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A MATLAB Script for Propagating Interplanetary Trajectories from Earth to Mars

A MATLAB Script for Propagating Interplanetary Trajectories from Earth to Mars

by

David Eagle (view profile)

 

Numerically integrate the orbital equations of motion of an Earth to Mars interplanetary trajectory.

pprop_e2m.zip
atan3.m
display1.m
eci2orb1.m
egm96.dat
eqxra.m
erot.m
etilt1.m
findca.m
findleap.m
findrm.m
fpa_event.m
funarg.m
gast4.m
gdate.m
geo_eqm.m
gravity.m
hel_eqm.m
jd2str.m
jdfunction.m
jplephem.m
julian.m
license.txt
mme2000.m
nut2000_lp.m
obliq.m
oeprint1.m
orb2eci.m
pprop_e2m.in
pprop_e2m.m
pprop_e2m.pdf
pprop_e2m_cm.dat
readdata.m
readgm.m
rm_event.m
rv2bp2.m
rv2hyper.m
soi_event.m
srp.m
svprint.m
times_novas.m

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