Araştırma Makalesi
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Determination of Coverage Oscillation for Inclined Communication Satellite

Yıl 2020, Cilt: 24 Sayı: 5, 973 - 983, 01.10.2020
https://doi.org/10.16984/saufenbilder.702190

Öz

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.

Teşekkür

We would like to thank Turksat Uydu Haberlesme ve Kablo TV AS for its invaluable support.

Kaynakça

  • E. M. Soop, “Introduction to Geostationary Orbits”, ESA, : pp. 232-235, 1983.
  • B. Gurol, , S. Gulgonul, , G. Gokay, , A. Okan, , I.Oz., “Optical monitoring of inter satellite distance between Turksat-2A And Turksat-3A. In Proceedings of 5th International Conference on Recent Advances in Space Technologies-RAST2011, pp.337-340, 2011.
  • S. Hu-Li, H Yan-Ben, M. Li-Hua, P.Jun, Y. Zhi- Qiang and J. Hai-Fu, “Beyond life-cycle utilization of geostationary communication satellites in end-of-life”, Satellite Communications, Nazzareno Diodato(Ed), Intech, ISBN: 978-953-307-135-0, pp.323-365, 2010.
  • L. Ma, “The Benefits of Inclined-Orbit Operations for Geostationary Orbit Communication Satellites”, Artificial Satellite, Vol.46, DOI: 10.2478/v10018-011-0007-1, 2011 .
  • I. Oz, “Evaluation of station location for orbit determination of geo satellites at different slots”, 8th International Conference on Recent Advances in Space Technologies (RAST), pp.375-379, 2017.
  • Z. Chang-Yin, Z. Ming-Jiang, W. Hong-Bo, X. Jian-Ning, Z. Ting-Lei, Z. Wei, “Analysis on the long-term dynamical evolution of the inclined geosynchronous orbits in the Chinese BeiDou navigation system, Advances in Space Research, 56 pp. 377–387, 2015.
  • Y. Han, L. Ma, Q. Qiao., Z.Yin, H.Shi, G. Ai, “Functions of retired GEO communication satellites in improving the PDOP value of CAPS”, Sci China Ser G-Phys Mech Astron, Vol. 52, No. 3, pp.423-433, 2009.
  • G.Dai, , X.Chen, , M.Zuo, , L. Peng, , M. Wang, Z.Song, “The Influence of Orbital Element Error on Satellite Coverage Calculation”. International Journal of Aerospace Engineering, 2018.
  • S. Y. Fu, Z. R. Wang, , H. L. Shi, , L. H. Ma, “The application of decommissioned GEO satellites to CAPS”, In IOP Conference Series: Materials Science and Engineering,Vol. 372, No. 1, pp. 012033, IOP Publishing, 2018.
  • C.Sun, H. Jiang, J. Zhang, Y. Tao, , B. Li, C. Zhao, “Modeling and Calibrating the Ground-Surface Beam Pointing of GEO Satellite”, IEEE Access, 7, 121897-121906, 2019.
  • S.Lee, “GEO Satellite Collision Avoidance Maneuver Strategy Against Inclied GSO Satellite”, In SpaceOps :1294441, 2012.
  • A. F. Yagli, M. Gokten, , S. Gulgonul, , I. Oz, O. Dalbay,“Regional positioning system using Turksat satellites”, In 6th International Conference on Recent Advances in Space Technologies RAST:2013: pp.237-240, 2013.
  • A. E. Emam, J. Victor, , M. A. Elghany, “Performance Assessment of GSO Satellite before and after Enhancing Pointing Effect”, World Academy of Science, Engineering and Technology, International Journal of Electrical, Computer, Energetic, Electronic and Communication Engineering, 12: pp. 1434-1440, 2015.
  • A. E. Emam, , M. A. Elghany, , “Collocation Assessment between GEO and GSO Satellites”, International Journal of Aerospace and Mechanical Engineering,: 9(12), pp. 2124-2132, 2015.
Yıl 2020, Cilt: 24 Sayı: 5, 973 - 983, 01.10.2020
https://doi.org/10.16984/saufenbilder.702190

