Component Software Reliability Analysis Method Considering Troubleshooting Process Based on Hisqm Queuing Model
A technique for troubleshooting, queuing model, applied in software testing/debugging etc.
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specific Embodiment approach 1
[0055] Specific implementation mode one: combine figure 1 This embodiment is described. The component software integration test in this embodiment refers to the process of assembling all the components in the application for testing, and all the components in the application work together. As tests are performed, faults are continuously discovered and eliminated, and the software application experiences an increase in reliability. The integration testing process includes the fault detection process and the troubleshooting process. An integration testing troubleshooting strategy links these two stochastic processes.
[0056] During the integration testing process, the troubleshooting activities are organized according to the troubleshooting strategy. Troubleshooting strategy According to the actual development characteristics and budget and schedule requirements, the troubleshooting resources are reasonably allocated, and the detected faults are assigned to the corresponding...
specific Embodiment approach 2
[0123] Specific implementation mode two: combination Figure 2 to Figure 13 This embodiment is described. The difference between this embodiment and the specific embodiment 1 lies in the experimental analysis of the HISQM queuing model. HISQM model parameter setting, the figure 2 The architecture model of the component software application is brought into the improved additive model, and the steady-state probability vector of the component in the application is calculated as
[0124] η=[0.1297, 0.1177, 0.1181, 0.0543, 0.1751, 0.0326, 0.0798, 0.1133, 0.0497, 0.1297]
[0125] Let the component execution time length be 1 time unit each time a component is accessed, and bring them and η into the improved additive model to calculate the execution time ratio of each component.
[0126] The failure behavior of each component is modeled with the improved Goel-Okumoto model, as shown in Equation 7. Without loss of generality, it is assumed that the failure models of all components ...
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