31th Congress of the International Council of the Aeronautical Sciences

06.2 - Flight Dynamics and Control (UAV related)

LONGITUDINAL FLIGHT CONTROL OF BIOINSPIRED FLAPPING-WING MICRO AIR VEHICLE WITH EXTENDED UNSTEADY VORTEX-LATTICE METHOD.

J.-W. Leeš, A.T. Nguyen, Le Quy Don Technical University , Vietnam; J.-H. Hanš; šKAIST, South Korea

This study suggests the flight control analysis of bioinspired FWMAVs with the unsteady aerodynamic model that combines the panel method and extended unsteady vortex-lattice(UVLM) method. The analysis method used in this study made it possible to overcome the limit of the flight control studies done with simple aerodynamic models by including Leading edge vortices effect and wing-wake interaction.


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