• 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