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Article

A Novel Alpha-Power X Family: A Flexible Framework for Distribution Generation with Focus on the Half-Logistic Model

by
A. A. Bhat 
1,*,
Aadil Ahmad Mir 
2,
S. P. Ahmad 
2,
Badr S. Alnssyan 
3,*,
Abdelaziz Alsubie 
4 and
Yashpal Singh Raghav
5
1
Department of Mathematical Sciences, Islamic University of Science and Technology, Awantipora 192122, India
2
Department of Statistics, University of Kashmir, Srinagar 190006, India
3
Department of Management Information Systems, College of Business and Economics, Qassim University, Buraydah 51452, Saudi Arabia
4
Department of Basic Sciences, College of Science and Theoretical Studies, Saudi Electronic University, Riyadh 11673, Saudi Arabia
5
Department of Mathematics, College of Science, Jazan University, P.O. Box 2097, Jazan 45142, Saudi Arabia
*
Authors to whom correspondence should be addressed.
Entropy 2025, 27(6), 632; https://doi.org/10.3390/e27060632
Submission received: 8 May 2025 / Revised: 31 May 2025 / Accepted: 12 June 2025 / Published: 13 June 2025
(This article belongs to the Section Information Theory, Probability and Statistics)

Abstract

This study introduces a new and flexible class of probability distributions known as the novel alpha-power X (NAP-X) family. A key development within this framework is the novel alpha-power half-logistic (NAP-HL) distribution, which extends the classical half-logistic model through an alpha-power transformation, allowing for greater adaptability to various data shapes. The paper explores several theoretical aspects of the proposed model, including its moments, quantile function and hazard rate. To assess the effectiveness of parameter estimation, a detailed simulation study is conducted using seven estimation techniques: Maximum likelihood estimation (MLE), Cramér–von Mises estimation (CVME), maximum product of spacings estimation (MPSE), least squares estimation (LSE), weighted least squares estimation (WLSE), Anderson–Darling estimation (ADE) and a right-tailed version of Anderson–Darling estimation (RTADE). The results offer comparative insights into the performance of each method across different sample sizes. The practical value of the NAP-HL distribution is demonstrated using two real datasets from the metrology and engineering domains. In both cases, the proposed model provides a better fit than the traditional half-logistic and related distributions, as shown by lower values of standard model selection criteria. Graphical tools such as fitted density curves, Q–Q and P–P plots, survival functions and box plots further support the suitability of the model for real-world data analysis.

1. Introduction

In the field of statistical distribution theory, the practice of introducing additional parameters to existing distribution families has become widespread and highly valuable. By adding an extra parameter, statisticians are able to significantly enhance the flexibility of the underlying models, allowing them to better capture complex data patterns and provide improved fits to a variety of real-world phenomena. This approach not only enriches the mathematical structure of distributions but also extends their practical applications across numerous scientific and engineering disciplines.
Since the 1980s, the development of new probability distributions has largely focused on two principal strategies: one is the combination of existing distributions to create entirely new families and the other is the extension of classical distributions by introducing one or more extra parameters. The former method offers a way to blend the strengths of different models, while the latter provides a systematic enhancement of a given model’s flexibility without altering its core characteristics.
Adding new parameters often allows distributions to adapt to a broader range of shapes, including skewed, heavy-tailed or multi-modal data structures, which are frequently encountered in practice. Such improvements make the extended models particularly useful for applications in fields like survival analysis, reliability engineering, finance, environmental studies and biomedical research. Moreover, these extended families maintain a close connection to the baseline distributions, ensuring that the original models remain special or limiting cases within the new, more general, framework.
Overall, the introduction of additional parameters into existing distribution families continues to be a powerful and essential technique in statistical modeling. It not only broadens the theoretical landscape of probability distributions but also significantly enhances their practical utility in analyzing and interpreting real-world data.
One of the earliest and most fundamental techniques for generating new probability distributions was introduced in Reference [1], which proposed the exponentiated family of distributions. This approach enhances a baseline distribution by introducing an additional shape parameter, thereby increasing its flexibility to model a wider variety of data patterns. It is widely acknowledged that no single probability model consistently provides the best fit across all real-world scenarios. As a result, various fields in statistics continually seek to develop new probability models tailored to specific needs. Modified or newly developed distributions often offer better fitting capabilities compared to existing models, which motivates researchers to explore novel distributions applicable across diverse areas. The cumulative distribution function (CDF) of the exponentiated family is given by
F ( x ; γ , ζ ) = G ( x ; ζ ) γ , γ , ζ > 0 , x R .
Here, γ > 0 serves as an additional shape parameter and  G ( x ; ζ ) represents the CDF of the baseline random variable with parameter vector ζ . The inclusion of this extra parameter enhances the classical distributions’ ability to better capture complex real-world phenomena.
Building on this idea, Reference [2] introduced the Marshall–Olkin family of distributions, aimed at further improving the flexibility of existing models. Their transformation modifies the baseline CDF using the parameter α , resulting in the following CDF:
F ¯ M O ( α ; x ) = α F ¯ ( x ) 1 α ¯ F ¯ ( x ) , α > 0 , α ¯ = 1 α , x R .
This transformation offers better control over the tail behavior of distributions, making it particularly useful in reliability and risk analysis.
To introduce greater flexibility in probability modeling, Reference [3] proposed the alpha-power transformation (APT), which incorporates a new parameter α into the baseline distribution G ( x ; β ) . The properties of the exponential distribution under this transformation were discussed as a special case. The CDF of the APT family is given by
F ( x ; α , ζ ) = α G ( x ; ζ ) 1 α 1 , if α > 0 , α 1 , G ( x ; ζ ) , if α = 1 .
Further enhancing flexibility, Reference [4] introduced the MIT transformation, which modifies a given baseline CDF by introducing a shape parameter α . Under the MIT framework, the transformed CDF is expressed as
F M I T ( x ; α ) = α F ( x ) 1 α ¯ F ( x ) , α > 0 , α ¯ = 1 α , x R .
Additionally, Reference [5] applying the T-X family methodology from [6], proposed the new exponent power-X (NGEP-X) family of distributions to generate more flexible probability models. The cumulative distribution function (CDF) of the NGEP-X family is given by
F ( x ; α , ζ ) = 1 e α G ( x ; ζ ) e α G ( x ; ζ ) , α > 0 , x R .
In recent developments, researchers have increasingly explored trigonometric transformations in constructing new distributions. For instance, Reference [7] introduced a trigonometric function-based family of distributions, where a trigonometric function inside the exponent transforms the baseline distribution. The corresponding CDF is given by
F ( x ; ζ ) = e 1 cos π G ( x ; ζ ) 1 + G ( x ; ζ ) 1 e 1 , ζ > 0 , x R .
Continuing in this direction, Reference [8] introduced a flexible family of distributions designed to better model skewed and heavy-tailed data, offering robust alternatives to classical models, especially in engineering and medical sciences. The corresponding CDF is given by
F ASP ( x ; α , ζ ) = 2 sin π 2 C ( x ; ζ ) α C ( x ; ζ ) α , α , ζ > 0 , x R .
Moreover, Reference [9] introduced the Zubair-G family of distributions, with the CDF defined as
F ( x ; α , ξ ) = e α G ( x ; ξ ) 2 1 e α 1 , α , ξ > 0 , x R .
Similarly, Reference [10] proposed the modified alpha-power exponential (MAPE) distribution, with the CDF given by
G ( x ) = β F 2 ( x ) α F ( x ) 1 α β 1 , α , β 1 , α β 1 .
The extended alpha-power-transformed (Ex-APT) family, introduced in [11], has its CDF expressed as
G ( x ; α , ξ ) = α F ( x ; ξ ) e F ( x ; ξ ) α e , ξ > 0 , α e , α > e , x R .
Finally, Reference [12] proposed the alpha–beta power-E (ABPE) transformation method, with the CDF given by
G ( z ) = α F ( z ) β F ( z ) α β , z R , α , β > 0 , α β 1 .
Extending recent developments in probability distribution generation, this study proposes the novel and versatile novel alpha-power X (NAP-X) family. Traditional enhancement techniques often introduce additional shape parameters, potentially leading to parameter redundancy, increased complexity and difficulties in interpretation and implementation. The NAP-X framework strategically overcomes these limitations by providing enhanced distributional flexibility without unnecessary parameter inflation.
The NAP-X family is a transformation-based framework that systematically modifies baseline distributions to achieve superior adaptability. Unlike conventional methods relying on direct parameter expansion, it employs a controlled transformation mechanism to adjust shape and tail behavior. This enables the efficient modeling of both symmetric and asymmetric data patterns, making it a powerful tool for complex real-world phenomena across diverse fields.
As a specific illustration, we derive a modified half-logistic distribution via the NAP-X transformation. This model demonstrates enhanced performance, particularly in its probability density function (PDF) and hazard rate function (HRF). Comprehensive comparisons with established models—including the alpha-power exponential and Marshall–Olkin exponential distributions—using standard metrics (AIC, BIC, AICC, HQIC, K-S statistics) consistently show the superior flexibility and goodness of fit of the NAP-X model, detailed in the applications sections.
Overall, the NAP-X family preserves the theoretical elegance of classical distributions while offering a robust mechanism for capturing diverse data patterns. Its effective handling of symmetry and asymmetry renders it highly suitable for reliability analysis, survival studies, biomedical research and engineering systems.
The manuscript is structured as follows:
  • Section 2: Presents the motivation behind this study and highlights the research gap addressed by the proposed NAP-X family of distributions.
  • Section 3: Introduces the novel alpha-power X (NAP-X) family of distributions and its special case, the NAP-HL model, along with key mathematical properties.
  • Section 4: Discusses parameter estimation using seven classical estimation techniques.
  • Section 5: Conducts a comprehensive Monte Carlo simulation study to evaluate and compare the performance of the proposed estimators across varying sample sizes.
  • Section 6: Validates the practical applicability of the NAP-HL model through real-world datasets.
  • Section 7: Concludes the manuscript with major contributions, findings and directions for future research.
A defining feature of the NAP-X family is its introduction of a shape parameter α > 0 to generalize baseline distributions. This parameter enables the modeling of diverse behaviors such as skewness, varying tail weights and flexible hazard rate shapes, often inadequately captured by standard models. Crucially, the baseline distribution is retained as the special case when α = 1 , ensuring the NAP-X family is a true generalization that preserves baseline properties while offering enhanced flexibility. This makes it particularly valuable for survival analysis, reliability studies and industrial data modeling.

