Home Statistical inference of constant-stress partially accelerated life tests under type II generalized hybrid censored data from Burr III distribution
Article Open Access

Statistical inference of constant-stress partially accelerated life tests under type II generalized hybrid censored data from Burr III distribution

  • Amal S. Hassan ORCID logo , Najwan Alsadat , Mohamed Kayid , Mohammed Elgarhy , Oluwafemi Samson Balogun and Ehab M. Almetwally ORCID logo EMAIL logo
Published/Copyright: July 21, 2025

Abstract

Accelerated life tests (ALTs) involve subjecting units to more extreme conditions than normal to reduce the duration of testing. These tests, whether fully accelerated or partially accelerated, are crucial in life testing research as they help save both time and money. When results from ALT cannot be extrapolated to normal circumstances, partial ALTs are performed. This study introduces a constant-stress partial ALT, which relies on a generalized Type-II hybrid censoring scheme and assumes that the lifetimes of units under the specified conditions follow the Burr III distribution. The estimates of parameters and accelerated factor of the Burr III distribution are obtained under normal use settings by applying the maximum likelihood and Bayesian techniques. Bayesian estimators are generated using symmetric and asymmetric loss functions through the Monte Carlo Markov Chain approach. Additionally, credible intervals and asymptotic confidence intervals are constructed. Simulation research is carried out using different censoring techniques and sample sizes in order to compare the suggested methodologies. Next, two data sets are analyzed to show the value of the proposed approaches. The study’s conclusion contains a summary of its main conclusions.

Notation

n

total number of experiment items, where n = n 1 + n 2

T 1 & T 2

termination time of the experiment, predetermined by the experimenter, where T 1 < T 2

y r:n

the time of the rth failure observed from n items under GTI-HCS

y s:n

the time of the sth failure observed from n items under GTII-HCS

r & s

the failure number obtained at time T 1 and T 2 under GTI-HCS and GTII-HCS, respectively

y 1i

the items allocated at use condition in CSPALT, under GTII-HCS, where, i = 1, …, n 1

y 2i

the items allocated at accelerated condition, in CSPALT, under GTII-HCS, where i = 1, …, n 2

r 1

the failed items observed from n 1 before the censoring time h 1, in case of used condition under GTII-HCS

r 2

the failed items observed from n 2 units before the censoring time h 2, in case of accelerated condition, under GTII-HCS

d 11 & d 21

the failure number obtained at time T 11 and T 21, respectively, at used condition in CSPALT under GTII-HCS

d 12 & d 22

the failure number obtained at time T 12 and T 22, respectively, at accelerated condition in CSPALT under GTII-HCS

D 1 & D 2

the number of total failures in the experiment up to time h 1 & h 2, respectively, in CSPALT under GTII-HCS

T 11 & T 12

time points predetermined by the experimenter in used condition of CSPALT under GTII-HCS

T 21 & T 22

time points predetermined by the experimenter in accelerated condition of CSPALT under GTII-HCS

Abbreviations

Abias

absolute Bias

AD

Anderson-Darling

AIC

Akaike information criterion

Asy-CIs

asymptotic confidence intervals

BCIs

Bayesian credible intervals

BEs

Bayesian estimates

BIC

Bayesian information criterion

BIIID

Burr III distribution

CAIC

corrected AIC

CDF

cumulative distribution function

CIs

confidence intervals

CP

coverage probability

CSPALT

constant-stress partial accelerated life testing

CVM

Cramer-von Mises

G1 & G2

first group and second group, respectively

GTI−HCS

generalized type I – hybrid censoring sampling

GTII−HCS

generalized type II – hybrid censoring sampling

HCS

hybrid censored sampling

HF

hazard rate function

HQIC

Hannan–Quinn information criterion

K-S

Kolmogorov–Smirnov

KSD

K-S distance

KSPV

K-S p-value

LACI

length of asymptotic confidence intervals

LCCI

length of Bayesian credible intervals

LXF

linear exponential loss function

MCMC

Markov chain Monte Carlo

MH

Metropolis-Hastings

MLE

maximum likelihood estimate

PALT

partial accelerated life test

PP

probability-probability

QQ

quantile-quantile

StEr

standard error

TTT

total time on test

V-CM

variance–covariance matrix

1 Introduction

In investigations of reliability and life testing, censored data are crucial when it becomes impossible to obtain all the data needed for the experiment due to factors like expense or schedule. Type-I and Type-II censoring are two of the most common types of censoring. A hybrid censored sampling (HCS) approach, which combines Type-I and Type-II censoring schemes, was proposed by Epstein [1]. Suppose that Y 1:n < Y 2:n <…< Y n:n denote the ordered failure times of the experimental units. In Type-I HCS (TI−HCS), the life-testing experiment ends at time T 1 = min (Y r:n , T), where Y r:n represents the time of the rth failure out of n items, and T is the maximum time point for the test, r ( 1 , 2 , , n ) , and T ( 0 , ) . The test continues until a predefined number of units fail, at which point the experiment is terminated. Since the maximum amount of time allowed for the test under this system is T, there is a chance that relatively few failures in this HCS strategy will happen before time T 1. As a result of this, Childs et al. [2] suggested a new HCS that ensures a fixed number of failures, known as Type-II HCS (TII−HCS). In this situation, the life test ends at time T 2 = max(Y r:n , T), where r ( 1 , 2 , , n ) , and T ( 0 , ) . Chandrasekar et al. [3] enhanced these censored sampling strategies by establishing two extensions of this kind, known as generalized TI−HCS (GTI−HCS) and generalized TII−HCS (GTII−HCS). In the context of GTI−HCS, s , r ( 1 , 2 , , n ) and T ( 0 , ) are fixed so that s < r. The experiment ends at Y s:n if the sth failure happens after time T. Thus, a minimal number s of failures is ensured in GTI−HCS. In GTII−HCS, one fixes r ( 1 , 2 , , n ) and T 1 , T 2 ( 0 , ) so that T 1 < T 2. The experiment ends at time T 1 if the rth failure happens before that time T 1. If the rth failure happens between T 1 and T 2, the experiment is ended at Y r:n . Lastly, the experiment ends at time T 2 if the rth failure happens after time T 2.

Rapid technological advancement, consumer demand for consistent products, and competitive markets have all placed pressure on producers to supply consistent, quality products. It is extremely difficult to observe the failure time for complicated, high-reliability devices during life testing, such as lasers, optical fibers, semiconductors, metal fatigue, electric cables, and insulating materials. Due to this, accelerated life testing (ALT) or partial ALT (PALT) is recommended in the industrial sector to gather the essential failure data quickly enough to determine the failure’s link to external stress factors. Test items in ALTs are only tested at accelerated circumstances, or pressures higher than normal, in order to cause an early failure. A physically acceptable statistical model then extrapolates the data gathered under such accelerated settings to predict the lifespan distribution under typical use conditions. This test might save a significant amount of money, time, labor, and resources. There are several ways to administer stress, such as step stress, progressive stress, and continuous stress (see [4]).

