Round or oval Earth orbit spacecraft the optimal pulse orbital maneuvering required. optimal impulsive maneuver required to de-orbit a spacecraft in a circular or elliptical Earth orbit

atan3.m
deltav_guess.m
deorbit1.in
deorbit2.in
deorbit3.in
deorbit_shoot.m
deorbit_snopt.m
deorbit_snopt.pdf
eci2fpc1.m
eci2orb1.m
gast1.m
gdate.m
geodet1.m
j2eqm.m
jd2str.m
julian.m
keycheck.m
license.txt
oeprint1.m
orb2eci.m
readdata.m
tof1.m

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