• DocumentCode
    724375
  • Title

    Review of studies on integrated guidance and control design approach

  • Author

    Xiangyu Sun ; Tao Chao ; Songyan Wang ; Ming Yang

  • Author_Institution
    Control & Simulation Centre, Harbin Inst. of Technol., Harbin, China
  • fYear
    2015
  • fDate
    23-25 May 2015
  • Firstpage
    3958
  • Lastpage
    3963
  • Abstract
    Ending game of vehicle has properties of nonlinearity and quick states variation. To solve these problems, a newly developing approach that integrated guidance and control design attracts attention. This article firstly introduces research significance and design direction of the approach, and then divides the development procedure into several research phases meanwhile summarizes the results of each one. This approach solves numerous problems in traditional separate design approach and reduces design cost. Through the analysis of the current research situation combined with the actual demand, many key problems still need to be solved in future. Some prospects about this design approach are shown at last.
  • Keywords
    control nonlinearities; control system synthesis; missile guidance; hypersonic vehicle ending game; integrated guidance and control design; nonlinearity; precision guided weapons; Finite-time; Integrated guidance and control; Nonlinear;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control and Decision Conference (CCDC), 2015 27th Chinese
  • Conference_Location
    Qingdao
  • Print_ISBN
    978-1-4799-7016-2
  • Type

    conf

  • DOI
    10.1109/CCDC.2015.7162615
  • Filename
    7162615