The PALT is the most appropriate test to use, especially when test items are administered under both normal and higher-than-normal stress levels [5,6,7,8]. It is also the most crucial technique to apply when calculating the acceleration factor and projecting the accelerated test results to the situation. PALT integrates both standard life and ALT. As a result, PALT makes sense for calculating the acceleration factor (β > 1), which is defined as “the ratio of the hazard rate at the accelerated condition to that at normal conditions.” PALT may be broadly classified into two categories: step-stress PALT and constant-stress PALT (CSPALT). In step-stress PALT, after a certain number of failures or at a predetermined period, the test conditions for the remaining objects in the experiment change from normal use to higher stress. In CSPALT, every group of test units is subjected to different usage and accelerated conditions, which is the primary focus of this work. CSPALTs were examined by several authors, such as [9,10] for the Pareto distribution, [11] inverse Weibull distribution, [12,13] Gompartz distribution, [14] Weibull distribution, [15] Kumaraswamy distribution, [16] Lomax distribution, [17] weighted Lomax distribution, and [18] linear exponential distribution. For more studies, refer to [19,20,21,22,23].

To fit different failure life time data, Burr [24] created 12 cumulative distribution functions (CDFs). A lot of attention has recently been paid to the Burr type-III distribution (BIIID) among others since it can accept various hazard lifetime data. It can also accurately approximate a wide range of popular distributions for fitting lifetime data, including the gamma, Weibull, and log-normal distributions. Many scientific domains have employed the BIIID. Examples of these include modeling forestry-related events [25], fracture roughness [26], actuarial literature [27], meteorological literature [28], reliability theory [29,30], and operational risk [31], among others. The probability density function (PDF) of the BIIID is given by:

(1) f 1 ( y ) = ϑ λ y ( λ + 1 ) ( 1 + y λ ) ϑ 1 ; y > 0 ,

where ϑ , λ > 0 , are the shape parameters. The CDF of the BIIID is

(2) F 1 ( y ) = ( 1 + y λ ) ϑ ; y > 0 .

The hazard rate function (HF) of the BIIID is given by:

(3) τ 1 ( y ) = ϑ λ y ( λ + 1 ) ( 1 + y λ ) ϑ 1 1 ( 1 + y λ ) ϑ .

Numerous scholars have examined inferences for the parameters of the BIIID. A Bayesian estimator for the BIIID based on double censoring was examined by Abd-Elfattah and Alharbey [32]. Kim and Kim [33] discussed the Bayesian and classical estimation methodologies of the BIIID parameters based on dual generalized order statistics. The BIIID’s estimate and prediction issues were addressed using TII censored and progressive Type II hybrid censored samples by Altindag et al. [34] and Gamchi et al. [35], respectively,. The unified hybrid censored sample was used by Panahi [36] to develop the statistical inference of a BIIID. Hassan et al. [37] addressed the estimation of the lifetime performance index for BIIID based on progressive censoring scheme. Dutta and Kayal [38] provided estimation and prediction for the BIIID using unified progressive hybrid censoring. Bayesian and non-Bayesian inferences of the BIIID under joint progressive TII censoring were examined by Hassen et al. [39].

So far, there have been no articles specifically focused on estimating parameters of the BIIID in CSPALT with GTII-HCS data. This article aims to address this gap, given the flexibility and versatility of the GTII-HCS, along with the widespread application of BIIID in modeling lifetime data. Consequently, this paper’s primary goals are as follows:

  1. Using the GTII-HCS, the classical (maximum likelihood) estimation method will be utilized to derive the point estimators and asymptotic confidence intervals (Asy-CIs) for the parameters and acceleration factor in CSPALT model.

  2. The Bayes procedure will be applied to obtain Bayesian estimators and the Bayesian credible intervals (BCIs) of the BIIID parameters. By assuming independent gamma priors for the parameters, we can compute Bayes estimates under different loss functions.

  3. The Markov chain Monte Carlo (MCMC) technique will be employed, implementing Gibbs sampling within the Metropolis Hastings (MH) framework, to generate samples from the posterior distributions.

  4. A simulation study will be conducted to assess the efficiency of the estimators based on several precision measures.

  5. To examine two real datasets to show the applicability of the proposed estimators.

The format of the paper is as follows: Section 2 presents the model description along with the assumptions made. In Section 3, we discuss the maximum likelihood (ML) and Asy-CI estimators for the model parameters and acceleration factor. Section 4 focuses on the Bayesian and BCI estimators for the model parameters and the acceleration factor. A simulation study to evaluate the performance of these estimates for the specified model is conducted in Section 5. The analysis of actual data is detailed in Section 6, while Section 7 concludes with some key findings.

2 Model description and assumption

This section gives a description of the model and its assumptions.

2.1 Model description

Suppose that total test items n are divided into two groups. Under used settings, n 1 randomly selected test items from n total are included in the first group (G1). The remaining n 2 = nn 1 test items in the second group (G2) are subjected to accelerated operating conditions. The items in each group are tested using a GTII-HCS. Let the lifetimes y i , i = 1, , n , = 1, 2 denoted two GTII−HSC, where y 1i , i = 1, …, n 1 be the lifetimes of items in G1 (normal use condition) and y 2:i , i = 1, …, n 2 be the lifetimes of items in G2 (accelerated condition). The experiment ends at time T 1 if the r th failure occurs before time T 1 . If the r th failure occurs between T 1 and T 2 , the experiment ends at y r . Lastly, the experiment ends at time T 2 if the r th failure occurs after time T 2 .

Suppose that y 1 i = ( y 11 < < y 1 n 1 ) , i = 1 , 2 , , n 1 , an ordered sample of size n 1, are tested under used condition. Under the GTII-HCS, one of the three observation categories can be obtained:

Case 1U: y 11 < < y 1 r 1 < < y 1 d 11 < T 11 if y 1 d 11 < T 11 ,

Case 2U: y 11 < < y 1 d 11 < < y 1 r 1 if T 11 < y 1 r 1 < T 12 ,

Case 3U: y 11 < < y 1 d 12 < < T 12 if y 1 r 1 > T 12 .

