• DocumentCode
    2292231
  • Title

    LDV approach to circular trajectory tracking of the underactuated hovercraft model

  • Author

    Ariaei, Fariba ; Jonckheere, Edmond

  • Author_Institution
    Dept. of Electr. Eng.-Syst., Southern California Univ., Los Angeles, CA
  • fYear
    2006
  • fDate
    14-16 June 2006
  • Abstract
    This paper shows that circular trajectory tracking of an underactuated hovercraft vehicle can be achieved by linear dynamically varying (LDV) techniques. LDV control is a technique for directing a controlled trajectory to be asymptotically synchronized with a preselected trajectory. A linearized tracking error model is obtained as a linear system parameterized by the nominal nonlinear dynamics. The nontrivial part of the LDV theory is to prove existence of a sufficiently well behaved solution to the partial differential Riccati equation. This in turn provides an exact solution to a Lyapunov inequality, showing that the underactuated hovercraft can be stabilized around the circular trajectory
  • Keywords
    Lyapunov methods; Riccati equations; hovercraft; linear systems; nonlinear dynamical systems; partial differential equations; position control; stability; Lyapunov inequality; circular trajectory tracking; linear dynamically varying technique; linearized tracking error model; nominal nonlinear dynamics; partial differential Riccati equation; underactuated hovercraft model; Closed loop systems; Differential equations; Linear systems; Nonlinear dynamical systems; Nonlinear equations; Partial differential equations; Riccati equations; State-space methods; Trajectory; Vehicle dynamics;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, 2006
  • Conference_Location
    Minneapolis, MN
  • Print_ISBN
    1-4244-0209-3
  • Electronic_ISBN
    1-4244-0209-3
  • Type

    conf

  • DOI
    10.1109/ACC.2006.1657329
  • Filename
    1657329