• DocumentCode
    2200126
  • Title

    Functional feedback in an extremum seeking loop

  • Author

    Banavar, R.N. ; Chichka, D.F. ; Speyer, J.L.

  • Volume
    2
  • fYear
    2001
  • fDate
    2001
  • Firstpage
    1316
  • Abstract
    We analyze the effect of functional feedback in an extremum seeking loop. Our study is motivated by a formation flight problem where the trailing aircraft experiences an outward rolling moment as the vortex effects of the leading aircraft come into play. Viewed as the extremized functional, this rolling moment feeds itself back to the lateral dynamics of the aircraft. In the initial half of the paper we impose restrictions on the curvature of the extremized functional and examine the effect under the assumption of a dynamic time-scale separation between the tracking loops of the linear dynamical system and the extremum seeking loop; in the latter half we remove both these assumptions and instead impose assumed functional forms on the extremized functional
  • Keywords
    aircraft control; feedback; function approximation; functional equations; linear systems; stability; dynamic time-scale separation; extremum seeking loop; formation flight problem; functional feedback; lateral dynamics; linear dynamical system; outward rolling moment; tracking loops; trailing aircraft; vortex effects; Aerodynamics; Aerospace engineering; Aircraft; Application specific integrated circuits; Control systems; Engines; Feedback loop; Feeds; Measurement; Tracking loops;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Decision and Control, 2001. Proceedings of the 40th IEEE Conference on
  • Conference_Location
    Orlando, FL
  • Print_ISBN
    0-7803-7061-9
  • Type

    conf

  • DOI
    10.1109/.2001.981072
  • Filename
    981072