• DocumentCode
    1442981
  • Title

    Analytical solution of α-β-Γ tracking filter with a noisy jerk as correlated target maneuver model

  • Author

    Arcasoy, C.C. ; Ouyang, Gaoxiang

  • Author_Institution
    Electr. & Electron. Eng. Dept., Eastern Mediterranean Univ., Famagusta, Cyprus
  • Volume
    33
  • Issue
    1
  • fYear
    1997
  • Firstpage
    347
  • Lastpage
    353
  • Abstract
    An analysis of a discrete constant gain α-β-Γ tracking filter where target acceleration is correlated in time is presented in the frequency domain. The steady-state gain solution for the same tracking filter was given by C.C. Arcasoy (1996) where the maneuver correlation coefficient θ was assumed to be zero. The target was assumed to be moving with constant acceleration motion. The closed-formed results for estimating optimum steady-state position, velocity, and acceleration of the target are given along with the code for a simple program that computes the gains for a given tracking index as a function of maneuver correlation coefficient. The gain can be calculated from the solution of the constant coefficient quartic equation for given system parameters that is in the same form as that given by Arcasoy. The stability analysis of the optimal tracking filter yields the selection of the quartic equation root.
  • Keywords
    circuit analysis computing; circuit noise; circuit stability; digital simulation; frequency-domain analysis; tracking filters; α-β-Γ tracking filter; analysis; closed-formed results; constant acceleration motion; constant coefficient quartic equation; correlated target maneuver model; discrete constant gain; frequency domain; maneuver correlation coefficient; noisy jerk; optimal tracking filter; optimum steady-state acceleration; optimum steady-state position; optimum steady-state velocity; quartic equation root; stability analysis; target acceleration; Acceleration; Covariance matrix; Equations; Frequency domain analysis; Frequency response; Kalman filters; MATLAB; Mathematical model; Stability analysis; Steady-state; Target tracking;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/7.570824
  • Filename
    570824