Modeling of an Unmanned Hybrid Aerial Vehicle

Abstract : 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.
Type de document :
Communication dans un congrès
Multi-conference on Systems and Control , Oct 2014, Antibes, France
Liste complète des métadonnées

https://hal.archives-ouvertes.fr/hal-01301730
Contributeur : Guillaume Ducard <>
Soumis le : mardi 12 avril 2016 - 17:18:24
Dernière modification le : mardi 30 mai 2017 - 01:17:21

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  • HAL Id : hal-01301730, version 1

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UNICE | UPMC | ISIR | I3S

Citation

Guillaume Ducard, Minh Duc Hua. Modeling of an Unmanned Hybrid Aerial Vehicle. Multi-conference on Systems and Control , Oct 2014, Antibes, France. <hal-01301730>

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