• DocumentCode
    85528
  • Title

    Missile guidance with constrained intercept body angle

  • Author

    Rusnak, Ilan ; Weiss, Haim ; Eliav, Rei ; Shima, Tal

  • Author_Institution
    RAFAEL, Haifa, Israel
  • Volume
    50
  • Issue
    2
  • fYear
    2014
  • fDate
    Apr-14
  • Firstpage
    1445
  • Lastpage
    1453
  • Abstract
    A linear quadratic based missile guidance law is presented that imposes a predetermined terminal body angle. Solutions are provided for arbitrary order autopilot dynamics, with explicit analytical expressions given for first-order and zero-lag dynamics. Performance is demonstrated through simulation in a planar interception scenario.
  • Keywords
    missile guidance; arbitrary order autopilot dynamics; constrained intercept body angle; explicit analytical expressions; first-order dynamics; linear quadratic based missile guidance law; missile guidance; planar interception scenario; terminal body angle; zero-lag dynamics; Acceleration; Aerodynamics; Equations; Geometry; Mathematical model; Missiles; Navigation;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/TAES.2014.120100
  • Filename
    6850166
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=85528