Modeling and Control of a Tilt tri-rotor AirplaneReport as inadecuate




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1 Heudiasyc - Heuristique et Diagnostic des Systèmes Complexes Compiègne 2 ASER LAFMIA - Laboratoire Franco-Mexicain d-Informatique et d-Automatique, Heudiasyc - Heuristique et Diagnostic des Systèmes Complexes Compiègne

Abstract : A helicopter offers the capability of hover, slow forward displacement, vertical take-off and landing while a conventional airplane has the performance of fast forward movement, long reach and superior endurance. The aim of this paper is to present the modelling and control of a tilt trirotor UAV-s configuration that combines the advantages of both rotary wing and fixed wing vehicle.





Author: Duc Anh Ta - Isabelle Fantoni - Rogelio Lozano -

Source: https://hal.archives-ouvertes.fr/



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