DocumentCode :
1005838
Title :
Monopulse-radar angle tracking in noise or noise jamming
Author :
Seifer, Arnold D.
Author_Institution :
Lockheed Sanders Inc., Nashua, NH, USA
Volume :
28
Issue :
3
fYear :
1992
fDate :
7/1/1992 12:00:00 AM
Firstpage :
622
Lastpage :
638
Abstract :
In many monopulse radars, feedback in the angle-tracking servo system is taken to be directly proportional to the monopulse ratio. In those radars, monopulse measurements are conditioned on simultaneous occurrences of receiver sum-channel video exceeding a detection threshold: if a detection fails to occur, the measurement is ignored, and the angle-tracking servo is made to coast. Such conditioning is shown to be necessary in order that the noise power be finite in the servo feedback. The conditional mean value and conditional variance of the monopulse ratio are derived and quantified in terms of threshold level as well as signal-to-noise ratio. The formulation permits the noise covariance between receiver difference and sum channels to be complex rather than only real-valued, so that the sources of noise jamming are not required to be positioned in the receiving-antenna mainlobe and to be copolarized with the antenna response there. Nonfluctuating and Rayleigh-fluctuating target cases are considered and compared, and fluctuation loss is quantified
Keywords :
jamming; radar interference; radar theory; servomechanisms; signal processing; telecommunications control; tracking; Rayleigh-fluctuating target; angle tracking; feedback; fluctuation loss; monopulse radars; monopulse ratio; noise jamming; receiving-antenna mainlobe; servo system; signal-to-noise ratio; threshold level; Baseband; Feedback; Fluctuations; Jamming; Noise level; Noise measurement; Radar detection; Radar measurements; Radar tracking; Receiving antennas; Servomechanisms; Signal to noise ratio; Threshold voltage;
fLanguage :
English
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9251
Type :
jour
DOI :
10.1109/7.256285
Filename :
256285
Link To Document :
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