• DocumentCode
    3477185
  • Title

    Control of a sight system flexible structure: A H design

  • Author

    Michelin, J.-M. ; Coustal, P.

  • Author_Institution
    SERE Co., Asnieres, France
  • fYear
    1991
  • fDate
    11-13 Dec 1991
  • Firstpage
    1640
  • Abstract
    The basic function of a helicopter-boarded sight system is to stabilize the optonic sensors´ lines of sight. Meeting this functional requirement is increasingly difficult (performance improvement, severe carrier environment, decreasing of size and weight). To solve this problem, the control of sight mechanical flexible structure must be considered. H design has proved to be successful in dealing with the different structural disturbances and constraints. A novel W4 weight is introduced in the H standard formulation to ensure the local positivity of the compensated open-loop plant. This property allows the system to be robust against damping variations encountered on flexible structures
  • Keywords
    aircraft instrumentation; control system synthesis; helicopters; image sensors; optimal control; stability; H design; W4 weight; compensated open-loop plant; control system synthesis; flexible structure control; helicopter boarded sight systems; lines of sight; optimal control; optronic sensors; severe carrier environment; stability; Control systems; Damping; Flexible structures; H infinity control; Helicopters; Mechanical sensors; Military aircraft; Modems; Optical sensors; Robustness; Sensor systems; Vibrations;
  • 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.1991.261685
  • Filename
    261685