• DocumentCode
    2847273
  • Title

    On tracking for the PVTOL model with bounded feedbacks

  • Author

    Gruszka, A. ; Malisoff, M. ; Mazenc, F.

  • Author_Institution
    Dept. of Math., Louisiana State Univ., Baton Rouge, LA, USA
  • fYear
    2011
  • fDate
    June 29 2011-July 1 2011
  • Firstpage
    1428
  • Lastpage
    1433
  • Abstract
    We study a class of feedback tracking problems for the planar vertical takeoff and landing (PVTOL) aircraft dynamics, which is a benchmark model in aerospace engineering. After a survey of the literature on the model, we construct new feedback stabilizers for the PVTOL tracking dynamics. The novelty of our contribution is in the boundedness of our feedback controllers and their applicability to cases where the velocity measurements may not be available, coupled with the uniform global asymptotic stability and uniform local exponential stability of the closed loop tracking dynamics, the generality of our class of trackable reference trajectories, and the input-to-state stable performance of the closed loop tracking dynamics with respect to actuator errors. Our proofs are based on a new bounded backstepping result. We illustrate our work in a tracking problem along a circle.
  • Keywords
    actuators; aerospace engineering; aircraft control; asymptotic stability; closed loop systems; feedback; tracking; PVTOL aircraft dynamics; PVTOL model; actuator errors; aerospace engineering; bounded feedbacks; closed loop tracking dynamics; feedback controllers; feedback tracking problems; global asymptotic stability; local exponential stability; planar vertical takeoff and landing aircraft dynamics; Actuators; Aircraft; Asymptotic stability; Atmospheric modeling; Backstepping; Tracking loops; Trajectory;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference (ACC), 2011
  • Conference_Location
    San Francisco, CA
  • ISSN
    0743-1619
  • Print_ISBN
    978-1-4577-0080-4
  • Type

    conf

  • DOI
    10.1109/ACC.2011.5990817
  • Filename
    5990817