• DocumentCode
    3496972
  • Title

    Optimal guidance for missiles with varying velocity

  • Author

    Cho, Hangju ; Chang Kyung Ryoo ; Tahk, Min-Jea

  • Author_Institution
    Agency for Defense Dev., Taejeon, South Korea
  • fYear
    1995
  • fDate
    26-28 Jul 1995
  • Firstpage
    1503
  • Lastpage
    1508
  • Abstract
    An optimal guidance law for missiles with time-varying velocity is investigated. The closed-form solution is derived and properties of the key variables of the solution such as a tgo-like function and the time-varying guidance gain are studied. Simulation studies show an excellent performance of the proposed guidance law
  • Keywords
    missile guidance; optimal control; time-varying systems; closed-form solution; missiles; optimal guidance law; tgo-like function; time-varying guidance gain; time-varying velocity; Art; Cathode ray tubes; Closed-form solution; Equations; Geometry; Gold; Missiles; Optimal control; Virtual manufacturing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    SICE '95. Proceedings of the 34th SICE Annual Conference. International Session Papers
  • Conference_Location
    Hokkaido
  • Print_ISBN
    0-7803-2781-0
  • Type

    conf

  • DOI
    10.1109/SICE.1995.526737
  • Filename
    526737
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=3496972