DocumentCode
613682
Title
A new efficient algorithm for tracking LEO satellites
Author
Khanlari, A. ; Mansourkiaie, Fatemeh
Author_Institution
Memorial Univ. of Newfoundland, St. John´s, NL, Canada
fYear
2013
fDate
15-18 April 2013
Firstpage
587
Lastpage
590
Abstract
The methods of tracking Low Earth Orbit (LEO) satellites can be grouped into two different categories: “signal-based” and “program-based” methods. In this paper, we employ a new program-based tracking method to trace satellites, using Two Line orbital Elements (TLE). Using TLE is a simple and well-known method for tracking satellites; however, this paper presents a new algorithm for tracking satellites, based on TLE files. This algorithm, uses an available TLE file to estimate the satellite´s position and to update the orbital elements, for any desired time that we are interested in tracing the satellite. The results show that the algorithm is accurate and reliable.
Keywords
artificial satellites; satellite navigation; LEO satellites tracking; TLE; low Earth orbit satellites; program-based tracking method; satellite position; signal-based method; two line orbital element; Equations; Low earth orbit satellites; Mathematical model; Orbits; Reliability; Vectors; LEO satellites; Orbital elements; Program-based tracking; TLE component;
fLanguage
English
Publisher
ieee
Conference_Titel
Systems Conference (SysCon), 2013 IEEE International
Conference_Location
Orlando, FL
Print_ISBN
978-1-4673-3107-4
Type
conf
DOI
10.1109/SysCon.2013.6549941
Filename
6549941
Link To Document