• DocumentCode
    3394071
  • Title

    Stable control for R/C helicopter

  • Author

    Tanaka, Kazuo ; Ohtake, Hiroshi ; Hori, Tsuyoshi

  • Author_Institution
    Dept. of Mech. Eng. & Intelligent Syst., Univ. of Electro-Commun., Chofu, Japan
  • Volume
    4
  • fYear
    2001
  • fDate
    25-28 July 2001
  • Firstpage
    2056
  • Abstract
    This paper presents the stable control for an R/C helicopter whose degree of freedom is reduced by fixing at a (joint) point. The nonlinear model of the R/C helicopter is constructed. After simplifying the nonlinear dynamics, we replace the simplified nonlinear dynamics with a Takagi-Sugeno fuzzy model. The control purpose is to realize good speed of response as well as stabilization with small control effort from practical control points of view. We present a decay rate condition and an input constraint condition that realize good speed of response and avoidance of actuator saturations, respectively. Both of them are represented in terms of linear matrix inequalities. By simultaneously solving them, we design a stable fuzzy controller that achieves good speed of response with small control effort
  • Keywords
    aircraft control; fuzzy control; helicopters; matrix algebra; robust control; R./C helicopter; Takagi-Sugeno model; aircraft control; dynamics; fuzzy control; linear matrix inequality; robust control; stabilization; Actuators; Control systems; Equations; Fuzzy control; Helicopters; Mechanical engineering; Nonlinear systems; Propellers; Stability; Takagi-Sugeno model;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    IFSA World Congress and 20th NAFIPS International Conference, 2001. Joint 9th
  • Conference_Location
    Vancouver, BC
  • Print_ISBN
    0-7803-7078-3
  • Type

    conf

  • DOI
    10.1109/NAFIPS.2001.944386
  • Filename
    944386