| Literature DB >> 28291913 |
Shi Liu1, Thomas R Mazur1, Harold Li1, Austen Curcuru1, Olga L Green1, Baozhou Sun1, Sasa Mutic1, Deshan Yang1.
Abstract
MOTIVATION: In this study, a method is reported to perform IMRT and VMAT treatment delivery verification using 3D volumetric primary beam fluences reconstructed directly from planned beam parameters and treatment delivery records. The goals of this paper are to demonstrate that 1) 3D beam fluences can be reconstructed efficiently, 2) quality assurance (QA) based on the reconstructed 3D fluences is capable of detecting additional treatment delivery errors, particularly for VMAT plans, beyond those identifiable by other existing treatment delivery verification methods, and 3) QA results based on 3D fluence calculation (3DFC) are correlated with QA results based on physical phantom measurements and radiation dose recalculations.Entities:
Keywords: IMRT; VMAT; quality assurance; radiation therapy
Mesh:
Year: 2016 PMID: 28291913 PMCID: PMC5689871 DOI: 10.1002/acm2.12017
Source DB: PubMed Journal: J Appl Clin Med Phys ISSN: 1526-9914 Impact factor: 2.102
Figure 1The general workflow of the VMAT delivery QA.
Normal tolerances and statistical distributions for various sources of errors of the Varian LINAC machines installed in our clinic
| Errors | Gantry | MU | Jaw | Collimator | MLC |
|---|---|---|---|---|---|
| Tolerance | 1° | 1 MU | 1 mm | 1° | 2 mm |
| Distribution | Uniformly | Uniformly | Uniformly | Uniformly | Gaussian |
Figure 2The diagram of the correlation study design between the 3DFC QA and the measurement‐based QA.
Figure 3Results of 3D and 2D fluences from a four‐arc lung VMAT plan. Top row is from the DICOM plan. Middle row is from the log file. Bottom row is obtained by calculating the corresponding fluence differences. The PTV contours in the respective 3D orthogonal views are overlaid on the 3D fluences.
QA results with simulated delivery errors
| Simulated errors | 3D Fluence | 2D Fluence | 2D Measurement | |||
|---|---|---|---|---|---|---|
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| Gantry | 7.4% | 6.2% | 0% | 0% | 2.3% | 1.4% |
| MU | 1.2% | 0.5% | 0% | 0% | 0.7% | 0% |
| Jaw | 2.7% | 1.6% | 0.2% | 0% | 2.5% | 0.2% |
| Collimator | 1.6% | 0.6% | 0.3% | 0% | 0% | 0% |
| MLC | 14.3% | 6.2% | 21.1% | 11.0% | 13.5% | 5.9% |
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| Gantry | 14.1% | 10.3% | 3.3% | 2.7% | 11.5% | 4.6% |
| MU | 51.5% | 37.7% | 43.3% | 24.2% | 47.1% | 36.9% |
| Jaw | 11.6% | 4.2% | 4.8% | 2.3% | 5.2% | 2.6% |
| Collimator | 12.5% | 7.3% | 4.1% | 9.3% | 10.4% | 3.5% |
| MLC | 26.3% | 9.3% | 38.9% | 24.7% | 22.1% | 5.9% |
Figure 4The axial views of fluence differences generating by simulated errors: (a) with fixed 1° gantry angle errors; (b) with fixed 2 mm shifting MLC leaf position errors; (c) 90% of the plan is interrupted during delivery; and (d) an incorrect version of the plan is delivered.
Figure 5Correlations between the simulated errors and the 3% fluence differences test failing rates for various types of errors using both 3DFC QA in solid lines and 2D fluence QA in dashed lines.
Results of correlation coefficients between P and P from all the error types
| Coefficients | Gantry | MU | Jaw | Collimator | MLC |
|---|---|---|---|---|---|
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| Pearson (r) | 0.5631 | 0.5489 | 0.7025 | 0.8575 | 0.5297 |
| Spearman ( | 0.9267 | 0.9183 | 0.9226 | 0.9515 | 0.6754 |
| Spearman (p) | 0.0427 | 0.0242 | 0.0475 | 0 | 0.0305 |
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| Pearson (r) | 0.6125 | 0.5987 | 0.7871 | 0.8824 | 0.5011 |
| Spearman ( | 0.9334 | 0.9423 | 0.9498 | 0.9817 | 0.7042 |
| Spearman (p) | 0.0375 | 0.0197 | 0.0420 | 0 | 0.0421 |
Results of correlation coefficients between P and P from all the error types
| Coefficients | Gantry | MU | Jaw | Collimator | MLC |
|---|---|---|---|---|---|
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| Pearson (r) | 0.4121 | 0.6514 | 0.5248 | 0.8554 | 0.4336 |
| Spearman ( | 0.9701 | 0.8997 | 0.9015 | 0.9810 | 0.7853 |
| Spearman (p) | 0.0232 | 0.0399 | 0.0425 | 0.0315 | 0.0652 |
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| Pearson (r) | 0.5771 | 0.5397 | 0.6541 | 0.7981 | 0.5026 |
| Spearman ( | 0.8653 | 0.9012 | 0.9520 | 0.9805 | 0.7916 |
| Spearman (p) | 0.04196 | 0.0356 | 0.0492 | 0.0157 | 0.0694 |