• DocumentCode
    1137237
  • Title

    Robust control design for aerospace applications

  • Author

    Yedavalli, Rama K.

  • Author_Institution
    Ohio State Univ., Columbus, OH, USA
  • Volume
    25
  • Issue
    3
  • fYear
    1989
  • fDate
    5/1/1989 12:00:00 AM
  • Firstpage
    314
  • Lastpage
    324
  • Abstract
    Time-domain control design for stability robustness of linear systems with structured uncertainty is addressed. Upper bounds on the linear perturbation of an asymptotically stable linear system are obtained, making it possible to maintain stability by using the structural information of the uncertainty. A quantitative measure called the stability robustness index is introduced and used to design controllers for robust stability. The proposed state feedback control design algorithm can be used, for a given set of perturbations, to select the range of control effort for which the system is stability-robust. Conversely it can be used, for a given control effort, to determine the size of the tolerable perturbation. The algorithm is illustrated with examples from aircraft control and large-space-structure control problems
  • Keywords
    aerospace control; aircraft control; control system synthesis; feedback; linear systems; stability; time-domain synthesis; aerospace applications; aircraft control; asymptotically stable linear system; large-space-structure control; linear perturbation; stability robustness; state feedback control design algorithm; structured uncertainty; time domain control; tolerable perturbation; Aerospace control; Asymptotic stability; Control design; Linear systems; Measurement uncertainty; Robust control; Robust stability; State feedback; Time domain analysis; Upper bound;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/7.30786
  • Filename
    30786