DocumentCode :
1680152
Title :
Kolmogorov-Arnold-Moser torus orbit prediction from two-line element sets
Author :
Abay, Rasit ; Wiesel, William E.
Author_Institution :
Turkish Air Force, Konya, Turkey
fYear :
2015
Firstpage :
137
Lastpage :
142
Abstract :
A new method for orbit prediction, which is as accurate as numerical methods and as fast as analytical methods, in terms of computational time, is needed. Kolmogorov-Arnold-Moser (KAM) torus orbit prediction method is a modern orbit determination that can meet the aforementioned needs. This paper presents a differential correction technique to create parameters needed by the new theory and an approximate accuracy analysis of the new orbit determination method by using Simplified General Perturbations 4 (SGP4) and Two-Line Element Set (TLE) as observational data.
Keywords :
Earth orbit; satellite communication; Kolmogorov-Arnold-Moser torus orbit prediction method; SGP4; TLE; approximate accuracy analysis; differential correction technique; modern orbit determination; simplified general perturbations 4; two-line element sets; Accuracy; Convergence; Covariance matrices; Fitting; Low earth orbit satellites; Orbits; Space vehicles; KAM torus; SGP4; TLE; differential correction; low eccentricity; orbit determination;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Recent Advances in Space Technologies (RAST), 2015 7th International Conference on
Conference_Location :
Istanbul
Print_ISBN :
978-1-4673-7760-7
Type :
conf
DOI :
10.1109/RAST.2015.7208329
Filename :
7208329
Link To Document :
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