• DocumentCode
    278454
  • Title

    Weighting function specification in H∞ design [battlefield helicopter]

  • Author

    Kellett, M.G. ; White, B A

  • Author_Institution
    R. Mil. Coll. of Sci., Shrivenham, UK
  • fYear
    1991
  • fDate
    33401
  • Firstpage
    42461
  • Lastpage
    42467
  • Abstract
    This paper describes the application of H∞ to the design of a controller for a battlefield helicopter. It shows the effect of the choice of the weighting functions on the performance of the resulting closed loop system, and indicates how to utilise the freedom of choice. The appropriate handling qualities requirements documents describe the response shapes that are desirable for particular flight conditions, and these can be used as guidelines for further development of the cost function weights. Bandwidths on selected channels can be manipulated to a certain extent by moving the sensitivity function weights, and overshoots can be corrected by careful targeting of the rate feedback channel weights. Actuator movements can be monitored by examining time responses, and these give useful indicators of the feasibility of any design changes
  • Keywords
    aircraft control; control system synthesis; helicopters; military equipment; optimal control; stability; H∞ design; actuator movement monitoring; battlefield helicopter; channel bandwidth manipulation; closed loop system; control design; cost function weights; handling qualities requirements; overshoot correction; rate feedback channel weights; response shapes; sensitivity function weights; time responses; weighting function specification;
  • fLanguage
    English
  • Publisher
    iet
  • Conference_Titel
    Practical Methods for Robust Control System Design, IEE Colloquium on
  • Conference_Location
    London
  • Type

    conf

  • Filename
    181751