Published: May 26, 2026

Enhanced broken-bar fault diagnosis in asynchronous motors using SVM classification

Ahmed Amrane1
Ali Chabane2
Khaled Benfriha3
Taha Chettibi4
1, 2, 4LIECPS, Ecole Nationale Supérieure des Technologies Avancées (ENSTA), Algiers, Algeria
3Arts et Métiers Institute of Technology, LCFC, 75013, Paris, France
44Department of Mechanics, University of Blida 1, Algeria
Corresponding Author:
Ahmed Amrane
Article in Press
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Abstract

This paper presents an enhanced broken-bar fault diagnosis approach for Asynchronous Motors, based on a simulation-driven Support Vector Machines (SVM) framework. To circumvent the lack of experimental fault data, a high-fidelity dynamic model is developed: the healthy multi-winding Asynchronous Motors is extended with fault-specific resistances to emulate 0, 1, 2, and 3 broken rotor bars under varying operating conditions. Electromechanical and electrical signals signatures (stator currents, speed, torque) are simulated and transformed into discriminative feature vectors, forming a labeled training dataset. A supervised SVM classifier is then implemented in two successive stages, first a binary classification to detect healthy versus faulty states and second a multi-class classification (one-vs-one) to identify the exact number of broken bars. Results show high accuracy when torque and speed features are combined, highlighting the method’s robustness and data efficiency. By integrating physical modeling with interpretable machine learning, the proposed approach offers a reproducible and scalable solution for predictive maintenance in industrial motor systems.

Enhanced broken-bar fault diagnosis in asynchronous motors using SVM classification

Highlights

  • A multi-winding dynamic model enables high-fidelity simulation of asynchronous motors, addressing the critical lack of experimental data for predictive maintenance and fault diagnosis.
  • A two-stage SVM framework optimizes diagnostic accuracy by separating detection (healthy vs. faulty) and quantification (fault severity), achieving a better accuracy-cost trade-off.
  • Feature extraction combining electromagnetic torque and rotational speed signatures maximizes detection accuracy for severe multi-class faults, even under variable load conditions.
  • The use of an interpretative RBF-kernel SVM provides clear decision boundaries, allowing engineers to visualize fault classification logic and enhance system reliability.
  • The study demonstrates up to 93.8% accuracy in complex fault scenarios, proving that torque-speed fusion is a superior method for quantifying broken rotor bar severity in industrial settings.

1. Introduction

In industrial settings, preventive maintenance is critical for anticipating equipment failures and mitigating unplanned downtime. By enabling early detection of incipient faults, it supports timely interventions that reduce operational disruptions, lower maintenance costs, and enhance both productivity and safety [1, 2]. Furthermore, such proactive strategies ensure compliance with quality and regulatory standards while significantly extending the service life of key machinery [3, 4].

Asynchronous Motors are the workhorses of modern industrial systems, widely deployed in production lines, machine tools, conveyors, pumps, and ventilation systems owing to their robustness, low cost, and high starting torque [5, 6]. Their capability for variable-speed operation and near maintenance-free service further consolidates their dominance as the most prevalent motor type in industry [6-8]. Nevertheless, despite their reliability, these machines are prone to critical faults, particularly in the rotor, whose early detection remains a key challenge for predictive maintenance.

Among the most critical faults affecting Asynchronous Motors are rotor-related defects, particularly broken rotor bars, which can lead to increased vibration, torque oscillations, overheating, and eventually catastrophic failure if left undetected [9]. Due to the difficulty of directly monitoring the rotor in operation, model-based approaches have emerged as promising alternative, relying on mathematical representations to capture fault signatures in measurable stator quantities. For instance, Amrane et al. [9] proposed a fault detection and isolation scheme using nonlinear analytical redundancy, demonstrating the potential of model-driven strategies to enhance reliability and support preventive maintenance. Nevertheless, such methods like other high-gain or adaptive observers used in electromechanical systems [10] remain sensitive to model inaccuracies, unmolded dynamics (friction, saturation), and parametric uncertainties, often requiring complex compensation mechanisms. This limitation motivates the integration of high-fidelity simulation with robust, geometry-aware classification techniques, as pursued in this work.

Recent advances in fault diagnosis have leveraged sophisticated signal processing and machine learning techniques to improve detection accuracy. For instance, time frequency decomposition methods such as Variation Mode Decomposition (VMD) [11] and Enhanced Reduced-order Symptom Recognition (ERSR) [12] have shown promise in enhancing spectral clarity and reducing data dimensionality, primarily for bearing and imbalance faults. Similarly, deep learning approaches, including CNN based classifiers trained on 2D vibration images [13] or hybrid schemes combining Bessel transform and neural networks [14], have achieved high performance in gear bearing compound fault scenarios. Even in the electromagnetic domain, wavelet-CNN architectures have been explored for modulation recognition in RF signals [15], underscoring the trend toward computationally intensive, data-hungry models. Ensemble methods and stochastic resonance techniques [16] further extend the toolbox for vibration-based monitoring of rolling elements, and unsupervised clustering such as K-means for failure mode classification [17] further extend the toolbox for vibration-based monitoring of rolling elements.

