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Article

Assessment of Current and Voltage Signature Analysis for the Diagnosis of Open-Phase Faults in Asymmetrical Six-Phase AC Permanent Magnet Synchronous Motor Drives

1
DEI—Department of Electrical, Electronic and Information Engineering—”Guglielmo Marconi”, University of Bologna, 40126 Bologna, Italy
2
DEE—Department of Electrical Engineering, LR-11-ES18, National Engineering School of Tunis, University of Tunis El Manar, Belvedere, Tunis 1002, Tunisia
*
Author to whom correspondence should be addressed.
Energies 2025, 18(11), 2856; https://doi.org/10.3390/en18112856
Submission received: 29 April 2025 / Revised: 22 May 2025 / Accepted: 27 May 2025 / Published: 29 May 2025
(This article belongs to the Special Issue Design, Analysis, Optimization and Control of Electric Machines)

Abstract

:
Multiphase permanent-magnet motors are very attractive solutions for a large variety of applications, and specifically for electric vehicle applications. However, with a higher number of stator phases, multiphase permanent-magnet motors are more subjected to stator failures. Thus, diagnosing the stator status is necessary to guarantee the required efficiency of the motor. This paper deals with two techniques suitable for detecting and localizing open-phase faults in closed-loop controlled six-phase AC permanent-magnet motors. More specifically, this paper is aimed at assessing the diagnosis of open-phase faults based on current and voltage signature analysis. It is shown that the presence of specific harmonics can significantly affect the diagnosis process. Here, two diagnostic space vectors elaborated in the fifth α-β plane, based on the current and voltage signals, are proposed to cope with this limitation. The main contributions of the proposed approach are its implementation simplicity, and the effective immunity of the current-based analysis and voltage-based analysis against harmonic disturbances. The effectiveness of the proposed diagnostic space vector has been analyzed by numerical simulations, then experimentally validated.

1. Introduction

Multiphase Drives (m-D) have experienced significant interest in a wide range of industry applications where the safety and high reliability of operation are key items. With an increased number of phases (more than three) and more degrees of freedom [1], multiphase machines provide more opportunities in terms of their fault diagnosis and fault tolerability, especially for applications such as electric vehicles, aerospace applications [2], energy generation [3], and automotive traction applications [4], where the safety and high reliability of the operation are key items.
Multiphase Permanent-Magnet Synchronous Motors (m-ph PMSMs) take advantage of the powerful strengths of multiphase machines, when compared to the classical three-phase machines, such as lowering the torque ripple, lower current harmonics, and a higher torque/power switch rating. The interest for m-ph PMSMs can be explained by the inherent active stator phase redundancy structure offering a greater degree of freedom which improves substantially the fault tolerance capabilities of the drive [1,5]. Among different topologies of multiphase drives, the multiple three-phase ones (dual, triple, or quadruple), based on the standard three-phase technology, are particularly attractive [6,7].
Having more than three phases, m-ph PMSMs are more exposed to several stator faults than 3-ph PMSMs. Generally, stator faults are initiated by the combination of different phenomena, namely electromechanical stresses, thermal cycling, damages in the contact surfaces, and/or insulations due to chemical stress accelerated by humidity and corrosion. If not detected, the propagation of the above phenomena can lead to excessive local overheating with the risk of dangerous arcing. Comprehensive descriptions and an analysis of stator faults mechanism propagation, introduced by a mixed effect of the above factors, are established in [8], and more recently in [9,10].
Therefore, it is important to perform an effective fault diagnosis process so the faults can be detected, and the risk of sudden catastrophic failure is eliminated. Furthermore, it provides an accurate basis for selecting the adequate subsequent fault-tolerant control strategy to be adopted, so a continuity of service can be ensured.
Different forms of stator failures can affect m-ph PMSMs such as Open-Phase (OPh), Inter-Turn Short-Circuit (ITSC), Phase-to-Phase (PP), Coil-to-Coil (CC), or Coil-to-Ground (CG). Obviously, the consequences on the safety and performance of the machine are different. Specifically, OPh faults are the most frequent stator faults affecting electrical machines.
The literature on fault diagnosis and fault-tolerant strategies for electrical machines has increased rapidly during the last two decades [11,12,13,14], where techniques for stator fault detection have considerably evolved, and even reached a significant maturity level for multiphase motors [15,16,17,18].
Commonly, fault diagnosis strategies can be roughly classified as model-based techniques (MB), knowledge-based techniques (KB), signal-based techniques (SB), and hybrid fault diagnosis approaches. Specifically, OPh fault diagnostic techniques can be classified into two main categories, MB techniques and SB techniques. MB techniques evaluate the difference between the instantaneous drive’s response and the expected response issued from a healthy model, which is adopted for fault detection [19,20,21]. However, these methods face key challenges, which are mainly related to the estimation errors that arise from the inherent inaccuracies of the idealized or assumed model against real-time operation, including the sensitivity to parameter changes, presence of noise and local disturbances, and the inevitable computational latency [17,22]. The above issues can be addressed using adaptive, robust, or intelligent control strategies; however, these algorithms commonly increase the complexity of treatments, leading inevitably to latency increments of the calculation [17,19,20,21,22].
