in this work, the authors investigate the design of an innovative hybrid-parallel fixed-wing UAV(Unmanned Aerial Vehicle) with VTOL (Vertical Take-Off and Landing) capabilities. The aim of this design is to obtain a system that conjugates hovering and maneuverability of a rotary-wing system with higher speed, efficiency, and autonomy offered by fixed-wing solutions. Also, multiple redundancies of power and propulsion system assure optimal fault mitigation and a high level of reliability that is required to work in dangerous harsh conditions. This work is mainly focused on system design and on simulation models that helped authors to shape and optimize the whole system.
Preliminary Design and Simulation of an Hybrid-Parallel, Fixed-Wing UAV with Eight-Rotors VTOL System / Luca Pugi; Lorenzo Berzi; Lorenzo Franchi; Armando Casazza; Giuseppe Mattei; Roberto Fiorenzan; Irene Domina. - ELETTRONICO. - (2022), pp. 0-0. (Intervento presentato al convegno 2022 IEEE International Conference on Environment and Electrical Engineering and 2022 IEEE Industrial and Commercial Power Systems Europe (EEEIC / I&CPS Europe)) [10.1109/EEEIC/ICPSEurope54979.2022.9854554].
Preliminary Design and Simulation of an Hybrid-Parallel, Fixed-Wing UAV with Eight-Rotors VTOL System
Luca Pugi;Lorenzo Berzi;Lorenzo Franchi;
2022
Abstract
in this work, the authors investigate the design of an innovative hybrid-parallel fixed-wing UAV(Unmanned Aerial Vehicle) with VTOL (Vertical Take-Off and Landing) capabilities. The aim of this design is to obtain a system that conjugates hovering and maneuverability of a rotary-wing system with higher speed, efficiency, and autonomy offered by fixed-wing solutions. Also, multiple redundancies of power and propulsion system assure optimal fault mitigation and a high level of reliability that is required to work in dangerous harsh conditions. This work is mainly focused on system design and on simulation models that helped authors to shape and optimize the whole system.File | Dimensione | Formato | |
---|---|---|---|
Preliminary_Design_and_Simulation_of_an_Hybrid-Parallel_Fixed-Wing_UAV_with_Eight-Rotors_VTOL_System.pdf
Accesso chiuso
Tipologia:
Pdf editoriale (Version of record)
Licenza:
Tutti i diritti riservati
Dimensione
701.79 kB
Formato
Adobe PDF
|
701.79 kB | Adobe PDF | Richiedi una copia |
I documenti in FLORE sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.