• DocumentCode
    3048599
  • Title

    Mixed strategy guidance based on target maneuver detection

  • Author

    Hua Wen-hua ; Chen Xing-lin

  • Author_Institution
    Sch. of Astronaut., Harbin Inst. of Technol., Harbin, China
  • fYear
    2010
  • fDate
    20-23 June 2010
  • Firstpage
    884
  • Lastpage
    889
  • Abstract
    With the general separation theorem consideration, two mixed strategy guidance approaches are presented. All based on the target maneuver detection, one approach mixes two available differential game guidance laws to reduce the effect of the estimation delay; the other incorporates one more proposed modified gain differential game guidance law, which increases the lateral acceleration command for estimation delay and short remaining time consideration. The simulation results show that these two approaches can improve the system performance significantly and the second approach has the best performance.
  • Keywords
    differential games; missile guidance; object detection; estimation delay; lateral acceleration command; mixed strategy guidance system; modified gain differential game guidance law; target maneuver detection; Acceleration; Automation; Delay effects; Delay estimation; Detectors; Equations; Space technology; State estimation; Switches; System performance; differential game; maneuver detection; mixed strategy; terminal guidance;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Information and Automation (ICIA), 2010 IEEE International Conference on
  • Conference_Location
    Harbin
  • Print_ISBN
    978-1-4244-5701-4
  • Type

    conf

  • DOI
    10.1109/ICINFA.2010.5512293
  • Filename
    5512293