Note that d 11 and d 12 are, respectively, the failure numbers obtained at time T 11 and T 12. Also, T 11 and T 12 are time points determined by the experimenter according to how the experiment should continue based on the information about the product. Also, the likelihood function in CSPALT, under GTII-HCS has the following form:

L 1 = n 1 ! ( n 1 D 1 ) ! i = 1 D 1 f 1 ( y 1 i ) [ 1 F 1 ( h 1 ) ] n 1 D 1 ,

where D 1 represents the total number of failures in the experiment up to time h 1 under normal use conditions, and its value is determined by:

( D 1 , h 1 ) = ( d 11 , T 11 ) case 1 U ( r 1 , y 1 r 1 ) case 2 U ( d 12 , T 12 ) case 3 U .

Similarly, suppose that y 2 i = ( y 21 < < y 2 n 2 ) , i = 1 , 2 , , n 2 , an ordered sample of size n 2, are tested under accelerated condition. Under GTII-HCS, one of the three observation categories can be obtained:

Case 1A: y 21 < < y 2 r 2 < < y 2 d 21 < T 21 if y 2 d 21 < T 21 ,

Case 2A: y 21 < < y 2 d 21 < < y 2 r 2 if T 21 < y 2 r 2 < T 22 ,

Case 3A: y 22 < < y 2 d 22 < < T 22 if y 2 r 2 > T 22 .

Note that d 21 and d 22 are, respectively, the number of failures observed at time T 21 and T 22. Also, T 21 and T 22 are time points determined by the experimenter according to how the experiment should continue based on the information about the product. Also, the likelihood function in CSPALT, under GTII-HCS has the following form:

L 2 = n 2 ! ( n 2 D 2 ) ! i = 1 D 2 f 2 ( y 2 i ) [ 1 F 2 ( h 2 ) ] n 2 D 2 ,

where D 2 is the number of total failures in the experiment up to time h 2 , under accelerated condition, and its value is determined by:

( D 2 , h 2 ) = ( d 21 , T 21 ) case 1 A ( r 2 , y 2 r 2 ) case 2 A ( d 22 , T 22 ) case 3 A .

2.2 Model assumptions

Under normal operating conditions, an item’s lifetime is assumed to follow the BIIID, with PDF, CDF, and HF obtained by Eqs. (1)–(3). On the other hand, when evaluating an item in accelerated conditions, its HF is represented as h 2(y) = ρ h 1(y), where the acceleration factor is ρ > 1 . So, the HF, CDF, and PDF of the BIIID, for y > 0, ϑ , λ > 0 , and ρ > 1 , under the accelerated condition are as follows:

τ 2 ( y ) = ϑ ρ λ y ( λ + 1 ) ( 1 + y λ ) ϑ 1 1 ( 1 + y λ ) ϑ ,

(4) F 2 ( y ) = 1 [ 1 ( 1 + y λ ) ϑ ] ρ , y > 0 ,

and,

(5) f 2 ( y ) = ρ λ ϑ y λ 1 ( 1 + y λ ) ϑ 1 [ 1 ( 1 + y λ ) ϑ ] ρ 1 , y > 0 .

3 ML estimators

This section provides the ML technique to generate the point estimators of the unknown parameters λ , ϑ , and acceleration factor ρ based on the GTII−HCS with CSPALT. Furthermore, the Asy-CIs of the model parameters and acceleration factor are determined.

Suppose that y 1 i = ( y 11 < < y 1 n 1 ) , i = 1 , , n 1 be n 1 GTII−HCS drawn from BIIID with PDF (1) and CDF (2) under normal usage conditions. Also, assume that y 2 i ( y 21 < < y 2 n 2 ) , i = 1 , 2 , , n 2 be n 2 GTII−HCS drawn from BIIID with PDF(5) and CDF(4) under accelerated conditions. Hence, the likelihood function in CSPALT for the BIIID under the GTII-HCS is obtained by combining the likelihood functions L 1 and L 2 as follows:

(6) L ( y ϑ , λ , ρ ) = = 1 2 n ! ( n D ) ! i = 1 D f ( y i ) [ 1 F ( h ) ] n D ,

where d , = 1 , 2 is the number of total failures in the experiment up to time h and their values are given by:

( D , h ) = ( d 1 , T 1 ) case 1 ( r , y r ) case 2 ( d 2 , T 2 ) case 3 .

Then, inserting Eqs. (1), (2), (4), (5) in (6) gives:

L ( y ζ ) = ϑ D 1 + D 2 λ D 1 + D 2 ρ D 2 = 1 2 n ! ( n D ) ! i = 1 D y i ( λ + 1 ) ( 1 + y i λ ) ϑ 1 [ 1 ( 1 + y i λ ) ϑ ] ρ 1 1 [ 1 ( 1 + h λ ) ϑ ] ρ 1 ( n D ) ,

where ζ ( λ , ϑ , ρ ) . The natural logarithms of likelihood function is

l = ( D 1 + D 2 ) ( log ϑ + log λ ) + D 2 log ρ ( λ + 1 ) i = 1 D 1 log y 1 i + i = 1 D 2 log y 2 i ( ϑ + 1 ) i = 1 D 1 log ( 1 + y 1 i λ ) + i = 1 D 2 log ( 1 + y 2 i λ ) + ( ρ 1 ) i = 1 D 2 log [ υ 1 ( y 2 i , λ , ϑ ) ] + ( n 1 D 1 ) × log [ υ 2 ( h 1 , λ , ϑ ) ] + ( n 2 D 2 ) ρ log [ υ 3 ( h 2 , λ , ϑ ) ] ,

where, υ 1 ( y 2 i , λ , ϑ ) = [ 1 ( 1 + y 2 i λ ) ϑ ] , υ 2 ( h 1 , λ , ϑ ) = [ 1 ( 1 + h 1 λ ) ϑ ] , and υ 3 ( h 2 , λ , ϑ ) = [ 1 ( 1 + h 2 λ ) ϑ ] .

