Modeling of an Unmanned Hybrid Aerial Vehicle
Résumé
In this paper, the mathematical modeling of a
hybrid aerial vehicle is presented. This vehicle is a combination
of a fixed-wing aircraft and a multirotor helicopter. This
vehicle is thus capable of vertical take off and landing (VTOL)
and of cruising forward flight. The thrust is generated by 4
propellers which can pivot and thus the direction of thrust is
controllable. This paper details the nonlinear dynamics of the
aircraft, including major aerodynamics effects and thrust-tilting
effects, resulting in a realistic simulator for control design and
validation.
Domaines
Sciences de l'ingénieur [physics]
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Ducard_Hua_ModelingVTOL_MSC2014_accepted_version.pdf (616.51 Ko)
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Licence : Copyright (Tous droits réservés)