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. 2025 Apr 22;15:13832. doi: 10.1038/s41598-025-98685-7

Critical sliding surface location method for anisotropic slope based on anisotropic yield criterion and optimization algorithm

Zhenfu Zhang 1, Yongjun Zhang 1, Sijia Liu 1,, Mingzhong Gao 2, Fei Liu 1, Jintao Wang 3
PMCID: PMC12015443  PMID: 40263384

Abstract

In slope stability analysis, identifying the critical slip surface has always been a complex challenge. This study proposes a method to determine the critical slip surface of heterogeneous slopes while accounting for anisotropy. This method is grounded in a generalized soil anisotropic constitutive model and establishes a global equilibrium framework. It integrates global optimization techniques and employs the well-established Morgenstern-Price method to formulate the optimization objective function. The reliability, applicability, and stability of the method are demonstrated through comparative analysis with the results of two classical slope cases and the improved log-spiral limit equilibrium method. Additionally, the study investigates the impact of anisotropy-related parameters on the stability of heterogeneous slopes, providing new insights into how anisotropy influences slope stability and failure mechanisms.

Keywords: Slope stability, Anisotropy, Safety factor, Critical slip surface

Subject terms: Engineering, Civil engineering

Introduction

Stability analysis of both natural and artificial slopes is a prominent issue in civil, geotechnical, and mining engineering. However, the presence of multi-scale discontinuities such as bedding planes, joints, fissures, and faults in natural rock masses introduces significant directional dependence in their mechanical properties1,2. This anisotropy poses new challenges for slope stability analysis. Therefore, understanding how to search for anisotropic slip surfaces and accurately quantify the safety factor is essential for better grasping slope failure mechanisms3,4.

Anisotropy in geotechnical materials is widespread in slope engineering. Different from homogeneous slopes, the stability of anisotropic slopes is influenced by the direction and degree of anisotropy in the strata. Current research methods addressing this issue include field monitoring57, kinematic analysis8, limit equilibrium methods9,10, limit analysis, and numerical computations11. In recent decades, researchers such as Kumar6 and Tan5 have conducted extensive field studies on the failure mechanisms of anisotropic slopes. These monitoring results have enhanced our understanding of anisotropy in practical engineering contexts. However, in-situ monitoring facilities may be limited in their ability to capture the entire failure evolution process of anisotropic slopes.

Consequently, numerical methods based on the finite element method, finite difference method, and material point method have been developed. Within these methods, the calculation strategies for anisotropic slope stability analysis can be categorized into three types: (I) constitutive models for anisotropy, (II) spatial variability of strata, and (III) pre-existing layered joints. These approaches address anisotropy at different scales. In the first category, researchers such as He et al.12, Badakhshan et al.13, and Nagendran et al.14 have applied various constitutive models to study anisotropic slope stability, advancing and refining stability analysis. In contrast, Griffiths and Fenton15 and Wang et al.16 adopted probabilistic finite element methods in investigating the failure characteristics and probabilities of transversely anisotropic slopes. Chen17 employed stochastic finite difference methods in probabilistic assessments to quantitatively evaluate the impact of general anisotropic spatial variability on slope reliability. Additionally, with advancements in numerical algorithms, techniques such as contact algorithms, discontinuous methods, and advanced meshing have been proposed to address the distribution of layered joints within rock slopes. Utilizing these algorithms, Tan et al.5 and Zang et al.18 have investigated the stability evolution of slopes with different joint distributions.

When dealing with non-circular failure surfaces, the number of control variables exceeds three, rendering the geometric grid method impractical. Due to its accuracy and straightforward application, the limit equilibrium method (LEM) has become a widely used technique in slope stability analysis. This method generally involves two main tasks: calculating the safety factor and identifying the critical slip surface. For simple slope structures, the slip surface is often assumed to be circular, with calculations performed using the Fellenius method19 or the simplified Bishop method20. The LEM is frequently combined with global optimization algorithms to identify the critical slip surface21. With advancements in computer hardware and optimization algorithms, research on the limit equilibrium method has progressed rapidly. Identifying the critical slip surface involves complex multi-constraint, multi-parameter optimization problems. Researchers have employed evolutionary algorithms22, quasi-physical intelligent algorithms23, population-based optimization algorithms24, and hybrid intelligent algorithms25 to find optimal objective function values, effectively addressing this complex issue. In studies on slope stability calculations using optimization algorithms, factors such as seismic activity26, seepage27, and external loads28 have been considered.

Existing research on slope stability has mainly focused on the anisotropy and spatial variability of geotechnical materials. Chen17 used the limit analysis upper bound method to derive stability solutions for slopes composed of anisotropic, heterogeneous clay. Stockton3 refined the traditional logarithmic spiral limit equilibrium method, extending it to stability analysis of soils with anisotropic cohesion and friction, and studied the impact of shear strength anisotropy on the depth of tensile cracks in slope engineering. Considering soil heterogeneity, researchers such as Karni and Shamrani29 and Dong et al.30 have used the limit equilibrium slice method to study the impact of strength anisotropy on slope stability. A finite element limit analysis method has enabled a more precise evaluation of the ultimate bearing capacity31. Building on this approach, Lai32 integrated an anisotropic undrained failure criterion to examine the undrained stability of tunnel portals with rigid walls in anisotropic clays. In parallel, Izadi33,34 and Pishvari et al.35 assessed the bearing capacity of foundations under cross-anisotropic and complex loading conditions using the second-order cone programming method. Additionally, numerous scholars have applied the random field theory proposed by Vanmarcke36 to slope stability analysis. Gravanis et al.37 integrated random field theory with the LEM to account for spatial variability in the parameters of soil strength. Huang et al.38, Liu et al.39, and Li et al.40 used the autocorrelation function combined with the Cholesky decomposition method to simulate random fields to investigate the impact of rotational anisotropy on slope failure mechanisms and stability. In slope stability analysis methods that combine global optimization techniques with limit equilibrium theory, the consideration of anisotropy remains insufficient. Therefore, it is necessary to establish a method for locating the critical slip surface that can be applied to heterogeneous and anisotropic geological environments.

