Review of Propulsion System Design Strategies for Unmanned Aerial Vehicles
The design of the propulsion system for Unmanned Aerial Vehicles (UAVs) demands an inclusive multidisciplinary approach from the earliest design phases, since every design choice strictly affects and is affected by the overall working conditions. This paper presents a review of the scientific litera...
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doaj-32c2cd5f7463441cb099cf0efa00e9822021-06-30T23:16:08ZengMDPI AGApplied Sciences2076-34172021-06-01115209520910.3390/app11115209Review of Propulsion System Design Strategies for Unmanned Aerial VehiclesCinzia Amici0Federico Ceresoli1Marco Pasetti2Matteo Saponi3Monica Tiboni4Simone Zanoni5Department of Mechanical and Industrial Engineering, University of Brescia, Via Branze, 38, 25123 Brescia, ItalyDepartment of Mechanical and Industrial Engineering, University of Brescia, Via Branze, 38, 25123 Brescia, ItalyDepartment of Information Engineering, University of Brescia, Via Branze, 38, 25123 Brescia, ItalyImbal Carton s.r.l., Via Gardesana, 54, 25080 Prevalle, ItalyDepartment of Mechanical and Industrial Engineering, University of Brescia, Via Branze, 38, 25123 Brescia, ItalyDepartment of Civil, Environmental, Architectural Engineering and Mathematics, University of Brescia, Via Branze, 43, 25123 Brescia, ItalyThe design of the propulsion system for Unmanned Aerial Vehicles (UAVs) demands an inclusive multidisciplinary approach from the earliest design phases, since every design choice strictly affects and is affected by the overall working conditions. This paper presents a review of the scientific literature focused on the design methods applied in defining and sizing the propulsion system of drones. The analysis, performed with a systematic approach, evaluated 123 papers according to two custom classification taxonomies, which investigated respectively the primary aim and specific content of the works. Finally, literature indications and hints were combined into an integrated framework for the functional design of the propulsion system of UAVs. The procedure aimed to support the designer in the preliminary selection of the propulsion candidates and the quick sizing of the supply system, during the first phases of the design process. According to the literature, design methods dramatically change depending on the expected applications and working conditions of UAVs, so that the detailed design of specific drone elements and propulsion components represents the focus of most of the papers in this field.https://www.mdpi.com/2076-3417/11/11/5209propulsion systemUnmanned Aerial Vehicles (UAVs)energy consumptionpower supply systemactuators’ characterizationdesign process |
collection |
DOAJ |
language |
English |
format |
Article |
sources |
DOAJ |
author |
Cinzia Amici Federico Ceresoli Marco Pasetti Matteo Saponi Monica Tiboni Simone Zanoni |
spellingShingle |
Cinzia Amici Federico Ceresoli Marco Pasetti Matteo Saponi Monica Tiboni Simone Zanoni Review of Propulsion System Design Strategies for Unmanned Aerial Vehicles Applied Sciences propulsion system Unmanned Aerial Vehicles (UAVs) energy consumption power supply system actuators’ characterization design process |
author_facet |
Cinzia Amici Federico Ceresoli Marco Pasetti Matteo Saponi Monica Tiboni Simone Zanoni |
author_sort |
Cinzia Amici |
title |
Review of Propulsion System Design Strategies for Unmanned Aerial Vehicles |
title_short |
Review of Propulsion System Design Strategies for Unmanned Aerial Vehicles |
title_full |
Review of Propulsion System Design Strategies for Unmanned Aerial Vehicles |
title_fullStr |
Review of Propulsion System Design Strategies for Unmanned Aerial Vehicles |
title_full_unstemmed |
Review of Propulsion System Design Strategies for Unmanned Aerial Vehicles |
title_sort |
review of propulsion system design strategies for unmanned aerial vehicles |
publisher |
MDPI AG |
series |
Applied Sciences |
issn |
2076-3417 |
publishDate |
2021-06-01 |
description |
The design of the propulsion system for Unmanned Aerial Vehicles (UAVs) demands an inclusive multidisciplinary approach from the earliest design phases, since every design choice strictly affects and is affected by the overall working conditions. This paper presents a review of the scientific literature focused on the design methods applied in defining and sizing the propulsion system of drones. The analysis, performed with a systematic approach, evaluated 123 papers according to two custom classification taxonomies, which investigated respectively the primary aim and specific content of the works. Finally, literature indications and hints were combined into an integrated framework for the functional design of the propulsion system of UAVs. The procedure aimed to support the designer in the preliminary selection of the propulsion candidates and the quick sizing of the supply system, during the first phases of the design process. According to the literature, design methods dramatically change depending on the expected applications and working conditions of UAVs, so that the detailed design of specific drone elements and propulsion components represents the focus of most of the papers in this field. |
topic |
propulsion system Unmanned Aerial Vehicles (UAVs) energy consumption power supply system actuators’ characterization design process |
url |
https://www.mdpi.com/2076-3417/11/11/5209 |
work_keys_str_mv |
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