• DocumentCode
    3009186
  • Title

    Adaptive control laws for F-8 flight test

  • Author

    Stein, G. ; Hartmann, G.L. ; Hendrick, R.C.

  • Author_Institution
    Honeywell Inc., Minneapolis, Minnesota
  • fYear
    1975
  • fDate
    10-12 Dec. 1975
  • Firstpage
    230
  • Lastpage
    230
  • Abstract
    This paper presents design and performance details for a set of adaptive flight control laws to be flight-tested in NASA´s F-8 digital fly-by-wire research aircraft. These control laws implement an explicit maximum likelihood identification algorithm to estimate key aircraft parameters. The parameter estimates are then used to compute gains in a quadraticoptimal command augmentation control law.
  • Keywords
    Adaptive control; Adaptive systems; Aerospace control; Aircraft; Equations; Maximum likelihood estimation; Parameter estimation; Processor scheduling; Programmable control; Testing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Decision and Control including the 14th Symposium on Adaptive Processes, 1975 IEEE Conference on
  • Conference_Location
    Houston, TX, USA
  • Type

    conf

  • DOI
    10.1109/CDC.1975.270682
  • Filename
    4045409
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=3009186