In this study, we extend a generalized anisotropic constitutive model into the limit equilibrium framework, building upon previous research utilizing the limit equilibrium method. We first establish global equilibrium equations at the element scale that account for anisotropy. These equations are then extended to the soil strip scale and integrated with the objective function from the Morgenstern-Price method. By employing global optimization techniques, the position of the critical slip surface can be accurately located. Overall, the innovative features of our developed method can be summarized as follows,

  • Through comparisons with multiple case studies, our results demonstrate excellent applicability across geological conditions of varying complexity.

  • By integrating an improved constitutive model into a generalized slip surface search framework, the approach ensures scalability for diverse geotechnical scenarios.

  • The method resolves the longstanding limitation of conventional slip surface search techniques in addressing anisotropic strata, which achieving capture of the anisotropic strength characteristics.

The paper is structured as follows. Our new slope stability analysis method considering material anisotropy is derived and introduced in Section “Method for searching critical sliding surface”. In Section “Numerical validation”, we analyze three classical cases to demonstrate the numerical implementation process and conduct a robustness analysis of the proposed method. Section “Numerical results and discussions” presents numerical experimental results, systematically examining the effects of slope angle and anisotropy ratio on slope stability. Finally, we draw conclusions in Section “Conclusions”.

Method for searching critical sliding surface

This chapter introduces a method for analyzing slope stability that takes into account the anisotropy of geotechnical materials. Section “Global equilibrium equations for anisotropic slopes” presents the global equilibrium equations for analyzing anisotropic slopes. Section “Generation of trial sliding surfaces” covers the model for generating trial slip surfaces. Section “Mechanical analysis for safety factor” details the methods for calculating the safety factor. Finally, Section “Optimization algorithm for slop stability analysis” introduces the firefly optimization algorithm used in the search for slip surfaces.

Global equilibrium equations for anisotropic slopes

The LEM analyzes the slope stability by applying the mechanical equilibrium conditions of the sliding body. As depicted in (Fig. 1), we define the landslide body Inline graphic as the region bounded by both the slope surface Inline graphic and the sliding surface Inline graphic with a dip angle Inline graphic. Normally, the landslide body is primarily influenced by gravitational, seismic, and external forces along the slope. When the sliding body is in the critical state, the following conditions for both force equilibrium and the critical limit equilibrium should be satisfied.

graphic file with name d33e472.gif 1a
graphic file with name d33e478.gif 1b
graphic file with name d33e484.gif 1c

where Inline graphic and Inline graphic represent the direction vectors in the horizontal and vertical components of stress at a point on the sliding surface, respectively. The parameter Inline graphic represents the vertical distance between the slope surface and the sliding surface at a certain point; Inline graphic denotes the density, Inline graphic is the gravitational acceleration, Inline graphic and Inline graphic are the normal and tangential stress, respectively, can be expressed in the form as:

graphic file with name d33e534.gif 2a
graphic file with name d33e540.gif 2b

where Inline graphic, Inline graphic and Inline graphic are the stress components acting upon an infinitesimally small rock mass element, as shown in (Fig. 1).

Fig. 1.

Fig. 1

Schematic of the potential sliding surface search and stress analysis.

The evolution of the internal structure is deeply associated with the macroscopic mechanical behavior of granular materials. According to the hypothesis proposed by Booker and Davis41, the mean normal stress Inline graphic and the principal stress direction Inline graphic are available for the characterization of the anisotropic yield surfaces of granular materials. Building on this hypothesis and consistent with experimental evidence that the internal friction angle is relevant to the direction of principal stress, Yuan et al.42 considered the yield surface in the stress space of deviatoric stress as an ellipse (Fig. 2), the anisotropic yield criterion can be written as follows:

graphic file with name d33e602.gif 3a
graphic file with name d33e608.gif 3b

where Inline graphic can be defined as the yield function, and Inline graphic represents the distance from the stress point to the origin of the coordinate system. Inline graphic is defined as the Anisotropic Increase Factor (AIF), and it plays a crucial role in capturing the anisotropic characteristics of strength. Inline graphic is the thermodynamic force associated with mean normal stress Inline graphic. The parameters Inline graphic and Inline graphic are the cohesion and the internal friction angle, respectively, where, Inline graphic is the maximum peak internal friction angle and Inline graphic is the minimum peak internal friction angle.

Fig. 2.

Fig. 2

The yield criterion considering the anisotropy: (a) yield surface in the principal stress space of three dimension and (b) yield surface in stress space of deviatoric stress.

For the point on the sliding surface, the AIF varies with the principal stress direction due to the consideration of the elliptic geometry, and is defined by the following formula:

graphic file with name d33e686.gif 4

Here, Inline graphic is the angle of the bedding plane measured counterclockwise from horizontal. It corresponds to the direction angle of the Inline graphic and ranges from Inline graphic to Inline graphic; Inline graphic is defined as the anisotropy ratio, which is used to represent the ratio of Inline graphic to Inline graphic, and is used to represent the anisotropy ratio. The value of Inline graphic ranges between 0 and 1. A smaller value of Inline graphic indicates a greater degree of anisotropy which was expressed by Inline graphic, and when Inline graphic, it recovers the isotropic Mohr–Coulomb yield criterion.