On the other hand, SB techniques are well suited to cope with the above main limitations of MB techniques, which justify the significant advances of SB techniques for diagnosing OPh faults in multiphase machines during the last decade [16,17].
In [23], OPh fault detection and localization is based on the current symmetrical components investigation. The proposed method is based on the pattern analysis of the magnitude and phase angle changes of the fundamental signal. This approach has shown its effectiveness under complicated conditions including a single OPh fault, two-phase adjacent fault, and two-phase nonadjacent fault. The approach proposed in [24] is based on the analysis of the magnetic field pendulous oscillation phenomenon, in which a significant “swing-like” pendulous oscillation in the magnetic field is observed in the case of OPh faults. To minimize the number of sensors, a phase-locked loop technique was developed to overcome the masking effect associated with the compensation action of the closed-loop vector-controlled drive. Thus, four current sensors and a speed sensor are required, which are typically available in five-phase PMSM drives. The performance of this technique has been proved for different OPh configurations, namely single OPh faults, two-adjacent OPh faults, and two non-adjacent OPh faults.
In [25], the approach for OPh fault detection is based on the simultaneous evaluation of the average value of the absolute value of the current and the instantaneous speed. In [26], the fault diagnosis algorithm is based on the interpretation of the reference current errors and the second-order harmonic of the secondary currents in a synchronous reference frame.
Diagnosis techniques for detecting and localizing OPh faults can be further partitioned into Phase Current Monitoring (PhCM) and Current-based Multiple-space Vector Transformation (C-MsVT). Different interesting techniques based on PhCM have been developed for the diagnosis of OPh faults [25,27,28]. Although these techniques are reliable, the large detection time remains the main problem of these approaches. Specifically, the checking process of whether the absolute or squared values of the phase currents are nearing zero during the required fundamental cycles, leading commonly to an easily triggered false alarm, remains the main problem of these approaches.
More recently, by taking advantage of the additional degrees of freedom in multiphase machines, different techniques using C-MsVT have been proposed for the diagnosis of OPh faults by exploiting the fault signatures in the different α-β subspaces. The use of the fundamental α11 and the secondary x–y subspaces, issued from C-MsVT, has shown very interesting results for diagnosing this type of faults in [29,30,31,32]. For a more effective and accurate diagnosis of OPh faults, an innovative technique based on the combined use of PhCM and C-MsVT has been proposed in [33]. Finally, it is worth noting that the interest for the secondary x–y subspaces is mainly justified by the fact that their values are decoupled from fundamental α11, and they typically exhibit significant changes under OPh faults.
Despite the advantages of the C-MsVT, the complexity of combining the fault signatures issued from the different subspaces remains the main limitation of these techniques. In addition, most of the C-MsVT’s proposed strategies are based on zero-current harmonics, and the sensitivity against the presence of harmonic disturbances is not analyzed, except for in [22,32].
In this context, an effective OPh fault diagnosis strategy that is independent of possible harmonic disturbances, and which exploits a single secondary x–y subspace, is highly recommended. In addition, an effective diagnostic process should not require extra hardware equipment and/or specialized sensors for acquiring the minimum of the measurements from the machine drive to be analyzed, so an accurate fault signature can be extracted in a minimum time. Despite the benefits of each diagnosis strategy, signal-based approaches are easy to implement and are generally the preferred approach [11,12,17].
Motivated by the potential of the C-MsVT, the lack of use of Voltage-based Multiple-space Vector Transformation (V-MsVT) and the need to overcome some of the above limitations related to MB and SB techniques, an effective strategy for the diagnosis of open-phase faults in closed-loop controlled six-phase AC permanent-magnet motors, which is based on the analysis of a single x–y subspace, is proposed in this paper.
Being the starting point of any category of a signal-based approach, the current signature analysis and voltage signature analysis for detecting an OPh fault in closed-loop vector-controlled asymmetrical six-phase PMSM are assessed. Specifically, it is shown that the presence of the relevant disturbing harmonics observed, when using V-MsVT, affects considerably the derived fault signature. To cope with this limitation a diagnostic space vector, issued from V-MsVT evaluated in the α55 subspace, is proposed here. The proposed approach has shown its effectiveness not only using V-MsVT, but also using C-MsVT, leading to sensible improvements of both fault signatures for detecting and localizing OPh faults.
This paper is organized as follows. Modeling in terms of the multiple-space vector transformation of the investigated 6-φ PMSM is presented in Section 2. Numerical simulations and experimental tests are presented and commented on Section 3 and Section 4, respectively.

