• DocumentCode
    146388
  • Title

    Modeling of propeller electric airplane and thrust control using advantage of electric motor

  • Author

    Takahashi, Koichi ; Fujimoto, Hiroshi ; Hori, Yoichi ; Kobayashi, Hideo ; Nishizawa, A.

  • Author_Institution
    Grad. Sch. of Frontier Sci., Univ. of Tokyo, Kashiwa, Japan
  • fYear
    2014
  • fDate
    14-16 March 2014
  • Firstpage
    482
  • Lastpage
    487
  • Abstract
    Electrical airplanes (EAs) have become practical in the recent years. Considering the increase of demand on smaller aircraft and the attention to environmental issues, the demand on small EAs is expected to grow in the coming decade. However, the accident rate of small aircrafts is higher than that of larger aircrafts, so ensuring higher safety of EA is very urgent. In this paper, the new thrust control method based on new EA propeller plant is proposed. This method can be applied to new advanced flight control systems of EA, which can be expected to improve the safety of EA. The effectiveness of the proposed method is verified through simulations and experiments.
  • Keywords
    aerospace accidents; aircraft control; electric motors; propellers; EA propeller plant; accident rate; aircraft; electric motor; flight control system; propeller electric airplane; thrust control method; Airplanes; Atmospheric modeling; Mathematical model; Propellers; Radiation detectors; Torque; Vectors;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Advanced Motion Control (AMC),2014 IEEE 13th International Workshop on
  • Conference_Location
    Yokohama
  • Type

    conf

  • DOI
    10.1109/AMC.2014.6823329
  • Filename
    6823329