DocumentCode
882599
Title
The α-β-Γ tracking filter with a noisy jerk as the maneuver model
Author
Sudano, J.J.
Author_Institution
GE Aerosp. Moorestown, NJ
Volume
29
Issue
2
fYear
1993
fDate
4/1/1993 12:00:00 AM
Firstpage
578
Lastpage
580
Abstract
The optimal gains and covariances of an α-β-Γ filter are computed. It is assumed that the maneuver model is an uncorrelated zero mean noise jerk. Input to the tracking filter is position updates. The measurement errors are modeled as uncorrelated zero mean noise processes
Keywords
Kalman filters; filtering and prediction theory; measurement errors; noise; position measurement; tracking; α-β-Γ tracking filter; Kalman filter; constant acceleration trajectory; covariances; maneuver model; measurement errors; optimal gains; position updates; uncorrelated zero mean noise jerk; Acceleration; Aerodynamics; Equations; Error correction; Filters; Mathematical model; Measurement errors; Noise measurement; Steady-state; Stochastic systems; Time measurement; Trajectory;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems, IEEE Transactions on
Publisher
ieee
ISSN
0018-9251
Type
jour
DOI
10.1109/7.210097
Filename
210097
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