• DocumentCode
    1597976
  • Title

    Missile endgame analysis

  • Author

    Juang, Jyh-Ching ; Lin, Ching-Fang ; Evers, J.H. ; Cloutier, James R.

  • Author_Institution
    American GNC Corp., Chatsworth, CA, USA
  • fYear
    1992
  • Firstpage
    744
  • Abstract
    An endgame analysis and design framework are described. The framework can aid in understanding of the endgame dynamics, identifying critical design parameters, and bringing insights to the guidance/control design. A worst-case analysis approach is introduced and applied to the HAVE DASH II system. The analysis approach generalizes the covariance analysis method and provides a more accurate prediction of the engagement performance. On the basis of the analysis framework and performance measure, robust control design methods can be applied to obtain a robust integrated guidance and control design
  • Keywords
    aerospace control; control system synthesis; missiles; navigation; HAVE DASH II system; aerospace control; covariance analysis; endgame analysis; endgame dynamics; guidance/control design; missiles; worst-case analysis; Acceleration; Aerodynamics; Equations; Missiles; Performance analysis; Pollution measurement; Random processes; Signal analysis; Stability; Virtual manufacturing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Applications, 1992., First IEEE Conference on
  • Conference_Location
    Dayton, OH
  • Print_ISBN
    0-7803-0047-5
  • Type

    conf

  • DOI
    10.1109/CCA.1992.269754
  • Filename
    269754