As indicated in Fig. 2, the cross-section of the anisotropic yield criterion is assumed to take the form of a rotated ellipse. With Inline graphic as a center point, the rotation angle of the ellipse is associated with the bedding plane angle, and the length of the major and minor axes of the ellipse is determined by Inline graphic and Inline graphic.

graphic file with name d33e784.gif 5

Combining Eqs. (1) ~ (5), we can obtain that:

graphic file with name d33e795.gif 6

Equation (6) is the limiting equilibrium condition modified by the anisotropic yield criterion.

The factor of safety Inline graphic can be used as a crucial design criterion in slope stability analysis. With the aim of preventing potential failures, the slope stability analysis efforts are dedicated in determining the factor of safety Inline graphic. According to stability criterion, safety factor is given by:

graphic file with name d33e820.gif 7

where Inline graphic is the shear resistance acting on a point of the sliding surface, and Inline graphic is the components of the forces acting on a point of the sliding surface that cause instability, which can be expressed as:

graphic file with name d33e840.gif 8a
graphic file with name d33e846.gif 8b

In this study, the LEM is used to identify the critical sliding surface and calculate the value of Inline graphic corresponding to this critical sliding surface. Therefore, the problem of searching the sliding surface can be defined as an optimization problem.

graphic file with name d33e860.gif 9

Generation of trial sliding surfaces

In order to locate the position of the critical sliding surface, a method proposed by Cheng43 for the generation of non-circular trial sliding surface is adopted. Establish a Cartesian coordinate system with the origin at Inline graphic, as illustrated in (Fig. 3).

Fig. 3.

Fig. 3

Generation of a non-circular sliding surface.

The method of slices involves dividing the failed soil mass into Inline graphic vertical slices. Within the framework of Chen’s method, the generated critical slip surface is essentially formed by creating soil slices and combining the bases of these slices to form the slip surface. Therefore, the sliding surface will be described using multiple control points Inline graphic, Inline graphic, …, Inline graphic, i.e.

graphic file with name d33e916.gif 10

The width of all slices is set to a fixed value, and the x-coordinate of all control points can be easily determined according to the position of Inline graphic and Inline graphic, as

graphic file with name d33e936.gif 11

To ensure the geometric topological requirement of being concave upward, the dynamic bound proposed by Cheng43 is used to limit the position of each control point. Based on the known y-coordinates of Inline graphic and Inline graphic, the y-coordinates of points Inline graphic through Inline graphic are determined by the slope geometry and the alignment of the known points, sequentially.

For each point except the two endpoints, define the upper bounds as Inline graphic and the lower bounds as Inline graphic. A detailed procedure for determining the upper and lower bounds can be referenced in Cheng’s study43, and their values are defined according to the following formula:

graphic file with name d33e990.gif 12a
graphic file with name d33e996.gif 12b

where Inline graphic represent the bed rock surface.

Finally, to ensure the geometric topology of each sliding surface, Inline graphic is used to map the y-coordinate value, which means the imaginary variable corresponding to variable Inline graphic and Inline graphic. In this case, Inline graphic is determined by the following formula:

graphic file with name d33e1035.gif 13

Mechanical analysis for safety factor

The Morgenstern-Price method is suitable to calculate the factor of safety of sliding surfaces with arbitrary shapes. In this study, we calculate Inline graphic according to the assumption of the Morgenstern-Price method, as follows:

graphic file with name d33e1051.gif 14

where, Inline graphic represents the normal force of the interslice and Inline graphic is the interslice shear force; Inline graphic is the direction of action of the interslice force; Inline graphic is the scaling factor, which can be obtained from the moment equilibrium of slice Inline graphic; and Inline graphic is a continuous function of the inter-slice force, and Inline graphic. Inline graphic is the ratio between the vertical and lateral interslice forces. Figure 4 illustrates the mechanical model of the Morgenstern-Price method for calculating the slope safety factor. As shown in Fig. 4, the sliding body is discretized into a certain number of vertical slices, each slice has the same safety factor, and a certain soil slice was taken as an isolation for analysis as (Fig. 4).

Fig. 4.

Fig. 4

Diagram of Morgenstern-Price method for critical slip surface.

According to Zhu44, the half-sine function is adopted as the interslice function:

graphic file with name d33e1130.gif 15

in which Inline graphic and Inline graphic are the specified non-negative values, and Inline graphic, Inline graphic.

In the limit equilibrium analysis using Morgenstern-Price method, the stress pair Inline graphic of any point on the potential sliding surface is assumed to be lie on the Mohr–Coulomb failure envelope with the reduced strength parameters, as expressed:

graphic file with name d33e1170.gif 16a
graphic file with name d33e1176.gif 16b

where Inline graphic and Inline graphic are the reduced strength parameters.

