DocumentCode
2170524
Title
Aerodynamic data model analysis and simulation of ducted fan UAV
Author
Shuai, Wang ; Xiao-hui, Qi
Author_Institution
Dept. of Opt. & Electron. Eng., Ordnance Eng. Coll., Shijiazhuang, China
fYear
2011
fDate
9-11 Sept. 2011
Firstpage
699
Lastpage
702
Abstract
The ducted fan UAV was simply introduced in this paper. The dynamics characteristic was also analysed. The dynamics scalar equation of mass centre motion and surround mass centre motion of aircraft were built. The lift, drag, yawing force and pitch, drift, roll moment of UAV were analyzed through FLUENT simulation software. Simulation image with good effect was got. The dynamics characteristic of ducted fan UAV was reflected well and truly. This article used a mass of analog simulation software for the test. Not only reduce investment outlay, but also save time and cost of the test. We could observe the dynamics characteristic of UAV from theory and experience through this paper. The research result can offer help for autonomous flight of ducted fan UAV.
Keywords
aerodynamics; aircraft; drag; remotely operated vehicles; FLUENT simulation software; aerodynamic data model analysis; aircraft; analog simulation software; drag; ducted fan UAV; dynamics scalar equation; lift; mass centre motion; roll moment; yawing force; Aerodynamics; Aircraft; Atmospheric modeling; Equations; Mathematical model; Vectors; Aerodynamics; Ducted Fan UAV; FLUENT; Modeling; Simulation;
fLanguage
English
Publisher
ieee
Conference_Titel
Electronics, Communications and Control (ICECC), 2011 International Conference on
Conference_Location
Ningbo
Print_ISBN
978-1-4577-0320-1
Type
conf
DOI
10.1109/ICECC.2011.6066382
Filename
6066382
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