However, most existing methods are validated on bearing or gear datasets [12]. They rely heavily on experimental data, which is often unavailable for rotor faults like broken bars. Moreover, their complexity may hinder interpretability and real-time deployment in industrial settings. Given that broken-bar faults predominantly exhibit electrical signatures (notably in stator current) rather than detectable vibration patterns, a diagnosis framework must prioritize physical interpretability, data efficiency, and robustness.

Recent studies have further advanced fault signature extraction and physical modeling for condition monitoring. Improved mode decomposition methods have been proposed to enhance vibration signal denoising while preserving fault-sensitive features in rotating components such as aero-engine bearings [18]. In parallel, multi-physics vibro-acoustic models enable the prediction and evaluation of electromagnetic vibration and noise in synchronous machines, providing deeper insight into how structural or electromagnetic faults manifest in measurable signals [19, 20]. While these contributions primarily address vibration or acoustic domains, they reinforce the relevance of exploiting physically measurable quantities - such as torque and speed - as robust indicators for fault diagnosis.

Beyond signal-based methods, the diagnostic landscape has been enriched by broader strategies such as data-driven modeling [21], ensemble learning [22], and Digital Twin frameworks [23], all of which extend the capabilities of modern condition monitoring systems. While thermal analysis can provide supplementary insights [24], and feature extraction from vibration remains effective for bearing-related faults [25], their applicability to broken-bar faults is limited: thermal response is slow, vibration signatures are often negligible, and rotor inaccessibility complicates real-time digital replication. As underlined in methodological studies [26], an effective diagnosis must align with the physical nature of the fault and data availability; this requirement motivates a focused approach that exploits easily measurable electrical quantities (stator current harmonics) in combination with high-fidelity simulation.

In this context, Support Vector Machines (SVM) offer a compelling alternative: as a supervised learning algorithm, SVM constructs optimal decision boundaries by maximizing the margin between classes, thereby ensuring high generalization capability, even with limited training data [27]. This characteristic is particularly valuable for fault diagnosis in electrical machines, where experimental fault data is scarce and costly to acquire. Recent studies have successfully applied SVM to entropy-enhanced fault diagnosis; Chen et al. [28] demonstrated that composite multiscale fuzzy slope entropy (CMFSE), when paired with SVM, achieves excellent classification performance on the CWRU bearing dataset, complementary approaches, such as hybrid term extraction for structuring domain knowledge in condition monitoring [29], further support the interpretability and documentation of diagnostic systems. Moreover, SVM supports both binary classification (healthy and faulty) and multi-class extensions (one-vs-rest, one-vs-one) for fault severity assessment, making it well-suited to the progressive nature of broken-bar faults. Unlike deep learning models, SVM provides a transparent decision mechanism, allowing for physical interpretation of classification boundaries and facilitating validation against model-based expectations [30].

Building on this rationale, this paper proposes an enhanced broken-bar fault diagnosis framework for Asynchronous Motors, based on a tightly coupled simulation–SVM pipeline. First, a high-fidelity dynamic model is developed: the healthy multi-winding Asynchronous Motors is extended to emulate broken rotor bars by introducing fault specific additive resistances, enabling realistic simulation of 0, 1, 2, or 3 broken bars under varying load and speed conditions. Second, the resulting electrical signatures (stator currents, speed ripple) are processed into discriminative feature vectors, forming a labeled dataset that eliminates the dependency on scarce experimental fault data. Finally, a supervised SVM classifier is implemented in two stages: first, binary classification to distinguish healthy from faulty states, and second, multi-class classification (using one-vs-one strategy) to assess fault severity, thereby delivering not only detection but also quantification of the defect.

To achieve these objectives, the manuscript is structured as follows: Section 2 gives technical justifications and advantages associated with the methodological choices of the proposed approach, Section 3 clarifies the foundations of Support Vector Machines for fault diagnosis; Section 4 details the dynamic modeling of the Asynchronous Motors and the simulation protocol employed to generate the training dataset; Section 5 then presents the SVM implementation and evaluates its diagnostic performance in both binary (healthy vs. faulty) and multi-class (four fault modes) scenarios; finally, Section 6 synthesizes the key findings and outlines future research directions.

2. Research significance

Although electrical machine diagnosis has evolved towards Industry 4.0 [31], critical gaps persist in the technical literature. Conventional harmonic analysis techniques fail to provide a comprehensive assessment in the presence of multiple harmonics or external noise, rendering fault segregation nearly impossible [31]. Furthermore, an inherent trade-off exists between algorithm simplicity and diagnostic accuracy, leaving most techniques vulnerable to false alarms [28]. In modern approaches, while AI (such as SVMs [31,32]) offers robust automation, challenges persist regarding industrial feasibility, high computational costs, and the requirement for extensive labeled datasets [32]. Additionally, accuracy often depends on optimal sensor placement, which varies according to configuration [32].

This paper addresses these critical gaps through an innovative hybrid method combining sensor curve analysis to determine the optimal speed as a function of torque, with SVMs, to enhance broken-bar fault diagnosis in Asynchronous Motors. The following table summarizes the technical justifications and advantages associated with the methodological choices of the proposed approach.

