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Izvestiya of Saratov University. Mathematics. Mechanics. Informatics, 2011, Volume 11, Issue 1, Pages 84–89
DOI: https://doi.org/10.18500/1816-9791-2011-11-1-84-89 (Mi isu205) 		 
This article is cited in 3 scientific papers (total in 3 papers)

Mechanics

Analytical solution of differential equations of circular spacecraft orbit orientation

I. A. Pankratov, Yu. N. Chelnokov

Saratov State University, Chair of Computational Experiment in Mechanics
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DOI: https://doi.org/10.18500/1816-9791-2011-11-1-84-89
Abstract: The problem of optimal reorientation of spacecraft's orbit with a limited control, orthogonal to the plane of spacecraft orbit is being investigated. We have found an analytical solution of differential equations of circular spacecraft orbit orientation by control that is permanent on adjacent parts of the active spacecraft's motion.
Key words: spacecraft, orbit, orientation, quaternion, optimal control.
Document Type: Article
UDC: 629
Language: Russian
Citation: I. A. Pankratov, Yu. N. Chelnokov, “Analytical solution of differential equations of circular spacecraft orbit orientation”, Izv. Saratov Univ. Math. Mech. Inform., 11:1 (2011), 84–89
Citation in format AMSBIB
\Bibitem{PanChe11}
\by I.~A.~Pankratov, Yu.~N.~Chelnokov
\paper Analytical solution of differential equations of circular spacecraft orbit orientation
\jour Izv. Saratov Univ. Math. Mech. Inform.
\yr 2011
\vol 11
\issue 1
\pages 84--89
\mathnet{http://mi.mathnet.ru/isu205}
\crossref{https://doi.org/10.18500/1816-9791-2011-11-1-84-89}
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    • This publication is cited in the following 3 articles:
    Citing articles in Google Scholar: Russian citations, English citations
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    		Известия Саратовского университета. Новая серия. Серия Математика. Механика. Информатика
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