In this study, to account for the effect of anisotropy in slope stability analysis, we use the anisotropic Mohr–Coulomb failure criterion proposed in Section “Global equilibrium equations for anisotropic slopes” as the limit equilibrium condition. In this framework, the relationship between Inline graphic and the principal stress direction Inline graphic is employed to capture the directional variation of the strength parameters. Based on the assumptions about the interslice forces and considering the force equilibrium of the slice Inline graphic, it can be obtained that:

graphic file with name d33e1218.gif 17a
graphic file with name d33e1224.gif 17b

For slice Inline graphic, Inline graphic is the normal force; Inline graphic is the mobilized shear strength; Inline graphic is the weight; Inline graphic is the width; Inline graphic is the dip angle; Inline graphic and Inline graphic,

According to Eq. (17 are the shear interslice forces acting on the left and right boundaries of the slice, respectively.), we can obtain:

graphic file with name d33e1283.gif 18

where Inline graphic is the sum of the shear resistances acting lie on the slide line; and Inline graphic is the sum of the forces that tending to cause instability. The resultant force Inline graphic and Inline graphic are expressed as:

graphic file with name d33e1315.gif 19a
graphic file with name d33e1321.gif 19b

By introducing the following variables

graphic file with name d33e1329.gif 20a
graphic file with name d33e1335.gif 20b

Equations (17) to (20) incorporate the anisotropic strength characteristics into the limit equilibrium analysis through the introduction of the AIF Inline graphic. Consequently, we obtain the simplified form of Eq. (18) as:

graphic file with name d33e1352.gif 21

Hence, the implicit expression of the factor of safety is derived as follows:

graphic file with name d33e1360.gif 22

In the calculation process of the Morgenstern-Price method, Inline graphic is computed iteratively. To this end, initial values for Inline graphic and Inline graphic need to be assumed. To ensure effective transmission of pressure, the initial values of Inline graphic and Inline graphic are restricted as:

graphic file with name d33e1399.gif 23a
graphic file with name d33e1405.gif 23b

According to the moment equilibrium of the side surface, Inline graphic can be obtained by the following equation:

graphic file with name d33e1420.gif 24

By iterating the above process, the difference between the values of Inline graphic and Inline graphic calculated in each iteration can be reduced to within the acceptable tolerance Inline graphic and Inline graphic. Figure 5 presents the flowchart for calculating Inline graphic considering the anisotropic yield criterion.

Fig. 5.

Fig. 5

Computational flowchart of Morgenstern-Price method.

Optimization algorithm for slop stability analysis

To enhance the efficiency and accuracy of searching for the critical sliding surface of slopes, researchers have explored various global optimization algorithms45. In the approach to analysis the slope stability considering anisotropy presented in this paper, the global optimization algorithm (Firefly Algorithm) in the artificial intelligence method is used for localization of critical sliding surfaces of slopes. In this study, the firefly algorithm is adopted based on the following two considerations46: (1) the algorithm’s ability to simultaneously search for both global and local optimal solutions; and (2) the characteristic of low interaction among subregions, which significantly improves computational efficiency. Two key aspects of the firefly algorithm (FA) are the calculation of light intensity and the formulation of attractiveness47. The brightness of each firefly is determined by its safety factor; the lower the safety factor, the higher the brightness, which in turn directs the individual to move toward other fireflies. A higher brightness value usually indicates a better solution, but this depends on the specific optimization problem and how the fitness function is defined. In this study, Inline graphic is used to represent the current position of fireflies Inline graphic. For a population size of Inline graphic fireflies, the brightness Inline graphic of the firefly Inline graphic can be defined as follows:

graphic file with name d33e1516.gif 25

where Inline graphic is the function for safety factor computation and the sliding surface function Inline graphic can be rewritten to the form in Eq. (26) according to the imaginary variable definition mentioned in Section “Generation of trial sliding surfaces”.

graphic file with name d33e1542.gif 26

In the framework of FA, the fireflies with lower brightness values will move towards the fireflies with higher brightness values according to the present movement criteria. We can define the function of the attractiveness as follows:

graphic file with name d33e1550.gif 27

where Inline graphic is Euclidean distance between any two fireflies and Inline graphic denotes the attractiveness for Inline graphic. Inline graphic is the light absorption coefficient, usually taken as a constant. In addition, regarding a problem in Inline graphic dimensions, the Euclidean distance between fireflies Inline graphic and Inline graphic can be defined as the following formula:

graphic file with name d33e1600.gif 28

in which Inline graphic represents the parameter value of the Inline graphic-th dimension for firefly Inline graphic.

Then, according to the movement rule defined by FA, the dimmer firefly is drawn towards the brighter one. The movement is determined by Eq. (29).

graphic file with name d33e1631.gif 29

It should be noted that Inline graphic is the randomization parameter between -0.5 and 0.5, introduces variability into the firefly movement. The appropriate step size will directly affect both the global and local search ability of the algorithm. So, set a value for the attenuation factor Inline graphic and initial value of the randomization parameter Inline graphic, the dynamic parameter Inline graphic can be defined by Eq. (30).

graphic file with name d33e1667.gif 30

In general, Eqs. (25) and (26) define the objective function, while Eqs. (27) to (30) outline the calculations for the necessary parameters and the movement criteria of the fireflies during the execution of the algorithm. To clearly state the numerical implementation of FA for locating critical slip surface, the algorithmic overview is presented in (Algorithm 1).

Algorithm 1.

Algorithm 1

Numerical implementation of FA for locating critical slip surface.

Numerical validation

This section presents numerical results obtained using the proposed analysis method. To verify the applicability and robustness of the proposed method, we report two typical benchmarks of isotropic slope and one anisotropic slope. Section “Slope in single soil layer” begins with a simple homogeneous slope to validate the reliability of the method in single soil layer condition. Section “Slope with weak interlayer” then analyzes a heterogeneous slope with a weak interlayer to verify the applicability of the proposed method under complex soil layer conditions. Subsequently, Section “Anisotropic slope with bedding plane” uses the proposed method to analyze slopes with different bedding plane angle, which further validating the ability of the method to analyze anisotropic slopes. To ensure the reliability and stability of the results, the calculations were repeated 50 times for each example. All simulations are implemented in MATLAB R2023a on a PC with an Intel Core (TM) i5-13600KF, 3.50 GHz processor and 32 GB RAM.

