Mean local time of the ascending node in matlab

The following Matlab project contains the source code and Matlab examples used for mean local time of the ascending node. This geometric relationship defines the orientation of the spacecraft’s orbital plane with respect to the mean Sun.

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
funarg.m 2032
gast2.m 1694
gdate.m 899
getdate.m 754
getmltan.m 916
gettime.m 892
jd2str.m 556
julian.m 1151
license.txt 1311
ltan2raan.m 1899
mltan.m 3546
MLTAN.pdf 402915
mltan2raan.m 1675
mltan2raan.txt 1059
nod.m 1441
nut80.csv 6148
raan2mltan.m 1616
raan2mltan.txt 969
sun2.m 4652