Geodesic
The use of mathematical modeling to determine the need configuration of unmanned aircraft having a variable structure in flight
Journal of computational and engineering mathematics, Tome 3 (2016) no. 2, pp. 3-13.

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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. 
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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. Journal of computational and engineering mathematics, Tome 3 (2016) no. 2, pp. 3-13. http://geodesic.mathdoc.fr/item/JCEM_2016_3_2_a0/

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