The ML estimators λ ˆ , ϑ ˆ , and ρ ˆ , of λ , ϑ , and ρ are produced by simultaneously solving the following normal equations:

(7) l λ = D 1 + D 2 λ + i = 1 D 1 ( ϑ + 1 ) log y 1 i 1 + y 1 i λ + i = 1 D 2 ( ϑ + 1 ) log y 2 i 1 + y 2 i λ + i = 1 D 2 ( ρ 1 ) υ 1 ( λ ) υ 1 ( y 2 i , λ , ϑ ) i = 1 D 1 log y 1 i i = 1 D 2 log y 2 i + ( n 1 D 1 ) υ 2 ( λ ) υ 2 ( h 1 , λ , ϑ ) + ( n 2 D 2 ) υ 3 ( λ ) υ 3 ( h 2 , λ , ϑ ) = 0 ,

(8) l ϑ = D 1 + D 2 ϑ i = 1 D 1 log ( 1 + y 1 i λ ) i = 1 D 2 log ( 1 + y 2 i λ ) + i = 1 D 2 ( ρ 1 ) υ 1 ( ϑ ) υ 1 ( y 2 i , λ , ϑ ) + ( n 1 D 1 ) υ 2 ( ϑ ) υ 2 ( h 1 , λ , ϑ ) + ( n 2 D 2 ) ρ υ 3 ( ϑ ) υ 3 ( h 2 , λ , ϑ ) = 0 ,

(9) l ρ = D 2 ρ + i = 1 D 2 log [ υ 1 ( y 2 i , λ , ϑ ) ] + ( n 2 D 2 ) log [ υ 3 ( h 2 , λ , ϑ ) ] = 0 ,

where

υ 1 ( λ ) = υ 1 ( y 2 i , λ , ϑ ) λ = ϑ ( 1 + y 2 i λ ) ϑ 1 y 2 i λ log y 2 i , υ 2 ( λ ) = υ 2 ( h 1 , λ , ϑ ) λ = ϑ ( 1 + h 1 λ ) ϑ 1 h 1 λ log h 1 ,

υ 3 ( λ ) = υ 3 ( h 2 , λ , ϑ ) λ = ϑ ( 1 + h 2 λ ) ϑ 1 h 2 λ log h 2 , υ 1 ( ϑ ) = υ 1 ( y 2 i , λ , ϑ ) ϑ = ( 1 + y 2 i λ ) ϑ log ( 1 + y 2 i λ ) ,

υ 2 ( ϑ ) = υ 2 ( h 1 , λ , ϑ ) ϑ = ( 1 + h 1 λ ) ϑ log ( 1 + h 1 λ ) , υ 3 ( ϑ ) = υ 3 ( h 2 , λ , ϑ ) ϑ = ( 1 + h 2 λ ) ϑ log ( 1 + h 2 λ ) .

One may determine the ML estimator of acceleration factor ρ as a function of the parameters λ and ϑ by using (9) and for fixed value, as seen below.

(10) γ ˆ ( ρ ) = D 2 i = 1 D 2 log [ υ 1 ( y 2 i , λ , ϑ ) ] + ( n 2 D 2 ) log [ υ 3 ( h 2 , λ , ϑ ) ] .

Then inserting Eq. (10) in (7) and (8) and solving them numerically, we get the ML estimators λ ˆ and ϑ ˆ . It is important to note that these equations cannot be solved analytically. Some numerical methods, such as the Newton-Raphson technique, can be used to get the necessary estimate. The ML estimator ρ ˆ of ρ is then produced by inserting λ ˆ and ϑ ˆ in Eq. (10).

It might be more useful to find a range of values that, with a given probability, include the unknown parameters rather than point estimates for them. Interval estimates are the name given to these ranges. The Asy-CIs of the unknown parameters ζ = ( λ , ϑ , ρ ) T are constructed here by employing the asymptotic characteristics of the ML estimators. Using the large sample theory, we can determine that the asymptotic distribution of the ML estimators ζ ˆ = ( λ ˆ , ϑ ˆ , ρ ˆ ) T is a normal distribution with a variance–covariance matrix (VC-M) of I 1 ( ζ ) and a mean of ζ . To estimate I 1 ( ζ ) , where the asymptotic VC-M I 1 ( ζ ˆ ) is employed, which may be generated by inverting the observed Fisher information matrix. The asymptotic VC-M in this instance is as follows:

I 1 ( ζ ˆ ) = 2 l λ 2 2 l λ ϑ 2 l λ ρ 2 l ϑ 2 2 l ϑ ρ 2 l ρ 2 ζ ˆ = ( λ ˆ , ϑ ˆ , δ ˆ ) 1 = σ ˆ 11 2 σ ˆ 12 2 σ ˆ 13 2 σ ˆ 22 2 σ ˆ 23 2 σ ˆ 33 2 .

In Appendix 1, the second partial derivatives are provided. Asymptotic normality of the ML estimators allows for the construction of the 100(1 − δ )% Asy-CIs of λ , ϑ , and ρ , respectively.

λ ˆ ± z δ / 2 σ ˆ 11 , ϑ ˆ ± z δ / 2 σ ˆ 22 , ρ ˆ ± z δ / 2 σ ˆ 33 ,

where z δ / 2 is the upper δ / 2 th percentile point of the standard normal distribution.

4 Bayesian estimation

In this part, the Bayes estimators for the unknown parameters λ , ϑ , and the acceleration factor ρ of the BIIID are presented. It is assumed that the independent parameter ρ has a truncated gamma distribution ρ 1 ∼ gamma ( a 3 , b 3 ) , and that the random variables λ and ϑ have independent gamma prior distributions, λ ∼ Gamma ( a 1 , b 1 ) , and ϑ ∼ Gamma ( a 2 , b 2 ) . The joint prior of parameters and acceleration factor is as follows:

(11) π ( ζ ) λ a 1 1 ϑ a 2 1 ( ρ 1 ) a 3 1 e ( b 1 λ + b 2 ϑ + b 3 ( ρ 1 ) ) ,

where, a 1 , a 2 , a 3 , b 1 , b 2 , and b 3 are the hyper-parameters. Interestingly, the gamma prior density for the acceleration factor ρ was first used by DeGroot and Goel [40]. In the Bayesian analysis, independent gamma priors have been used because of the gamma distribution’s remarkable flexibility (see, for instance, Dey et al. [41] and Kundu and Howlader [42]). The likelihood function (6) and the joint prior distribution (11) are used to get the joint posterior distribution of λ , ϑ , and ρ using Bayes theorem.

(12) π ( ζ y ) = M λ a 1 + D 1 + D 2 1 ϑ a 2 + D 1 + D 2 1 ( ρ 1 ) a 3 + D 2 1 × e ( b 1 λ + b 2 ϑ + b 3 ( ρ 1 ) ) i = 1 D 1 y 1 i ( λ + 1 ) ( 1 + y 1 i λ ) ϑ 1 × i = 1 D 2 y 2 i ( λ + 1 ) ( 1 + y 2 i λ ) ϑ 1 [ 1 ( 1 + y 1 i λ ) ϑ ] [ 1 ( 1 + y 2 i λ ) ϑ ] ( ρ 1 ) 1 × [ 1 ( 1 + h 1 λ ) ϑ ] ( n 1 D 1 ) [ 1 ( 1 + h 2 λ ) ϑ ] ( ρ 1 ) ( n 2 D 2 ) ,

where,

M 1 = 0 0 0 π ( ζ y ̲ ) d λ d ϑ d ρ .

