Aerodynamic modeling of the Skywalker X8 Fixed-Wing Unmanned Aerial Vehicle

被引：0

作者：

Gryte, Kristofer ^{[1
]}

Hann, Richard ^{[1
]}

Alam, Mushfiqul ^{[2
]}

Rohac, Jan ^{[2
]}

Johansen, Tor Arne ^{[1
]}

Fossen, Thor I. ^{[1
]}

机构：

[1] Norwegian Univ Sci & Technol, Dept Engn Cybernet, Ctr Autonomous Marine Operat & Syst NTNU AMOS, Trondheim, Norway

[2] Czech Tech Univ, Prague, Czech Republic

来源：

2018 INTERNATIONAL CONFERENCE ON UNMANNED AIRCRAFT SYSTEMS (ICUAS) | 2018年

关键词：

OBSERVER; UAV;

D O I：

暂无

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：

With advanced control, estimation and simulation requirements in unmanned aerial systems comes the need for sophisticated aerodynamic models. This paper reviews two common means for establishing such models; numerical design tools and wind tunnel testing, by presenting strengths and potential problems, in a "lessons learned"-manner. As a case study throughout the paper, a six degrees-of-freedom aerodynamic model of the Skywalker X8 fixed-wing unmanned aerial vehicle is presented.

引用

页码：826 / 835

页数：10

共 33 条

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