DocumentCode :
1123922
Title :
Reduction of Radar Glint for Complex Targets by Use of Frequency Agility
Author :
Nicholls, L.A.
Author_Institution :
Australian Defence Scientific Service Weapons Research Establishment Salisbury, South Australia
Issue :
4
fYear :
1975
fDate :
7/1/1975 12:00:00 AM
Firstpage :
647
Lastpage :
650
Abstract :
A result of Morinaga et al. [6] for the autocorrelation function of phase rate of narrowband Gaussian noise when averaged over accompanying wideband Gaussian noise is used to derive the power specturm of inherent glint and, thereby, its variance for a frequency-agile radar assuming Gaussian random angular motion of a complex target. The zero-frequency spectral density of inherent glint is shown to be ¿9.8 dB relative to that for a fixed-frequency radar under similar conditions. This result is not sensitive to the product of the agility bandwidth and the radial target extent, provided this product is adquate (as is normally ensured by current design practice for given target types). The associated glint variance with adequate agility bandwidth is shown to be 0.142 ¿20, where ¿o is the relevant radius of gyration of the collection of radar scatterers comprising the target. A theoretical relation due to Durrani and Greated [8], derived in another context, indicates that the wideband echo spectrum resulting from frequency agility needs, in fact, to have a bandwidth of the order of 103 times that of the narrowband echo spectrum associated with target angular motion to achieve the above 9.8-dB improvement factor. For the lesser bandwidth ratios of 102 and 10, the indicated improvement factors fall to 9.4 dB and 6.5 dB, respectively.
Keywords :
Aerospace and electronic systems; Autocorrelation; Bandwidth; Frequency estimation; Gaussian noise; Narrowband; Radar cross section; Radar scattering; Statistics; Wideband;
fLanguage :
English
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9251
Type :
jour
DOI :
10.1109/TAES.1975.308132
Filename :
4101463
Link To Document :
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