Bounded attitude control of a biomimetic flapping robot
Résumé
Flapping micro Unmanned Air Vehicles (UAVs) can be considered as high frequency periodic systems. Based on the averaging theory, only the mean aerodynamic forces and torques over a wingbeat affect the movement of the body. Therefore, a nonlinear bounded state feedback control law is calculated upon the averaged model and applied to the time varying system represented by the flapping body in order to stabilize its attitude.
Domaines
Automatique / RobotiqueOrigine | Fichiers produits par l'(les) auteur(s) |
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