Design and Testing of a Low-Order Flight Control System for Quad-Tilt-Wing UAV
Journal of Guidance, Control, and Dynamics ; 39 , 10 ; 2426-2433
01.08.2016
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Design and Testing of a Low-Order Flight Control System for Quad-Tilt-Wing UAV
Online Contents | 2016
|Design of flight control system for quad tilt-wing UAV
IEEE | 2015
|Quad Tilt Wing VTOL UAV: Aerodynamic Characteristics and Prototype Flight
British Library Conference Proceedings | 2009
|