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
Link To Document :
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