Comments on "The /spl alpha/-/spl beta/-/spl Gamma/ tracking filter with a noisy jerk as the maneuver model"

Author

Hoffman, S.A. ; Blair, W.D.

Author_Institution

Dept. of Syst. Res. & Technol., Naval Surface Warfare Center, Dahlgren, VA, USA

Volume

30

Issue

3

fYear

1994

fDate

7/1/1994 12:00:00 AM

Firstpage

925

Lastpage

927

Abstract

In ibid, vol. AES-29, p.578-590 (Apr. 1993), J Sudano presented the optimal steady-state gains and associated error covariances for an /spl alpha/-/spl beta/-/spl Gamma/ filter with a piecewise constant jerk as a maneuver model. While the results given in that article are correct, the gains and error covariances can be found in a much simpler manner. The simplified expressions for the gains and the error covariances are given, along with the code for a simple program that computes the gains for a given tracking index.<>

Keywords

error analysis; filtering and prediction theory; parameter estimation; signal processing; statistical analysis; tracking; white noise; /spl alpha/-/spl beta/-/spl Gamma/ tracking filter; error covariances; maneuver model; mathematical model; noisy jerk; optimal steady-state gains; piecewise constant jerk; Acceleration; Covariance matrix; Equations; Error analysis; Gain measurement; Kalman filters; State estimation; Steady-state; Target tracking; Time measurement;

fLanguage

English

Journal_Title

Aerospace and Electronic Systems, IEEE Transactions on

Publisher

ieee

ISSN

0018-9251

Type

jour

DOI

10.1109/7.303763

Filename

303763