784
twobody2.m 2755
uvector.m 311

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