• DocumentCode
    1325018
  • Title

    Assignment of reduced sensitivity eigenstructure

  • Author

    Ensor, J. ; Davies, R.

  • Author_Institution
    Dept. of Electron., York Univ., UK
  • Volume
    147
  • Issue
    1
  • fYear
    2000
  • fDate
    1/1/2000 12:00:00 AM
  • Firstpage
    104
  • Lastpage
    110
  • Abstract
    The presented technique addresses the problem of maintaining the powerful design simplicity and visibility of eigenstructure assignment, while reducing closed-loop eigenstructure sensitivity to dominant parameter variations. The method results from consideration of the allowable eigenvector subspace as a complete description of the eigenstructure assignment problem. Variations in open-loop system dynamics can thus be visualised as movements of the closed-loop allowable subspace. If a nonlinear model is linearised about two operating points with intersecting subspaces, assignment from the intersection will yield the same closed-loop eigenstructure at both operating points. This hypothesis is proven, and the analysis extended to include the case of non-intersecting subspaces. This reduced subspace design method has been tested on an eighth-order helicopter model that exhibits significant nonlinearity when forward speed is varied. The results demonstrate a considerable reduction in variation of the closed-loop eigenstructure over conventional techniques
  • Keywords
    aircraft control; closed loop systems; control system synthesis; dynamics; eigenstructure assignment; helicopters; linear systems; sensitivity analysis; state feedback; closed-loop systems; dynamics; eigenstructure assignment; eigenvectors; helicopter control; linear time invariant systems; sensitivity analysis; state feedback;
  • fLanguage
    English
  • Journal_Title
    Control Theory and Applications, IEE Proceedings -
  • Publisher
    iet
  • ISSN
    1350-2379
  • Type

    jour

  • DOI
    10.1049/ip-cta:20000137
  • Filename
    838056