Öz

Kaynakça

  • E. M. Soop, “Introduction to Geostationary Orbits”, ESA, : pp. 232-235, 1983.
  • B. Gurol, , S. Gulgonul, , G. Gokay, , A. Okan, , I.Oz., “Optical monitoring of inter satellite distance between Turksat-2A And Turksat-3A. In Proceedings of 5th International Conference on Recent Advances in Space Technologies-RAST2011, pp.337-340, 2011.
  • S. Hu-Li, H Yan-Ben, M. Li-Hua, P.Jun, Y. Zhi- Qiang and J. Hai-Fu, “Beyond life-cycle utilization of geostationary communication satellites in end-of-life”, Satellite Communications, Nazzareno Diodato(Ed), Intech, ISBN: 978-953-307-135-0, pp.323-365, 2010.
  • L. Ma, “The Benefits of Inclined-Orbit Operations for Geostationary Orbit Communication Satellites”, Artificial Satellite, Vol.46, DOI: 10.2478/v10018-011-0007-1, 2011 .
  • I. Oz, “Evaluation of station location for orbit determination of geo satellites at different slots”, 8th International Conference on Recent Advances in Space Technologies (RAST), pp.375-379, 2017.
  • Z. Chang-Yin, Z. Ming-Jiang, W. Hong-Bo, X. Jian-Ning, Z. Ting-Lei, Z. Wei, “Analysis on the long-term dynamical evolution of the inclined geosynchronous orbits in the Chinese BeiDou navigation system, Advances in Space Research, 56 pp. 377–387, 2015.
  • Y. Han, L. Ma, Q. Qiao., Z.Yin, H.Shi, G. Ai, “Functions of retired GEO communication satellites in improving the PDOP value of CAPS”, Sci China Ser G-Phys Mech Astron, Vol. 52, No. 3, pp.423-433, 2009.
  • G.Dai, , X.Chen, , M.Zuo, , L. Peng, , M. Wang, Z.Song, “The Influence of Orbital Element Error on Satellite Coverage Calculation”. International Journal of Aerospace Engineering, 2018.
  • S. Y. Fu, Z. R. Wang, , H. L. Shi, , L. H. Ma, “The application of decommissioned GEO satellites to CAPS”, In IOP Conference Series: Materials Science and Engineering,Vol. 372, No. 1, pp. 012033, IOP Publishing, 2018.
  • C.Sun, H. Jiang, J. Zhang, Y. Tao, , B. Li, C. Zhao, “Modeling and Calibrating the Ground-Surface Beam Pointing of GEO Satellite”, IEEE Access, 7, 121897-121906, 2019.
  • S.Lee, “GEO Satellite Collision Avoidance Maneuver Strategy Against Inclied GSO Satellite”, In SpaceOps :1294441, 2012.
  • A. F. Yagli, M. Gokten, , S. Gulgonul, , I. Oz, O. Dalbay,“Regional positioning system using Turksat satellites”, In 6th International Conference on Recent Advances in Space Technologies RAST:2013: pp.237-240, 2013.
  • A. E. Emam, J. Victor, , M. A. Elghany, “Performance Assessment of GSO Satellite before and after Enhancing Pointing Effect”, World Academy of Science, Engineering and Technology, International Journal of Electrical, Computer, Energetic, Electronic and Communication Engineering, 12: pp. 1434-1440, 2015.
  • A. E. Emam, , M. A. Elghany, , “Collocation Assessment between GEO and GSO Satellites”, International Journal of Aerospace and Mechanical Engineering,: 9(12), pp. 2124-2132, 2015.
Toplam 14 adet kaynakça vardır.

Ayrıntılar

Birincil Dil İngilizce
Bölüm Araştırma Makalesi
Yazarlar

İbrahim Öz 0000-0003-4593-917X

Ümit Cezmi Yılmaz 0000-0001-5886-9743

Yayımlanma Tarihi 1 Ekim 2020
Gönderilme Tarihi 11 Mart 2020
Kabul Tarihi 21 Temmuz 2020
Yayımlandığı Sayı Yıl 2020 Cilt: 24 Sayı: 5

Kaynak Göster

APA Öz, İ., & Yılmaz, Ü. C. (2020). Determination of Coverage Oscillation for Inclined Communication Satellite. Sakarya University Journal of Science, 24(5), 973-983. https://doi.org/10.16984/saufenbilder.702190
AMA Öz İ, Yılmaz ÜC. Determination of Coverage Oscillation for Inclined Communication Satellite. SAUJS. Ekim 2020;24(5):973-983. doi:10.16984/saufenbilder.702190
Chicago Öz, İbrahim, ve Ümit Cezmi Yılmaz. “Determination of Coverage Oscillation for Inclined Communication Satellite”. Sakarya University Journal of Science 24, sy. 5 (Ekim 2020): 973-83. https://doi.org/10.16984/saufenbilder.702190.
EndNote Öz İ, Yılmaz ÜC (01 Ekim 2020) Determination of Coverage Oscillation for Inclined Communication Satellite. Sakarya University Journal of Science 24 5 973–983.
IEEE İ. Öz ve Ü. C. Yılmaz, “Determination of Coverage Oscillation for Inclined Communication Satellite”, SAUJS, c. 24, sy. 5, ss. 973–983, 2020, doi: 10.16984/saufenbilder.702190.
ISNAD Öz, İbrahim - Yılmaz, Ümit Cezmi. “Determination of Coverage Oscillation for Inclined Communication Satellite”. Sakarya University Journal of Science 24/5 (Ekim 2020), 973-983. https://doi.org/10.16984/saufenbilder.702190.
JAMA Öz İ, Yılmaz ÜC. Determination of Coverage Oscillation for Inclined Communication Satellite. SAUJS. 2020;24:973–983.
MLA Öz, İbrahim ve Ümit Cezmi Yılmaz. “Determination of Coverage Oscillation for Inclined Communication Satellite”. Sakarya University Journal of Science, c. 24, sy. 5, 2020, ss. 973-8, doi:10.16984/saufenbilder.702190.
Vancouver Öz İ, Yılmaz ÜC. Determination of Coverage Oscillation for Inclined Communication Satellite. SAUJS. 2020;24(5):973-8.

Sakarya University Journal of Science (SAUJS)