• DocumentCode
    307269
  • Title

    Synthesis of optimal H controllers via LQG-based loop shaping design

  • Author

    Yang, Ciann-Dong ; Chang, Chia-Yuan ; Sun, Yun-Ping

  • Author_Institution
    Inst. of Aeronaut. & Astronaut., Nat. Cheng Kung Univ., Tainan, Taiwan
  • Volume
    1
  • fYear
    1996
  • fDate
    11-13 Dec 1996
  • Firstpage
    739
  • Abstract
    Synthesis of optimal H controllers is formulated as a loop-shaping problem where the desired closed-loop shape to be pursued is a flat frequency response of the largest singular value. The weighted H2 optimization technique used in LQG/LTR is exploited in the loop shaping procedures to generate a sequence of H2 controllers converging to the optimal H controller. The resulting optimal H controller not only has the inherent robust property due to H criterion but also possesses the nice H2 control structure, being easy to compute and implement. A flight control example is demonstrated to show that the numerical accuracy of the present LQG-based H synthesis is comparable to the conventional H approach, i.e. γ-iteration
  • Keywords
    H control; aircraft control; control system synthesis; frequency response; linear quadratic Gaussian control; military aircraft; optimisation; robust control; transfer function matrices; γ-iteration; H criterion; H2 controllers; LQG-based loop shaping design; LQG/LTR; closed-loop shape; flat frequency response; flight control; numerical accuracy; optimal H controllers; weighted H2 optimization technique; Aerospace control; Control system synthesis; Control systems; Frequency response; Hydrogen; Optimal control; Robust control; Shape control; Stability criteria; Sun;
  • 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.1996.574441
  • Filename
    574441