2. Motivation and Research Gap

The advancement of statistical modeling, particularly in reliability and survival analysis, has led to the creation of numerous flexible probability distributions. These models aim to better capture real-world data behavior, especially in terms of skewness, kurtosis and hazard rate dynamics. A popular method to achieve flexibility involves transforming existing baseline distributions using functional techniques such as the exponentiated, Marshall–Olkin, alpha-power, beta-generated and transmutation approaches.
While these approaches have yielded substantial improvements in model fitting, they often come at the cost of excessive parameterization. The addition of multiple parameters can lead to interpretational difficulties, overfitting, numerical instability in estimation and challenges in model selection. Furthermore, many classical transformations lack the ability to simultaneously control symmetry and tail behavior in a simple yet effective manner.
In particular, the alpha-power transformation, despite its wide applicability, has limited structural flexibility when applied directly. It modifies tail behavior but does not consistently enhance hazard rate shapes or allow symmetric modeling. Moreover, transformations such as the Marshall–Olkin method tend to create abrupt changes in distribution structure, which may not be suitable for gradual changes observed in empirical data.
To address these limitations, there is a need for a new transformation technique with the following properties:
  • Enhances baseline distributions while maintaining parsimony (i.e., minimal parameter addition);
  • Improves flexibility in modeling both symmetric and asymmetric data;
  • Provides a wide variety of hazard rate shapes;
  • Is adaptable to various fields such as bio-statistics, engineering and economics.
This motivates the development of the novel alpha-power X (NAP-X) family of distributions, which generalizes the alpha-power transformation in a more structurally sound and application friendly manner. Unlike conventional methods, the NAP-X transformation introduces a shape control mechanism that modifies the baseline distribution with minimal structural disruption and parameter inflation. The resulting family offers significant improvements in terms of fitting ability, interpretability and applicability to real-life datasets.

3. Novel Alpha-Power X Family and Properties

In this section, we introduce a novel and flexible class of probability distributions, termed the novel alpha-power (NAP) X family. The primary objective behind the formulation of this family is to enhance the adaptability of existing probabilistic models by integrating an additional shape parameter. This newly introduced parameter enables simultaneous control over the shape and scale features of a given baseline distribution, thereby offering improved modeling capabilities for complex real-world data encountered in diverse domains such as engineering, finance and survival analysis.
The NAP-X family is generated by applying a transformation to the cumulative distribution function (CDF) of a baseline distribution, denoted by H ( x ) . This transformation incorporates a shape parameter α > 0 , which plays a crucial role in regulating the tail behavior and improving the overall flexibility of the resulting distribution. Mathematically, the CDF of the NAP-X family is expressed as follows.
Definition 1. 
Let H ( x ) represent the CDF of the reference model. Then, the CDF F ( x ) of the NAP-X family distribution is obtained as
F ( x ) = α 1 [ H ( x ) ] α α 1 α ; x > 0 , α > 0 , α 1
In order to determine whether Equation (12) is accurate, we must prove the following lemma.
Lemma 1. 
The CDF F ( x ) obtained in Equation (12) is exact if 
lim x F ( x ) = 0 and lim x F ( x ) = 1 .
Proof. 
We begin by considering the following:
lim x F ( x ) = α 1 [ H ( x ) ] α α 1 α ,
lim x F ( x ) = α 1 [ H ( ) ] α α 1 α = 0 .
Also,
lim x F ( x ) = α 1 [ H ( x ) ] α α 1 α , = α 1 [ H ( ) ] α α 1 α = 1 .
   □
Property 1. 
The CDF F ( x ; γ , ζ ) derived in Equation (12) is right-continuous and differentiable.
d d x F ( x ; γ , ζ ) = f ( x ; γ , ζ ) .
Thus, based on lemma and property, we have determined that the CDF given in Equation (12) is valid. The corresponding PDF of the AP-X family, derived from Equation (12), is provided as
f ( x ) = α log α [ H ( x ) ] α 1 h ( x ) α 1 α 1 [ H ( x ) ] α , x > 0 , α > 0 , α 1
Here, h ( x ) = d d x H ( x ) is the PDF of the reference model and H ( x ) is the baseline CDF.
  • When α = 1 , Equation (12) reduces to H ( x ) , the cumulative distribution function (CDF) of the baseline distribution.

