• DocumentCode
    1368952
  • Title

    Adaptive Output Feedback Design Using Asymptotic Properties of LQG/LTR Controllers

  • Author

    Lavretsky, Eugene

  • Author_Institution
    Boeing Co., Huntington Beach, CA, USA
  • Volume
    57
  • Issue
    6
  • fYear
    2012
  • fDate
    6/1/2012 12:00:00 AM
  • Firstpage
    1587
  • Lastpage
    1591
  • Abstract
    This technical note introduces an observer-based adaptive output feedback tracking control design for multi-input-multi-output dynamical systems with matched uncertainties. The reported methodology exploits asymptotic behavior of LQG/LTR regulators. Sufficient conditions for closed-loop stability and uniform ultimate boundedness of the corresponding tracking error dynamics are formulated. This method is valid for systems whose nominal linearized dynamics are controllable and observable. We assume that the number of the system measured outputs (sensors) is greater than the number of the control inputs (actuators) and that the system output-to-input matrix product has full column rank. In this case, the system can be “squared-up” (i.e., augmented) using pseudo-control signals to yield relative degree one minimum-phase dynamics. Since it is known that the “squaring-up” problem is solvable for any controllable observable triplet (A, B, C), the proposed design is applicable to systems whose regulated output dynamics may be non-minimum phase or have a high relative degree. A simulation example is presented to demonstrate key design features.
  • Keywords
    MIMO systems; adaptive control; aerospace control; asymptotic stability; closed loop systems; control system synthesis; feedback; linear quadratic Gaussian control; linearisation techniques; matrix multiplication; observers; uncertain systems; LQG/LTR controllers; LQG/LTR regulators; MIMO system; asymptotic properties; closed loop stability; controllable observable triplet; full column rank; linearized dynamics; matched uncertainties; minimum-phase dynamics; multiple-input multiple-output dynamical systems; nonminimum phase; observer-based adaptive output feedback tracking control design; pseudocontrol signals; squaring-up problem; sufficient conditions; system output-to-input matrix product; tracking error dynamics; uniform ultimate boundedness; Aerodynamics; Control design; Observers; Output feedback; Uncertainty; Vehicle dynamics; Vehicles; Flight control; optimal and adaptive control; output feedback;
  • fLanguage
    English
  • Journal_Title
    Automatic Control, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9286
  • Type

    jour

  • DOI
    10.1109/TAC.2011.2174692
  • Filename
    6069834