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Artificial Satellites

The Journal of Space Research Centre of Polish Academy of Sciences

4 Issues per year


CiteScore 2016: 0.33

SCImago Journal Rank (SJR) 2016: 0.179
Source Normalized Impact per Paper (SNIP) 2016: 0.560

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Online
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2083-6104
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Volume 46, Issue 1 (Jan 2011)

Issues

The Benefits of Inclined-Orbit Operations for Geostationary Orbit Communication Satellites

Lihua Ma
Published Online: 2011-04-06 | DOI: https://doi.org/10.2478/v10018-011-0007-1

The Benefits of Inclined-Orbit Operations for Geostationary Orbit Communication Satellites

Geostationary orbit (GEO) communication satellites can be extended in lifetime by switching to inclined-orbit operations. In this mode, a small amount of propellant is reserved to maintain the assigned orbit longitude. Inclination is allowed to build up at a rate of approximately 0.8○ per year. Developing these space resources can bring out a number of benefits. Besides communication application, these satellites can be used to construct navigation constellation of the Chinese Area Positioning System (CAPS). In this present paper, the realization way of communication and navigation applications is studied and the benefits and problems are explained.

Keywords: Chinese Area Positioning System (CAPS); geostationary orbit satellite; inclined-orbit operations; communication application; navigation application

  • Agrawal B. (1986) Design of geosynchronous spacecraft. Prentice-Hall, Englewood Cliffs, NJ.Google Scholar

  • Ai G, Sheng P, Du J, Zheng Y, Cai X, Wu H, Hu Y, Hua Y, Li X. (2009) Barometric altimetry system as virtual constellation applied in CAPS. Sci China Ser G-Phys Mech Astron, Vol. 52, No. 3, 376-383.Google Scholar

  • Ai G, Shi H, Wu H, Yan Y, Bian Y, Hu Y, Li Z, Guo J, Cai X. (2008) Positioning system based satellite communication and Chinese Area Positioning System (CAPS). Chin J Astron Astrophys, Vol. 8, No. 6, 611-630.Web of ScienceGoogle Scholar

  • Atia A, Day S, Westerlund L. (1990) Communications satellite operation in inclined orbit ‘The Comsat Maneuver’. In: AIAA International Communication Satellite Systems Conference and Exhibit, 13th, Los Angeles, CA, Mar. 11-15, 1990, Technical Papers. Part 2 (A90-25601 09-32). Washington, DC, American Institute of Aeronautics and Astronautics, p. 452-455.Google Scholar

  • Bauer R, Krawczyk R, Irwin D, et al. (2002) Extending ACTS operations through a university-based consortium. Space Commun, Vol. 18, No. 1-2, 7-12.Google Scholar

  • Han Y, Ma L, Qiao Q, Yin Z, Shi H, Ai, G. (2009) Functions of retired GEO communication satellites in improving the PDOP value of CAPS. Sci China Ser G-Phys Mech Astron, Vol. 52, No. 3, 423-433.Web of ScienceGoogle Scholar

  • Jwo D. (2001) Efficient DOP calculation for GPS with and without altimeter aiding. J Navig, Vol. 54, No. 2, 269-279.Google Scholar

  • Kaplan E, Hegarty C. (2006) Understanding GPS: Principles and Applications. 2nd ed. Artech House, Boston.Google Scholar

  • Li Y, Hao H. (1996) Satellite communication geosynchronous orbit with small inclination. Chin Space Sci Tech, Vol. 16, No. 3, 22-28.Google Scholar

  • Ma L, Hu C, Han Y, Qiao Q, Pei J. (2010) Simulation analysis of polarization matching for APSTAR-1 satellite in CAPS. J Syst Simul, Vol. 22, No. 10, 2446-2449.Google Scholar

  • Ma L, Jing Y, Ji H, Zhang L. (2011) The evolvement analysis of GEO satellite orbit in end of life based on STK software. Astron Res Tech (in press)Google Scholar

  • Ma L, Wang M, Zhang L, Ji H. (2011) Mathematical aspects of CAPS horizontal position error. Adv Space Res. (under reviewing)Google Scholar

  • Shi H, Ai G, Han Y, Ma L, Chen J, Geng J. (2009) Multi-life cycles utilization of retired satellites. Sci China Ser G-Phys Mech Astron, Vol. 52, No. 3, 323-327.Google Scholar

  • Shi H, Sun X and Li Z. (2009) Principle of transponder satellite navigation. Science Press, Beijing.Google Scholar

  • Wu H, Bian Y, Lu X, Li X, Wang D. (2009) Time synchronization and carrier frequency control of CAPS navigation signals generated on the ground. Sci China Ser G-Phys Mech Astron, Vol. 52, No. 3, 393-401.Web of ScienceGoogle Scholar

  • Zhang R. (1998) Dynamics and control of satellite orbit and attitude. Beihang University Press, Beijing.Google Scholar

About the article


Published Online: 2011-04-06

Published in Print: 2011-01-01


Citation Information: Artificial Satellites, ISSN (Online) 2083-6104, ISSN (Print) 0208-841X, DOI: https://doi.org/10.2478/v10018-011-0007-1.

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