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Zhang et al. / IJOCTA, Vol.15, No.4, pp.649-669 (2025)

























            Figure 10. The first six intrinsic mode function (IMF) components (A) and their corresponding frequency
            spectra (B) obtained from the empirical mode decomposition of the simulated signal






















            Figure 11. The first six intrinsic mode function (IMF) components (A) and their corresponding frequency
            spectra (B) obtained from the ensemble empirical mode decomposition of the simulated signal

                Comparing the spectra in Figures 7, 10, and       As shown in Figure 13, the envelope spectra
            11, it can be observed that the decomposition re-  of the sensitive IMF1 component obtained from
            sults of EMD and EEMD are not ideal. The IMF      EMD and EEMD are both chaotic.        Although
            components obtained from both methods exhibit     spectral lines exist at the fault frequency, there
            varying degrees of mode mixing, with the IMF1     are many interference components, and the spec-
            component being the most significant. The fre-    trum does not exhibit regular variations. As a re-
            quency spectrum of IMF1 shows a highly chaotic    sult, the fault frequency could not be accurately
            pattern, with spectral lines scattered across all  identified, and the required valid information was
            frequency ranges. This influences the accuracy of  not obtained, thus complicating the fault diagno-
            the features extracted from the signal.           sis process. The primary reason for this issue is
                                                              that the EMD method suffers from mode mix-
                However, it is necessary to select the IMF
            components that effectively represent the signal  ing due to its inherent algorithmic limitations.
            characteristics in EMD and EEMD. The compre-      While the EEMD method can address this is-
            hensive evaluation factor for each IMF component  sue to some extent, the white noise added to the
            was calculated (Figure 12).                       signal cannot be completely neutralized, signifi-
                                                              cantly affecting the accuracy of the decomposition
                The largest difference between EMD and        method.
            EEMD occurs between IMF1 and IMF2, as seen
            in Figure 12. Therefore, IMF1 was chosen as the       Based on the above analysis, it can be con-
            sensitive IMF component, and its envelope was     cluded that GJO–VMD can adaptively determine
            demodulated. Figure 13 presents the resulting en-  the most suitable key decomposition parameters
            velope spectrum.                                  according to the characteristics of the signal.
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