In this study, the parameters related to the firefly algorithm can be set as (Table 1): population size Inline graphic is 30, the light absorption coefficient Inline graphic is 1, the attenuation factor Inline graphic is 0.99, Inline graphic is 0.8, Inline graphic is 0.3.

Table 1.

Parameters of the firefly algorithm.

Parameters Inline graphic Inline graphic Inline graphic Inline graphic Inline graphic M
Value 1 0.8 0.3 0.99 30 30

Slope in single soil layer

The first benchmark is a simple homogeneous slope, which is taken from the work on Yamagami and Ueta48 and extensively used by scholars in the verification of applicability of their methods. In this benchmark, referring to the reported literature49, the following mechanical parameters can be used in the simulations: the effective friction angle Inline graphic is 10°, the coefficient of cohesion Inline graphic is 9.8 kPa, the unit weight Inline graphic is 17.64 kN/m3. The maximum number of function evaluations Inline graphic is 500. In order to compare with the results of other scholars, we set the number of soil slices Inline graphic to 30 and define the continuous function of the inter-slice force function as Inline graphic 1.

This benchmark has been analyzed by other scholars, and it was reanalyzed using the proposed method in this study, with the aim of verifying the reliability of the proposed method. Figure 6 shows the geometric features of the slope in benchmark 1 and the reanalyzed result of the critical sliding surface located by the proposed method, while comparing with the results of other scholars4951]. From the point of view of the shape of the critical sliding surface, it is obvious that the critical sliding surfaces obtained from the present study and results of other scholars are approximately equal, and present a shape of an approximate circular arc. The Inline graphic calculated using the proposed method is 1.3237, with a standard deviation of 0.00068. From the point of view of the Inline graphic, Table 2 provides a comparative summary of minimum Inline graphic and the standard deviation. The calculated results of the proposed method and the standard deviation of the results obtained by repeating 50 independent runs are within an acceptable range. The accuracy of the proposed method was verified by comparing the research results.

Fig. 6.

Fig. 6

Slope geometry and critical slip surface for benchmark 1.

Table 2.

Comparison of minimum Inline graphic and standard deviation from Teaching–learning-based optimization algorithm49, Imperialistic competitive algorithm50, Enhanced fireworks algorithm51 and present study.

Optimization method Inline graphic Standard deviation
Teaching-learning-based optimization algorithm (TLBO)49 1.324 0.00062
Imperialistic competitive algorithm (ICA)50 1.321 0.00692
Enhanced fireworks algorithm (EFWA)51 1.322 0.000331
Present study 1.324 0.00068

With the aim to further demonstrate the robustness of our method, we study the numerical convergence for different population size Inline graphic. Previous studies have shown that population size significantly affects the convergence rate51. The iteration curves for Inline graphic 20, 30 and 40 are presented in (Fig. 7a). As observed, the convergence rate is faster in the early stages when Inline graphic 40. The small differences in the convergence results can be attributed to the stochastic nature of the algorithm. Nevertheless, we can assume that the results obtained under the three population sizes are essentially consistent. To ensure robustness, we repeated each experiment 300 times independently. Figure 7b presents the quantile–quantile plots of the results for each population size. While the maximum Inline graphic value differ considerably across the conditions, the minimum Inline graphic values remain approximately the same. This indicates that a larger population size results in a more accurate distribution of Inline graphic, but does not affect the minimum Inline graphic. In summary, the above comparative tests demonstrate that the method exhibits excellent stability and rapid convergence in the stability analysis of homogeneous slopes.

Fig. 7.

Fig. 7

Effect of population size Inline graphic on convergence for the slope in single soil layer.

Slope with weak interlayer

The second benchmark is based on the work of Bolton et al.52, which was often used to verify the applicability of slope stability analysis methods under complex soil conditions. Referring to the reported literature50, we can obtain the parameters of the soil layers. The parameters for the first and third layers are the same. Specifically, Inline graphic and Inline graphic is 28.73°, the coefficient of cohesion Inline graphic and Inline graphic is 28.5 kPa, the unit weight Inline graphic and Inline graphic is 18.84 kN/m3. For the second layer, the soil parameters are Inline graphic 10°, Inline graphic 0 kPa and Inline graphic 18.84 kN/m3. The computational parameters related to FA in Benchmark 2 are the same as those in Benchmark 1 as listed in (Table 1), except that Inline graphic is set to 1000.

We applied the proposed method to reanalyze the slope in benchmark 2 to verify the accuracy and applicability of the method under complex soil conditions. We can obtain the geometric features from (Fig. 8). It is worth noting that the top height of the slope is 40 m, the bottom height is 27.75 m, the slope gradient is 0.5, and the location of the weak interlayer is located between the height of 26.5 and 27 m. In addition, the critical sliding surface obtained by the proposed method is also shown in (Fig. 8), while comparing with the research results of other scholars. By comparison, it is found that the results of these critical sliding surfaces all have a flat sliding surface close to the bottom of the weak interlayer. This feature is caused by the presence of the weak interlayer. The minimum Inline graphic calculated using the proposed method is 1.2423, with a standard deviation of 0.0225. And the solution recommended by ACADS experts is 1.26. It has been comparatively studied by Gandomi53,54 and Xiao51. Table 3 presents a comparative summary of the minimum Inline graphic and standard deviation. The comparison of standard deviations clearly highlights the stability of the results obtained by the proposed method. Furthermore, these results effectively demonstrate the accuracy and reliability of the proposed method under complex soil conditions.

Fig. 8.

Fig. 8

Slope geometry and critical slip surface for benchmark 2.

Table 3.

Comparison of minimum Inline graphic and standard deviation of EFWA51, Particle swarm optimization53, Biogeography-based optimization54, and present study method for benchmark 2.

