DocumentCode :
1066342
Title :
A tracking filter for maneuvering sources
Author :
Abutaleb, Ahmed S.
Author_Institution :
MIT Lincoln Lab., Lexington, MA, USA
Volume :
34
Issue :
4
fYear :
1989
fDate :
4/1/1989 12:00:00 AM
Firstpage :
471
Lastpage :
475
Abstract :
An adaptive filter that is based on the Pontryagin minimum principle and the method of invariant imbedding is introduced and applied to the problem of tracking maneuvering sources. The major advantages of this approach are: (1) no model for the target dynamics is required, and (2) the signal-to-noise ratio of the observation and stations need to be known. The performance of the proposed approach (with unknown system dynamics) is compared to that of the extended Kalman filter (with known system dynamics) for the maneuvering reentry vehicle. Examples are given for different target scenarios
Keywords :
aerospace control; filtering and prediction theory; maximum principle; tracking; Pontryagin minimum principle; S/N ratio; adaptive filter; invariant imbedding; maneuvering target tracking; reentry vehicle; tracking filter; Adaptive filters; Electrons; Gain measurement; Noise measurement; Performance loss; Phased arrays; Q measurement; Radar tracking; Stability; Target tracking;
fLanguage :
English
Journal_Title :
Automatic Control, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9286
Type :
jour
DOI :
10.1109/9.28030
Filename :
28030
Link To Document :
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