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Mathematical model of an unmanned aerial vehicle with elliptical wing

Abstract

Mathematical model of an unmanned aerial vehicle with elliptical wing

Gorbunov A.A., Sinyutin S.A.

Incoming article date: 04.03.2015

The article describes the slow flying drones with reference to problems of aerial photography. As an alternative to multicopter proposed aerodynamic design, elliptical flying wing. It has been shown that this scheme allows ensure uniform distribution of lifting force along the wing span, respectively, does not allow on loss of unmanned speed bogged down into a tailspin. The results of mathematical modeling and flight test a prototype of this type of UAV.

Keywords: unmanned aerial vehicle; elliptical wing; control laws; mathematic modeling; drone aircraft