According to the Bayes method, selecting a loss function that matches each potential estimator will help determine which estimator is the best. In this case, estimates are obtained for two distinct categories of loss functions: symmetric and asymmetric loss functions. The first kind will be represented by the squared error loss function (SLF), and the second type will be illustrated by the use of the linear exponential loss function (LXF). The SLF is inappropriate when either an overestimation or an underestimating takes place. As an alternate choice to estimate the parameters in this situation, LXF can be used. When there is more substantial overestimation than underestimation, and vice versa, the LXF is helpful. Bayes estimates of the function U ( ζ ) = U ( λ , ϑ , ρ ) , under SLF and LXF, are given, respectively, by:

U ˜ SLF ( ζ ) = E ( U ( ζ ) ) ,

and

U ˜ LXF ( ζ ) = 1 q ln [ E ( e q U ( ζ ) ) ] , q 0 ,

where the parameter q represents the sign that indicates the direction of asymmetry. The integral given by Eq. (12) cannot generally be obtained in a closed form. Here, the MCMC method is used to generate samples from the posterior distributions, and the Bayesian estimators for each parameter and acceleration factor are then computed. Making a decision from several MCMC plans that are offered might be difficult. Notable subclasses of MCMC methods include Gibbs sampling and the more general Metropolis inside Gibbs samplers. With the MCMC methodology, we can always achieve an appropriate parameter interval estimate since we generate the probability intervals based on the empirical posterior distribution, which gives it an edge over the ML method. This is commonly unavailable while using an ML estimator. The MCMC samples may actually be used to completely quantify the posterior uncertainty about the parameters λ , ϑ , and ρ . This also applies to any function that depends on the inputs by employing a kernel estimate of the posterior distribution. The following are λ , ϑ , and ρ ’s conditional posterior densities: The conditional posterior densities of λ , ϑ , and ρ are as follows:

π 1 ( λ ϑ , ρ , y ) λ a 1 + D 1 + D 2 1 i = 1 D y i ( λ + 1 ) ( 1 + y i λ ) ϑ 1 × [ 1 ( 1 + y i λ ) ϑ ] ( ρ 1 1 ) 1 [ [ 1 ( 1 + h λ ) ϑ ] ( ρ 1 1 ) ] n D ,

π 2 ( ϑ λ , ρ , y ) ϑ a 2 + D 1 + D 2 1 i = 1 D ( 1 + y i λ ) ϑ 1 × [ 1 ( 1 + y i λ ) ϑ ] ( ρ 1 1 ) 1 [ [ 1 ( 1 + h λ ) ϑ ] ( ρ 1 1 ) ] n D ,

and

π 3 ( ρ ϑ , ρ , y ) ( ρ 1 ) a 3 + D 2 1 i = 1 D [ 1 ( 1 + y i λ ) ϑ ] ( ρ 1 1 ) 1 × [ 1 ( 1 + h λ ) ϑ ] ( ρ 1 1 ) ( n D ) .

The following MH-within-Gibbs sampling steps can be used to obtain samples of λ , ϑ , and ρ .

Step 1: Set the initial values λ ( 0 ) = λ ˆ , ϑ ( 0 ) = ϑ ˆ and ρ ( 0 ) = ρ ˆ .

Step 2: Set I = 1.

Step 3: Generate λ from a normal distribution with a mean ( λ ˆ ) and variance ( V λ ˆ ) , represented as N ( λ ˆ , V λ ˆ ) . Similarly, generate ϑ from the normal distribution with a mean ( ϑ ˆ ) and variance ( V θ ˆ ) , represented as N ( ϑ ˆ , V ϑ ˆ ) . Also, generate ρ from the normal distribution with a mean ( ρ ˆ ) and variance ( V ρ ˆ ) , represented as N ( ρ ˆ , V ρ ˆ ) .

Step 4: Obtain λ = min 1 , π ( λ ϑ ( I 1 ) , ρ ( I 1 ) , y ̲ ) π ( λ ( I 1 ) ϑ ( I 1 ) , ρ ( I 1 ) , y ̲ ) , ϑ = min 1 , π ( ϑ λ ( I 1 ) , ρ ( I 1 ) , y ̲ ) π ( ϑ ( I 1 ) λ ( I 1 ) , ρ ( I 1 ) , y ̲ ) , and ρ = min 1 , π ( ρ λ ( I 1 ) , ϑ ( I 1 ) , y ̲ ) π ( ρ ( I 1 ) λ ( I 1 ) , ϑ ( I 1 ) , y ̲ ) .

Step 5: Generate samples U j ; j = 1 , 2 , 3 from the uniform U(0, 1) distribution.

Step 6: If U 1 λ , U 2 ϑ , and U 3 ρ , then set λ ( I ) = λ , ϑ ( I ) = ϑ , ρ ( I ) = ρ ; otherwise λ ( I ) = λ ( I 1 ) , ϑ ( I ) = ϑ ( I 1 ) , and ρ ( I ) = ρ ( I 1 ) , respectively.

Step 7: Set I = I + 1.

Step 8: Repeat steps 3–7 B times and obtain λ ( I ) , ϑ ( I ) , and ρ ( I ) , for I = 1, 2, …, B.

5 Simulation study

This section explores the model’s performance through simulations. First, we present an illustrative example using a simulated dataset. Subsequently, we conduct a more extensive Monte Carlo simulation study. All results are accompanied by detailed discussions to explain their significance. It is important to note that finding exact solutions for the model parameters (mentioned earlier) is mathematically challenging due to the system of nonlinear equations involved. In our case, with three parameters, we were dealing with three complex equations. Therefore, we employed numerical methods to estimate the desired parameters. Since we were able to derive the first and second derivatives of the objective functions (functions used for parameter estimation), we employed Newton’s method to find the ML estimates (MLEs). Convergence issues can arise in optimization processes if researchers don’t pick good starting values. To address this, we randomly generated initial values close to the actual model parameters. For brevity, we won’t delve into the details of Newton’s method, which is known for its efficient convergence properties.

This section focuses on a simulation study designed to compare the performance of different parameter estimation methods and their corresponding confidence intervals in Tables 16. We’ll be evaluating two types of estimates: MLEs and Bayesian estimates (BEs). The comparison will involve two key metrics:

  • Mean squared error (MSE) and absolute bias (Abias): These metrics will be used to assess the accuracy of the estimates themselves. Lower MSE and Abias indicate estimates that are closer to the true parameter values on average.

