• DocumentCode
    700710
  • Title

    A toy more difficult to control than the real thing

  • Author

    Mullhaupt, P. ; Srinivasan, B. ; Levine, J. ; Bonvin, D.

  • Author_Institution
    Inst. d´Autom., Ecole Polytech. Fed. de Lausanne, Lausanne, Switzerland
  • fYear
    1997
  • fDate
    1-7 July 1997
  • Firstpage
    1652
  • Lastpage
    1657
  • Abstract
    Standard helicopters use the propeller angle to alter the aerodynamic force and have been shown to be feedback linearizable with the pitch, yaw and roll angles being the flat outputs. In this work, a-two-degree-of-freedom, laboratory-scale helicopter-like system (termed the toycopter), where the aerodynamic force is manipulated using the propeller speed, is considered. For such a system the yaw and pitch angles are not flat outputs contrarily of the real helicopters. Moreover, the system does not seem to be flat and is shown to admit at most a one dimensional defect. Various properties of this system are investigated to illustrate the difficulties that arise in the control of the toycopter.
  • Keywords
    aerodynamics; helicopters; propellers; aerodynamic force; feedback linearization; pitch angles; propeller speed; toycopter control; two-degree-of-freedom laboratory-scale helicopter-like system; yaw angles; Aerodynamics; Blades; Couplings; Force; Helicopters; Propellers; Torque; Differential Flatness; Helicopters; Modeling; Underactuated systems;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Conference (ECC), 1997 European
  • Conference_Location
    Brussels
  • Print_ISBN
    978-3-9524269-0-6
  • Type

    conf

  • Filename
    7082340