Development of a High Power Density Drive System for Unmanned Aerial Vehicles

被引:25
|
作者
Schiestl, Martin [1 ]
Marcolini, Federico [2 ]
Incurvati, Maurizio [1 ]
Capponi, Fabio Giulii [2 ]
Starz, Ronald [1 ]
Caricchi, Federico [2 ]
Rodriguez, Alejandro Secades [1 ]
Wild, Lukas [1 ]
机构
[1] MCI Management Ctr Innsbruck, Dept Mechatron, A-6020 Innsbruck, Austria
[2] Univ Roma La Sapienza, Dept Astronaut Elect & Energy Engn, I-00185 Rome, Italy
关键词
Propellers; Density measurement; Power system measurements; Power electronics; Unmanned aerial vehicles; Resilience; Reliability; Aerospace safety; fault tolerance; gallium nitride; integrated design; motor drives; thermal analysis; thermal modeling; unmanned aerial vehicles (UAVs); variable speed drives; PERMANENT-MAGNET MACHINE; AXIAL-FLUX; DESIGN; DRONES;
D O I
10.1109/TPEL.2020.3013899
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
Unmanned aerial vehicles are characterized by a set of requirements, like high efficiency, resiliency, and reliability that conflict with the other main requirement of high power density aimed at minimizing the overall weight and size. This article proposes a novel, modular multiphase drive for a quadrotor drone, realized through the integration of an axial flux permanent magnet machine and a GaN-based power electronic converter. After an overview of the design process, starting from the propeller choice, a brief description of the system components is presented. Focusing specifically on the power electronic converter, the article then presents a full analysis of its electrical and thermal performance. Extensive experimental tests allows to validate the predictions of the design and simulation stages and demonstrated the expected high power density levels.
引用
收藏
页码:3159 / 3171
页数:13
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