Source Inline graphic standard deviation
Enhanced fireworks algorithm (EFWA)51 1.225
Particle swarm optimization (PSO)53 1.246 0.0931
Biogeography-based optimization (BBO)54 1.221 0.437
Present study 1.242 0.0225

In addition, to further explore the distribution of the firefly population during the convergence process and study the convergence behavior of the proposed method, the firefly population distribution was recorded for each iteration and Fig. 9 shows the population distribution at iteration numbers 1, 200, 1000, where the black dots represent the fireflies in the search space. As shown in Fig. 9, the distribution of fireflies in the initial state is relatively decentralized. After 200 iterations, the population gradually moves towards the region for best fitness and the optimal position is continuously refined and updated. Eventually, under the influence of the attraction force, the firefly population converges well, with all individuals becoming evenly distributed around the best position. These results demonstrate that the proposed method exhibits excellent global search capability, robustness, and convergence performance.

Fig. 9.

Fig. 9

Firefly search applied to the safety factor function at iteration numbers of (a) 1, (b) 200 and (c) 1000.

Anisotropic slope with bedding plane

The third benchmark involves the stability analysis of an anisotropic geological situation. Referring to the previous work of Ezra3, the associated mechanical parameters are assumed as follows: Inline graphic 10°, Inline graphic 25 kPa, Inline graphic 12.5 kN/m3, anisotropy ratio Inline graphic 0.5 and the height of the slope Inline graphic is 20 m. The maximum number of function evaluations Inline graphic of FA is set to 500.

In this benchmark, we aim to demonstrate the applicability and accuracy of the proposed method under anisotropic geotechnical conditions. Specifically, we analyze the stability and the shapes of the sliding surfaces depicted in Fig. 10 for various bedding plane angle Inline graphic of −30, 0, 60, and 90°. In addition, the numerical results of the sliding surface from Ezra3 using the modified log-spiral limit equilibrium (MLSLE) are also plotted for comparison. As shown in Fig. 10, the bedding plane angle has a significant influence on the morphology of the critical sliding surface. With the increase of Inline graphic from -30° to 0°, the control point at the top of the slope shifts in the direction of x-coordinate. However, when Inline graphic increases from 0 to 60°, this control point moves in the opposite direction. The difference between the results at 60° and 90° is relatively small.

Fig. 10.

Fig. 10

Comparison between the locations of the critical slip surfaces determined by the present method with the MLSLE and MLSLE with tension cracks at various bedding plane angle: (a) Inline graphic −30°, (b) Inline graphic 0°, (c) Inline graphic 60°, (d) Inline graphic 90°.

Through the conversion of the stability number, the comparative results of the safety factor are presented in (Table 4). From this comparison, it becomes evident that the interaction between the bedding plane angle Inline graphic and the alignment of the failure geometry significantly affects the value of Inline graphic. This effect is most pronounced in (Fig. 10a,c), the maximum and minimum values of Inline graphic occur when the failure mechanism is orthogonal to and aligned with Inline graphic, respectively. The results obtained by the proposed method are slightly higher than those reported by Ezra3, as shown in (Table 4). The difference may arise from variations in the internal force assumptions or differences in how equilibrium is satisfied in the two methods. However, the trend in the variation of Inline graphic remains consistent with the findings in the comparative literature, suggesting that the overall behavior of the system is well captured by our approach. The comprehensive results indicate that the proposed method is both highly applicable and accurate, providing reliable predictions of slope stability under anisotropic conditions.

Table 4.

Comparison of minimum Inline graphic of MLSLE 3, MLSLE with tension cracks 3 and present study method.

Method Factor of safety Inline graphic
Inline graphic-30° Inline graphic Inline graphic 60° Inline graphic 90°
Present study 0.484 0.401 0.274 0.353
MLSLE 3 0.450 0.357 0.236 0.299
MLSLE with tension cracks 3 0.399 0.325 0.184 0.227

Numerical results and discussions

The comparative experiments above demonstrate the reliability, stability, and applicability of the method proposed in this study under different conditions. In this section, we investigate the influence of anisotropic shear strength on slope stability by varying three key parameters: the slope angle Inline graphic, the bedding plane angle Inline graphic and the anisotropy ratio Inline graphic. Since anisotropy in rock and soil strength parameters significantly affects slope stability3,55, both cohesion anisotropy and frictional anisotropy are considered. The deterministic parameters of the numerical model are set as follows: Inline graphic is 12°, Inline graphic is 40 kPa, Inline graphic is 12 kN/m3, and Inline graphic is 20 m.

In the parametric study, Inline graphic is varied from 35° to 90° in increments of 5°, Inline graphic is varied from 0° to 180° in increments of 5° and Inline graphic is varied from 0.6 to 1 in increments of 0.1. Note that when Inline graphic 1, the intensity parameter is isotropic. To further elucidate the effects of anisotropy on slope stability and failure mechanisms, the following numerical model case is analyzed based on the method proposed in this study.

Effect of slope angle

The slope angle Inline graphic significantly influences both the stability of a slope and its mode of failure. In this study, slope stability is represented by Inline graphic, and the classification of slope failure modes follows the approach proposed by Cheng56. Hicks57 defined the sliding depth as the vertical distance from the slope’s apex to the base of the sliding surface. Building upon this definition, Cheng categorized slope failure into three distinct patterns based on the relative relationship between sliding depth and toe height.