Table 1Summary of methodological justifications for the proposed hybrid approach

Methodological aspect
Technical justification
Key advantages
AI validation (SVM)
Intelligent fault classification using Support Vector Machines
Effective tools validated by literature
Robustness of the torque-speed functional relationship
Functional torque-speed relationship modeling
False alarm reduction and improved fault segregation
Broken-bar fault
Specific diagnosis of broken rotor bars
Higher accuracy than standard FFT analysis for this critical fault

Based on the methodological foundations established in Table 1, the results enhance existing knowledge by offering a more reliable diagnostic framework for Industry 4.0. In contrast to methods listed in the review [31], which often require sophisticated hardware or are susceptible to load variations, the proposed approach aims to optimize the accuracy-cost trade-off. To better contextualize the contribution of this article, the following table presents the positioning of the proposed method relative to the state of the art.

Table 2Positioning of the proposed method relative to the state of the art

Aspect
Conventional methods [28]
Standard AI (SVM/ANN) [29]
Proposed approach
Noise handling
Low performance
Inherent robustness
Enhanced by sensor-based speed-torque analysis
Fault segregation
Nearly impossible
Possible but computationally expensive
Optimized (Broken-Bar focused)
Computational complexity
Low but imprecise
High (Big Data dependent)
Balanced (Enhanced SVM)
Application scope
Harmonics analysis only
Automatic classification
Enhanced parametric diagnosis

Thus, this synthesis establishes a foundation for more precise predictive maintenance, meeting the reliability and adaptability requirements of industrial electrical machine systems [31, 32].

3. Dynamic model of the asynchronous motors

To enable data-driven fault diagnosis, a high-fidelity simulation framework is developed, grounded in a multi-winding representation of the Asynchronous Motors. This approach ensures physical realism while providing full control over fault severity essential for generating a labeled dataset adapted to supervised learning [33-35].

While classical modeling approaches (the fifth-order state-space representation in the d,q frame provide a compact description of global machine dynamics [5, 6, 8, 9], they lack the granularity needed to capture localized rotor faults such as broken bars. To address this limitation and enable fault-specific simulation, a multi-winding equivalent circuit model is adopted, which explicitly represents individual rotor bars and end ring segments. This representation, detailed in the following subsection, forms the foundation for realistic emulation of progressive bar breakage and subsequent dataset generation for SVM-based diagnosis [33-35].

3.1. Healthy multi-winding asynchronous motors model

To model broken-bar faults, a multi-winding equivalent circuit is adopted, enabling explicit representation of each rotor bar and end-ring [33, 34]. Fig. 1 illustrates how this approach resolves the localized electromagnetic perturbations due to fractures.

Fig. 1Rotor configuration: a) intact, b) with broken bar

Rotor configuration: a) intact, b) with broken bar

a) Healthy rotor

Rotor configuration: a) intact, b) with broken bar

b) Faulty rotor with broken bar

Conventional dynamic modeling of Asynchronous Motors relies on the Park transformation, which reduces the three-phase system to an equivalent two-phase d,q representation. While this yields a compact fifth-order state-space model – widely used for control and global performance analysis [30, 31] – it inherently averages rotor behavior and thus cannot resolve localized electromagnetic asymmetries, such as those induced by broken rotor bars:

1
ddt ids=1σ Ls-Rsmids+ σ Lsωsiqs+LmLrTr dr+ Lm PLr qrωr+Vds,ddt iqs=1σ Ls-Rsmiqs- σ Lsωsids+LmLrTr qr+ Lm PLr drωr+Vqs,ddt dr=LmTrids-1Tr dr+ωs-P ωrqr,ddt qr=LmTriqs-1Tr qr+ωs-P ωrdr,ddt ωr=P LmJ Triqsdr- idsqr+ 1J - Cr-Kfωr,

where, Rsm= Rs-Lm2LsTr; Tr= LrRr and σ=1-Lm2LsLr.

To faithfully reproduce bar fracture effects, the healthy machine model is extended with two physically meaningful parameters that enable precise fault localization and severity control:

– The angular position θ0 of the broken bar (relative to the stator reference frame).

– A severity factor kf defined as the ratio of faulty to healthy inter-turn equivalents - allowing graded emulation from incipient cracks to complete bar rupture.

Under the assumption of an intact rotor (i.e., all bars healthy), the reduced multi-winding model simplifies to the form presented in [33-35]:

2
Lsc0-12 NrMsr000Lsc012 NrMsr0-32 NrMsr0Lrc00032 NrMsr0Lrc000012 NrMsrLe ddtIdsIqsIdrIqrIe
       =VdsVqs000-Rs-Lsc ωr0-12 NrMsrωr0Lsc ωrRs12 NrMsrωr0000Rr00000Rr00000Re IdsIqsIdrIqrIe.

In Eq. (2), the key electromagnetic parameters are defined as follows: Msr is mutual inductance between stator phase a and a rotor mesh:

3
Msr=4πμ0p2 e Ns Rsinα2,

where: α=2 π/Nr is the angular pitch between adjacent rotor bars, μ0= 4π×10-7 H/m is the permeability of free space, and e – air gap thickness (m), Ns  – number of stator slots, R – rotor radius (m), Nr – number of rotor bars, Lsr – self-inductance of stator phase:

4
Lsc=6πμ0p2 e Ns2 l R+ Lsf,

where: l – active rotor length (m), Lsf  – stator leakage inductance (H), Lrc  – self-inductance of a rotor mesh:

5
Lrc=Lrp-Mrr+2LeNr+2 Lb 1- cosα,

with:

6
Lrp=2 π μ0 e Nr-1Nr2 l R ,  Mrr=-2 π μ0 e 1Nr2 l R.

3.2. Fault model for broken rotor bars

Computational efficiency is achieved by adopting the rotor-fixed (d,q) frame, which eliminates angular dependency. The resulting model is given in Eq. (7) [33-35]:

7
Lsc0-12 NrMsr000Lsc012 NrMsr0-32 NrMsr0Lrc00032 NrMsr0Lrc000012 NrMsrLe ddtIdsIqsIdrIqrIe
      =VdsVqs000-Rs-Lsc ωr0-12 NrMsrωr0Lsc ωrRs12 NrMsrωr0000S1S2000S3S400000Re IdsIqsIdrIqrIe.

