• DocumentCode
    2857811
  • Title

    Nonlinear H∞ control of aerospace plane ascent

  • Author

    McEneaney, William M. ; Mease, Kenneth D.

  • Author_Institution
    Dept. of Math., Carnegie Mellon Univ., Pittsburgh, PA, USA
  • Volume
    4
  • fYear
    1995
  • fDate
    13-15 Dec 1995
  • Firstpage
    3994
  • Abstract
    Nonlinear H∞ theory is applied to design the fast part of a composite control for guiding the ascent of an aerospace plane to orbit. The viscosity solution of the corresponding Isaacs equation is obtained at any point by a generalized method of characteristics
  • Keywords
    H∞ control; aerospace control; attitude control; fuel optimal control; game theory; nonlinear control systems; state-space methods; Isaacs equation; aerospace plane; ascent guidance; game theory; minimum fuel control; nonlinear H∞ control; space vehicles; state space method; viscosity solution; Additives; Aerodynamics; Aerospace control; Argon; Attenuation; Equations; H infinity control; Optimal control; State-space methods; Viscosity;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Decision and Control, 1995., Proceedings of the 34th IEEE Conference on
  • Conference_Location
    New Orleans, LA
  • ISSN
    0191-2216
  • Print_ISBN
    0-7803-2685-7
  • Type

    conf

  • DOI
    10.1109/CDC.1995.479229
  • Filename
    479229
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=2857811