2. Control and Modeling of Six-Phase PMSM

The principle of multiple-space vector transformation for a set of six variables and then the analytical modeling of the six-phase drive system are presented in this section.
The mathematical model of an asymmetrical six-phase machine could be expressed in terms of phase variables ( x A 1 , x A 2 , x B 1 , x B 2 , x C 1 , x C 2 ). However, due to the mutual magnetic coupling among the six stator windings, the equations would turn out to be closely interconnected and, therefore, difficult to interpret and solve.
The Multiple-space Vector Transformation (MsVT) concept is a very useful approach for the modeling, analysis, and control design of multiphase machines and drives [34]. It allows the decomposition of the R 6 space in three orthogonal and independent planes, leading to a more compact and simpler machine model, which is constituted by independent equations.
Note that the transformation to be used depends on the relative position of the magnetic axes of the six stator windings. For an asymmetrical six-phase machine, having the six stator windings distributed as shown in Figure 1a, the proper direct and inverse transformations, which correlate the set of six real variables, x A 1 , x A 2 , x B 1 , x B 2 , x C 1 , and x C 2 , to a new set of three complex variables (space vectors), y ¯ s 1 , y ¯ s 3 , and y ¯ s 5 , can be formulated by (1) and (2), respectively.
y ̄ s 1 = 1 3 x A 1 + x A 2 α ̄ + x B 1 α ̄ 4 + x B 2 α ̄ 5 + x C 1 α ̄ 8 + x C 2 α ̄ 9 y ̄ s 3 = 1 3 x A 1 + x A 2 α ̄ 3 + x B 1 + x B 2 α ̄ 3 + x C 1 + x C 2 α ̄ 3 y ̄ s 5 = 1 3 x A 1 + x A 2 α ̄ 5 + x B 1 α ̄ 8 + x B 2 α ̄ + x C 1 α ̄ 4 + x C 2 α ̄ 9 ,
x A 1 = e [ y ̄ s 3 ] + y ̄ s 1 1 + y ̄ s 5 1 x B 1 = e [ y ̄ s 3 ] + y ̄ s 1 α ̄ 4 + y ̄ s 5 α ̄ 4 x C 1 = e [ y ̄ s 3 ] + y ̄ s 1 α ̄ 8 + y ̄ s 5 α ̄ 8 x A 2 = I m [ y ̄ s 3 ] + y ̄ s 1 α ̄ + y ̄ s 5 α ̄ 7 x B 2 = I m [ y ̄ s 3 ] + y ̄ s 1 α ̄ 5 + y ̄ s 5 α ̄ 11 x C 2 = I m [ y ̄ s 3 ] + y ̄ s 1 α ̄ 9 + y ̄ s 5 α ̄ 3 .
where α ¯ = e j π / 6 , the symbol “.” identifies the scalar product, and “*” is the complex conjugate.
It should be emphasized that the behavior of the six-phase electrical quantities of the machine (voltages, currents, and fluxes) can be described by the trajectories of the three space vectors y ¯ s 1 , y ¯ s 3 , and y ¯ s 5 , which independently move within their orthogonal subspaces, α11, α33, and α55, respectively.
The considered machine is a 30° asymmetrical six-phase AC surface-mounted PMSM, as illustrated in Figure 1a.
The dynamic model of the asymmetrical six-phase surface-mounted PMSM relies on the typical simplifying assumptions adopted for analyzing AC rotating electrical machines. In particular, the iron losses in stator and rotor cores are neglected, the magnetic materials’ permeability is assumed to be very high, the saturation effects are supposed to be negligible, and all cross sections of the machine are considered equivalent. The model, which is valid in a steady state as well as transient operating conditions, takes the effects of the magnetic field in the air gap up to the eleventh spatial harmonic into account. Based on the concept of MsVT, the electrical quantities are developed in a stationary reference frame.
The six stator voltage equations can be formulated for the two sets (k = 1, 2) of three phase systems as
v s A k = R s   i s A k + d ϕ s A k d t ; v s B k = R s   i s B k + d ϕ s B k d t ; v s C k = R s   i s C k + d ϕ s C k d t ;     k = 1 ,   2 .
Based on the direct transformation (1), the stator voltage expressions (3) can be reformulated, leading to a new set of three stator voltage space vectors given by:
v ̄ s 1 = R s i ̄ s 1 + d ϕ ̄ s 1 d t ,
v ̄ s 3 = R s i ̄ s 3 + d ϕ ̄ s 3 d t ,
v ̄ s 5 = R s i ̄ s 5 + d ϕ ̄ s 5 d t ,
where v ̄ s ρ   ( ρ = 1 ,   3 ,   5 ) , i ̄ s ρ   ρ = 1 ,   3 ,   5 , and ϕ ̄ s ρ   ( ρ = 1 ,   3 ,   5 ) are the space vectors in the α ρ β ρ planes of the stator voltages, stator currents, and linkage fluxes, respectively, whereas R s is the stator resistance.
The stator flux space vectors can be expressed by
ϕ ̄ s 1 = L s 1 i ̄ s 1 + 2   ϕ M 1   c o s γ   e j   θ + 2   ϕ M 11   c o s 11   γ   e j   11   θ ,
ϕ ̄ s 3 = L s 3 i ̄ s 3 + 2   ϕ M 3   c o s 3   γ   e j   3   θ + 2   ϕ M 9   c o s 9   γ   e j   9   θ ,
ϕ ̄ s 5 = L s 5 i ̄ s 5 + 2   ϕ M 5   c o s 5   γ   e j   5   θ + 2   ϕ M 7   c o s 7   γ   e j   7   θ ,
In (7)–(9), θ is the rotor position in electrical radians, whereas the constant values ϕ M ρ can be expressed as in (10), respectively. Furthermore, L s 1 , L s 3 , and L s 5 are given by (11)–(13), respectively.
ϕ M ρ = 2   μ 0   N s   L   τ   H r , m a x   K W s ρ π 2 ,                                     ρ = 1 ,   3 ,   5 ,   7 ,   9 ,   11 .  
L s 1 = L s d 1 + 3 μ 0   N S 2   L   τ π 2 δ   P K W s 1 2 + K W s 11 2 121
L s 3 = L s d 3 + 3 μ 0   N S 2   L   τ π 2 δ   P K W s 3 2 9 + K W s 9 2 81
L s 5 = L s d 5 + 3 μ 0   N S 2   L   τ π 2 δ   P K W s 5 2 25 + K W s 7 2 49
Taking the previous equations into account, and considering a power balance, the electromagnetic torque can be formulated as the sum of six contributions by
T e m = T e m , 1 + T e m , 2 + T e m , 3 + T e m , 4 + T e m , 5 + T e m , 6
where
T e m , 1 = 6   P   ϕ M 1   i ̄ s 1 · j   c o s γ   e j   θ
T e m , 2 = 18   P   ϕ M 3   i ̄ s 3 · j   c o s 3   γ   e j   3   θ
T e m , 3 = 30   P   ϕ M 5   i ̄ s 5 · j   c o s 5   γ   e j   5   θ
T e m , 4 = 42   P   ϕ M 7   i ̄ s 5 · j   c o s 7   γ   e j   7   θ
T e m , 5 = 54   P   ϕ M 9   i ̄ s 3 · j   c o s 9   γ   e j   9   θ
T e m , 6 = 66   P   ϕ M 11   i ̄ s 1 · j   c o s 11   γ   e j   11   θ
It can be noted that, besides the fundamental component T e m , 1 , the torque contains several additional oscillating contributions that can be compensated by using a suitable machine design and current control techniques.
An improved FOC scheme is adopted to control the six-phase PMSM (Figure 2).
For a better analysis of the FOC strategy, it is useful to reformulate the voltage equations in the rotating reference frames. As the stator windings design has two separated neutral points (Figure 1a), the current space vector in the third subspace is equal to zero. Hence, the set of three voltage Equations (4)–(6) expressed in the stator reference frame, can be limited to the 1st and 5th subspaces.
Assuming the adopted stator windings design, the voltage equations written in the rotating reference frames lead to:
        v ̄ s 1 r = R S   i ̄ s 1 r + L s 1   d i ̄ s 1 r d t + j   ω   L s 1   i ̄ s 1 r + j   2   ω   ϕ M 1   c o s γ j   22   ω   ϕ M 11   c o s 11   γ   e j   12   θ ,
v ̄ s 5 r = R S   i ̄ s 5 r + L s 5   d i ̄ s 5 r d t + j   5   ω   L s 5   i ̄ s 5 r + j   10   ω   ϕ M 5   c o s 5   γ             j   14   ω   ϕ M 7   c o s 7   γ   e j   12   θ
Basically, four current regulators (PI+1,d, PI+1,q) and (PI+5,d, PI+5,q) have been implemented in the 1st and 5th d-q rotor reference frames, respectively.
In order to enhance the current tracking performance in planes d1-q1 and d5-q5, and to reduce the torque ripple, an improved (IFOC) is adopted, which includes four additional regulators, (PI−11,d, PI−11,q) and (PI−7,d, PI−7,q), implemented in reference frames synchronous with the eleventh and seventh harmonics of the back-emfs, respectively.
In this way, the fifth and seventh harmonics of the stator current are zero and, consequently, the fifth and seventh harmonics of the reference voltage in the fifth space v̅S5,ref coincide with the fifth and seventh harmonic of the EMFs, respectively.
In the next sections, the spectral aspects of the current and voltage space vectors in the fifth plane, with and without the presence of an OPF, will be analyzed by simulations and experimental tests.

