• DocumentCode
    488246
  • Title

    Optimization of Linear, Controlled Structures

  • Author

    Hunziker, K.Scott ; Kraft, Raymond H. ; Kosut, Robert T. ; Armstrong, Ernest S.

  • Author_Institution
    Boeing Aerospace and Electronics, Seattle, Washington
  • fYear
    1990
  • fDate
    23-25 May 1990
  • Firstpage
    854
  • Lastpage
    859
  • Abstract
    This paper describes an approach for the integrated design of linear controlled structures which is being investigated as part of NASA´s Control-Structures Interaction (CSI) methodology development program. The approach is integrated in the sense that the structure and its controller are simmultaneously designed. The design methodology employs constrained nonlinear optimization procedures based on analytically obtained gradients of the structural responses. Design of the controller is based on the so-called Q-parameterization theory, which parameterizes all closed-loop input/output maps achievable with stabilizing linear controllers. Very general objective and constraint functions are possible, and structural shape can be included in the design variables. This method has been partially implemented and demonstrated; early findings are reported.
  • Keywords
    Actuators; Aerospace electronics; Assembly; Control systems; Damping; Design methodology; Design optimization; Equations; Open loop systems; Wheels;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, 1990
  • Conference_Location
    San Diego, CA, USA
  • Type

    conf

  • Filename
    4790851