DocumentCode :
2264665
Title :
Investigation on low-angle tracking technique for HRR radar
Author :
She, Shang ; Shouhong, Zhang ; Xiushe, Zhang
Author_Institution :
Nat. Lab. of Radar Signal Process., Xidian Univ., Xi´´an, China
fYear :
2001
fDate :
2001
Firstpage :
839
Lastpage :
842
Abstract :
Accurate tracking of targets flying at low altitudes above a smooth surface is difficult because of the multipath propagation effects. In order to address this problem, a new method for eliminating the effects of specular components on the performance of radar low-angle tracking is presented. Using stepped frequency high range resolution (HRR) radar, one can obtain the target range profile from applying inverse fast Fourier transforms (IFFT) to the target echoes. By auto-correlation of target range profile, the path difference between the target and its specula can also be extracted, hence, the target altitude is estimated. The results of simulation and a range profile obtained from a stepped-frequency ultra-wideband trail radar (using 4GHz bandwidth) are also discussed
Keywords :
fast Fourier transforms; radar interference; radar resolution; radar tracking; target tracking; 4 GHz; HRR radar; IFFT; computer simulations; high range resolution radar; inverse fast Fourier transforms; low altitude flying targets; low-angle tracking; multipath propagation effects; path difference extraction; radar bandwidth; smooth ground surface; specular component effect elimination; stepped frequency HRR; target altitude estimation; target echoes; target range profile auto-correlation; target specula; tracking accuracy; tracking performance; ultra-wideband trail radar; Bandwidth; Data mining; Doppler radar; Frequency; Local oscillators; Radar antennas; Radar tracking; Sea surface; Target tracking; Ultra wideband technology;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Radar, 2001 CIE International Conference on, Proceedings
Conference_Location :
Beijing
Print_ISBN :
0-7803-7000-7
Type :
conf
DOI :
10.1109/ICR.2001.984842
Filename :
984842
Link To Document :
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