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
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;
Conference_Titel :
Electrical and Control Engineering (ICECE), 2011 International Conference on
Conference_Location :
Yichang
Print_ISBN :
978-1-4244-8162-0
DOI :
10.1109/ICECENG.2011.6057856