• DocumentCode
    1695968
  • Title

    Design of Guidance Law for Homing Missile Via Feedback Linearization

  • Author

    Bezick, Scott ; Rusnak, Ilan ; Gray, W. Steven

  • Author_Institution
    Department of Electrical and Computer Engineering, Drexel University, PA
  • fYear
    1993
  • Firstpage
    729
  • Lastpage
    733
  • Keywords
    Acceleration; Control system synthesis; Control systems; Feedback; Geometry; Kinematics; Missiles; Navigation; Nonlinear control systems; Virtual manufacturing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Control Systems, 1993. Proceedings. The First IEEE Regional Conference on
  • Type

    conf

  • DOI
    10.1109/AEROCS.1993.721029
  • Filename
    721029
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=1695968