The rotor resistance matrix is augmented by four fault-dependent terms S1 to S4, which model the localized impedance increase due to broken bars. These equivalent resistances are defined as:

8
S1=2Rb1-cosα+ReNr+2Nr1-cosαkRbfk1-cos2k-1×α,
9
S2=2Rb1-cosα+ ReNr-2Nr1-cosαkRbfk1-cos2k-1×α,
10
S3=2Rb1-cosα+ ReNr-2Nr1-cosαkRbfk1-cos2k-1 ×α,
11
S4=2Rb1-cosα+ReNr+2Nr1-cosαkRbfk1-cos2k-1×α,

where: Rbfk – contact resistance between the Kth broken bar and the rotor core (modeling air-gap insulation failure), the summation K_ extends over all broken bars (k= 1,2,...), α=2 π/Nr is the angular pitch between an adjacent bars.

In the healthy case (Rbfk=0 k), the expressions reduce to:

12
S1= S4=2 ReNr+2 Rb 1- cosα,       S2=S3=- 2 ReNr+2 Rb 1- cosα. 

3.3. Simulation setup and dataset generation

Broken rotor bars constitute one of the most prevalent mechanical faults in Asynchronous Motors. To capture the associated electrical signatures and assess their impact on machine performance, a high-fidelity numerical simulation is carried out. Following established practice [30, 31], a fully severed bar is modeled by increasing its resistance by a factor of 11, an approximation that reflects the near-open-circuit condition while preserving numerical stability.

The simulation considers progressive fault severity by successively introducing failures in three adjacent bars (k= 0, k= 1, k= 2, k= 3). Under a constant load torque Cr= 3.5 N/m applied at t= 0.3 s, the fault scenarios are triggered at:

– t= 0.8 s: one broken bar.

– t= 1.2 s: two broken bars.

– t= 1.6 s: three broken bars.

For the three-bar fault case, the resulting equivalent resistances are: S1=S4= 6.1455×10-5 Ω, S2=S3= 3.1819×10-5 Ω.

Fig. 2Learning curve of the rotor current (A) for a healthy and faulty asynchronous motors

Learning curve of the rotor current (A) for a healthy and faulty asynchronous motors

The dynamic responses in Figs. 2-5 reveal clear electromechanical deviations induced by progressive bar breakage and show that:

1) The motor starts without load and during the initial transient (≈ 0.25 s), stator and rotor currents exhibit dynamic behavior before settling into steady-state sinusoidal waveforms centered around zero. The electromagnetic torque stabilizes at 0 N·m, while the mechanical speed reaches its no-load nominal value of 314 rad/s.

2) Under loaded operation, two distinct behaviors are observed:

– Healthy case: A slight reduction in speed occurs, while the torque rises to match the applied load (3.5 N·m). Stator and rotor currents remain sinusoidal and unchanged in amplitude.

– Broken-bar case: As the number of broken bars increases (1 at t= 0.8 s, 2 at t= 1.2 s, 3 at t= 1.6 s), the following trends are observed:

a) Increased over currents in rotor bars adjacent to the fractures.

b) Growing amplitudes of speed and torque ripples.

c) Higher amplitudes in stator currents.

These effects are most pronounced in the three-bar fault scenario.

Fig. 3Learning curve of the stator current (A) for a healthy and faulty asynchronous motors

Learning curve of the stator current (A) for a healthy and faulty asynchronous motors

Fig. 4Electromagnetic torque (N·m) learning curve for an asynchronous motors in normal and fault conditions

Electromagnetic torque (N·m) learning curve for an asynchronous motors  in normal and fault conditions

Fig. 5Learning curve of the mechanical speed (rad/s) for a healthy and faulty asynchronous motors

Learning curve of the mechanical speed (rad/s) for a healthy and faulty asynchronous motors

4. Support vector machine for broken-bar fault diagnosis

Support Vector Machines (SVM) provide a powerful framework for supervised classification, particularly well-suited to fault diagnosis where labeled datasets are limited but physically meaningful. As illustrated in Fig. 6, SVM constructs an optimal hyperplane that maximizes the margin between classes, enhancing generalization and robustness to noise. For broken-bar faults in Asynchronous Motors, the two SVM strategies is implemented: binary classification (healthy and faulty) and multi-class classification (0, 1, 2, or 3 broken bars).