  • Average length and coverage probability (CP): We’ll compare the average lengths of two types of CIs: Asy-CIs (LACI) and BCIs (LCCI). Additionally, we’ll examine their CP. Ideally, CIs should have an average length that captures the true parameter value within a certain confidence level (e.g., 95%) most of the time.

Table 1

Points estimation by ML and Bayesian methods for parameters: λ = 0.5 , ϑ = 0.6 , ρ = 0.6

(T 11, T 12), (T 21, T 22) ML SLF LXF (q = −1.25) LXF (q = 1.25)
r/n n Abias MSE Abias MSE Abias MSE Abias MSE
(0.2, 0.5), (5, 20) 0.6 20, 15 λ 0.0327 0.2650 0.0391 0.1132 0.0327 0.1067 0.0206 0.0956
ϑ 0.0332 0.2585 0.0419 0.1427 0.0331 0.1364 0.0164 0.1258
ρ 0.0580 0.3162 0.0715 0.2003 0.0580 0.1858 0.0326 0.1617
50, 40 λ 0.0108 0.1454 0.0130 0.0589 0.0108 0.0577 0.0064 0.0556
ϑ 0.0151 0.1626 0.0186 0.0752 0.0151 0.0736 0.0082 0.0708
ρ 0.0228 0.1897 0.0279 0.1047 0.0228 0.1012 0.0130 0.0952
100, 120 λ 0.0062 0.0883 0.0068 0.0447 0.0061 0.0444 0.0047 0.0438
ϑ 0.0045 0.1097 0.0055 0.0606 0.0044 0.0603 0.0023 0.0598
ρ 0.0079 0.1210 0.0091 0.0669 0.0079 0.0664 0.0053 0.0655
200, 150 λ 0.0034 0.0670 0.0038 0.0329 0.0034 0.0328 0.0026 0.0326
ϑ 0.0026 0.0840 0.0032 0.0441 0.0026 0.0440 0.0015 0.0438
ρ 0.0011 0.0902 0.0019 0.0531 0.0011 0.0529 0.0004 0.0527
(0.2, 0.5), (5, 20) 0.8 20, 15 λ 0.0325 0.2492 0.0384 0.1108 0.0324 0.1049 0.0210 0.0948
ϑ 0.0310 0.2553 0.0394 0.1284 0.0310 0.1226 0.0149 0.1131
ρ 0.0497 0.3087 0.0625 0.1712 0.0497 0.1590 0.0258 0.1389
50, 40 λ 0.0138 0.1363 0.0160 0.0516 0.0138 0.0597 0.0096 0.0574
ϑ 0.0117 0.1602 0.0150 0.0747 0.0117 0.0752 0.0052 0.0728
ρ 0.0261 0.1791 0.0270 0.1021 0.0260 0.1055 0.0164 0.0993
100, 120 λ 0.0053 0.0778 0.0060 0.0446 0.0053 0.0444 0.0040 0.0439
ϑ 0.0054 0.1048 0.0065 0.0592 0.0054 0.0589 0.0033 0.0583
ρ 0.0119 0.1117 0.0132 0.0656 0.0119 0.0650 0.0093 0.0640
200, 150 λ 0.0030 0.0599 0.0035 0.0311 0.0031 0.0310 0.0023 0.0309
ϑ 0.0019 0.0764 0.0025 0.0427 0.0019 0.0426 0.0008 0.0424
ρ 0.0044 0.0871 0.0052 0.0520 0.0044 0.0518 0.0028 0.0514
(1, 3), (14, 20) 0.8 20, 15 λ 0.0206 0.1769 0.0246 0.0846 0.0206 0.0816 0.0129 0.0764
ϑ 0.0323 0.2028 0.0390 0.1132 0.0323 0.1085 0.0194 0.1007
ρ 0.0504 0.2692 0.0619 0.1725 0.0504 0.1617 0.0289 0.1435
50, 40 λ 0.0094 0.1049 0.0108 0.0470 0.0093 0.0462 0.0063 0.0449
ϑ 0.0122 0.1267 0.0148 0.0651 0.0122 0.0639 0.0071 0.0619
ρ 0.0228 0.1637 0.0270 0.0998 0.0227 0.0967 0.0143 0.0912
100, 120 λ 0.0053 0.0648 0.0058 0.0338 0.0053 0.0336 0.0043 0.0332
ϑ 0.0043 0.0893 0.0052 0.0481 0.0043 0.0478 0.0024 0.0474
ρ 0.0054 0.0998 0.0066 0.0615 0.0054 0.0612 0.0031 0.0605
200, 150 λ 0.0032 0.0474 0.0035 0.0256 0.0032 0.0255 0.0026 0.0254
ϑ 0.0006 0.0635 0.0010 0.0359 0.0006 0.0359 0.0004 0.0357
ρ 0.0040 0.0768 0.0047 0.0480 0.0040 0.0478 0.0025 0.0474
Table 2

Intervals estimation by ML and Bayesian methods for parameters: λ = 0.5 , ϑ = 0.6 , ρ = 0.6

