• DocumentCode
    1442002
  • Title

    Tracking an incoming ballistic missile using an extended interval Kalman filter

  • Author

    Siouris, George M. ; Chen, Guanrong ; Wang, Jianrong

  • Author_Institution
    Air Force Inst. of Technol., Wright-Patterson AFB, OH, USA
  • Volume
    33
  • Issue
    1
  • fYear
    1997
  • Firstpage
    232
  • Lastpage
    240
  • Abstract
    The important tracking problem by radar of an incoming ballistic missile system, which contains uncertainty in modeling and noise in both dynamics and measurements, is studied. The classical extended Kalman filter (EKF) is no longer applicable to such an uncertain system, and so a new extended interval Kalman filter (EIKF) is developed for tracking the missile system. Computer simulation is presented to show the effectiveness of the EIKF algorithm for this uncertain and nonlinear ballistic missile tracking problem.
  • Keywords
    Kalman filters; digital simulation; military computing; missiles; noise; nonlinear systems; radar signal processing; radar tracking; simulation; uncertainty handling; dynamics; extended interval Kalman filter; incoming ballistic missile; measurements; modeling; nonlinear ballistic missile tracking; uncertainty; Aerospace engineering; Azimuth; Force measurement; Laser radar; Military computing; Missiles; Optical devices; Radar measurements; Radar tracking; Target tracking;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/7.570753
  • Filename
    570753