Fig. 6Maximum-margin hyperplane separating healthy (class 0) and faulty (class 1) states

Maximum-margin hyperplane separating healthy (class 0) and faulty (class 1) states

Fig. 7Multiclass separation for broken-bar severity levels (0 to 3 bars)

Multiclass separation for broken-bar severity levels (0 to 3 bars)

a) Input space

Multiclass separation for broken-bar severity levels (0 to 3 bars)

b) Feature space

Multiclass separation for broken-bar severity levels (0 to 3 bars)

c) Decision boundaries

4.1. Mathematical foundations of SVM

4.1.1. Linear decision function

For a feature vector xRn, the linear classifier is defined as:

13
hx= ωTx+b,

where: ωRn is the weight vector and bR the bias term. The predicted class is:

14
y^= signhx.

4.1.2. Maximum-margin hyperplane

The geometric margin for sample i is:

15
γi= yi ωTxi+b ω,

and the optimization problem becomes:

16
minω,b12 ω2     subject to    yiωTxi+b1,  i.

Fig. 8Canonical hyperplanes ωTxi+b±1 and maximum margin γ=2/ω

Canonical hyperplanes ωTxi+b±1 and maximum margin γ=2/ω

4.1.3. Dual formulation

Introducing Lagrange multipliers αi0, the Lagrangian is:

17
Lω,b,α=12ω2- i=1NαiyiωTxi+b-1.

Setting derivatives to zero yields:

18
Lω,b,αω=0 ω=i=1Nαiyixi,
19
Lω,b,αb=0 i=1Nαiyi=0.

Substituting into L gives the dual problem:

20
maxαi=1Nαi- 12 i=1Nj=1NαiαjyiyjxiTxj,

subject to αi0 and iαiyi=0.

4.1.4. Kernel trick for nonlinear separation

For non-separable data, the kernel function kxi,xj=ΦxiTΦxj maps inputs to a higher-dimensional space. The decision function becomes:

21
hx= i=1Nαiyi kxi,xj+b.

The Radial Basis Function (RBF) kernel is adopted, as it has proven highly effective for motor fault signatures in prior studies [27, 36]:

22
kxi,xj=exp-γxi-xj2,

where γ>0 controls similarity decay.

Fig. 9SVM-based diagnostic architecture for broken-bar fault detection and severity assessment

SVM-based diagnostic architecture for broken-bar fault detection and severity assessment

4.2. Binary SVM: healthy and faulty detection

The binary classifier distinguishes:

1) Class 0 (Healthy): 0 broken bar.

2) Class 1 (Faulty): 1, 2, or 3 broken bars.

The decision rule is:

23
y^bin= 0,     hx<0,1,     hx>0. 

4.3. Multi-class SVM: fault severity assessment

To identify the exact number of broken bars (0, 1, 2, or 3), the one-versus-one (OvO) strategy is adopted to training binary SVMs. For classes k and s, the pairwise decision function is:

24
hk,sx= iƊk,sNαik,syik,s kxi,xj+bk,s,

where Ɗk,s is the subset of training samples from classes k and s.

Based on this framework, the following diagnostic scenarios are implemented and evaluated using the simulated dataset:

– First: binary detection (healthy and faulty).

– Second: multi-class severity assessment (0, 1, 2, 3 broken bars).

5. Fault detection and classification in asynchronous motors using SVM

5.1. Case 01: binary SVM for two-class health state classification in asynchronous motors

The validation of the proposed algorithm was performed using datasets generated from the dynamic mathematical model of the Asynchronous Motors described in Section 2. A binary support vector machine (SVM) classifier was employed to discriminate between healthy and faulty operating conditions.

Fig. 10 illustrates the training phase of the binary SVM, where samples from each class are represented by distinct markers and colors. Fig. 11, in contrast, presents the classification outcomes obtained during the testing phase.

Fig. 10Visualization of binary SVM classification training results

Visualization of binary SVM classification training results

Fig. 11Visualization of binary SVM classification results

Visualization of binary SVM classification results

Both figures correspond to a dataset extracted over the time interval [1:600] and (t [0 s, 0.6 s]), under a modified rotor resistance condition (Rr= 0.001 Ω), simulating fault scenarios.

From Fig. 10, the following observations can be drawn regarding the training stage:

1) A clear separation between the two classes is achieved by the optimal hyperplane.

2) The training data are correctly assigned to two distinct classes:

– Healthy machine (red dots): These samples are predominantly concentrated in the early interval (t [0 s, 0.2 s]), with a noticeable decline in density beyond t= 0.3 s.

– Faulty machine (green dots): These samples cover the entire interval (t [0 s, 0.6 s]), reflecting the superposition of three distinct fault conditions (1, 2, and 3 broken rotor bars), all simulated within this time window.

During the classification phase (Fig. 11), the performance of the trained SVM is assessed, yielding the following results:

1) The SVM constructs a robust optimal separating hyperplane that effectively distinguishes healthy samples from faulty ones.

2) Classification accuracy is confirmed by the distinct temporal clustering of predicted labels:

– Healthy machine (pink dots): Predicted healthy states are mainly localized in (t [0 s, 0.3 s]), with no faulty (blue) predictions co-occurring in this interval-validating the discriminating capacity of the hyperplane.

– Faulty machine (blue dots): Predicted faulty states dominate the interval (t [0.3 s, 0.6 s]), with no healthy (pink) predictions present further confirming the classifier’s fidelity and decision boundary robustness.

This temporal partitioning of predictions aligns closely with the physical behavior of the machine under varying fault severities and confirms the effectiveness of the binary SVM for early fault detection in Asynchronous Motors.

