• DocumentCode
    3075685
  • Title

    H robust control synthesis for a fighter performing a coordinated bank turn

  • Author

    Thompson, Peter M. ; Chiang, Richard Y.

  • Author_Institution
    Syst. Technol. Inc., Hawthorne, CA, USA
  • fYear
    1990
  • fDate
    5-7 Dec 1990
  • Firstpage
    3362
  • Abstract
    H synthesis techniques are used to design a bank angle autopilot which commands a coordinated bank turn. Two variations of the H design are compared to a multivariable classical design. Both of the H designs have better performance and actuator robustness measures. The first H design, however, contains an undesirable cancellation of a lightly damped Dutch roll mode, which causes a poor parameter robustness measure. The second H design corrects this problem by using the same inner loop yaw damper as used by the classical design
  • Keywords
    aerospace computer control; aircraft control; control system synthesis; military equipment; optimal control; stability; H robust control synthesis; bank angle autopilot; coordinated bank turn; fighter aircraft; inner loop yaw damper; lightly damped Dutch roll; Actuators; Aircraft; Control system synthesis; Cost function; Feedback control; H infinity control; Optimal control; Robust control; Robustness; System performance;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Decision and Control, 1990., Proceedings of the 29th IEEE Conference on
  • Conference_Location
    Honolulu, HI
  • Type

    conf

  • DOI
    10.1109/CDC.1990.203419
  • Filename
    203419