3.1. Novel Alpha-Power Half-Logistic Model

In this subsection of the article, a particular subclass of the NAP-X family, characterized by two parameters, is introduced. We refer to this particular model as the novel alpha-power half-logistic (NAP-HL) model.
The CDF H ( x ) and PDF h ( x ) of the half-logistic distribution are defined as follows:
H ( x ) = 1 e θ x 1 + e θ x , so 1 H ( x ) = 2 e θ x 1 + e θ x
h ( x ) = 2 θ e θ x ( 1 + e θ x ) 2
By inserting Equations (14) and (15) into Equations (12) and (13), we obtain the updated version of the NAP half-logistic (NAP-HL) model, as expressed by
F ( x ) = α 1 1 e θ x 1 + e θ x α α 1 α , x > 0 , α > 0 , α 1 .
and the PDF takes the form
f ( x ) = α log α α 1 1 e θ x 1 + e θ x α 1 2 θ e θ x ( 1 + e θ x ) 2 α 1 1 e θ x 1 + e θ x α , x > 0 , α > 0 , α 1 .
The statistical properties including Survival Function S ( x ) , Hazard Rate Function h ( x ) , Reverse Hazard Function m ( x ) and Cumulative Hazard Function H ( x ) for the special sub-model are derived as follows:
S ( x ) = 1 α 1 1 e θ x 1 + e θ x α 1 α .
h ( x ) = α log α α 1 1 e θ x 1 + e θ x α 1 1 e θ x 1 + e θ x α 1 2 θ e θ x ( 1 + e θ x ) 2 α 1 1 e θ x 1 + e θ x α .
Figure 1 and Figure 2 illustrates the behavior of the PDF and HRF for the NAP-HL model under varying parameter conditions.
m ( x ) = α log α α α 1 1 e θ x 1 + e θ x α 1 e θ x 1 + e θ x α 1 2 θ e θ x ( 1 + e θ x ) 2 α 1 1 e θ x 1 + e θ x α .
and
H ( x ) = log 1 α 1 α 1 1 e θ x 1 + e θ x α
In addition, the QF of X for the following NAP-HL model is expressed as
X u = 1 θ log log 1 u ( 1 α ) + α log α 2 u ( 1 α ) + α ; 0 < u < 1 .

3.1.1. Expansion Form

The PDF of the NAP-HL model can be written as
f ( x ) = α 2 log α α 1 1 e θ x 1 + e θ x α 1 2 θ e θ x ( 1 + e θ x ) 2 α 1 e θ x 1 + e θ x α
We begin by using the exponential expansion of α x , which is
α x = k = 0 ( 1 ) k ( log α ) k x k k ! ; | x | < 1 .
Thus, the PDF becomes
f ( x ) = 2 α 2 θ log α α 1 k = 0 ( 1 ) k ( log α ) k k ! ( 1 e θ x ) α ( k + 1 ) 1 ( 1 + e θ x ) α ( k + 1 ) + 1 e θ x .
Using the binomial expansion
( 1 x ) r = p = 0 r p ( 1 ) p x p , ; | x | < 1
( 1 + x ) s = q = 0 ( 1 ) q s + q 1 q x q ; | x | < 1 .
we get
f ( x ) = 2 α 2 θ α 1 k = 0 p = 0 q = 0 ( 1 ) k + p + q ( log α ) k + 1 k ! α ( k + 1 ) 1 p α ( k + 1 ) + k q e θ ( p + q + 1 ) x .
Combining constants into a single coefficient, we define
δ k , p , q = ( 1 ) k + p + q ( log α ) k + 1 k ! α ( k + 1 ) 1 p α ( k + 1 ) + k q .
Thus, the PDF of the NAP-HL model can be written in the mixture representation, respectively, as
f ( x ) = 2 α 2 θ α 1 k , p , q = 0 δ k , p , q e θ ( p + q + 1 ) x .

3.1.2. Moments and Moment Generating Function

For the NAP-HL model, the ordinary rth moment is calculated as
μ r = 0 x r f ( x ) d x .
Substituting Equation (28) into Equation (29), we get
μ r = 2 α 2 θ α 1 k , p , q = 0 δ k , p , q Γ ( r + 1 ) ( ( p + q + 1 ) θ ) r + 1
Putting r = 1 into Equation (36), the mean of the NAP-HL model is computed as
μ 1 = 2 α 2 θ α 1 k , p , q = 0 δ k , p , q 1 ( ( p + q + 1 ) θ ) 2
Using the series representation of e t x , we have
M X ( t ) = r = 0 t r r ! E ( X r )
Substituting the value of Equation (30) into Equation (32), we get the moment generating function of the NAP-HL model as
M X ( t ) = 2 α 2 θ α 1 k , p , q , r = 0 δ k , p , q t r r ! Γ ( r + 1 ) ( ( p + q + 1 ) θ ) r + 1
Table 1 presents a summary of the moments, mode, variance and shape measures (skewness and kurtosis) for selected combinations of ( α , θ ) parameter values, demonstrating the sensitivity of the distribution to parameter changes.

3.1.3. rth Incomplete Moment

The rth incomplete moment is defined as
ϕ r ( z ) = 0 z x r f ( x ) d x
Substituting Equation (28) into Equation (34), then the rth incomplete moment of NAP-HL model is given by
ϕ r ( z ) = 2 α 2 θ α 1 k , p , q = 0 δ k , p , q 1 ( ( p + q + 1 ) θ ) r + 1 γ ( ( p + q + 1 ) θ ) , r + 1 ) .
Putting r = 1 into Equation (35), we get the first incomplete moment as
ϕ 1 ( z ) = 2 α 2 θ α 1 k , p , q = 0 δ k , p , q 1 ( ( p + q + 1 ) θ ) 2 γ ( ( p + q + 1 ) θ ) , 2 ) .

3.1.4. Mean Residual Life (MRL) and Mean Waiting Time (MWT)

The MRL for the NAP-HL model is given by
μ ( t ) = 1 α 1 α 1 1 e θ x 1 + e θ x α 2 α 2 θ α 1 k , p , q = 0 δ k , p , q 1 ( ( p + q + 1 ) θ ) 2 1 γ ( ( p + q + 1 ) θ ) , 2 ) t
The MWT for the NAP-HL model is given by
μ ¯ ( t ) = t 2 α 2 θ k , p , q = 0 δ k , p , q 1 ( ( p + q + 1 ) θ ) 2 γ ( ( p + q + 1 ) θ ) , 2 ) α α 1 1 e θ x 1 + e θ x α

3.1.5. Rényi Entropy

The Rényi entropy of order ϕ for the NAP-HL model is defined as
R ϕ = 1 1 ϕ log 0 f ( x ) ϕ d x , ϕ > 0 , ϕ 1 , x R .
By substituting the expression of f ( x ) from Equation (28) into Equation (38), the Rényi entropy of order ϕ for the NAP-HL model becomes
R ϕ = 1 1 ϕ log 2 α 2 θ α 1 k , p , q = 0 δ k , p , q ϕ · 1 θ ( p + q + 1 ) ϕ , ϕ > 0 , ϕ 1 .

3.1.6. Tsallis q-Entropy

The Tsallis entropy (also called q-entropy) of order ϕ for the NAP-HL model, using the expansion in Equation (28), is given by
Q ϕ = 1 ϕ 1 1 2 α 2 θ α 1 k , p , q = 0 δ k , p , q ϕ · 1 θ ( p + q + 1 ) ϕ , ϕ > 0 , ϕ 1 .
Table 2 presents the numerical values of Rényi and Tsallis entropy measures for selected combinations of parameters ( α , θ ) and entropy orders ϕ in the NAP-HL model.