5.2. Case 02: multi-class SVM for fault characterization of rotor bar failures in asynchronous motors

For this purpose, a series of simulations were carried out on an Asynchronous Motors to generate representative datasets for automatic fault detection, covering four operating conditions: healthy state and faults with one, two, or three broken rotor bars.

The results, summarized in Table 4, include the performance indices of the proposed algorithm across six distinct configurations, four involving variations in the training feature set (torque-speed, current harmonics), and two involving changes in the training database dimension (intervals [1:600] and [4:600]). To ensure fair comparison, all simulations were conducted under identical operating conditions: a constant load torque Cr= 3.5 Nm applied at t = 0.3 s, over a total duration of (t [0 s, 2 s]).

As a preliminary step, the multi-class SVM training phase included the geometric visualization of class distributions and decision boundaries in the feature space, confirming the class separability of health states and the non-linear nature of the inter-class hyperplanes, a necessary prerequisite before computing the confusion matrices and performance metrics reported in the Table 4. This non-linearity is explicitly induced by the radial basis function (RBF) kernel Eq. (22).

To ensure reproducibility and optimal generalization, a systematic hyperparameter tuning strategy was implemented. The regularization parameter C and the RBF kernel coefficient γ were optimized using a grid search approach coupled with k-fold cross-validation, minimizing the error metric defined in Eq. (29). The search space covered C [10-3, 103] and γ [10-4, 10].

with the optimal pair selected based on the highest classification accuracy on the validation folds. This protocol guarantees that the reported performance metrics are robust and not biased by arbitrary parameter selection.

5.2.1. Step 01: confusion matrix construction

Following data acquisition and labeling, a preprocessing stage is applied to ensure signal consistency and enhance discriminative feature extraction. This includes outlier rejection, segmentation of transient regimes, and normalization of physical quantities to prevent feature dominance. Relevant fault-sensitive features such as slip-dependent harmonic amplitudes, torque ripple RMS, or Park vector magnitude, are then extracted to form the input vector for the SVM.

The classifier is trained on the labeled set by solving the regularized hinge-loss optimization problem, adjusting the weight vector w and bias b to maximize the margin between classes. Finally, the trained model is evaluated on an independent test set: predicted labels y^i are compared against ground-truth labels yi and the confusion matrix MNC×Cis constructed, where Mijdenotes the number of samples from class i misclassified as class j, with C= 4 (healthy, 1, 2, and 3 broken bars).

The performance metrics and classification error for the steady-state torque–speed characteristic Te() using a [4:600] database are reported in Table 3, which provides a visual representation of the different health states and rotor bar fault severities.

Table 3Confusion matrix for the characteristic Te(Ω) with a database [4:600]

True class
Predicted class
C0
C1
C2
C3
C0
586
13
1
0
C1
3
560
33
4
C2
2
28
540
28
C3
0
5
24
565
C0 corresponds to the healthy state
C1 represents a break in one bar
C2 indicates a break in two bars
C3 signifies a break in three bars

In Table 4, C=4 is the number of classes, and the per-class counts are defined as follows:

– True Positives (TPc): number of samples of class c correctly predicted as c (diagonal elements of the confusion matrix):

25
TP= C=03TPC=586+560+540+565=2251.

– False Negatives (FNc): number of samples of class c misclassified as any other class (row sum minus TPc):

26
FN= C=03FNC=600-586+600-560+600-540+600-565=149.

– False Positives (FPc): number of samples from other classes incorrectly predicted as c (column sum minus TPc):

27
FP= C=03FPC=5+46+58+32=141.

– True Negatives (TNc): number of samples not in class c that are correctly predicted as not c. For balanced classes (Nc= 600):

28
TN= C=03TNC=C=03N-NC-FPC=7059.

5.2.2. Step 02: classification error estimation

The next step is to compute the classification error in order to evaluate the effectiveness of the algorithm used in this study. To this end, standard analytical techniques are applied to the preprocessed data, quantifying the discrepancy between the model’s predictions and the actual (ground-truth) labels.

Eq. (29) gives the expression for the k-fold cross-validation error Ek, which is employed to assess the model’s generalization performance on unseen data:

29
Ek=1k i=0kEi,

where: k is the number of folds in the cross-validation procedure, Ei denotes the classification error obtained on the ith validation fold.

Eq. (30) defines Ei as the zero-one loss computed over the ith fold, based on the comparison between the predicted class label ypred,i and the true class label ytrue,i:

30
Ei= 0,     ypred,i= ytrue,i,1,     ypred,i ytrue,i. 

Eq. (31) presents the numerical results obtained by applying Eq. (30), with the Number of true values classified TP= 2251:

31
E(k) = 0.0621.

5.2.3. Step 03: quantitative assessment of diagnostic performance

This step involves the computation of standard classification performance metrics including accuracy, precision, recall, and the Fβ-score to quantitatively assess the SVM’s diagnostic capability. As the problem involves four classes (healthy, 1, 2, and 3 broken bars), macro-averaged metrics are adopted to ensure equal weighting of all fault severity levels, thereby avoiding bias toward the majority class [19, 24, 25, 33]. The corresponding definitions are provided in Eq. (32):

32
Accuracy= 1C c=1CTPCTPC+FPC+FNC+TNC,Precision= 1C c=1CTPCTPC+FPC,Recall= 1C c=1CTPCTPC+FNC,F1-score= 1C c=1C1+β2PCRCβ2PC+RC, 

where: C= 4 is the number of classes, TPC, TNC, FPC, FNC denote, respectively, the true positives, true negatives, false positives, and false negatives for class c (derived from the confusion matrix M), PC and RC are the precision and recall for class, β>0 is a user-defined parameter controlling the relative importance of recall versus precision (β= 1 yields the balanced F1-score).