3. Simulation Results

In order to assess the detectability and localization aspects of OPh faults, based on CSA and VSA, a complete simulation scheme of a six-phase PMSM controlled by the IFOC scheme shown in Figure 2 has been implemented in Matlab/SimulinkTM. The main machine parameters are reported in Table 1. A duration of 10 s with a sampling rate of 5.0 kHz for data acquisition and frequency domain analysis have been adopted.
Simulations were first carried out under a healthy condition with 150 rpm and 25% of the rated load. The behavior of the healthy machine under the healthy condition is shown in Figure 3, Figure 4 and Figure 5. The time-domain waveforms of the six-phase currents are reported in Figure 3, where the currents are balanced due to the identical-stator six-phase impedances. The spectra of the current space vectors, evaluated in the first and fifth subspaces, are reported in Figure 4a,b, respectively, where only the fundamental component is present in i ¯ S 1 , whereas a zero dB is observed in i ¯ S 5 .
In terms of the voltage space vectors, the spectra of v̅S1,ref and v̅S5,ref are represented in Figure 4c,d, respectively, where the fundamental component in the first plane is evidenced, and the presence of the 5th and 7th harmonics in the fifth plane are verified. The reference results, corresponding to the healthy condition, confirm the analysis anticipated in the previous section for the adopted IFOC strategy (Figure 2).
The loci of the current space vectors, evaluated in the first and fifth subspaces, are depicted in Figure 5a,b, respectively. The resulting circular behavior of the current locus in the α11 plane, and the null current value α55 plane confirm the proper operation of the system. The corresponding voltage space vectors, evaluated in the first and fifth planes, are depicted in Figure 5c,d, respectively.
Similarly, the voltage space vector in the α11 plane exhibits a circular behavior, whereas small variations can be evidenced in the α55 plane due to the small effect of the +5th and −7th harmonic components observed in Figure 4d, and already established in [35]. The loci derived from CSA and VSA reported in Figure 5 are considered as a reference for the faulty phase cases.
The behavior of the drive under the OPh fault in phase A1 is reported in Figure 6. Under this fault condition, the current cannot flow through phase A1, leading to an evident current imbalance (Figure 6).
Considering the reported spectra in Figure 4 as references, the corresponding spectra under OPh faults in phase A1 (blue dotted line) and B1 (red solid line) have been computed and reported in Figure 7.
Let us consider the spectra corresponding to the first OPh fault in phase A1 (blue dotted line). By comparing the spectra of i ¯ S 1 for the healthy (Figure 4a) and faulty (Figure 7a) conditions, the magnitude evolution of the inverse component at −f is evident, which is classically expected in the α11 plane, leading to a first spectral fault detection signature of the Oph fault. For the same fault condition, the spectrum of the space vector i ¯ S 5 , is depicted in (Figure 7b). With reference to the healthy case (Figure 4b), the relevant magnitude variation of the fault components at ±f are clearly evidenced, leading to a second more relevant spectral fault detection signature of the Oph fault.
In terms of VSA, the spectra of v̅S1,ref and v̅S5,ref are reported in Figure 7c,d, respectively. Compared to the healthy case (Figure 4c), the spectrum of v̅S1,ref shows an inverse component at −f under the faulty condition (Figure 7c), whereas the voltage space vector v̅S5,ref has shown a relevant magnitude variation of the fault components ±f. Considering the magnet pole arc design, the magnitudes of the 5th and 7th harmonics remain unchanged.
By comparing the spectra obtained in the healthy condition (Figure 4) and those corresponding to an OPh fault in phase A1 (blue dotted line in Figure 7), both CSA and VSA can be considered for OPh fault detection. However, by observing the similarities of the spectra obtained under OPh faults in phase A1 (blue dotted line) and B1 (red solid line), reported in Figure 7, one can note that a possible solution for faulty phase identification cannot be based on the spectral analysis, even considering CSA or VSA.
The current locus evaluated in the α11 plane (Figure 8a) shows a quasi-circular trajectory and does not show a particular shape when compared to the healthy condition (Figure 5a). Nevertheless, when compared to the healthy case (Figure 5b), the current space vector evaluated in the α55 plane (Figure 8b) indicates a significant variation, leading to a clear detection of the tested fault. Specifically, the current locus exhibits a particular orientation of 180° with the real axis, which corresponds to the direction of the phase A1 angle shown in Table 2. The voltage space vectors, evaluated in the first and fifth planes, are reported in Figure 8c,d. In the α11 plane, the voltage locus does not change significantly, showing a particular shape corresponding to the introduced OPh fault. Conversely, when compared to the healthy case (Figure 5d), the voltage space vector evaluated in the fifth plane shows a different shape due to the introduced OPh fault.
Due to the dominance of the fundamental component in the α11 plane for both the current and voltage space vectors, the corresponding loci have shown a quasi-circular shape and then make the detection of an OPh fault difficult. As far as the current and voltage loci evaluated in the fifth plane are concerned, their relevant variations are useful for OPh fault detection.
In order to explore the feasibility of OPh fault localization through CSA and VSA, a series of simulations were performed considering different OPh fault configurations. The behavior of the drive, under the six OPh fault configurations, in terms of CSA and VSA evaluated in the first and fifth planes, are reported in Figure 9, Figure 10, Figure 11, Figure 12 and Figure 13, respectively.
As a first comment, the very low sensitivity of CSA to an OPh fault, evaluated in the first plane, is confirmed by the reported loci in Figure 9a, Figure 10a, Figure 11a, Figure 12a, Figure 13a, corresponding to the different configurations of an OPh fault, respectively. The same comment is valid for the results in terms of VSA, evaluated in the first plane, and reported in Figure 9c, Figure 10c, Figure 11c, Figure 12c, Figure 13c.
The results reported in Figure 9b, Figure 10b, Figure 11b, Figure 12b, Figure 13b are the current loci evaluated in the α55 plane, where the current space vectors exhibit distinct orientations, relative to the real axis depending on the OPh fault location. With a less precise orientation, the same comment is also valid for the voltage space vectors, evaluated in the same subspace and reported in Figure 9d, Figure 10d, Figure 11d, Figure 12d, Figure 13d, for the different OPh fault configurations, respectively. In Table 2, obtained ideal directions of the current or voltage loci, evaluated in the α55 plane, are shown.
Based on the current space vector direction, evaluated in the α55 plane, OPh fault detection and localization are clearly evidenced. However, using the corresponding space vector in terms of VSA, due to the disturbing presence of the +5th and −7th harmonic components [35], only OPh fault detection is possible.
To refine the accuracy of angle tracking through Current Space Analysis (CSA), and more importantly, to make possible the use of Voltage Space Analysis (VSA) for localizing an OPh fault, two diagnostic space vectors are proposed, which adeptly merge the isolated contributions of the ±1 fault harmonic components under the OPh fault condition.
A flowchart illustrating the proposed strategy with the computation of the diagnostic space vectors D ¯ v and D ¯ i , is shown in Figure 14.
Due to the two independent neutral points of the stator windings, four current sensors are sufficient to determine the values of the six stator currents. By applying the MsVT transformation (1), the current space vector i ¯ s 5 is calculated. The space vector v ¯ s 5 , r e f is available in the control scheme at the output of the current regulators based on PI+5 and PI−7, as shown in Figure 2. As can be seen in Figure 14, i ¯ s 5 and v ¯ s 5 , r e f are then processed by some dedicated low-pass filters, implemented in reference frames synchronous with the fault harmonic components +1 and −1 in the α55 plane.
In Figure 15, the behaviors of the proposed diagnostic space vector, under healthy and OPh fault conditions in phase A1, are reported.
In Figure 15a,c, the behaviors of the diagnostic space vector D ¯ i   under healthy and OPh fault conditions in phase A1 are reported, respectively. Comparing the loci obtained from healthy to faulty conditions, it is evident that the detection and specifically the 0° orientation of the vector under faulty conditions (Figure 15c) is slightly improved when compared to the current space vector i ¯ S 5   reported in Figure 8b.
On the other hand, the results based on the diagnostic space vector D ¯ v   under healthy and OPh fault conditions in phase A1 are reported in Figure 15b and d, respectively. Under the healthy condition, comparing the obtained zero value of vector v̅S5,±1, (Figure 15b) to vector v̅S5,ref (Figure 5d), it is evident that the detectability of the healthy case has been improved. More importantly, comparing the same quantities, reported in Figure 8d and Figure 15d, respectively, the 0° orientation of the vector D ¯ v   is clearly evidenced, which is in total agreement with the orientation of vector D ¯ i , leading to an evident localization of the faulty phase A1.