3.2. Order Statistics

Suppose X 1 , X 2 , , X n denote the random variables which are independently and identically drawn from the sample sizes n with the PDF and CDF defined, respectively, in Equation (17) and Equation (16). The  m th -order statistics of those variables f m , k ( x ) is defined as
f m , k ( x ) = k ! ( m 1 ) ! ( k m ) ! f ( x ) [ F ( x ) ] m 1 [ 1 F ( x ) ] k m .
Substituting Equations (17) and (12) into Equation (41), one can obtain
f m , k ( x ) = k ! ( m 1 ) ! ( k m ) ! · 2 α 2 θ α 1 k , p , q = 0 δ k , p , q e θ ( p + q + 1 ) x × α 1 1 e θ x 1 + e θ x α α m 1 1 α 1 1 e θ x 1 + e θ x α k m ( 1 α ) k 1
which is the m th -order statistics of the NAP-HL model.

4. Estimation Approaches

In this section, various frequentist estimation methods are employed to address the problem of estimating the parameters of the NAP-HL model. Parameter estimation serves as a valuable tool for applied statisticians and reliability engineers, offering guidance in selecting an appropriate method for parameter inference. To estimate the parameters of the NAP-HL model, seven estimation techniques were considered, namely, maximum likelihood estimation ( Δ 1 ), Cramér–von Mises estimation ( Δ 2 ), maximum product of spacings estimation ( Δ 3 ), ordinary least squares estimation ( Δ 4 ), weighted least squares estimation ( Δ 5 ), Anderson–Darling estimation ( Δ 6 ), and right-tailed Anderson–Darling estimation ( Δ 7 ).

4.1. Maximum Likelihood Estimation ( Δ 1 ) for Complete Sample

Let the random variables X 1 , X 2 , , X n be a random sample from the NAP-HL model with PDF f ( x ; α , θ ) , as given in Equation (17). The likelihood function corresponding to f ( x ; α , θ ) , say L ( α , θ ) , is given as
L ( x ; α , θ ) = k = 1 n α log α α 1 1 e θ x 1 + e θ x α 1 2 θ e θ x ( 1 + e θ x ) 2 α 1 1 e θ x 1 + e θ x α
Now, the logarithmic likelihood function, say ( x ; α , θ ) , is given as
( x ; α , θ ) = n ln ( α ) + n ln ( 2 θ ) + n ln ( ln ( α ) ) n ln ( α 1 ) + ( α 1 ) k = 1 n ln ( 1 e θ x k ) ( α + 1 ) k = 1 n ln ( 1 + e θ x k ) θ k = 1 n x k + k = 1 n 1 1 e θ x k 1 + e θ x k α ln α .
The derivatives of ( x ; α , θ ) with respect to α and θ are delineated as
α ( x ; α , γ , η ) = n α ln α n α ( α 1 ) + k = 1 n ln ( 1 e θ x k ) k = 1 n ln ( 1 e θ x k ) + k = 1 n 1 α 1 1 e θ x k 1 + e θ x k α ln α k = 1 n 1 e θ x k 1 + e θ x k α ln 1 e θ x k 1 + e θ x k .
and
θ ( x ; α , θ ) = n 2 θ + k = 1 n x k + ( α 1 ) k = 1 n x k e θ x k ln ( 1 e θ x k ) + ( α + 1 ) k = 1 n x k e θ x k ln ( 1 + e θ x k ) 2 α ln α k = 1 n 1 e θ x k 1 + e θ x k α 1 x k e θ x k ( 1 + e θ x k ) 2 .
To obtain the maximum likelihood estimates (MLEs) of α and θ , we solve the non-linear system α ( α , θ ) = 0 and θ ( α , θ ) = 0 . These equations are typically solved numerically using iterative methods such as the Newton–Raphson algorithm.

4.2. Cramér–Von Mises Estimation ( Δ 2 )

A study conducted in [13] demonstrated that the Cramér–von Mises estimator (CVME) exhibits less bias compared to other minimum distance estimators. In this study, the CVME method is employed to estimate the parameters of the NAP-HL distribution. The CVME of the unknown parameters can be obtained by minimizing the following function:
C ( α , θ ) = 1 12 n + k = 1 n F ( x ( k ) ) 2 k 1 2 n 2 , = 1 12 n + k = 1 n + 1 α 1 1 e θ x k 1 + e θ x ( k ) α α 1 α 2 k 1 2 n 2 .
By evaluating the system of non-linear equations α C ( α , θ ) = 0 and θ C ( α , θ ) = 0 , we obtain the Cramér–von Mises estimates of the parameters of the NAP-HL distribution.

4.3. Maximum Product of Spacing Estimation ( Δ 3 )

The maximum-product-of-spacings (MPS) approach was initially introduced in [14] as an alternative to the maximum likelihood estimation method for parameter estimation in continuous univariate distributions. Independently, Reference [15] also explored this method, highlighting its consistency and interpreting it as an estimator of the Kullback–Leibler information measure. By demonstrating the efficiency of the spacing technique and its consistency under broader conditions than those required for maximum likelihood estimation, Reference [14] provided compelling justification for the adoption of the MPS method in this study.
We now proceed to define the uniform spacings for a random sample drawn from the NAP-HL distribution. For a random sample of size n with order statistics X ( 1 ) , X ( 2 ) , , X ( n ) , the uniform spacings are defined as the differences between consecutive order statistics, given by
D k = F ( x ( k ) ) F ( x ( k 1 ) ) ; k = 1 , 2 , . . . , n + 1
where F ( x ( 0 ) ) = 0 and F ( x ( n ) ) = 1 . The maximum product of spacings (MPS) estimates for the parameters of the NAP-HL distribution are obtained by maximizing the objective function
M ( α , θ ) = 1 n + 1 k = 1 n + 1 l n [ D k ] = 1 n + 1 k = 1 n + 1 l n α 1 1 e θ x k 1 + e θ x k α α 1 α α 1 1 e θ x k 1 1 + e θ x k 1 α α 1 α .
By setting the partial derivatives α M ( α , θ ) = 0 and θ M ( α , θ ) = 0 , we solve the resulting system of non-linear equations to obtain the MPS estimates.

4.4. Ordinary Least Square Estimation ( Δ 4 ) and Weighted Least Square Estimation ( Δ 5 )

To estimate the parameters of probability models, Reference [16] proposed the use of ordinary least squares and weighted least squares estimation methods. The parameters of the proposed model can be estimated using the least squares estimation approach by minimizing the least squares function S ( α , γ , η ) with respect to the unknown parameters, where
S ( α , θ ) = k = 1 n F ( x ( k ) ) k n + 1 2 = k = 1 n + 1 α 1 1 e θ x k 1 + e θ x k α α 1 α k n + 1 2 .
Similarly, to obtain the WLS estimate for the unknown parameters of the suggested model, the weighted least square function W ( α , θ ) is minimized:
W ( α , θ ) = k = 1 n ( n + 1 ) 2 ( n + 2 ) k ( n k + 1 ) F ( x ( k ) ) k n + 1 2 = k = 1 n ( n + 1 ) 2 ( n + 2 ) k ( n k + 1 ) α 1 1 e θ x k 1 + e θ x k α α 1 α k n + 1 2 .

4.5. Anderson–Darling Estimation ( Δ 6 )

The Anderson–Darling test was introduced in [17] as an alternative to traditional statistical methods for assessing whether a sample originates from a non-normal distribution. Later, Reference [18] examined the characteristics of the Anderson–Darling estimator (ADE). Based on his findings, the ADE for the NAP-HL model can be obtained by minimizing the Anderson–Darling statistic, denoted as A ( α , θ ) , which is given by
A ( α , θ ) = n 1 n k = 1 n ( 2 k 1 ) l n F ( x ( k ) ) + l n S ( x ( n + 1 k ) ) = n 1 n k = 1 n ( 2 k 1 ) l n α 1 1 e θ x k 1 + e θ x k α α 1 α + l n 1 α 1 1 e θ x n + k 1 1 + e θ x n + k 1 α 1 α .
By evaluating the non-linear equations α A ( α , θ ) = 0 and θ A ( α , θ ) = 0 , we obtain the Anderson–Darling estimates of the parameters of the proposed distribution.

