34th Congress of the International Council of the Aeronautical Sciences

06.1 - Flight Dynamics and Control (Control & Modelling)

ATTITUDE CONTROL DESIGN FOR A FLYING-CRAWLING INTEGRATED FLAPPING-WING MICRO AIR VEHICLE

Z.Y. Yuan¹, W.Y. Yang¹, J.X. Xuan¹; ¹nwpu, China

This paper introduce the dynamic modeling and attitude control design of a flying- crawling integrated bionic flapping-wing micro air vehicle, enhancing its overall flight performance.


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