DocumentCode :
279410
Title :
Recursive eigenstructure-based technique for low-angle tracking using frequency agile waveforms
Author :
Yu, Kai-bor
Author_Institution :
GE Res. & Dev. Center, Schenectady, NY, USA
fYear :
1992
fDate :
12-13 Oct 1992
Firstpage :
50
Lastpage :
53
Abstract :
The author outlines a technique for solving the low-elevation target angle tracking problem. The technique involves frequency-agile waveforms together with recursive eigenstructure-based algorithms. Frequency agility decorrelates the coherence between the direct signal and specular component as well as provides some robustness to the fading phenomena. Fast algorithms for updating the eigenvalue decomposition as well as for tracking the corresponding minimum-norm polynomial zeros can be used for efficient implementation of the recursive eigenstructure-based high-resolution algorithm. The algorithm is illustrated for tracking a low-flying target as it pops up from the horizon. Fading occurs for monopulse processing for the entire tracking duration when the direct and reflected angles are out of phase. The recursive minimum-norm algorithm smooths out the fading by using snapshots within a sliding window for covariance matrix estimation. Simulation verifies that the technique works well in resolving and tracking the direct signal and the specular component, even though the separation between the signal components incident on the array may be a small fraction of a beamwidth
Keywords :
eigenvalues and eigenfunctions; radar theory; signal processing; tracking; covariance matrix estimation; direct angles; direct signal; frequency-agile waveforms; low-elevation target angle tracking; low-flying target; minimum-norm polynomial zeros; monopulse processing; radar; recursive eigenstructure-based algorithms; reflected angles; sliding window; specular component; tracking duration;
fLanguage :
English
Publisher :
iet
Conference_Titel :
Radar 92. International Conference
Conference_Location :
Brighton
Print_ISBN :
0-85296-553-2
Type :
conf
Filename :
187041
Link To Document :
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