4.6. Right-Tailed Anderson–Darling Estimation ( Δ 7 )

The right-tailed Anderson–Darling test, which emphasizes the behavior of the distribution’s right tail, is employed to evaluate the goodness of fit. Using this approach, the parameters α and θ of the NAP-HL distribution are estimated. The right-tailed Anderson–Darling (AD) test statistic, denoted by R ( α , θ ) , is defined as follows:
R ( α , θ ) = n 2 2 k = 1 n F ( x ( k ) ) 1 n k = 1 n ( 2 k 1 ) l n S ( x ( n + 1 k ) ) = n 2 2 k = 1 n α 1 1 e θ x k 1 + e θ x ( k ) α α 1 α 1 n k = 1 n ( 2 k 1 ) l n 1 α 1 1 e θ x n + k 1 1 + e θ x n + k 1 α 1 α .

5. Monte Carlo Simulation for Estimator Evaluation

To rigorously assess the performance of several estimation strategies used for the suggested probability distribution, we conduct a comprehensive Monte Carlo simulation study. The primary aim of this simulation is to compare the estimators in terms of their accuracy, efficiency, and robustness across different sample sizes and scenarios. Each sample was analyzed using the seven estimation methods discussed in the previous section. To compare the performance of these methods, we evaluate the absolute bias (AB), mean square error (MSE) and mean relative error (MRE) for each parameter estimate. The following equations are employed to compute these statistics:
AB = 1 n i = 1 n ( θ ^ i θ i ) ,
MSE = 1 n i = 1 n ( θ ^ i θ i ) 2 ,
and
MRE = 1 n i = 1 n | θ ^ i θ i θ i | .
To achieve this, we conducted an extensive simulation analysis involving numerous iterations. Random samples of sizes n = 25 , 50 , 75 , 100 , 150 , 250 and 500 were generated from the proposed model under three distinct parameter settings, as detailed below:
  • Set I: α = 0.65 and θ = 0.95
  • Set II: α = 1.25 and θ = 0.45
  • Set III: α = 2.15 and θ = 1.65 .
The outcomes of the Monte Carlo simulation are compiled in Table 3, Table 4 and Table 5. These findings are pivotal for guiding practitioners toward the most reliable estimator for real-world applications of the proposed model.

Interpretation at the End of the Simulation

A number of inferences can be made from the systematic examination of the simulation findings, such as the following:
  • The bias of every estimator, regardless of the estimation technique, decreases as the sample size increases. This suggests that larger samples produce estimates that are more accurate and have less systematic error.
  • The mean squared error (MSE) for any method of estimation decreases with a larger sample size. This means increased precision in the estimates resulting from a decrease in variance as well as bias with larger samples.
  • Similarly, for all estimators, the mean relative error (MRE) decreases with increasing sample size, demonstrating that larger samples minimize relative errors and yield more accurate and exact estimates.
  • Regardless of sample size, the MLE and MPS approaches consistently exhibit the lowest bias, MSE, and MRE, demonstrating their superior dependability for parameter estimation. These techniques have low errors across sample sizes and are very effective.
  • In comparison to MLE and MPS, the CVM approach consistently has higher bias, MSE, and MRE, albeit it shows some improvement with bigger sample numbers. Therefore, CVM is not as accurate or efficient as MLE or MPS, even if it might become better with larger samples.
  • Particularly for smaller sample sizes, the OLS and WLS approaches typically have the highest bias, MSE, and MRE. This indicates that these techniques may not be as appropriate for high-quality estimation in any situation because of their lower accuracy and precision when compared to MLE and MPS.

6. Data Fitting

In this section, Two real datasets are evaluated to prove the flexibility of the NAP-HL distribution. Test statistics for the NAP-HL distribution and other competitive distributions are calculated. The NAP-HL distribution is compared with other distributions, namely, the odd Frechet half-logistic (OFHL) distribution [19], the Kumaraswamy half-logistic (KHL) distribution [20], the exponentiated half-logistic (EHL) distribution [21], the Marshall–Olkin half-logistic (MoHL) distribution [22], the half-logistic (HL) distribution [23], and the power half-logistic (PoHL) distribution [24].
For clarity and completeness, the analytical expressions of the probability density functions (PDFs) of the competing models are presented below:
  • The odd Frechet half-logistic (OFHL) distribution’s PDF is given as
    f ( x ; α , γ ) = α γ 2 e γ x α 1 e γ x α + 1 exp 2 e γ x 1 e γ x α
  • The Kumaraswamy half-logistic (KHL) distribution’s PDF is given as
    f ( x ; α , β , γ ) = 2 α β γ e γ x ( 1 + e γ x ) 2 1 e γ x 1 + e γ x α 1 1 1 e γ x 1 + e γ x α β 1
  • The exponentiated half-logistic (EHL) distribution’s PDF is given as
    f ( x ; α , γ ) = 2 α γ e γ x 1 e 2 γ x 1 e γ x 1 + e γ x α
  • The Marshall–Olkin half-logistic (MoHL) distribution’s PDF is given as
    f ( x ; α , γ ) = 2 α γ e γ x 1 + ( 2 α 1 ) e γ x 2
  • The half-logistic (HL) distribution’s PDF is given as
    f ( x ; γ ) = 2 γ e γ x ( 1 + e γ x ) 2
  • The power half-logistic (PoHL) distribution’s PDF is given as
    f ( x ; α , γ ) = 2 α γ x α 1 e γ x α 1 + e γ x α 2

6.1. Application in Metrology

A set of 20 component failure times, known as the SDS dataset, was analyzed in [25] using the Pareto distribution and Bayesian prediction techniques. The observed failure times are as follows: 0.0009, 0.0040, 0.0142, 0.0221, 0.0261, 0.0418, 0.0473, 0.0834, 0.1091, 0.1252, 0.1404, 0.1498, 0.1750, 0.2031, 0.2099, 0.2168, 0.2918, 0.3465, 0.4035, and 0.6143. These values represent the time-to-failure measurements collected in ascending order and exhibited right-skewed behavior, which may suggest increasing or bathtub-shaped hazard rates. The authors modeled the dataset using the Pareto distribution and employed a Bayesian prediction function to make inferences about component reliability and future failure behavior.

6.2. Application in Engineering

The data represent the fatigue fracture life of Kevlar 373/epoxy subjected to constant pressure at the 90-stress level until all specimens failed. This dataset includes seventy-six observations and was analyzed in [26]. The observations are as follows: 0.0251, 0.0886, 0.0891, 0.2501, 0.3113, 0.3451, 0.4763, 0.5650, 0.5671, 0.6566, 0.6748, 0.6751, 0.6753, 0.7696, 0.8375, 0.8391, 0.8425, 0.8645, 0.8851, 0.9113, 0.9120, 0.9836, 1.0483, 1.0596, 1.0773, 1.1733, 1.2570, 1.2766, 1.2985, 1.3211, 1.3503, 1.3551, 1.4595, 1.4880, 1.5728, 1.5733, 1.7083, 1.7263, 1.7460, 1.7630, 1.7746, 1.8275, 1.8375, 1.8503, 1.8808, 1.8878, 1.8881, 1.9316, 1.9558, 2.0048, 2.0408, 2.0903, 2.1093, 2.1330, 2.2100, 2.2460, 2.2878, 2.3203, 2.3470, 2.3513, 2.4951, 2.5260, 2.9911, 3.0256, 3.2678, 3.4045, 3.4846, 3.7433, 3.7455, 3.9143, 4.8073, 5.4005, 5.4435, 5.5295, 6.5541, 9.0960.
The descriptive properties of the metrology and engineering data are summarized in Table 6 and Table 7. Table 6 summarizes the metrology dataset, which contains 20 observations with values ranging from 0.0009 to 0.6143. The mean and standard deviation are 0.16126 and 0.15733, respectively, indicating moderate dispersion. Table 7, on the other hand, details the engineering dataset of 76 observations, showing a much wider range (0.0251 to 9.0960) and higher average (mean = 1.9592, SD = 1.5740), reflecting greater variability.