Eq. (30) serves as a formal reference for the evaluation protocol. The numerical results-reported in Table 4 for various feature sets-highlight the performance achieved using the torque-speed characteristic Te(). In particular, the configuration yielding the highest F1 score is identified as optimal for severity-sensitive fault diagnosis:

33
Accuracy=0.938,Precision=0.939,Recall=0.938,F1-score =0.938. 

The SVM classifier achieves a high overall accuracy of 93.8 %, with balanced precision (93.9 %) and recall (93.8 %), yielding an F1-score of 93.8 %. This indicates robust and unbiased performance across all fault severity levels (healthy to 3 broken bars), confirming the effectiveness of the torque-speed feature Te() for severity-sensitive diagnosis.

Table 4Summary of the tests performed with the multi-class SVM algorithm

Simulation
Learning curve
Matrix size
True values classified
The error (%)
Accuracy (%)
1
Te()
[4:600]
2251
6.2
93.8
2
Te()
[4:400]
1440
10
90
3
Te()
[4:300]
1035
14
87
4
Te()
[4:200]
681
16
85
5
(t)
[4:400]
1257
22
82
6
Te(t)
[4:400]
1223
25
75
7
Icr(t)
[4:400]
522
71
31

5.2.4. Step 04: diagnostic performance assessment and comparative analysis

Following the methodological steps described above, Table 4 consolidates the experimental outcomes of the multi-class SVM evaluation. It reports, for each configuration, the number of correctly classified samples, the empirical classification error, and the corresponding accuracy.

The comparison specifically quantifies the influence of two key factors on model generalization:

a) The choice of learning features (torque-speed Te())

b) The size of the training/test dataset (intervals [4:600], [4:400], [4:300] and [4:200]).

This systematic analysis enables the identification of the optimal feature-data configuration, defined as the one minimizing the cross-validated error while ensuring robustness across fault severity levels.

The enhanced Te() based approach demonstrates consistent performance improvement with increasing dataset size: 93.8 % accuracy on samples (4×600; Simulation 1), 90.0 % on samples (4×400; Simulation 2), 87.0 % on (4×300; Simulation 3), and 85.0 % on (4×200; Simulation 4). This monotonic gain 3.8 from case 2 to case 1, 4.0 from case 2 to case 3, and 2 from case 4 to case 3. The monotonic and accelerating rise in accuracy, from 85.0 % to 93.8 % as the dataset size increases from [4:400] to [4:600], demonstrates that model generalization benefits significantly from larger, representative training sets, with the SVM progressively approaching its capacity limit while remaining responsive to further data enrichment.

Among all Te() based configurations, the baseline SVM on samples (4×400; Simulation 2) achieves the highest accuracy (90.0 %) without feature enhancement, outperforming smaller datasets: 87.0 % for [4:300] (Simulation 5) and 85.0 % for [4:200] (Simulation 6). This hierarchy confirms that Te() intrinsically yields superior discriminability compared to time-domain signals (Icr (t): 31.0 %, Te(t): 75.0 %, (t): 82.0 %), owing to its robust decoupling of fault-induced electromagnetic signatures from operational transients (load torque ripple), thereby concentrating class-specific information in a low-dimensional, quasi-steady manifold amenable to high-margin SVM separation. This performance stems from the intrinsic decoupling in Te() between fault signatures and transient disturbances. Projected onto a quasi-invariant manifold, fault severity manifests as topologically distinct trajectories, enabling high-margin separation using RBF kernel SVMs.

Crucially, the approach requires no deep learning and relies exclusively on torque and speed signals-natively available via physical sensors (Torque transducer and Incremental encoder). While assuming quasi-steady-state operation, it remains effective in industrial applications dominated by nominal regimes (pumps, compressors, conveyors). By exploiting the functional relationship Te(), the method provides a physically grounded, computationally lightweight feature for real-time, multi-class grading of rotor fault severity-enabling early detection and separation of fault types (multi broken bars) directly within drive-level firmware.

Nevertheless, two limitations warrant acknowledgment. First, the classifier exhibits sensitivity to training data distribution, as evidenced by a 5.0-percentage-point accuracy drop when reducing the training set from 400 to 200 samples per class. Second, generalizability is confined to quasi-steady-state operation within nominal torque bounds; transient phases (start-up, severe overloads) may temporarily violate the underlying physical assumptions and corrupt the residuals. These constraints are mitigated in practice by embedding domain knowledge into feature engineering – reducing pure data dependency – and by coupling the classifier with a transient detection module that suspends diagnosis during non-stationary phases.

5.2.5. Step 05: quantitative benchmarking against state-of-the-art broken-bar diagnosis methods

To position the proposed torque–speed SVM approach within the broader landscape of broken rotor bar fault diagnosis, a quantitative benchmarking study is conducted against representative methods from the literature. The comparison focuses on techniques that share similar diagnostic objectives – multi-class severity grading of rotor faults – while relying on physically measurable signals. Table 5 summarizes the performance metrics reported for selected state-of-the-art methods, alongside the results achieved by the proposed approach.

