Sentence examples for fault detection results from inspiring English sources

The fault detection results and the comparison show the superiority of SFM-MSKPCA in fault detection.

From the computation results, it can be also shown that the FD capability in case 2 is stronger than that in case 3 and case 4. From the comparison results of the same-order FD filters, it is clear to see that the fault detection results in polytopic uncertain TRs are less conservative than those in incompletely known and completely unknown TRs.

This work also discusses the importance of selecting an appropriate window length of previous data to be used when computing the maximum likelihood estimates (MLEs) and maximizing the GLR statistic, keeping all fault detection criteria in mind in order to ensure that the desired fault detection results are obtained.

This further improves the fault detection effect.

In general, the fault detection (FD) results can be classified into three types: filter- or observer-based approaches [6 8]; the identification-based FD scheme [9, 10]; and statistic approach [11].

Next, these are practically applied to nonlinear time series identification, prediction, and fault detection problems resulting in higher mapping accuracy, faster learning speed, higher fault sensitivity, and decision reliability in compare to conventional approaches.

There still lacks effective approaches to provide reliable fault detection and classification results for a comprehensive diagnosis.

To this aim, a global active methodology is defined in order to synthesize an additive optimal control input from fault detection and isolation results.

Results show that DTW based on residual signal analysis through the introduction of a reference signal allows the supply components to be suppressed well so that the fault related sideband components are highlighted for obtaining accurate fault detection and diagnosis results.

Introducing a form of analytical redundancy of these measurements can increase the fault detection performance and result in a weight reduction of the aircraft because there is no necessity anymore for the redundant hardware.

The resulted fault detection filter acts then as a reference model.