• DocumentCode
    488098
  • Title

    Missile Altitude Adaptive Control: A Case Study

  • Author

    Duque, M. ; Landau, L. ; M´Saad, M. ; Manguin, B. ; Houdement, J. ; Martin, A.

  • Author_Institution
    Laboratoire d´´Automatique de Grenoble, U.A. C.N.R.S. 228 E.N.S.I.E.G. - I.N.P.G., B.P.46 -38402 St- Martin d´´Hÿres, France
  • fYear
    1989
  • fDate
    21-23 June 1989
  • Firstpage
    2813
  • Lastpage
    2818
  • Abstract
    This paper presents some missile attack angle control simulation studies. Both linear and adaptive control are considered using the partial state model reference adaptive control approach proposed in [1]. The main control problems are due to the unmeasured disturbances, unstable or undamped modes and important dynamics variations.
  • Keywords
    Adaptive control; Computer aided software engineering; Context modeling; Control design; Missiles; Polynomials; Predictive control; Predictive models; Programmable control; Rockets; Partial state model reference control; adaptive control; generalized predictive control; missile altitude control; robust parameter estimator;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, 1989
  • Conference_Location
    Pittsburgh, PA, USA
  • Type

    conf

  • Filename
    4790669
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=488098