Development of an Unmanned Vertical Take-off and Landing Aircraft for Medical Express UAV Challenge

被引:0
|
作者
Czyba, Roman [1 ]
Lemanowicz, Marcin [2 ]
Simon, Michal [3 ]
Kudala, Tomasz [3 ]
Gorol, Zbigniew [1 ]
Galeja, Maciej [1 ]
Hanke, Karol [1 ]
Sikora, Adam [1 ]
Grabowski, Wojciech [1 ]
Ryczko, Lukasz [3 ]
Zurawski, Mateusz [3 ]
Kapala, Paulina [3 ]
Kreihs, Karol [1 ]
Langner, Piotr [3 ]
机构
[1] Silesian Tech Univ, Dept Automat Control, Fac Automat Control Elect & Comp Sci, 16 Akad St, PL-44100 Gliwice, Poland
[2] Silesian Tech Univ, Fac Chem, Dept Chem Engn & Proc Design, 16 Akad St, PL-44100 Gliwice, Poland
[3] Silesian Tech Univ, Fac Mech Engn, 16 Akad St, PL-44100 Gliwice, Poland
关键词
CA If; VTOL; CAD Design; CTD; Control System;
D O I
暂无
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This paper presents a design process of unmanned vertical take-off and landing aircraft, developed by the High Flyers team from Silesian University of Technology, who decided to participate in the Medical Express UAV Challenge competition. The designed system is described as a hybrid platform, where different operating modes correspond to the vertical flight, transition and spatial flight in the airframe system. Explanation of an iterative design process with the contribution of CAD design, CFD analysis and control system design in particular flight modes is presented. Simulation results are carried out to corroborate the design control system. Finally, the fast prototyping of proposed control stratep: as well as manufacturing process is shown.
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页码:461 / 466
页数:6
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