• DocumentCode
    3330789
  • Title

    A study of chattering suppression in sliding mode-based missile guidance law

  • Author

    Yuan Liying ; Wu Junfeng ; Yu Lianyong ; Cui Jiashan ; Sun Lili

  • Author_Institution
    Sch. of Autom., Harbin Univ. of Sci. & Technol., Harbin, China
  • Volume
    2
  • fYear
    2011
  • fDate
    22-24 Aug. 2011
  • Firstpage
    924
  • Lastpage
    926
  • Abstract
    A sliding mode controller with chattering suppression for missiles guidance law is designed under the presence of target maneuvering. To reduce the chattering in sliding mode control, constitute a continuous function instead of signal function which guarantees the practicability of the control scheme. In the numerical simulation, it is obviously that the proposed guidance law reduces the chattering phenomenon and.
  • Keywords
    military systems; missile guidance; target tracking; variable structure systems; chattering suppression; signal function; sliding mode based missile guidance law; sliding mode control; target maneuvering; Azimuth; Robustness; Missile; guidance law; maneuvering target; sliding mode control;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Strategic Technology (IFOST), 2011 6th International Forum on
  • Conference_Location
    Harbin, Heilongjiang
  • Print_ISBN
    978-1-4577-0398-0
  • Type

    conf

  • DOI
    10.1109/IFOST.2011.6021171
  • Filename
    6021171
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=3330789