• DocumentCode
    1139181
  • Title

    Missile Acceleration in Proportional Navigation

  • Author

    Guelman, M.

  • Author_Institution
    Ministry of Defence Armament Development Authority Tel-Aviv, Israel
  • Issue
    3
  • fYear
    1973
  • fDate
    5/1/1973 12:00:00 AM
  • Firstpage
    462
  • Lastpage
    463
  • Abstract
    In a previous paper, the author obtained conditions for the acceleration of a missile pursuing a maneuvering target according to proportional navigation, to be bounded. This correspondence extends previous work, and new boundaries are obtained for the missile acceleration.
  • Keywords
    Acceleration; Equations; Missiles; Navigation;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/TAES.1973.309733
  • Filename
    4103150
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=1139181