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