• DocumentCode
    2257461
  • Title

    H2 optimal proportional navigation guidance law

  • Author

    Mengxiang, Chen ; Weidong, Zhang

  • Author_Institution
    Key Laboratory of System Control and Information Processing, Ministry of Education of China, Shanghai Jiao Tong University, Shanghai, 200240
  • fYear
    2015
  • fDate
    28-30 July 2015
  • Firstpage
    5041
  • Lastpage
    5046
  • Abstract
    This paper proposes an H2 optimal control based proportional navigation guidance law, in which the autopilot´s dynamic property is taken into account. The derived guidance law is analytical and requires only the missile parameters. Simulation result shows the proposed guidance law can nullify the line-of-sight rate at a fast speed and has better interception performance than the traditional proportional guidance for multiple kinds of targets.
  • Keywords
    Acceleration; Adaptive systems; Mathematical model; Missiles; Navigation; Optimal control; H2 Optimal Control; Optimal Navigation Law; Proportional Navigation;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Conference (CCC), 2015 34th Chinese
  • Conference_Location
    Hangzhou, China
  • Type

    conf

  • DOI
    10.1109/ChiCC.2015.7260424
  • Filename
    7260424
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=2257461