Journals / Sakarya University Journal of Science / 2020 / Cilt: 24 Sayı: 5

Determination of Coverage Oscillation for Inclined Communication Satellite

Pages
973–983
Publication Date
2020-10-01
DOI
—
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AI Summary & Key Takeaways

AI Insight
⚡ TL;DR(Too Long; Didn't Read)

The proposed method provides the results that are consistent with the results of measurements and the results of satellite operators’ professional tools.

📌 3 Key Takeaways

🎯
Objective & Hypothesis:The communication engineers need to evaluate footprint movement to deploy a ground station.
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Key Findings & Data:On the other hand, a satellite communication engineer does not need a very accurate inclination angle value to design a ground station for required service availability.
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Conclusion & Impact:The proposed method provides the results that are consistent with the results of measurements and the results of satellite operators’ professional tools.
🔬Design:Research Article
📍Scope:Comprehensive Sample
⚙️Variables:coverage oscillation · geo satellite · communication

Abstract

The communication engineers need to evaluate footprint movement to deploy a ground station. Geostationary communication satellite’s inclination angle causes the movement of a satellite footprint. The calculation of the inclination angle requires complex astronomical knowledge and mathematical calculations. On the other hand, a satellite communication engineer does not need a very accurate inclination angle value to design a ground station for required service availability. We propose a practical method called trigonometric curve fitting for the inclination to solve the problem. The past and the future value of inclination can be evaluated by using the curve-fitting method. It is a simplified practical method and does not need advanced orbital dynamics knowledge. The orbit geometry and evaluated inclination angle are used for estimation of a coverage area movement. A satellite communication engineer can evaluate coverage area oscillation quickly and design a better link for an inclined orbit satellite by using the proposed method. We have evaluated the inclination angle of the communication satellite Sat-1 with the proposed method. Sat-1 spot beam movements and wide beam coverage area movements are estimated to obtain EIRP and G/T fluctuation for link budget purposes. The proposed method provides the results that are consistent with the results of measurements and the results of satellite operators’ professional tools.

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Cite This Article

ÖZ, İ., YILMAZ, Ü. C. (2020). Determination of Coverage Oscillation for Inclined Communication Satellite. Sakarya University Journal of Science, Cilt: 24 Sayı: 5, 973–983. https://ajindex.com/articles/941879

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