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Journal of Computational and Engineering Mathematics, 2016, Volume 3, Issue 2, Pages 3–13
DOI: https://doi.org/10.14529/jcem1602001 (Mi jcem58) 		 
Engineering Mathematics

The use of mathematical modeling to determine the need configuration of unmanned aircraft having a variable structure in flight

A. L. Kartashev, A. S. Pantileev

South Ural State University, Chelyabinsk, Russian Federation
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DOI: https://doi.org/10.14529/jcem1602001
Abstract: A balancer control in conjunction with the classical aerodynamic controls will significantly reduce the landing distance. We find the equations of motion both taking into account a movable load and without it, for unmanned aerial vehicle having a variable structure in flight.
Keywords: differential equations of motion, variable structure, unmanned aerial vehicle.
Received: 03.06.2016
Bibliographic databases:
Document Type: Article
UDC: 629.12.053.13
MSC: 70E55
Language: English
Citation: A. L. Kartashev, A. S. Pantileev, “The use of mathematical modeling to determine the need configuration of unmanned aircraft having a variable structure in flight”, J. Comp. Eng. Math., 3:2 (2016), 3–13
Citation in format AMSBIB
\Bibitem{KarPan16}
\by A.~L.~Kartashev, A.~S.~Pantileev
\paper The use of mathematical modeling to determine the need configuration of unmanned aircraft having a variable structure in flight
\jour J. Comp. Eng. Math.
\yr 2016
\vol 3
\issue 2
\pages 3--13
\mathnet{http://mi.mathnet.ru/jcem58}
\crossref{https://doi.org/10.14529/jcem1602001}
\mathscinet{https://mathscinet.ams.org/mathscinet-getitem?mr=3527951}
\elib{https://elibrary.ru/item.asp?id=26399832}
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