• DocumentCode
    2224836
  • Title

    Fuzzy Controller for small size unmanned aerial vehicles

  • Author

    Stojcsics, Dániel

  • Author_Institution
    John von Neumann Fac. of Inf., Obuda Univ., Budapest, Hungary
  • fYear
    2012
  • fDate
    26-28 Jan. 2012
  • Firstpage
    91
  • Lastpage
    95
  • Abstract
    The AERObot autopilot for small and medium size unmanned aerial vehicles (UAVs) developed at Óbuda Universtiy has multiple control systems. It is possible to switch between the control systems even during in flight. The purpose of the current research was to examine the applicability of full fuzzy flight control (takeoff, cruise and land) in unmanned aerial vehicles instead of partial or hybrid control [1, 2, 3]. The easy tuning of the parameters and features is quite important because one autopilot should control different sized and designed planes. Since the safety of the flight, life and value is the most important, real test flights should always be performed after many hours of computer simulation. For this purpose Hardware In the Loop simulation was used. The advantage of this simulation is that the very same environment can be created as in real flights (e.g. atmospheric, aerodynamic, propulsion model, different weather conditions). After successful simulations the real test flights can be started.
  • Keywords
    aerospace control; air safety; autonomous aerial vehicles; fuzzy control; microrobots; AERObot autopilot; Óbuda Universtiy; UAV; cruise control; flight safety; fuzzy flight control; hardware-in-the-loop simulation; land control; life safety; medium-size unmanned aerial vehicles; small-size unmanned aerial vehicles; takeoff control; value safety; Atmospheric modeling; Computational modeling; Control systems; Informatics; Mathematical model; Navigation; Unmanned aerial vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Applied Machine Intelligence and Informatics (SAMI), 2012 IEEE 10th International Symposium on
  • Conference_Location
    Herl´any
  • Print_ISBN
    978-1-4577-0196-2
  • Type

    conf

  • DOI
    10.1109/SAMI.2012.6208935
  • Filename
    6208935