4. Experimental Results

In order to validate the results obtained in simulations, a complete drive system has been installed in the Laboratory and some experimental tests have been performed. The setup consists of a six-phase MOSFET inverter and a 5.5 kW asymmetrical six-phase surface-mounted PMSM. The main parameters of the six-phase PMSM are indicated in Table 1, where four poles, 48 slots, and double-layer, short pitch stator windings, having two slots per pole and per phase, are considered. Some pictures of the experimental bench are shown in Figure 16, where a detailed schematic diagram of the built test bench is illustrated in Figure 16c. The six-phase motor is coupled to a three-phase induction motor acting as the load. The FOC scheme of Figure 2 was implemented in a TMS–320F2812-based electronic control board. Having 32-bit CPU, 150 MHz as the operating frequency, and a high-performance fixed-point DSP operation, the adopted control board meets the implementation requirements for the adopted control and the proposed associated diagnosis strategy. The accuracy of the current sensors is of ±1.5%, with a linearity of ±1.5%, and a frequency bandwidth of (−3 dB) 80 kHz. The encoder resolution is of 2048 pulses per revolution.
The VSI switching frequency is of 5.5 kHz with a deadtime of 3.2 µs, whereas a sampling rate of 5.0 kHz for the data acquisition and frequency domain analysis was adopted.
The performance of the six-phase drive was first assessed under healthy conditions and during steady-state conditions for a constant speed of 150 r/min and a torque setpoint of 5 Nm. The corresponding results are reported in Figure 17, Figure 18 and Figure 19.
The stator currents of phases A1, B1, A2, and B2 are reported in Figure 17. As can be seen, the stator currents are almost balanced and sinusoidal.
The corresponding current i ¯ S 5 and voltage v̅S5,ref space vectors, evaluated in the fifth plane, are depicted in Figure 18a,b, respectively. As expected, due to the action of the current regulators (PI+5 and PI−7), the current locus shows a quasi-null value (Figure 18a); the residual quantity observed on the figure is mainly due to noise and local disturbance effects. With reference to the voltage locus, the effects of the emfs harmonics are clearly shown (Figure 18b), as anticipated in the previous sections. As can be seen, the obtained experimental current (Figure 18a) and voltage (Figure 18b) loci evaluated in the α55 plane corroborate the Simulation Results (Figure 5b,d), respectively, for the healthy machine.
It should be noted that the observed small disturbances for the current space vector i ¯ S 5   are mainly due to the intrinsic manufacturing asymmetries of the motor, temperature effects, inverter nonlinearity (dead times and voltage drops on the switches), and current sensors tuning, which can affect the accuracy of the locus not only in healthy conditions, but also under the presence of OPh faults. It is worth noting that adding these disturbing effects to the presence of the 5th and 7th harmonics due to the magnet pole arc design will complicate further the use of the voltage space vector v̅S5,ref locus for detecting and localizing an OPh fault. These effects are expected to be eliminated using the proposed diagnostic space vector.
In Figure 19, and under the same healthy operating conditions, the behaviors of the proposed diagnostic space vectors, in terms of the current and voltage, are reported, where clear zero current and voltage are evidenced. These experimental results corroborate the anticipated Simulation Results reported in Figure 15 for the healthy case, which validate the performance of the proposed strategy.
Specifically, comparing the current loci of the space vectors i ¯ S 5   and D ¯ i   and represented in Figure 18a and Figure 19a, respectively, it is clear that the proposed diagnostic space vector D ¯ i   provides a high immunity against noise and the disturbing effects discussed above, leading to an accurate diagnosis of the healthy state of the machine, as D ¯ i   is practically equal to zero.
On the other hand, by comparing the voltage loci of the space vectors v̅S5 and D ¯ v   reported in Figure 18b and Figure 19b, respectively, one can note that the proposed diagnostic space vector D ¯ v   eliminates the disturbing effects of the 5th and 7th harmonics, leading to a clear detection of the healthy state of the machine, as D ¯ v   is practically equal to zero.
In order to assess the capability of CSA and VSA in detecting and localizing OPh faults, a series of tests have been performed.
In Figure 20, the behavior of the six-phase drive is shown during a transition from a normal operation to an OPh fault in phase A1. During the test, the healthy conditions are maintained during the first 2.5 s, where the currents are quite balanced and sinusoidal. At t = 2.5 s, an OPh fault is applied in phase A1, where a null current value is evidenced, leading to an imbalance in the phase currents.
Current and voltage loci, evaluated in the α55 plane, are depicted in Figure 21a,b, respectively. As can be seen, the current locus in the α55 plane (Figure 21a) is different from zero and shows a vector orientation of 0° with respect to the real axis, as predicted by the Simulation Results (Figure 8b), enabling the detection and localization of the OPh fault applied to phase A1. In terms of VSA, the voltage locus evaluated in the α55 plane is depicted in Figure 21b. When compared to the reference voltage locus of Figure 19b, the voltage space vector changes significantly in the presence of the fault, as anticipated by the simulation (Figure 8d), leading to an evident detection of the fault, whereas the localization of the opened phase based on a clear angular orientation remains difficult.
For the same operating condition, a second test was carried out under an OPh fault in phase B1, where the obtained current and voltage loci, evaluated in the α55 plane, are depicted in Figure 22a,b, respectively. As can be seen, current and voltage paths in the α55 plane (Figure 22a) reveals a distinct orientation of 60° with respect to the real axis, enabling the detection and localization of the Oph fault in phase B1. It is worth noting that the difficulty of interpretation for detection and, more importantly, localization purposes observed for the voltage space vector v̅S5,ref under the OPh fault in phase A1 (Figure 21b) are also valid for this second faulty case (OPh-B1). After several experiments, it should be noted that the same difficulties have been observed for the remaining faulty phase cases.
The loci of the diagnostic space vector, under the OPh fault in phase A1 and B1, are reported in Figure 23 and Figure 24, respectively.
When examining the reported current loci in Figure 23a and Figure 24a, using the proposed diagnostic space vector D ¯ i , with reference to those obtained using i ¯ S 5   reported in Figure 21a and Figure 22a, respectively, the improvements in terms of the angular orientation accuracy are evident, leading to a more accurate OPh fault localization.
In terms of VSA, by comparing the loci reported in Figure 23b and Figure 24b to those reported in Figure 21b and Figure 22b, one comes to the conclusion that based on the proposed diagnostic voltage space vector D ¯ v , an accurate detection and localization of an OPh fault is validated.

5. Conclusions

Multiphase machines provide a higher reliability performance compared to the three-phase machines configuration; however, with more stator phases, multiphase machines are more subjected to different potential stator anomalies and, more, specifically OPh faults. In this paper, current and voltage signature analyses have been assessed for the diagnosis of OPh faults in asymmetrical six-phase ac PMSM drives. It was shown that the current and voltage spectral-based analysis are effective for detecting open-phase faults; however, the limitation of this strategy for fault localization was evidenced. However, current and voltage space vectors, evaluated in the α55 plane, have shown a relative sensitivity to the fault location, with a certain limitation of the voltage use due to the imposed disturbing effect of the fifth and seventh harmonics.
To cope with this issue, two diagnostic space vectors elaborated in the fifth α-β plane, based on the current and voltage signals, respectively, have been proposed.
The effectiveness of the proposed diagnostic space vectors has been validated by means of numerical simulations and experimental tests.

Author Contributions

Conceptualization, Y.G., C.R., and A.T.; Funding acquisition, C.R.; Investigation, Y.G., and A.T.; Methodology, Y.G., A.T. and D.C.; Project administration, C.R. and D.C.; Software, Y.G. and A.T.; Writing—original draft, Y.G., A.T., C.R. and D.C. All authors have read and agreed to the published version of the manuscript.

Funding

This work was supported in part by the Italian MUR for financial support through the MOST—Sustainable Mobility Center, Centro Nazionale per la Mobilita` Sostenibile, Spoke 13 of the National Recovery and Resilience Plan (PNRR). Mission 4, component 2, investment 1.4 e D.D. 1033 17/06/2022, CN00000023.

Data Availability Statement

Data is contained within the article.

Conflicts of Interest

The authors declare no conflicts of interest.

