DocumentCode
1990252
Title
The stability performance analysis of ducted fan UAV based on fluent
Author
Wang, Shuai ; Qi, Xiaohui
Author_Institution
Dept. of Opt. & Electron. Eng., Ordnance Eng. Coll., Shijiazhuang, China
fYear
2011
fDate
16-18 Sept. 2011
Firstpage
1370
Lastpage
1373
Abstract
In this paper the fluent software was used to solve the stability of ducted fan UAV problems. The researchers calculated, programming, before and after repeated treatment and so on inputs, inefficient labor was reduced. More energy and time was considered into the nature of the problem, optimization algorithm selection and parameter setting, so the work efficiency was improved. The pneumatic parameter of the wing was introduced importantly. The basic control parameters were set, and the posture of wing was simulated in the 0-15 degrees. Finally, the results showed that the stability of the ducted fan UAV in the 0-10 degrees was better than after 10 degrees, the reliability of aerodynamic parameters was decreased rapidly.
Keywords
aerodynamics; aerospace components; aerospace computing; aerospace robotics; aircraft control; computational fluid dynamics; fans; mobile robots; pneumatic systems; remotely operated vehicles; CFD; FLUENT software; aerodynamic parameter reliability; ducted fan UAV; optimization algorithm selection; pneumatic parameter; stability performance analysis; wing; work efficiency; Aerodynamics; Atmospheric modeling; Equations; Mathematical model; Power system stability; Software; Stability analysis; Ducted fan; FLUENT; Stability; UAV;
fLanguage
English
Publisher
ieee
Conference_Titel
Electrical and Control Engineering (ICECE), 2011 International Conference on
Conference_Location
Yichang
Print_ISBN
978-1-4244-8162-0
Type
conf
DOI
10.1109/ICECENG.2011.6057856
Filename
6057856
Link To Document