• DocumentCode
    2984423
  • Title

    The Precision Analysis and Simulation Based on SLAM

  • Author

    Yang, Ping ; Bin Zhang ; Dong, Guo-fang ; Kuang, Shen-Qing

  • Author_Institution
    Dept. of Commanding, Commanding Commun. Acad., Wuhan, China
  • fYear
    2010
  • fDate
    25-27 June 2010
  • Firstpage
    5810
  • Lastpage
    5813
  • Abstract
    Precision analysis is one of the key factors which must be considered in the process of Anti-air missile guidance system design . In this paper, a homing guidance system of anti-aircraft missile systems is analyzed, and finally statistical linearization adjoint method (SLAM) is chosen. Considering the system with disturbance of target maneuver, glint, atmosphere nois s and so on, a typical proportional navigation engagement simulation model is stablished. The simulation results show that the SLAM can not only get the root mean square miss distance, but also the total impact of the miss distance due to the different random input signal of the system, which results into a higher accuracy of guidance system in practice.
  • Keywords
    linearisation techniques; mean square error methods; missile guidance; statistical analysis; anti-air missile guidance system; homing guidance system; precision analysis; root mean square miss distance; statistical linearization adjoint method; Aerospace control; Atmospheric modeling; Missiles; Monte Carlo methods; Physics; Publishing; Simultaneous localization and mapping; adjoint method(SLAM); homing guidance system; precision analysis; statistical linearization;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Electrical and Control Engineering (ICECE), 2010 International Conference on
  • Conference_Location
    Wuhan
  • Print_ISBN
    978-1-4244-6880-5
  • Type

    conf

  • DOI
    10.1109/iCECE.2010.1458
  • Filename
    5630106