Figure 11 shows the critical sliding surfaces for slope angles Inline graphic of 90, 60, 50 and 35° with a fixed Inline graphic of 0°. It can be observed from Fig. 10 that, as the slope angle decreases, the depth of the critical sliding surface increases progressively. Correspondingly, the slope failure mode shifts from shallow failure to deeper failure. From the perspective of slope stability, a general increase in stability is observed as Inline graphic decreases. Moreover, comparing the critical slip surfaces at the same slope angle but varying anisotropy ratios reveals that lower horizontal shear strength (i.e., a smaller Inline graphic) leads to a deeper critical failure surface.

Fig. 11.

Fig. 11

Anisotropic failure mechanism of slope in a two-layer soil with different Inline graphic at Inline graphic 0° (a): Inline graphic 90°, (c):Inline graphic 60°, (b): Inline graphic 50°, (d): Inline graphic 35°.

Figure 12 illustrates the relationship between Inline graphic and Inline graphic when Inline graphic is fixed at 0°. The results indicate that steeper slopes are more prone to instability. In particular, Inline graphic decreases continuously as Inline graphic increases between 35 and 45° and again between 60° and 90°. Among these ranges, Inline graphic is more sensitive to changes in Inline graphic between 35 and 45°. When Inline graphic is between 45 and 60°, Inline graphic remains relatively constant, showing only slight variations.

Fig. 12.

Fig. 12

Function relation between Inline graphic and Inline graphic when Inline graphic 0°.

Hicks57 noted that slope steepness affects the failure mode and identified 53° as the threshold angle separating shallow from deep sliding modes. As shown in Fig. 12, the results of this study are generally consistent with that observation. According to the calculations from the slope stability analysis program used here, within the range of 35 to 45°, the critical slip surface is relatively deep, indicating a deep failure mode. From 45 to 60°, the slip depth is closer to the slope toe, suggesting an intermediate failure mode. For slopes with angles from 60 to 90°, the slip depth occurs above the toe of the slope, indicating a shallow failure mode.

Additionally, the anisotropy ratio Inline graphic significantly influences the factor of safety. As Inline graphic decreases from 1.0 (isotropic) to 0.6, the degree of anisotropy in geotechnical materials increases, exerting a greater effect on slope stability. For instance, when Inline graphic is approximately 40°, reducing Inline graphic from 1.0 to 0.6 causes Inline graphic to drop from 1.47 to 1.02, a reduction of about 30%. In contrast, when Inline graphic is 90°, lowering Inline graphic from 1.0 to 0.6 only decreases Inline graphic from 0.82 to 0.71, roughly a 13% reduction. These findings indicate that gentler slopes are more sensitive to variations in strength anisotropy than steeper slopes.

Effect of bedding plane angle

The bedding plane angle Inline graphic plays a critical role in slope stability. Cho4 demonstrated that variations in anisotropic shear strength distribution significantly influence slope behavior, highlighting the importance of incorporating anisotropy into stability analyses. Figure 13 presents the critical sliding surfaces and their corresponding safety factors for different bedding plane angles at Inline graphic = 80° with Inline graphic values of 0.6 and 1.0. The results indicate that when the critical sliding surface is either perpendicular or parallel to the bedding plane direction, the slope exhibits its lowest or highest stability (Fig. 13b,d), especially the Inline graphic of 45 and 135°.

Fig. 13.

Fig. 13

Distribution of slip surfaces under different bedding plane angle: (a) Inline graphic 0°, (b) Inline graphic 45°, (c) Inline graphic 90°, (d) Inline graphic 135°, when Inline graphic 80°.

At maximum slope stability (Inline graphic 135°), the factor of safety reaches 0.9314, and both the critical sliding surface and Inline graphic closely resemble those observed under isotropic conditions. In contrast, when slope stability is minimized (Inline graphic 45°), the sliding surface aligns more closely with the bedding plane angle, yielding an Inline graphic of 0.6916. Compared to the maximum stability condition, Inline graphic decreases by approximately 25.7%.

To further examine the influence of Inline graphic on slope stability, we analyzed Inline graphic as a function of Inline graphic under various slope angles (see Fig. 14). As shown in Fig. 14a, Inline graphic reaches its minimum near Inline graphic = 45° and its maximum near Inline graphic = 135°. Although varying Inline graphic affects the magnitude of Inline graphic, it does not alter the Inline graphic angles at which Inline graphic attains its minimum or maximum. As Inline graphic decreases from 90° to 35°, the Inline graphic values corresponding to these extremal Inline graphic points shift gradually from 45 and 135 to 15 and 105°, respectively. Figure 14 also illustrates that the impact of strength anisotropy on slope stability becomes more pronounced for gentler slopes. At Inline graphic = 90°, Inline graphic decreases by up to about 25%, while at Inline graphic = 35°, the maximum decrease approaches nearly 31%.

Fig. 14.

Fig. 14

Inline graphic of slope in a two-layer soil under different Inline graphic versus the bedding plane angle: (a) Inline graphic 90°, (b) Inline graphic 75°, (c) Inline graphic 50°, (d) Inline graphic 35°.

Moreover, the effect of anisotropy ratio Inline graphic on the maximum Inline graphic for a given slope angle is particularly noteworthy. In steep slopes (Inline graphic = 90 and 75°), variations in Inline graphic have a negligible effect on Inline graphic at maximum stability (Fig. 14a,b). In these cases, Inline graphic values are similar to those under isotropic conditions. In contrast, as the slope angle decreases, differences in Inline graphic at maximum stability become more pronounced across different Inline graphic values (Fig. 14c,d). This phenomenon can be attributed to changes in the failure mode. As the failure mode transitions from shallow to deep, the spatial relationship between the failure surface and Inline graphic shifts from a simple orthogonal or aligned orientation to a more complex arrangement. Consequently, the Inline graphic values corresponding to different Inline graphic values, initially nearly identical, diverge as the slope reaches maximum stability.

