• 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