(T 11, T 12), (T 21, T 22) ML SLF LXF (q = −1.25) LXF (q = 1.25)
r/n N LACI CP LCCI CP LCCI CP LCCI CP
(0.2, 0.5), (5, 20) 0.6 20, 15 λ 0.3986 94.80% 0.4168 94.80% 0.3984 94.80% 0.3660 94.10%
ϑ 0.5190 95.10% 0.5351 94.10% 0.5190 94.10% 0.4890 95.10%
ρ 0.6926 94.59% 0.7336 94.80% 0.6922 94.60% 0.6212 95.00%
50, 40 λ 0.2223 94.99% 0.2253 94.90% 0.2222 95.00% 0.2166 95.00%
ϑ 0.2825 96.00% 0.2859 95.29% 0.2823 95.60% 0.2758 95.48%
ρ 0.3871 95.70% 0.3959 95.50% 0.3869 95.60% 0.3700 95.40%
100, 120 λ 0.1725 95.40% 0.1733 95.50% 0.1725 95.40% 0.1709 95.40%
ϑ 0.2359 96.69% 0.2365 95.47% 0.2358 95.70% 0.2344 95.70%
ρ 0.2587 96.30% 0.2599 95.83% 0.2586 95.83% 0.2560 95.50%
200, 150 λ 0.1280 96.09% 0.1283 95.61% 0.1280 95.60% 0.1274 95.60%
ϑ 0.1724 96.79% 0.1727 95.80% 0.1723 95.80% 0.1716 95.80%
ρ 0.2077 96.52% 0.2081 96.30% 0.2076 95.90% 0.2066 95.90%
(0.2, 0.5), (5, 20) 0.8 20, 15 λ 0.3916 94.70% 0.4074 94.79% 0.3915 94.70% 0.3627 95.70%
ϑ 0.4655 95.10% 0.4793 95.00% 0.4652 95.10% 0.4398 94.70%
ρ 0.5928 95.40% 0.6252 94.80% 0.5925 94.40% 0.5355 94.90%
50, 40 λ 0.2276 94.99% 0.2306 94.90% 0.2277 95.00% 0.2221 95.80%
ϑ 0.2917 95.40% 0.2851 95.20% 0.2915 95.40% 0.2849 95.20%
ρ 0.4010 95.59% 0.3900 94.90% 0.4010 94.60% 0.3840 95.10%
100, 120 λ 0.1728 95.19% 0.1734 95.39% 0.1728 95.60% 0.1715 95.90%
ϑ 0.2300 95.95% 0.2307 95.50% 0.2298 95.70% 0.2281 95.40%
ρ 0.2507 96.69% 0.2519 95.68% 0.2507 94.70% 0.2483 95.50%
200, 150 λ 0.1211 95.89% 0.1214 95.90% 0.1211 95.90% 0.1207 96.90%
ϑ 0.1670 96.60% 0.1673 95.70% 0.1670 95.90% 0.1663 95.60%
ρ 0.2025 96.99% 0.2030 95.80% 0.2024 95.00% 0.2013 95.90%
(1, 3), (14, 20) 0.8 20, 15 λ 0.3099 94.20% 0.3176 94.80% 0.3098 94.60% 0.2953 94.10%
ϑ 0.4066 95.50% 0.4167 95.20% 0.4065 95.50% 0.3877 95.60%
ρ 0.6029 94.99% 0.6314 94.50% 0.6026 95.00% 0.5512 95.30%
50, 40 λ 0.1776 94.50% 0.1794 95.25% 0.1776 95.50% 0.1743 95.40%
ϑ 0.2462 95.70% 0.2486 95.70% 0.2460 95.70% 0.2412 95.70%
ρ 0.3685 95.40% 0.3768 95.40% 0.3685 95.40% 0.3533 95.50%
100, 120 λ 0.1300 95.40% 0.1304 95.40% 0.1300 95.74% 0.1293 95.80%
ϑ 0.1868 95.79% 0.1874 95.80% 0.1868 95.90% 0.1856 95.80%
ρ 0.2390 95.95% 0.2399 95.90% 0.2389 95.90% 0.2369 95.90%
200, 150 λ 0.0994 96.40% 0.0995 95.90% 0.0994 96.40% 0.0990 96.40%
ϑ 0.1406 96.79% 0.1409 95.97% 0.1407 96.80% 0.1402 96.80%
ρ 0.1868 96.20% 0.1872 96.30% 0.1867 96.20% 0.1858 96.10%
Table 3

Points estimation by ML and Bayesian methods for parameters: λ = 2 , ϑ = 0.6 , ρ = 0.6

(T 11, T 12), (T 21, T 22) ML SLF LXF (q = −1.25) LXF (q = 1.25)
r/n n Abias MSE Abias MSE Abias MSE Abias MSE
(0.8, 1.8), (2.2, 5) 0.6 20, 15 λ 0.0114 0.5361 0.0190 0.3146 0.0158 0.3035 0.0669 0.2965
ϑ 0.0427 0.1951 0.0485 0.1201 0.0425 0.1151 0.0309 0.1064
ρ 0.0487 0.2431 0.0596 0.1779 0.0486 0.1658 0.0281 0.1461
50, 40 λ 0.0106 0.3677 0.0014 0.2248 0.0150 0.2221 0.0418 0.2203
ϑ 0.0204 0.1246 0.0228 0.0774 0.0202 0.0759 0.0153 0.0733
ρ 0.0251 0.1545 0.0293 0.0970 0.0251 0.0942 0.0170 0.0894
100, 120 λ 0.0032 0.2474 0.0005 0.1296 0.0032 0.1294 0.0084 0.1293
ϑ 0.0067 0.0881 0.0075 0.0487 0.0067 0.0484 0.0050 0.0480
ρ 0.0081 0.0967 0.0093 0.0572 0.0081 0.0568 0.0059 0.0561
200, 150 λ 0.0028 0.2005 0.0004 0.0958 0.0028 0.0957 0.0056 0.0957
ϑ 0.0028 0.0665 0.0032 0.0353 0.0028 0.0352 0.0019 0.0350
ρ 0.0031 0.0795 0.0037 0.0473 0.0030 0.0471 0.0016 0.0468
(0.8, 1.8), (2.2, 5) 0.8 20, 15 λ 0.0053 0.4384 0.0257 0.3066 0.0068 0.2958 0.0643 0.2884
ϑ 0.0417 0.1820 0.0476 0.1204 0.0417 0.1159 0.0303 0.1080
ρ 0.0450 0.2352 0.0605 0.1623 0.0502 0.1525 0.0308 0.1360
50, 40 λ 0.0046 0.3403 0.0188 0.2028 0.0061 0.1989 0.0188 0.1945
ϑ 0.0115 0.1126 0.0137 0.0683 0.0114 0.0674 0.0070 0.0657
ρ 0.0244 0.1541 0.0283 0.0916 0.0244 0.0889 0.0167 0.0841
100, 120 λ 0.0011 0.2256 0.0038 0.1197 0.0012 0.1192 0.0040 0.1186
ϑ 0.0066 0.0848 0.0080 0.0462 0.0072 0.0460 0.0056 0.0455
ρ 0.0077 0.0948 0.0089 0.0570 0.0078 0.0565 0.0056 0.0558
200, 150 λ 0.0010 0.1816 0.0032 0.0915 0.0011 0.0914 0.0007 0.0912
ϑ 0.0022 0.0630 0.0034 0.0341 0.0029 0.0340 0.0021 0.0339
ρ 0.0029 0.0779 0.0051 0.0447 0.0044 0.0445 0.0030 0.0442
(1.2, 3), (2.2, 5) 0.8 20, 15 λ 0.0191 0.3993 0.0034 0.2487 0.0185 0.2409 0.0608 0.2362
ϑ 0.0376 0.1696 0.0422 0.1031 0.0376 0.0987 0.0286 0.0909
ρ 0.0299 0.2053 0.0378 0.1322 0.0298 0.1230 0.0147 0.1076
50, 40 λ 0.0086 0.3219 0.0206 0.1952 0.0088 0.1917 0.0145 0.1876
ϑ 0.0155 0.1101 0.0176 0.0627 0.0154 0.0616 0.0112 0.0596
ρ 0.0198 0.1463 0.0234 0.0832 0.0198 0.0810 0.0128 0.0771
100, 120 λ 0.0021 0.2282 0.0047 0.1162 0.0022 0.1160 0.0028 0.1160
ϑ 0.0064 0.0798 0.0072 0.0447 0.0064 0.0444 0.0049 0.0440
ρ 0.0068 0.0890 0.0078 0.0537 0.0067 0.0533 0.0046 0.0526
200, 150 λ 0.0042 0.1792 0.0028 0.0892 0.0041 0.0892 0.0067 0.0892
ϑ 0.0032 0.0597 0.0036 0.0335 0.0032 0.0334 0.0024 0.0332
ρ 0.0030 0.0734 0.0037 0.0449 0.0030 0.0448 0.0016 0.0444
Table 4