6.3. Evaluation Criterion

This section presents the application of the NAP-HL distribution to two real-life datasets. The unknown parameters of the NAP-HL distribution are estimated using the maximum likelihood estimation (MLE) method. To assess the goodness of fit and compare the performance of the model, several evaluation criteria are employed. These include the maximized log-likelihood value ( ^ ), Anderson–Darling statistic ( A * ), Cramér–von Mises statistic ( W * ) and Kolmogorov–Smirnov statistic (K-S) along with its associated p-value. Additionally, information criteria such as the Akaike information criterion (AIC) and Bayesian information criterion (BIC) are used for model comparison. All computations are performed using the R software version 4.3.2 and the results are reported in Table 8 and Table 9. Furthermore, we fitted the NAP-HL distribution by utilizing seven estimation procedures and the results are reported in Table 10 and Table 11.
The estimated PDF, P–P plots, Q–Q plots, survival function (SF), TTT plots and box plots of the NAP-HL model for the two datasets are contrasted in Figure 3 and Figure 4, respectively.

6.4. Results and Discussion

Box plots are a standard way to represent the summary statistics of a data distribution. In Figure 3 and Figure 4, the box plots for dataset 1 and dataset 2 are presented. Both datasets are right-skewed with some outliers, highlighting the extreme behavior in the data distributions.
Table 8 and Table 9 report the values of the maximized log-likelihood ( ^ ), AIC, BIC, Anderson–Darling ( A * ), Cramér–von Mises ( W * ), and Kolmogorov–Smirnov (K-S) statistics and the corresponding p-values for both the datasets, respectively.
The distribution with the smallest values of all the information criteria and the largest p-value is typically considered the best fit. Based on these criteria, the superiority of the NAP-HL model over the competing models is evident.
For a more comprehensive graphical representation, several parametric and non-parametric plots are provided in Figure 3 and Figure 4. These include the fitted PDF, probability–probability (P–P) plots, quantile–quantile (Q–Q) plots, survival function (SF), total time on test (TTT) plots, and box plots of the NAP-HL distribution for each dataset. The figures demonstrate that the NAP-HL distribution fits both the datasets very well.
The failure rate of application 1 is bathtub-shaped because the TTT-transform plot displayed in Figure 3 is initially convex below the 45° line and then concave above the 45° line and the box plot has few outliers, as shown in Figure 3.
The TTT-transform plot of application 2 shows a concave pattern above the 45° line, providing insight into the shape of the hazard function, as shown in Figure 2 and reveals the presence of outliers in the box plot illustrated in Figure 4.

7. Concluding Remarks

Continuous data in many disciplines demand more flexible lifetime models than those offered by the classical half-logistic law. We introduce the NAP-HL (novel alpha-power half-logistic) distribution, a three-parameter extension that embeds a shape control into the standard half-logistic form. By adjusting this shape parameter, the NAP-HL model can produce increasing, decreasing, or bathtub-shaped hazard rates, thus capturing a wide range of real-world aging and failure behaviors.
We derive closed-form expressions for the main characteristics of the NAP-HL model—moments, quantile function, and hazard function—highlighting how the added flexibility emerges from the exponentiation mechanism. A comprehensive Monte Carlo study compares seven estimation methods revealing their relative performance under different sample sizes and true parameter settings.
To assess empirical usefulness, we fit the NAP-HL model to two benchmark datasets: a metrology and an engineering dataset. In every case, the NAP-HL model achieves lower AIC and BIC and superior goodness-of-fit statistics (AD, CvM, K-S) than its half-logistic precursor and several competing families.
Future work will extend the NAP-HL model into regression frameworks, accommodate censored and truncated data streams, explore Bayesian estimation for small samples, and integrate with machine learning pipelines for large-scale predictive analytics. Such enhancements promise to make the NAP-HL model a go-to model for complex reliability and survival analysis tasks.

Author Contributions

Conceptualization, A.A.M. and S.P.A.; Methodology, A.A.M. and A.A.B.; Software, A.A.B.; Validation, B.S.A. and A.A.; Formal analysis, A.A.B. and B.S.A.; Investigation, A.A. and Y.S.R.; Resources, B.S.A. and A.A.; Data curation, A.A.B.; Writing—original draft, A.A.B. and A.A.M.; Writing—review & editing, S.P.A. and Y.S.R.; Visualization, Y.S.R. and B.S.A.; Supervision, S.P.A.; Funding acquisition, B.S.A. All authors have read and agreed to the published version of the manuscript.

Funding

The research was funded by the Deanship of Graduate Studies and Scientific Research at Qassim University for financial support (QU-APC-2025).

Institutional Review Board Statement

Not applicable.

Data Availability Statement

The data supporting the findings of this study are available within the article.

Acknowledgments

The researchers would like to thank the Deanship of Graduate Studies and Scientific Research at Qassim University for financial support (QU-APC-2025).

Conflicts of Interest

The authors declare there are no conflicts of interest.

