This work is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License
|
||||||||
|
Paper Details
Paper Title
An Application of Ray Tracing Modeling Technique to design Aeronautical Satellite Communication
Authors
  A.B.Chandrika,  T.Vajra Deepthi
Abstract
In this paper , to achieve safe aeronautical communication, reliable propagation simulation and modeling are absolutely necessary in aeronautical traffic system. This paper mainly applies a ray-tracing method on propagation to model satellite-to-aircraft communication. The main aim of this paper is to reproduce data link power and time delay of direct and scatter signal power loss and time delay of received signal on the aircraft antenna. In aeronautical satellite communication system, Ray-tracing models are mainly designed for simulation results which show the carrier-to-noise ratio is less than 100dB below 17 degree of aircraft elevation angle. For Boeing aircraft , the maximum Doppler shift being 220Hz with a differential time delay is less than 30μs below 20 degree aircraft elevation angle.
Keywords- Air traffic control, Doppler shift,, Geocentric equatorial, Ionospheric Propagation, Power system modeling, Ray tracing
Publication Details
Unique Identification Number - IJEDR1802041Page Number(s) - 233-237Pubished in - Volume 6 | Issue 2 | April 2018DOI (Digital Object Identifier) -    Publisher - IJEDR (ISSN - 2321-9939)
Cite this Article
  A.B.Chandrika,  T.Vajra Deepthi,   "An Application of Ray Tracing Modeling Technique to design Aeronautical Satellite Communication", International Journal of Engineering Development and Research (IJEDR), ISSN:2321-9939, Volume.6, Issue 2, pp.233-237, April 2018, Available at :http://www.ijedr.org/papers/IJEDR1802041.pdf
Article Preview
|
|
||||||
|