• DocumentCode
    1440727
  • Title

    Tracking Reentry Ballistic Targets using Acceleration and Jerk Models

  • Author

    Ghosh, Shrabani ; Mukhopadhyay, Siddhartha

  • Author_Institution
    Defence R&D Organ., India
  • Volume
    47
  • Issue
    1
  • fYear
    2011
  • fDate
    1/1/2011 12:00:00 AM
  • Firstpage
    666
  • Lastpage
    683
  • Abstract
    In this paper an acceleration model and a jerk model are proposed for estimation of the kinematic state of reentry ballistic targets (RBTs) using extended Kalman filters (EKF). The models proposed here use the equations of target kinematics only and do not assume any model parameterization for variation of the ballistic coefficient and air density a priori, as found in the literature. The novelty lies in estimation of the ratio (γ) of air density and ballistic coefficient and its time derivatives using a separate Kalman filter (KF) (γ-filter) which utilizes pseudo measurements of γ computed from the velocity and acceleration estimated by the EKF at each time step. The parameter γ and its derivatives estimated by the γ-filter are, in turn, used for the estimation of position, velocity, acceleration, and jerk in the EKF. The use of the pseudo measurements of γ makes the algorithms inherently adaptive to variations of the ballistic coefficient and air density during reentry. A comparative assessment of several dynamic models for reentry of ballistic targets reported in the literature and those proposed here demonstrates that the estimation errors in velocity and acceleration are significantly less for the proposed models compared with the existing ones.
  • Keywords
    Kalman filters; acceleration measurement; ballistics; position measurement; target tracking; velocity measurement; acceleration estimation; acceleration model; air density; extended Kalman filters; jerk model; kinematic state; position estimation; pseudomeasurements; reentry ballistic target tracking; target kinematics equations; velocity estimation; Acceleration; Atmospheric modeling; Computational modeling; Equations; Kinematics; Mathematical model; Noise;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/TAES.2011.5705698
  • Filename
    5705698