• DocumentCode
    184017
  • Title

    Attitude tracking control of a quadrotor based on absolutely continuous fractional integral sliding modes

  • Author

    Munoz-Vazquez, Aldo-Jonathan ; Parra-Vega, Vicente ; Sanchez-Orta, Anand ; Garcia, O. ; Izaguirre-Espinoza, Carlos

  • Author_Institution
    Robot. & Adv. Manuf. Div., Res. Center for Adv. Studies (Cinvestav), Saltillo, Mexico
  • fYear
    2014
  • fDate
    8-10 Oct. 2014
  • Firstpage
    717
  • Lastpage
    722
  • Abstract
    The model-free sliding mode control based on fractional order sliding surface is built upon: i) An absolutely continuous control structure that does not require the exact dynamic model to induce a fractional sliding motion in finite time, and ii) A methodology to design fractional references with a clear counterpart in the frequency domain is proposed. This in order to improve the system response, in particular the transient period, and to generate a high-performance during the sliding motion. Numerical simulations support the proposal and illustrates the closed-loop system, which provides a better insight of the proposed scheme.
  • Keywords
    attitude control; closed loop systems; frequency-domain analysis; helicopters; numerical analysis; variable structure systems; absolutely continuous control structure; absolutely continuous fractional integral sliding modes; closed-loop system; exact dynamic model; fractional order sliding surface; fractional sliding motion; model-free sliding mode control; numerical simulations; quadrotor attitude tracking control; Attitude control; Frequency-domain analysis; Laplace equations; Manifolds; Robots; Sliding mode control; Transient analysis;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Applications (CCA), 2014 IEEE Conference on
  • Conference_Location
    Juan Les Antibes
  • Type

    conf

  • DOI
    10.1109/CCA.2014.6981425
  • Filename
    6981425