• DocumentCode
    722935
  • Title

    Flexible membrane wing warping using tendon-sheath mechanism

  • Author

    Shian Lee ; Tjahjowidodo, Tegoeh ; Seung Ki Moon

  • Author_Institution
    Sch. of Mech. & Aerosp. Eng., Nanyang Technol. Univ., Singapore, Singapore
  • fYear
    2015
  • fDate
    16-19 June 2015
  • Firstpage
    624
  • Lastpage
    629
  • Abstract
    Flexible membrane wings have many advantages, but has very little roll control authority. In this paper, the flexible membrane wing is actuated using a tendon-sheath mechanism to achieve roll control and also allowing the wing to fold. The characteristics of the flexible wing, as well as the wing warping actuation approach is discussed in this paper. The experimental setup and results are shown. The characteristics of the tendon-sheath is shown to be suitable for flexible wing actuation. A simple nonlinear curve fitting model is also presented.
  • Keywords
    aerospace components; autonomous aerial vehicles; curve fitting; nonlinear control systems; UAV; flexible membrane wing warping; nonlinear curve fitting model; roll control; tendon-sheath mechanism; unmanned aerial vehicles; wing warping actuation approach; Aerodynamics; Force; Friction; Hysteresis; Servomotors; Shape; Tendons; Flexible membrane wing; hysteresis modeling; tendon-sheath mechanism; wing warping;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control and Automation (MED), 2015 23th Mediterranean Conference on
  • Conference_Location
    Torremolinos
  • Type

    conf

  • DOI
    10.1109/MED.2015.7158816
  • Filename
    7158816