• DocumentCode
    3022837
  • Title

    Development of an AAA gunner model based on reduced-order observer theory

  • Author

    Kou, R.S. ; Glass, B.G. ; Vikmanis, M.M. ; Day, C.N.

  • Author_Institution
    Systems Research Laboratories, Inc., Dayton, Ohio
  • fYear
    1979
  • fDate
    10-12 Jan. 1979
  • Firstpage
    104
  • Lastpage
    112
  • Abstract
    A systematic study of threat effectiveness for anti-aircraft artillery (AAA) systems requires the development of a mathematical model for the gunner´s tracking response. An anti-aircraft gunner model based on the Luenberger reduced-order observer theory is developed in this paper. It is composed of three main parts - a reduced-order observer, a feedback controller, and a remnant element. The highlights of this model are simplicity in model structure and accuracy in the tracking error predictions. A parameter identification program based on the least squares curve-fitting method and the Gauss-Newton gradient algorithm is developed to systematically determine the model parameters. Computer simulation results of the AAA tracking task with this model are in excellent agreement with the empirical data obtained from manned AAA simulation experiments conducted at the Aerospace Medical Research Laboratory, Wright-Patterson Air Force Base, Ohio. A comparison between this model and the optimal control model by Kleinman, Baron, Levison is also given.
  • Keywords
    Adaptive control; Computer errors; Computer simulation; Curve fitting; Least squares methods; Mathematical model; Newton method; Parameter estimation; Predictive models; Recursive estimation;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Decision and Control including the 17th Symposium on Adaptive Processes, 1978 IEEE Conference on
  • Conference_Location
    San Diego, CA, USA
  • Type

    conf

  • DOI
    10.1109/CDC.1978.267901
  • Filename
    4046088