DocumentCode :
2515243
Title :
A Method for Truncation Compensation for Pinhole Tomography
Author :
Yoder, Bryan C. ; Lalush, David S.
Author_Institution :
Joint Dept. of Biomed. Eng., North Carolina Univ., Chapel Hill, NC
Volume :
6
fYear :
2006
fDate :
Oct. 29 2006-Nov. 1 2006
Firstpage :
3441
Lastpage :
3444
Abstract :
We investigate the effect of multiple circular orbits offset transaxially to improve truncation artifacts. A simulated phantom was placed at a distance from a pinhole collimator that ensured transaxial truncation for the projections. To compensate this truncation, two pinhole scans were then simulated with the axes of rotation (AOR) shifted symmetrically about the central ray. In effect, each scan is used to view half of the object, and the two halves are combined using an OSEM reconstruction. SPECT phantom simulations were performed to compare the dual-orbit approach to a traditional single-orbit acquisition. Further evaluation of the dual-orbit approach with point sources showed that the dual-orbit scan provided higher sensitivity than the single orbit-scan with no loss in resolution. We conclude that the resolution-noise tradeoff for small-field-of-view cameras can be improved with the dual scan procedure.
Keywords :
collimators; image reconstruction; phantoms; single photon emission computed tomography; OSEM reconstruction; SPECT phantom simulation; axes of rotation; dual-orbit scan; multiple circular orbits; pinhole collimator; pinhole tomography; resolution-noise tradeoff; simulated phantom; single orbit-scan; transaxial truncation; truncation artifact; truncation compensation; Apertures; Cameras; Collimators; Geometry; Image reconstruction; Image resolution; Imaging phantoms; Orbits; Solid modeling; Tomography;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Nuclear Science Symposium Conference Record, 2006. IEEE
Conference_Location :
San Diego, CA
ISSN :
1095-7863
Print_ISBN :
1-4244-0560-2
Electronic_ISBN :
1095-7863
Type :
conf
DOI :
10.1109/NSSMIC.2006.353741
Filename :
4179783
Link To Document :
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