• DocumentCode
    306714
  • Title

    Output tracking and steady state for nonlinear systems

  • Author

    Hunt, L.R. ; Meyer, George ; Ramakrishna, Viswanath

  • Author_Institution
    Center for Eng. Math., Texas Univ., Richardson, TX, USA
  • Volume
    2
  • fYear
    1996
  • fDate
    11-13 Dec 1996
  • Firstpage
    2064
  • Abstract
    The problem driving this work is exact output tracking using stable inversion for nonlinear systems (models of aircraft). The problem of stable inversion evolves to a time varying nonlinear system with inputs and the search for a unique bounded continuous solution on (-∞,∞) in response to a bounded input on (-∞,∞). We want to show that all bounded continuous solutions on 0⩽t<∞ converge to this unique one as t→∞ under the appropriate assumptions. The bounded and continuous solution on (-∞,∞) can be thought of as a nonlinear steady state. This exactly parallels the idea of steady state for a time invariant linear system whose homogenous part has no eigenvalues on the imaginary axis. In response to a bounded input on (-∞,∞) is the unique bounded and continuous solution on (-∞,∞). All bounded and continuous solutions on 0⩽t<∞ must converge to this unique one, which is called the steady state. Hence, under appropriate assumptions, steady state solutions exist for nonlinear systems even though the principle of superposition does not hold
  • Keywords
    aircraft control; nonlinear control systems; stability; time-varying systems; aircraft; exact output tracking; nonlinear systems; stable inversion; steady state; time invariant linear system; time-varying nonlinear system; unique bounded continuous solution; Aircraft; Differential equations; Eigenvalues and eigenfunctions; Linear systems; NASA; Nonlinear systems; Regulators; Steady-state; Time varying systems; Trajectory;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Decision and Control, 1996., Proceedings of the 35th IEEE Conference on
  • Conference_Location
    Kobe
  • ISSN
    0191-2216
  • Print_ISBN
    0-7803-3590-2
  • Type

    conf

  • DOI
    10.1109/CDC.1996.572890
  • Filename
    572890