KALMAN FILTER BASED TRACKING SCHEME WITH INPUT ESTIMATION

被引:284
作者
CHAN, YT
HU, AGC
PLANT, JB
机构
[1] Royal Military College of Canada, Department of Electrical Engineering, Royal Military College of Canada, Kingston, Ont.
关键词
D O I
10.1109/TAES.1979.308710
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Beginning with the derivation of a least squares estimator that yields an estimate of the acceleration input vector, this paper first develops a detector for sensing target maneuvers and then develops the combination of the estimator, detector, and a “simple” Kalman filter to form a tracker for maneuvering targets. Finally, some simulation results are presented. A relationship between the actual residuals, assuming target maneuvers, and the theoretical residuals of the “simple” Kalman filter that assumes no maneuvers, is first formulated. The estimator then computes a constant acceleration input vector that best fits that relationship. The result is a least squares estimator of the input vector which can be used to update the “simple” Kalman filter. Since typical targets spend considerable periods of time in the constant course and speed mode, a detector is used to guard against automatic updating of the “simple” Kalman filter. A maneuver is declared, and updating performed, only if the norm of the estimated input vector exceeds a threshold. The tracking scheme is easy to implement and its capability is illustrated in three tracking examples. Copyright © 1979 by The Institute of Electrical and Electronics Engineers, Inc.
引用
收藏
页码:237 / 244
页数:8
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