DocumentCode :
2270126
Title :
Achieving sub-pixel registration accuracy for radar imagery
Author :
Witzgall, Hanna E. ; Gural, Peter ; Mahen, Edward C.
Author_Institution :
Adv. Res. & Eng. Solutions Div., Sci. Applications Int. Corp., Chantilly, VA
fYear :
0
fDate :
0-0 0
Abstract :
This paper describes a robust and computationally efficient procedure to obtain sub-pixel registration accuracy. The new approach is based on the well-known phase correlation method which replaces image correlations with multiplications in the Fourier domain. Important to the new process is the observation that the phase correlation matrix has unity rank. This allows the phase shift information to be found in a rank one subspace with two one-dimensional reduced rank autoregressive weight vectors. The reduced rank subspace employed is not based on the common eigenvector approach but on reduced order correlation kernel estimation technique (ROCKET) that maximizes the mutual information criteria. The performance results show that the new algorithm is very robust to aliasing and edge distortion and can achieve high registration accuracy with reduced computational complexity compared to several recently published sub-pixel registration algorithms
Keywords :
computational complexity; correlation methods; image registration; radar imaging; Fourier domain; coherent change detection; edge distortion; image correlations; phase correlation matrix; phase shift information; radar imaging; reduced computational complexity; reduced order correlation kernel estimation technique; sub-pixel registration accuracy; Convolution; Correlation; Discrete Fourier transforms; Fourier transforms; Image edge detection; Image resolution; Military computing; Radar imaging; Robustness; Rockets; ROCKET; coherent change detection; phase correlation method; radar imagery; registration; sub-pixel registration;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2006 IEEE
Conference_Location :
Big Sky, MT
Print_ISBN :
0-7803-9545-X
Type :
conf
DOI :
10.1109/AERO.2006.1655934
Filename :
1655934
Link To Document :
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