Figure 15 illustrates the functional relationship between Inline graphic and Inline graphic under different anisotropy ratios. Specifically, Fig. 15a presents the results for Inline graphic = 0.6. By comparing the curves with different Inline graphic, it is evident that anisotropy has a relatively greater impact on gentler slopes. Additionally, when examining the Inline graphic corresponding to the peak factor of safety Inline graphic at various slope angles, it becomes clear that as Inline graphic decreases, the Inline graphic associated with the peak Inline graphic also decreases.

Fig. 15.

Fig. 15

Inline graphic of slope in a two-layer soil under anisotropy ratio Inline graphic versus the bedding plane angle: (a) Inline graphic 0.6, (b) Inline graphic 0.7, (c) Inline graphic 0.8, (d) Inline graphic 0.9.

Comparing Fig. 15a,d reveals that a smaller anisotropy ratio Inline graphic leads to a greater influence of anisotropy on slope stability. Notably, the curves depicting the relationship between bedding plane angles and the factor of safety for Inline graphic = 45° and Inline graphic = 60° exhibit different trends. Overall, Inline graphic shows a gradual increasing trend as Inline graphic decreases. However, the changes in Inline graphic are relatively subtle for Inline graphic = 45° and Inline graphic = 60°, which is consistent with the trends observed in (Fig. 12).

When combined with the analysis in Fig. 11 regarding changes in slope failure patterns, the results in Fig. 15 further emphasize that alterations in failure patterns significantly impact slope stability. While the influences of Inline graphic and Inline graphic on slope stability generally follow a consistent pattern, within certain slope angle ranges (45 to 60°), anisotropy can have a complex and critical effect on slope stability.

Based on the numerical model shown in (Fig. 13a) (Inline graphic 80°, Inline graphic 0°), we further investigated the impact of lower anisotropy ratios (Inline graphic 0.5, 0.4, 0.3, 0.2, and 0.1) on slope stability and obtained some meaningful results. Figure 16 presents the corresponding safety factors and critical slip surfaces distributions for different Inline graphic values. The study indicates that as Inline graphic gradually decreases, the Inline graphic consistently declines at an accelerating rate. Additionally, the spatial distribution of the critical slip surface exhibits notable variations with changes in Inline graphic: as Inline graphic decreases, the critical slip surface expands in the direction away from the slope, and the rate of expansion continuously increases. Nevertheless, given the exceedingly low likelihood of encountering such extreme Inline graphic values in practical engineering applications, this paper does not provide an in-depth and systematic analysis of the influence mechanism of extreme Inline graphic values on slope stability.

Fig. 16.

Fig. 16

Distribution of critical slip surfaces for different Inline graphic (Inline graphic=80°, Inline graphic=0°).

Conclusions

This study introduces a novel method for identifying the critical slip surface of heterogeneous slopes by incorporating the anisotropic yield criterion into the limit equilibrium approach. This method refines the limit equilibrium conditions to fully account for the influence of anisotropic shear strength parameters on slope stability by integrating an anisotropic yield criterion. Numerical benchmarks, including slope in a single soil layer, slope with weak interlayer and anisotropic slope with bedding plane, highlight our model’s ability to capture weak interlayer features and anisotropic characteristics. Numerical convergence studies are also conducted to demonstrate the robustness and reliability of our method.

Additionally, we apply the proposed method to investigate the underlying mechanisms of slope failure under various anisotropic conditions. The results indicate that slopes with anisotropic characteristics generally exhibit lower stability compared to those evaluated under isotropic assumptions. Notably, failure tends to initiate along the direction of minimal shear strength relative to the layering orientation—a trend that is particularly pronounced in steep slopes or in cases of shallow failure modes. A lower anisotropy ratio signifies a higher degree of anisotropy, thereby intensifying its impact on slope stability. This effect is particularly pronounced for slopes with lower gradients, where the anisotropy ratio can lead to a safety factor reduction of up to 31%. Moreover, when the slip surface is orthogonal or parallel to Inline graphic, the safety factor reaches its maximum or minimum, with these extremes becoming more pronounced as the slope angle decreases. These findings highlight the critical importance of accounting for anisotropic properties in slope stability assessments, especially in environments with complex geological layering and varying slope angles. For future research, we plan to extend this method to three-dimensional analyses and assess its applicability under more complex engineering conditions, such as seismic activity, seepage, external loads, and other factors.

Acknowledgements

This work was financially supported by the National Science Fund for Distinguished Young Scholars (Grant No. 52225403), the National Natural Science Foundation of China (Grant No. 52104089), the National Key Research and Development Program of China (Grant No. 2023YFF0615400), the Shandong Provincial Natural Science Foundation (Grant No. ZR2022QD102) and Demonstration Project of Benefiting People with Science and Technology of Qingdao, China (23-2-8-cspz-13-nsh).

Author contributions

Yongjun Zhang: Methodology, Writing—review & editing. Zhenfu Zhang: Methodology, Writing—original draft, Visualization. Sijia Liu: Supervision, Conceptualization. Mingzhong Gao: Supervision, Resources. Fei Liu: Supervision, Methodology. Jintao Wang: Investigation, Funding acquisition.

Data availability

The data used during the current study is available from the corresponding author on reasonable request.

Declarations

Competing interests

The authors declare no competing interests.

Footnotes

Publisher’s note

Springer Nature remains neutral with regard to jurisdictional claims in published maps and institutional affiliations.

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Associated Data

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Data Availability Statement

The data used during the current study is available from the corresponding author on reasonable request.


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