• DocumentCode
    3513983
  • Title

    Turn Rate Estimation Techniques in IMM Estimators for ESA Radar Tracking

  • Author

    Veeraraghavan, S. ; Rathi, A. ; Sagayaraj, M.J. ; Nagar, C.V.R.

  • Author_Institution
    Electron. & Radar Dev. Establ., Bangalore
  • fYear
    2008
  • fDate
    1-8 March 2008
  • Firstpage
    1
  • Lastpage
    8
  • Abstract
    Electronically steered array-antenna (ESA) radars are used to perform multiple roles, such as surveillance and dedicated tracking. The beam positioning agility of ESA radars can be used to efficiently track maneuvering targets. Maneuvers made by targets are often modeled using turn models. The success of using turn models relies on the correct estimation of turn-rate. Various schemes have been proposed in literature for estimation of turn rate. This paper makes a comparative study of turn rate estimation techniques for ESA radar tracking. An adaptive revisit scheme is used for tracking maneuvering targets, using the interacting multiple-model (IMM) approach. Better turn-rate estimation techniques in this adaptive framework can significantly bring down the demand for resources while tracking maneuvering targets. Simulation studies are carried out using the benchmark target trajectories defined for phased array radar tracking. Monte-Carlo simulation results against six maneuvering target scenarios are presented and discussed.
  • Keywords
    antenna arrays; radar antennas; radar tracking; target tracking; ESA radar tracking; IMM estimators; Monte-Carlo simulation; electronically steered array-antenna; interacting multiple-model approach; track maneuvering targets; turn rate estimation techniques; Acceleration; Angular velocity; Equations; Motion estimation; Phased arrays; Radar tracking; Resource management; Surveillance; Target tracking; Trajectory; ESA radar; IMM; target tracking; turn-rate estimation;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2008 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    978-1-4244-1487-1
  • Electronic_ISBN
    1095-323X
  • Type

    conf

  • DOI
    10.1109/AERO.2008.4526441
  • Filename
    4526441