• DocumentCode
    3467858
  • Title

    Generalized singular robust control design

  • Author

    Juang, J.C. ; Lin, C.F. ; Cloutier, J.R. ; Evers, J.H.

  • Author_Institution
    American GNC Corp., Chatsworth, CA, USA
  • fYear
    1991
  • fDate
    11-13 Dec 1991
  • Firstpage
    2995
  • Abstract
    A generalized singular robust control approach for missile autopilot design is described. This approach unifies the generalized singular linear quadratic linear quadratic Gaussian, and worst-case H control design methods using the generalized Hamiltonian formulation and structure algorithm. Extensions of this method to multiple-criterion autopilot design problems are also discussed. The approach considered provides a constructive algorithm to design a multiple-criterion controller and offers new insights into the relationship between multiple H2/H and multiple H /H designs
  • Keywords
    aerospace control; control system synthesis; missiles; optimal control; LQG control; aerospace control; generalized Hamiltonian formulation; generalized singular robust control; missile autopilot; multiple-criterion autopilot; singular linear quadratic control; worst-case H control; Aerodynamics; Algorithm design and analysis; Control design; Drag; Force control; Missiles; Observability; Robust control; Robust stability; Robustness; Uncertainty;
  • 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.1991.261096
  • Filename
    261096