(IEEE, 2015-10) Kulik M.S.; Antonov V.K.; Glazok O.M.; Olefir O.I.; Глазок, Олексій Михайлович; Глазок О.М.; Глазок, Алексей Михайлович; Глазок А.М.
A configuration of an unmanned aircraft with closed wing is considered. The method of identification designed for researching the aerodynamic qualities of the model is proposed.