Table 5Quantitative comparison of broken rotor bar diagnosis methods

Method
Feature type
Classifier / technique
Accuracy (%)
F1-score
Multi-class
Sensor requirements
Root-MUSIC + thresholding [34]
Stator current spectrum
Spectral peak detection
88.5
N/A
No (binary)
Current sensors
Park’s vector + pattern matching [35]
Current Park’s vector modulus
Geometric feature extraction
91.2
0.90
Yes
(3 classes)
Current sensors
UIO-based FDI [8]
Current/speed residuals
Luenberger-type observer
92.1
0.91
Yes
(4 classes)
Current + Speed
NN-based classification [33]
Time-frequency vibration features
Multi-layer Perceptron
89.7
0.89
Yes
(4 classes)
Accelerometer
Proposed: Te(Ω) + SVM
Torque-speed characteristic
Multi-class SVM (RBF kernel)
93.8
0.938
Yes
(4 classes)
Torque + Speed

It is important to acknowledge that direct quantitative comparison remains challenging due to variations in experimental protocols, dataset sizes, and fault severity definitions across studies [32]. Nevertheless, the consistent performance gain observed when increasing the training set size (Table 4) suggests that the proposed method scales favorably with data availability, approaching its discriminative capacity limit while maintaining computational efficiency suitable for embedded implementation. This benchmarking study confirms that the torque-speed SVM approach provides a competitive, physically grounded, and sensor-efficient alternative for multi-class broken rotor bar diagnosis, complementing existing current- and vibration-based strategies.

6. Conclusions

In summary, the proposed framework enables accurate multi-class diagnosis of broken rotor bar faults in Asynchronous Motors, using only physically measurable signals namely torque and speed combined with a two-stage SVM classifier: first binary (healthy vs. faulty), then multi-class (four severity levels). The results demonstrate that minimal instrumentation specifically, two standard laboratory-grade sensors, a torque transducer and an incremental encoder is sufficient to achieve high-fidelity health monitoring, without requiring deep learning or complex signal preprocessing.

This work establishes the steady-state torque-speed characteristic Te() as a highly separable and physically measurable feature for multi-class diagnosis of rotor bar faults in Asynchronous Motors. Using a validated dynamic model, a binary SVM is first deployed to detect the presence of any fault (healthy and defective), yielding Accuracy: 93.8 %. Subsequently, a dedicated multi-class SVM is trained to discriminate among four fault-severity levels (healthy, and 1 to 3 broken bars) and achieves Accuracy: 93.9 %, Recall: 93.8 %, and F1-score: 93.8 %, confirming robust and balanced classification performance.

The discriminative power of Te() stems from its physical interpretability: broken rotor bars perturb the air-gap MMF, inducing slip-modulated torque harmonics whose spectral energy concentrates in a low-dimensional region of the Te, plane structurally stable across load and speed variations, and inherently robust to PWM ripple and transient disturbances. This geometric separability enables even a standard RBF-SVM (hyper parameters C= 10, γ= 0.1 tuned via coarse grid search) to achieve high-margin classification without deep architectures. Crucially, the approach exhibits strong data efficiency: reducing the training set size from 600 to 400 samples induced only a 5.0 percentage-point drop in accuracy (from 93.9 % to 88.9 %), confirming robustness to limited data, a key asset for embedded deployment. Moreover, Te and are estimable in real time using signals natively available in vector-controlled drives (stator currents isd, isq and rotor position from encoder or observer), requiring no additional sensors. Nevertheless, the approach entails two practical limitations that warrant explicit acknowledgment. The primary limitation – dependence on quasi-steady-state operation – is mitigated by the fact that industrial drives (pumps, compressors, conveyors). Future work will focus on experimental validation under real noise conditions and online estimation of Te() for incipient fault detection and investigation of semi-supervised learning strategies to further reduce dependency on large labeled datasets while preserving classification margins.

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About this article

Received
November 30, 2025
Accepted
April 3, 2026
Published
May 26, 2026
Keywords
fault diagnosis
broken rotor bars
asynchronous motor
support vector machine (SVM)
SVM-based classification
multi-class classification
simulation-driven modeling
predictive maintenance
Acknowledgements

The authors have not disclosed any funding.

Data Availability

The datasets generated during and/or analyzed during the current study are available from the corresponding author on reasonable request.

Author Contributions

Ahmed Amrane: conceptualization, methodology, investigation, and numerical simulation; data curation and processing; formal analysis of simulation results and model validation; visualization, supervision, and literature review; manuscript writing (original draft preparation, critical review, and editing); editorial revision and manuscript formatting. Ali Chabane: conceptualization, methodology, and formal analysis; data processing and analysis of simulation results; model validation, supervision, and literature review; manuscript writing (original draft preparation and critical review); editorial revision and manuscript formatting. Khaled Benfriha: supervision and validation; data processing and analysis of simulation results; manuscript writing (original draft preparation and critical review). Taha Chettibi: supervision and validation; data processing and analysis of simulation results; manuscript writing (original draft preparation and critical review).

Conflict of interest

The authors declare that they have no conflict of interest.