Modeling and Control of a Convertible Mini-UAV
Résumé
The aim of this paper is to present a UAV's configuration that combines the manoeuvrability of a rotary wing vehicle (helicopter) such as slow forward displacement, vertical take off and landing, and the performance of a fixed wing vehicle (plane) such as fast forward movement, long reach and superior endurance.
Origine | Fichiers produits par l'(les) auteur(s) |
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