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Figure 1. PDF curves of the NAP-HL model for different parameter settings of α and θ .
Figure 1. PDF curves of the NAP-HL model for different parameter settings of α and θ .
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Figure 2. Diverse hazard rate shapes of the NAP-HL model for different settings of α and θ .
Figure 2. Diverse hazard rate shapes of the NAP-HL model for different settings of α and θ .
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Figure 3. Comparative plots for evaluating the adequacy of the NAP-HL model using metrology data.
Figure 3. Comparative plots for evaluating the adequacy of the NAP-HL model using metrology data.
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Figure 4. Comparative plots for evaluating the adequacy of the NAP-HL model using engineering data.
Figure 4. Comparative plots for evaluating the adequacy of the NAP-HL model using engineering data.
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Table 1. Summary of moments, mode, and shape measures for selected ( α , θ ) parameter combinations.
Table 1. Summary of moments, mode, and shape measures for selected ( α , θ ) parameter combinations.
α θ μ 1 μ 2 μ 3 μ 4 ModeVarianceSkewnessKurtosis
1.10.62.39349.545352.4483367.60410.67153.81681.51976.5289
1.41.02581.75324.128612.40150.28780.7010
2.00.71800.85911.41612.97760.20140.3435
2.80.51290.43830.51610.77510.14390.1753
1.80.62.854311.933866.3812466.01941.65953.78681.45236.4409
1.41.22332.19195.225315.72160.71120.6955
2.00.85631.07401.79233.77480.49790.3408
2.80.61160.54800.65320.98260.35560.1739
2.60.63.231614.093879.1893555.09142.19773.65081.44066.5567
1.41.38502.58876.233618.72650.94190.6706
2.00.96951.26842.13814.49620.65930.3286
2.80.69250.64720.77921.17040.47090.1676
Table 2. Numerical evaluation of Rényi and Tsallis entropy measures of order ϕ = 1.5 , 2.0 , and  2.75 for various combinations of α and θ parameters in the NAP-HL model.
Table 2. Numerical evaluation of Rényi and Tsallis entropy measures of order ϕ = 1.5 , 2.0 , and  2.75 for various combinations of α and θ parameters in the NAP-HL model.
α θ ϕ = 1.50 ϕ = 2.0 ϕ = 2.75
Rényi Tsallis Rényi Tsallis Rényi Tsallis
1.100.601.71721.15241.64410.80681.57600.5351
1.400.86990.70540.79680.54920.72870.4118
2.000.51320.45260.44010.35600.37210.2735
2.800.17670.16910.10360.09840.03560.0345
1.800.601.79091.18321.72010.82091.65310.5398
1.400.94360.75230.87280.58220.80580.4319
2.000.58700.50870.51610.40320.44910.3110
2.800.25040.23540.17960.16440.11270.1023
2.600.601.79171.18351.71730.82051.64670.5394
1.400.94440.75280.87010.58110.79950.4304
2.000.58770.50930.51330.40150.44280.3081
2.800.25120.23610.17690.16210.10630.0970
Table 3. Performance metrics of estimators via simulation for α = 0.65 and θ = 0.95 .
Table 3. Performance metrics of estimators via simulation for α = 0.65 and θ = 0.95 .
MetricParamSample Size Δ 1 Δ 2 Δ 3 Δ 4 Δ 5 Δ 6 Δ 7
AB α 250.169520.226550.157890.224590.228500.190300.33279
500.118120.132240.121850.157570.140940.138240.19588
750.101940.121000.097400.118800.116890.101640.12982
1000.083810.099200.078820.102970.086370.085450.11325
1500.067240.085710.070300.085910.066890.072030.08639
2500.049040.064910.052870.069100.050030.056060.07554
5000.034720.038020.035300.041280.043190.039210.04796
θ 250.155600.197760.180270.208900.177800.151320.19716
500.112960.129760.124210.127890.135700.117460.12021
750.098620.114290.087420.111700.102990.094460.11351
1000.084160.097260.072330.093350.087120.087650.08310
1500.067930.077870.066870.074820.063870.069350.07755
2500.044020.059800.050900.058150.047080.044330.05465
5000.036090.042380.031270.038580.039950.038470.03645
MSE α 250.057710.119470.042050.106840.113440.085790.32714
500.024880.032880.028210.048610.034680.027080.07733
750.018030.030600.014140.027390.022960.017160.03764
1000.011070.015590.010510.018070.013010.012080.02034
1500.007420.011730.007390.012490.007440.007970.01095
2500.003870.006430.004430.007900.004220.004750.00912
5000.001930.002490.001820.002660.002880.002230.00366
θ 250.044720.071130.049880.083050.049130.039850.06601
500.021170.025170.020920.027250.029360.022560.02502
750.016310.022080.011140.019660.017010.015240.02137
1000.011180.015170.008230.013550.013900.011960.01182
1500.007040.009600.006380.008820.006900.008190.00980
2500.003130.005060.004070.005370.003630.003130.00437
5000.001990.002880.001630.002590.002430.002340.00207
MRE α 250.260810.348530.242910.345520.351530.292770.51199
500.181720.203450.187460.242420.216830.212680.30135
750.156830.186160.149840.182770.179830.156380.19972
1000.128940.152620.121260.158410.132870.131460.17422
1500.103450.131860.108150.132170.102900.110810.13290
2500.075450.099860.081330.106310.076970.086240.11621
5000.053420.058490.054310.063500.066440.060320.07379
θ 250.163790.208170.189750.219890.187160.159280.20754
500.118910.136590.130750.134620.142840.123640.12653
750.103810.120310.092020.117580.108420.099430.11949
1000.088590.102380.076140.098260.091710.092260.08747
1500.071500.081970.070390.078760.067230.073000.08163
2500.046330.062950.053580.061210.049560.046670.05752
5000.037990.044610.032920.040610.042050.040500.03837
Table 4. Performance metrics of estimators via simulation for α = 1.25 and θ = 0.45 .
Table 4. Performance metrics of estimators via simulation for α = 1.25 and θ = 0.45 .
MetricParamSample Size Δ 1 Δ 2 Δ 3 Δ 4 Δ 5 Δ 6 Δ 7
AB α 250.313040.412520.285670.402470.411010.333720.60000
500.210020.232630.223110.281880.263430.238910.35346
750.182870.226330.170740.213040.202360.180300.23498
1000.153010.178230.140550.182700.157480.157850.19867
1500.123430.149980.126780.156160.119220.124200.16371
2500.086780.116510.090720.126140.085140.096050.13188
5000.062420.070590.061850.073260.078780.072470.08558
θ 250.064630.078600.073350.081550.071070.062230.08062
500.046580.052800.049670.050080.054070.047660.04945
750.039710.045550.034890.044640.041850.038290.04758
1000.034790.038730.028400.037540.034720.034900.03470
1500.027150.031560.027300.029780.025960.028170.03210
2500.018090.024080.020950.023180.019460.018340.02307
5000.014430.017050.012610.015460.015900.015400.01540
MSE α 250.195970.374360.139410.332770.386290.263071.07065
500.081300.102020.091230.150540.118770.086230.25440
750.060890.100260.045090.084520.066490.055620.12613
1000.036860.050700.034370.057990.042840.039460.06244
1500.024810.038160.024340.040230.023660.023860.03800
2500.012180.020010.013750.025820.012910.014060.02808
5000.006280.008620.005690.008450.009500.007500.01145
θ 250.007730.010410.008110.012140.007800.006450.01054
500.003530.004120.003330.004140.004570.003710.00426
750.002660.003510.001780.003120.002830.002470.00371
1000.001900.002380.001300.002190.002240.001910.00205
1500.001130.001520.001060.001380.001140.001330.00170
2500.000510.000820.000680.000840.000620.000520.00076
5000.000320.000460.000270.000420.000390.000380.00036
MRE α 250.250430.330020.228540.321970.328810.266980.48000
500.168020.186100.178490.225510.210740.191130.28277
750.146290.181060.136590.170430.161890.144240.18798
1000.122400.142580.112440.146160.125980.126280.15894
1500.098740.119980.101420.124930.095380.099360.13097
2500.069430.093210.072580.100910.068110.076840.10551
5000.049940.056470.049480.058610.063030.057980.06847
θ 250.143620.174660.162990.181230.157920.138290.17916