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Figure 1. System block scheme: (a) six-phase drive based on asymmetrical AC six-phase surface-mounted permanent-magnet synchronous motor for electric vehicle applications. (b) Three MOSFETs in parallel.
Figure 1. System block scheme: (a) six-phase drive based on asymmetrical AC six-phase surface-mounted permanent-magnet synchronous motor for electric vehicle applications. (b) Three MOSFETs in parallel.
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Figure 2. Block scheme of the adopted IFOC strategy.
Figure 2. Block scheme of the adopted IFOC strategy.
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Figure 3. Simulation results: time-domain waveforms of the six-phase currents under healthy condition.
Figure 3. Simulation results: time-domain waveforms of the six-phase currents under healthy condition.
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Figure 4. Simulation results: behavior of the drive under healthy operating condition. (a) Spectrum of i ¯ S 1 , (b) Spectrum of i ¯ S 5 . (c) Spectrum of v̅S1,ref. (d) Spectrum of v̅S5,ref.
Figure 4. Simulation results: behavior of the drive under healthy operating condition. (a) Spectrum of i ¯ S 1 , (b) Spectrum of i ¯ S 5 . (c) Spectrum of v̅S1,ref. (d) Spectrum of v̅S5,ref.
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Figure 5. Simulation results: behavior of the drive under healthy operating condition. (a) Current locus in the α11 plane (1 A/div). (b) Current locus in the α55 plane (1 A/div). (c) Voltage locus in the α11 plane (5 V/div). (d) Voltage locus in the α55 plane (0.5 V/div).
Figure 5. Simulation results: behavior of the drive under healthy operating condition. (a) Current locus in the α11 plane (1 A/div). (b) Current locus in the α55 plane (1 A/div). (c) Voltage locus in the α11 plane (5 V/div). (d) Voltage locus in the α55 plane (0.5 V/div).
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Figure 6. Simulation results: time-domain waveforms of the six-phase currents under OPh fault in phase A1.
Figure 6. Simulation results: time-domain waveforms of the six-phase currents under OPh fault in phase A1.
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Figure 7. Simulation results: behavior of the drive under OPh faults in phase A1 (blue dotted line) and B1 (red solid line). (a) Spectrum of i ¯ S 1 , (b) Spectrum of i ¯ S 5 . (c) Spectrum of v̅S5,ref. (d) Spectrum of v̅S5,ref.
Figure 7. Simulation results: behavior of the drive under OPh faults in phase A1 (blue dotted line) and B1 (red solid line). (a) Spectrum of i ¯ S 1 , (b) Spectrum of i ¯ S 5 . (c) Spectrum of v̅S5,ref. (d) Spectrum of v̅S5,ref.
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Figure 8. Simulation results: behavior of the drive under OPh fault in phase A1 condition. (a) Current locus in the α11 plane (1 A/div). (b) Current locus in the α55 plane (1 A/div). (c) Voltage locus in the α11 plane (5 V/div). (d) Voltage locus in the α55 plane (0.5 V/div).
Figure 8. Simulation results: behavior of the drive under OPh fault in phase A1 condition. (a) Current locus in the α11 plane (1 A/div). (b) Current locus in the α55 plane (1 A/div). (c) Voltage locus in the α11 plane (5 V/div). (d) Voltage locus in the α55 plane (0.5 V/div).
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Figure 9. Simulation results: behavior of the drive under OPh fault in phase B1 condition. (a) Current locus in the α11 plane (1 A/div). (b) Current locus in the α55 plane (1 A/div). (c) Voltage locus in the α11 plane (5 V/div). (d) Voltage locus in the α55 plane (0.5 V/div).
Figure 9. Simulation results: behavior of the drive under OPh fault in phase B1 condition. (a) Current locus in the α11 plane (1 A/div). (b) Current locus in the α55 plane (1 A/div). (c) Voltage locus in the α11 plane (5 V/div). (d) Voltage locus in the α55 plane (0.5 V/div).
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Figure 10. Simulation results: behavior of the drive under OPh fault in phase C1 condition. (a) Current locus in the α11 plane (1 A/div). (b) Current locus in the α55 plane (1 A/div). (c) Voltage locus in the α11 plane (5 V/div). (d) Voltage locus in the α55 plane (0.5 V/div).
Figure 10. Simulation results: behavior of the drive under OPh fault in phase C1 condition. (a) Current locus in the α11 plane (1 A/div). (b) Current locus in the α55 plane (1 A/div). (c) Voltage locus in the α11 plane (5 V/div). (d) Voltage locus in the α55 plane (0.5 V/div).
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Figure 11. Simulation results: behavior of the drive under OPh fault in phase A2 condition. (a) Current locus in the α11 plane (1 A/div). (b) Current locus in the α55 plane (1 A/div). (c) Voltage locus in the α11 plane (5 V/div). (d) Voltage locus in the α55 plane (0.5 V/div).
Figure 11. Simulation results: behavior of the drive under OPh fault in phase A2 condition. (a) Current locus in the α11 plane (1 A/div). (b) Current locus in the α55 plane (1 A/div). (c) Voltage locus in the α11 plane (5 V/div). (d) Voltage locus in the α55 plane (0.5 V/div).
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Figure 12. Simulation results: behavior of the drive under OPh fault in phase B2 condition. (a) Current locus in the α11 plane (1 A/div). (b) Current locus in the α55 plane (1 A/div). (c) Voltage locus in the α11 plane (5 V/div). (d) Voltage locus in the α55 plane (0.5 V/div).
Figure 12. Simulation results: behavior of the drive under OPh fault in phase B2 condition. (a) Current locus in the α11 plane (1 A/div). (b) Current locus in the α55 plane (1 A/div). (c) Voltage locus in the α11 plane (5 V/div). (d) Voltage locus in the α55 plane (0.5 V/div).
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Figure 13. Simulation results: behavior of the drive under OPh fault in phase C2 condition. (a) Current locus in the α11 plane (1 A/div). (b) Current locus in the α55 plane (1 A/div). (c) Voltage locus in the α11 plane (5 V/div). (d) Voltage locus in the α55 plane (0.5 V/div).
