• DocumentCode
    3049393
  • Title

    Model reference adaptive control for a relaxed static stability aircraft

  • Author

    Sobel, K.M.

  • Author_Institution
    Lockheed California Co., Burbank, CA
  • fYear
    1982
  • fDate
    8-10 Dec. 1982
  • Firstpage
    1369
  • Lastpage
    1373
  • Abstract
    A direct model reference adaptive control algorithm is utilized for the design of a stability augmentation system for the longitudinal axis of a transport aircraft. Control system performance is evaluated for a scenario which includes takeoff, climb and cruise conditions. The adaptive law is compared with a fixed gain controller designed via pole placement. The adaptive controller is shown to be superior for controlling the short period mode.
  • Keywords
    Adaptive control; Aerospace control; Aircraft; Control systems; Linear feedback control systems; Processor scheduling; Programmable control; Stability; State feedback; System performance;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Decision and Control, 1982 21st IEEE Conference on
  • Conference_Location
    Orlando, FL, USA
  • Type

    conf

  • DOI
    10.1109/CDC.1982.268384
  • Filename
    4047487
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=3049393