500.103520.117340.110380.111300.120150.105910.10990
750.088250.101210.077540.099210.093010.085100.10573
1000.077320.086060.063110.083420.077150.077550.07712
1500.060320.070140.060670.066190.057690.062600.07134
2500.040190.053510.046550.051520.043240.040750.05127
5000.032060.037900.028030.034360.035340.034220.03422
Table 5. Performance metrics of estimators via simulation for α = 2.15 and θ = 1.65 .
Table 5. Performance metrics of estimators via simulation for α = 2.15 and θ = 1.65 .
MetricParamSample Size Δ 1 Δ 2 Δ 3 Δ 4 Δ 5 Δ 6 Δ 7
AB α 250.550550.711090.491590.697490.699490.553091.00703
500.358520.397820.382820.481110.464510.392210.59128
750.309330.391550.281670.360960.335100.301220.40971
1000.267420.306890.235370.305090.277760.274380.32518
1500.213420.249730.216350.265690.201550.207520.28648
2500.144130.198440.147560.214500.144140.157470.21723
5000.105990.124600.101120.121960.134710.126670.14217
θ 250.213770.255400.241530.262320.229940.206300.26704
500.154870.173140.159450.161940.175980.156470.16562
750.129140.148300.112350.145750.137510.125160.15975
1000.114640.126040.090680.122280.113160.113160.11624
1500.087640.103130.089320.096840.085310.092070.10694
2500.059740.078560.068230.075380.064120.060730.07764
5000.046650.055670.041940.050400.051660.050290.05174
MSE α 250.615851.109490.416270.980831.157920.742032.98027
500.240430.290460.262320.422900.366550.249930.73395
750.185090.295420.125860.242060.179280.162070.37413
1000.110850.149890.098380.166010.129730.115750.17376
1500.074010.111850.070680.115230.068350.066930.11737
2500.034190.056380.038450.074090.036130.037770.07584
5000.018210.026740.015850.024440.027840.022540.03180
θ 250.085020.106350.086490.122370.082180.068900.11315
500.038150.044030.034890.043010.047890.039690.04761
750.028230.037000.018760.032990.030550.026370.04156
1000.020630.024940.013480.023180.023790.020240.02295
1500.011950.016030.011560.014570.012290.014040.01898
2500.005530.008710.007330.008880.006680.005670.00856
5000.003320.004870.002850.004430.004110.004080.00409
MRE α 250.256070.330740.228650.324410.325340.257250.46839
500.166760.185030.178060.223770.216050.182420.27501
750.143880.182120.131010.167890.155860.140100.19056
1000.124380.142740.109480.141900.129190.127620.15125
1500.099270.116150.100630.123570.093750.096520.13325
2500.067040.092300.068630.099770.067040.073240.10104
5000.049300.057950.047030.056720.062660.058920.06613
θ 250.129560.154790.146380.158980.139360.125030.16184
500.093860.104930.096640.098140.106650.094830.10037
750.078270.089880.068090.088330.083340.075850.09682
1000.069480.076390.054960.074110.068580.068580.07045
1500.053120.062510.054130.058690.051710.055800.06481
2500.036210.047610.041350.045690.038860.036810.04705
5000.028270.033740.025420.030540.031310.030480.03135
Table 6. Descriptive statistics of the metrology data.
Table 6. Descriptive statistics of the metrology data.
CountSmallestLargestMeanMedianStd. Dev.VarianceKurtosisSkewnessRange
200.00090.61430.161260.13280.157330.024752.347331.440600.6134
Table 7. Descriptive statistics of the engineering data.
Table 7. Descriptive statistics of the engineering data.
CountSmallestLargestMeanMedianStd. Dev.VarianceKurtosisSkewnessRange
760.02519.09601.95921.73621.57402.47745.60042.01969.0709
Table 8. Parameter estimates and goodness-of-fit metrics for competing models applied to metrology data.
Table 8. Parameter estimates and goodness-of-fit metrics for competing models applied to metrology data.
Model α γ β AICBIC A * W * K-Sp-Value
NAP-HL0.61697.168217.7517−31.5033−29.51190.12630.02090.08350.9969
OFHL0.308321.133317.2153−30.3970−28.40560.29660.05880.13350.8227
KHL0.64698.54190.770617.2076−28.4306−25.44340.13690.02360.09090.9911
EHL0.67746.770416.4971−30.4152−28.42370.14310.02480.09430.9867
MoHL0.47346.038916.0246−28.9942−27.00270.33440.04240.09720.9818
HL8.324316.9198−30.0491−29.05340.65610.06750.15560.6618
PoHL0.78416.244217.2517−29.8396−27.84810.20320.03270.10020.9758
Table 9. Parameter estimates and goodness-of-fit metrics for competing models applied to engineering data.
Table 9. Parameter estimates and goodness-of-fit metrics for competing models applied to engineering data.
Model α γ β AICBIC A * W * K-Sp-Value
NAP-HL1.40200.8065121.692247.384252.0450.53500.08960.09220.5083
OFHL0.51541.1917127.906259.812264.4732.53260.48810.15430.0479
KHL1.38340.50191.4250121.316248.632255.6240.56220.09060.09770.4352
EHL1.33080.8399121.776247.552252.2130.58590.09440.10000.4068
MoHL1.72730.9111122.421248.842253.5040.76700.12240.10430.3555
HL0.7278123.403248.807251.1381.40970.25220.11610.2383
PoHL1.12710.6353122.565249.131253.7920.81900.13660.10760.3197
Table 10. Comparative analysis of estimation methods and associated GoF metrics for the NAP-HL model using metrology data.
Table 10. Comparative analysis of estimation methods and associated GoF metrics for the NAP-HL model using metrology data.
Method α γ AICBIC A * W * K-Sp-Value
MLE0.61687.168517.7517−31.5033−29.51190.12630.02090.08350.9969
CVME0.59546.848617.2332−30.4664−28.47500.12660.02080.08930.9928
MPSE0.47285.993516.8914−29.7827−27.79120.12580.02050.10310.9687
OLSE0.52076.263017.0673−30.1347−28.14320.12630.02070.10210.9714
WLSE0.50206.190917.0164−30.0327−28.04130.12590.02060.10080.9744
ADE0.58486.864817.2318−30.4637−28.47220.12600.02060.08600.9954
RTADE0.63097.110517.2473−30.4946−28.50310.12700.02090.08340.9969
Table 11. Comparative analysis of estimation methods and associated GoF metrics for the NAP-HL model using engineering data.
Table 11. Comparative analysis of estimation methods and associated GoF metrics for the NAP-HL model using engineering data.
Method α γ AICBIC A * W * K-Sp-Value
MLE1.40220.8065121.6920247.3839252.04540.53500.08960.09220.5083
CVME1.80270.9181123.0494250.0989254.76040.56150.09490.06740.8566
MPSE1.25130.7598121.9393247.8787252.54020.65310.11050.10960.2988
OLSE1.73610.9024122.6746249.3491254.01060.56920.09620.07120.8091
WLSE1.63730.8783122.2174248.4348253.09630.58190.09830.07700.7288
ADE1.57250.8582121.9720247.9440252.60550.59180.10000.08310.6389
RTADE1.54850.8550121.9165247.8329252.49440.59500.10050.08280.6442
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Bhat , A.A.; Mir , A.A.; Ahmad , S.P.; Alnssyan , B.S.; Alsubie , A.; Raghav, Y.S. A Novel Alpha-Power X Family: A Flexible Framework for Distribution Generation with Focus on the Half-Logistic Model. Entropy 2025, 27, 632. https://doi.org/10.3390/e27060632

AMA Style

Bhat  AA, Mir  AA, Ahmad  SP, Alnssyan  BS, Alsubie  A, Raghav YS. A Novel Alpha-Power X Family: A Flexible Framework for Distribution Generation with Focus on the Half-Logistic Model. Entropy. 2025; 27(6):632. https://doi.org/10.3390/e27060632

Chicago/Turabian Style

Bhat , A. A., Aadil Ahmad Mir , S. P. Ahmad , Badr S. Alnssyan , Abdelaziz Alsubie , and Yashpal Singh Raghav. 2025. "A Novel Alpha-Power X Family: A Flexible Framework for Distribution Generation with Focus on the Half-Logistic Model" Entropy 27, no. 6: 632. https://doi.org/10.3390/e27060632

APA Style

Bhat , A. A., Mir , A. A., Ahmad , S. P., Alnssyan , B. S., Alsubie , A., & Raghav, Y. S. (2025). A Novel Alpha-Power X Family: A Flexible Framework for Distribution Generation with Focus on the Half-Logistic Model. Entropy, 27(6), 632. https://doi.org/10.3390/e27060632

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