Figure 13. Simulation results: behavior of the drive under OPh fault in phase C2 condition. (a) Current locus in the α11 plane (1 A/div). (b) Current locus in the α55 plane (1 A/div). (c) Voltage locus in the α11 plane (5 V/div). (d) Voltage locus in the α55 plane (0.5 V/div).
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Figure 14. Flowchart of the proposed diagnosis process with the computation of the diagnostic space vectors D ¯ v and D ¯ i .
Figure 14. Flowchart of the proposed diagnosis process with the computation of the diagnostic space vectors D ¯ v and D ¯ i .
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Figure 15. Simulation results: behavior of the diagnostic space vector under healthy and OPh fault in phase A1. (a) Locus of D ¯ i   in healthy condition. (b) Locus of D ¯ v   in healthy condition. (c) Locus of vector D ¯ i   under OPh-A1. (d) Locus of D ¯ v   under OPh-A1.
Figure 15. Simulation results: behavior of the diagnostic space vector under healthy and OPh fault in phase A1. (a) Locus of D ¯ i   in healthy condition. (b) Locus of D ¯ v   in healthy condition. (c) Locus of vector D ¯ i   under OPh-A1. (d) Locus of D ¯ v   under OPh-A1.
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Figure 16. Experimental setup details: (a) View of the laboratory test bench; (b) Six-phase inverter; (c) Schematic diagram of the experimental setup.
Figure 16. Experimental setup details: (a) View of the laboratory test bench; (b) Six-phase inverter; (c) Schematic diagram of the experimental setup.
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Figure 17. Experimental results: behavior of the drive under healthy condition with time-domain waveforms of the stator currents (1 A/div, 500 ms/div).
Figure 17. Experimental results: behavior of the drive under healthy condition with time-domain waveforms of the stator currents (1 A/div, 500 ms/div).
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Figure 18. Experimental results: behavior of the drive under healthy condition. (a) Current locus in the α55 plane (2.5 mA/div). (b) Voltage locus in the α55 plane (500 mV/div).
Figure 18. Experimental results: behavior of the drive under healthy condition. (a) Current locus in the α55 plane (2.5 mA/div). (b) Voltage locus in the α55 plane (500 mV/div).
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Figure 19. Experimental results: behavior of the diagnostic space vector under healthy condition. (a) Locus of the diagnostic space vector D ¯ i   (2.5 mA/div). (b) Locus of the diagnostic space vector D ¯ v (200 mV/div).
Figure 19. Experimental results: behavior of the diagnostic space vector under healthy condition. (a) Locus of the diagnostic space vector D ¯ i   (2.5 mA/div). (b) Locus of the diagnostic space vector D ¯ v (200 mV/div).
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Figure 20. Experimental results: behavior of the drive under an OPh fault in phase A1 with time-domain waveforms of the stator currents (1 A/div, 500 ms/div).
Figure 20. Experimental results: behavior of the drive under an OPh fault in phase A1 with time-domain waveforms of the stator currents (1 A/div, 500 ms/div).
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Figure 21. Experimental results: behavior of the drive under an OPh fault in phase A1. (a) Current locus in the α55 plane (2.5 mA/div). (b) Voltage locus in the α55 plane (500 mV/div).
Figure 21. Experimental results: behavior of the drive under an OPh fault in phase A1. (a) Current locus in the α55 plane (2.5 mA/div). (b) Voltage locus in the α55 plane (500 mV/div).
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Figure 22. Experimental results: behavior of the drive under an OPh fault in phase B1. (a) Current locus in the α55 plane (2.5 mA/div). (b) Voltage locus in the α55 plane (500 mV/div).
Figure 22. Experimental results: behavior of the drive under an OPh fault in phase B1. (a) Current locus in the α55 plane (2.5 mA/div). (b) Voltage locus in the α55 plane (500 mV/div).
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Figure 23. Experimental results: behavior of the diagnostic space vector under an OPh fault in phase A1. (a) Locus of the diagnostic space vector D ¯ i   (2.5 mA/div). (b) Locus of the diagnostic space vector D ¯ v (200 mV/div).
Figure 23. Experimental results: behavior of the diagnostic space vector under an OPh fault in phase A1. (a) Locus of the diagnostic space vector D ¯ i   (2.5 mA/div). (b) Locus of the diagnostic space vector D ¯ v (200 mV/div).
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Figure 24. Experimental results: behavior of the diagnostic space vector under an OPh fault in phase B1. (a) Locus of the diagnostic space vector D ¯ i   (2.5 mA/div). (b) Locus of the diagnostic space vector D ¯ v (200 mV/div).
Figure 24. Experimental results: behavior of the diagnostic space vector under an OPh fault in phase B1. (a) Locus of the diagnostic space vector D ¯ i   (2.5 mA/div). (b) Locus of the diagnostic space vector D ¯ v (200 mV/div).
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Table 1. Parameters of the asymmetrical six-phase surface-mounted PMSM.
Table 1. Parameters of the asymmetrical six-phase surface-mounted PMSM.
Parameter
Phase resistance0.36Ohm
Pole number4-
Phase inductance1.44mH
Stator inner radius150mm
Stator outer radius240mm
Slot number48-
Stator winding pitch165°el. degrees
Magnet pole arc151°el. degrees
Magnet radial thickness5mm
Table 2. Current and voltage loci orientations under an open-phase fault in asymmetrical six-phase machine.
Table 2. Current and voltage loci orientations under an open-phase fault in asymmetrical six-phase machine.
Index of the Opened Phase
A1B1C1A2B2C2
i ¯ S 5 or v̅S504π/32π/3−π/6−5π/6π/2
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MDPI and ACS Style

