Active Disturbance Rejection Attitude Control for Flapping Wing Micro Aerial Vehicle With Nonaffine-in-Control Characteristics

This study presents attitude control research of flapping wing micro aerial vehicles with nonaffine-in-control characteristics via the active disturbance rejection control technique. With consideration of the uncertainties in moment of inertia caused by wings flapping and external disturbances, an e...

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Autors principals:	Cong Feng, Qing Wang, Changhua Hu, Ligang Gong
Format:	Artigo
Idioma:	Inglês
Publicat:	IEEE 2020-01-01
Col·lecció:	IEEE Access
Matèries:	Active disturbance rejection control dynamic inversion control extended state observer flapping wing micro aerial vehicle nonaffine-in-control
Accés en línia:	https://ieeexplore.ieee.org/document/8964390/
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