Numerical Optimization Method of Spacecraft Antenna Retargeting Point Calculations

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Abstract:

This article describes a numerical method that determines the position of motorized onboard antennas of the spacecraft using telemetry values. There is results of testing this algorithm in the conclusion of the article.

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566-571

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June 2015

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© 2015 Trans Tech Publications Ltd. All Rights Reserved

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[1] I. I. Savenko, M.S. Sukhodoyev, N.A. Kosmynina, D.N. Ryzhkov, S.G. Tsapko, Automation Method of Reconfiguration of Communications Satellite's Onboard Repeater, J. Components of Scientific and Technological Progress. 1 (2014) 31-33.

Google Scholar

[2] G. Maral, M. ve Bousquet, Satellite Communications Systems, John Wiley & Sons, New York, A.B.D., (1998).

Google Scholar

[3] M. Teresa, Braun Satellite Communication and system, John Wiley & Sons, New York, A.B.D., (2012).

Google Scholar

[4] S. Gulgonul, E. Koklukaya, I. Erturk, A.Y. ve Tesneli, Communication Satellite Payload Redundancy Reconfiguration, Satellite Telecommunications (ESTEL), 2012 IEEE First AESS European Conference on, 1-4, (2012).

DOI: 10.1109/estel.2012.6400090

Google Scholar

[5] V.E. Kamnev, V.V. Cherkasov, G.V. Chechin, Satellite communication network: tutorial, Al'pina Pablisher, Moscow, (2004).

Google Scholar

[6] V.N. Guschin, Spacecraft devices foundations: tutorial, Mashinostroenie, Moscow, (2003).

Google Scholar