Gritli, Y.; Rossi, C.; Tani, A.; Casadei, D. Assessment of Current and Voltage Signature Analysis for the Diagnosis of Open-Phase Faults in Asymmetrical Six-Phase AC Permanent Magnet Synchronous Motor Drives. Energies 2025, 18, 2856. https://doi.org/10.3390/en18112856

AMA Style

Gritli Y, Rossi C, Tani A, Casadei D. Assessment of Current and Voltage Signature Analysis for the Diagnosis of Open-Phase Faults in Asymmetrical Six-Phase AC Permanent Magnet Synchronous Motor Drives. Energies. 2025; 18(11):2856. https://doi.org/10.3390/en18112856

Chicago/Turabian Style

Gritli, Yasser, Claudio Rossi, Angelo Tani, and Domenico Casadei. 2025. "Assessment of Current and Voltage Signature Analysis for the Diagnosis of Open-Phase Faults in Asymmetrical Six-Phase AC Permanent Magnet Synchronous Motor Drives" Energies 18, no. 11: 2856. https://doi.org/10.3390/en18112856

APA Style

Gritli, Y., Rossi, C., Tani, A., & Casadei, D. (2025). Assessment of Current and Voltage Signature Analysis for the Diagnosis of Open-Phase Faults in Asymmetrical Six-Phase AC Permanent Magnet Synchronous Motor Drives. Energies, 18(11), 2856. https://doi.org/10.3390/en18112856

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