• DocumentCode
    3469412
  • Title

    Discrete time H control laws for a high performance helicopter

  • Author

    Walker, D. ; Postlethwaite, I.

  • Author_Institution
    Dept. of Eng., Leicester Univ., UK
  • fYear
    1991
  • fDate
    11-13 Dec 1991
  • Firstpage
    128
  • Abstract
    An application of the 2 Ricatti equation theory for discrete-time H optimization is presented. Two helicopter flight control laws are designed. The first design is based on a normalized coprime factor stabilization. The second uses a standard 2-block sensitivity and robustness formulation. The designs presented here are novel in that the problem is posed from the outset as a discrete-time (DT) problem which is solved using recent game-theoretic formulae for DT H optimization. It is shown that by suitable choice of weighting functions it is possible to obtain directly DT controllers that give good levels of performance and robustness
  • Keywords
    aircraft control; control system synthesis; discrete time systems; game theory; helicopters; optimal control; optimisation; stability; 2-block sensitivity; Ricatti equation; aircraft control; control system synthesis; discrete-time H optimization; helicopter; normalized coprime factor stabilization; optimal control; robustness; Aerodynamics; Aerospace control; Aerospace engineering; Aircraft propulsion; Design optimization; Equations; H infinity control; Helicopters; Open loop systems; Riccati equations; Robust control; Robust stability; Robustness;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Decision and Control, 1991., Proceedings of the 30th IEEE Conference on
  • Conference_Location
    Brighton
  • Print_ISBN
    0-7803-0450-0
  • Type

    conf

  • DOI
    10.1109/CDC.1991.261269
  • Filename
    261269