DocumentCode :
3368630
Title :
Robust strain rate estimation using two-dimensional cubic B-splines
Author :
D´hooge, J. ; Claus, P. ; Bijnens, B. ; Thoen, J. ; van de Werf, F. ; Sutherland, G.R. ; Suetens, P.
Author_Institution :
Dept. of Electr. Eng., Univ. Hosp. Gasthuisberg, Leuven, Belgium
Volume :
2
fYear :
2002
fDate :
8-11 Oct. 2002
Firstpage :
1881
Abstract :
In this study, the use of cubic B-splines for robust ultrasonic strain and strain rate estimation is demonstrated. To do this, radio-frequency data sets of cyclically compressed gelatine phantoms were acquired during M-mode imaging. Velocities were estimated by tracking temporally successive RF windows. Subsequently, a two-dimensional cubic smoothing B-spline was fitted through the velocity estimates for both depth and time. Strain rate could then be defined analytically as the cubic B-spline being the partial derivative of the velocity B-spline surface in the depth direction. Similarly, a strain B-spline surface could be defined as the analytical temporal integral of the strain rate B-spline. The method was shown to give accurate strain and strain rate estimates. Comparing this method to conventional processing, it was shown to produce less noisy strain rate and strain estimates.
Keywords :
biomedical measurement; biomedical ultrasonics; splines (mathematics); stress-strain relations; ultrasonic measurement; M-mode imaging; cyclically compressed gelatine phantoms; less noisy strain rate; radio-frequency data sets; robust strain rate estimation; robust ultrasonic strain estimation; strain estimates; two-dimensional cubic B-splines; two-dimensional cubic smoothing B-spline; velocity estimates; Biomedical imaging; Capacitive sensors; Image coding; Imaging phantoms; Myocardium; Phased arrays; Polynomials; Radio frequency; Robustness; Spline;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Ultrasonics Symposium, 2002. Proceedings. 2002 IEEE
ISSN :
1051-0117
Print_ISBN :
0-7803-7582-3
Type :
conf
DOI :
10.1109/ULTSYM.2002.1192665
Filename :
1192665
Link To Document :
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