@inproceedings{ca69430ea5d046289289d922d31ecae7,

title = "Drag coefficient estimation using satellite attitude and orbit data",

abstract = "Current spacecraft decay models assume a constant value of 2.2 for the coefficient of drag. This assumption is driven by the difficulty in accurately modeling the spacecraft's cross-sectional area exposed to the direction of motion. This research discards the assumption of a constant coefficient of drag; instead, it uses attitude data from the Swift spacecraft to determine the cross-sectional area and directly calculates the coefficient of drag over the nine years of orbital data. This method partially validates the NRLMSISE-00 atmospheric model and encourages a new examination of the coefficient of drag value used to determine the decay of spacecraft orbits.",

author = "Hassa, {Christopher L.} and Spencer, {David B.} and Bil{\'e}n, {Sven G.}",

year = "2014",

language = "English (US)",

series = "Advances in the Astronautical Sciences",

publisher = "Univelt Inc.",

pages = "1985--2002",

editor = "Mackison, {Donald L.} and Ossama Abdelkhalik and Wilson, {Roby S.} and Renato Zanetti",

booktitle = "Advances In The Astronautical Sciences",

address = "United States",

note = "24th AAS/AIAA Space Flight Mechanics Meeting, 2014 ; Conference date: 26-01-2014 Through 30-01-2014",

}