Intervals estimation by ML and Bayesian methods for parameters: λ = 2 , ϑ = 0.6 , ρ = 0.6

(T 11, T 12), (T 21, T 22) ML SLF LXF (q = −1.25) LXF (q = 1.25)
r/n n LACI CP LCCI CP LCCI CP LCCI CP
(0.8, 1.8), (2.2, 5) 0.6 20, 15 λ 1.1878 94.19% 1.2314 94.40% 1.1895 94.30% 1.1330 94.20%
ϑ 0.4194 94.79% 0.4308 94.70% 0.4196 94.80% 0.3993 94.90%
ρ 0.6219 95.00% 0.6576 94.60% 0.6216 94.60% 0.5622 94.60%
50, 40 λ 0.8676 94.40% 0.8815 95.40% 0.8692 95.40% 0.8485 95.40%
ϑ 0.2868 95.30% 0.2902 95.20% 0.2870 95.30% 0.2810 95.40%
ρ 0.3563 95.20% 0.3625 95.20% 0.3561 95.20% 0.3441 95.20%
100, 120 λ 0.5076 95.40% 0.5081 95.70% 0.5074 95.90% 0.5061 95.83%
ϑ 0.1883 95.90% 0.1887 96.00% 0.1882 95.90% 0.1871 95.90%
ρ 0.2207 95.50% 0.2215 95.80% 0.2206 95.39% 0.2189 95.91%
200, 150 λ 0.3754 95.89% 0.3757 95.90% 0.3753 96.39% 0.3745 95.97%
ϑ 0.1376 95.99% 0.1378 96.29% 0.1376 96.49% 0.1371 96.70%
ρ 0.1844 96.79% 0.1850 96.19% 0.1844 95.80% 0.1833 96.80%
(0.8, 1.8), (2.2, 5) 0.8 20, 15 λ 1.1604 94.99% 1.1982 94.90% 1.1601 94.90% 1.1026 94.20%
ϑ 0.4243 94.99% 0.4336 95.10% 0.4241 95.00% 0.4066 95.30%
ρ 0.5651 95.20% 0.5906 95.10% 0.5649 95.20% 0.5195 95.37%
50, 40 λ 0.7799 95.40% 0.7918 95.40% 0.7796 95.40% 0.7591 95.00%
ϑ 0.2603 95.50% 0.2626 95.40% 0.2603 95.50% 0.2560 95.50%
ρ 0.3354 95.80% 0.3417 95.80% 0.3354 95.80% 0.3235 95.70%
100, 120 λ 0.4679 95.59% 0.4692 95.63% 0.4677 95.60% 0.4650 95.40%
ϑ 0.1781 95.95% 0.1786 95.63% 0.1781 95.73% 0.1771 95.83%
ρ 0.2197 95.95% 0.2207 95.94% 0.2197 95.94% 0.2177 95.84%
200, 150 λ 0.3577 96.99% 0.3588 96.00% 0.3584 95.90% 0.3575 96.10%
ϑ 0.1330 96.29% 0.1332 95.90% 0.1330 95.90% 0.1326 95.90%
ρ 0.1737 96.40% 0.1741 96.50% 0.1736 96.30% 0.1728 95.90%
(1.2, 3), (2.2, 5) 0.8 20, 15 λ 0.9397 94.39% 0.9752 94.40% 0.9418 94.30% 0.8952 94.60%
ϑ 0.3580 94.89% 0.3688 95.00% 0.3580 94.90% 0.3383 94.80%
ρ 0.4680 95.70% 0.4968 96.00% 0.4679 95.70% 0.4179 95.30%
50, 40 λ 0.7508 96.10% 0.7612 96.10% 0.7509 96.10% 0.7334 96.00%
ϑ 0.2337 94.99% 0.2359 95.20% 0.2338 95.00% 0.2297 95.20%
ρ 0.3080 95.20% 0.3131 95.20% 0.3078 95.20% 0.2981 95.20%
100, 120 λ 0.4552 95.50% 0.4554 95.30% 0.4550 95.40% 0.4547 95.30%
ϑ 0.1724 95.60% 0.1729 95.60% 0.1724 95.60% 0.1714 95.70%
ρ 0.2072 95.30% 0.2083 95.00% 0.2073 95.30% 0.2054 95.20%
200, 150 λ 0.3493 95.40% 0.3496 95.50% 0.3493 95.40% 0.3489 95.20%
ϑ 0.1303 95.40% 0.1304 95.50% 0.1303 95.40% 0.1299 95.40%
ρ 0.1752 96.20% 0.1757 96.20% 0.1751 96.20% 0.1741 96.30%
Table 5

Points estimation by ML and Bayesian methods for parameters: λ = 2 , ϑ = 1.6 , ρ = 1.5

(T 11, T 12), (T 21, T 22) ML SLF LXF (q = −1.25) LXF (q = 1.25)
r/n n Abias MSE Abias MSE Abias MSE Abias MSE
(1.4, 3.5), (1.5, 4) 0.6 20, 15 λ 0.0209 0.3769 0.0117 0.2413 0.0210 0.1400 0.0389 0.1435
ϑ 0.0317 0.3435 0.0399 0.1551 0.0316 0.1465 0.0157 0.1336
ρ 0.0401 0.4721 0.0028 0.1766 0.0401 0.1763 0.0632 0.1833
50, 40 λ 0.0050 0.2487 0.0021 0.1255 0.0049 0.1244 0.0174 0.1239
ϑ 0.0088 0.2070 0.0137 0.1053 0.0086 0.1035 0.0014 0.1010
ρ 0.0114 0.3284 0.0024 0.1758 0.0116 0.1747 0.0297 0.1716
100, 120 λ 0.0043 0.1692 0.0020 0.1023 0.0041 0.1021 0.0084 0.1021
ϑ 0.0032 0.1532 0.0051 0.0910 0.0032 0.0906 0.0004 0.0899
ρ 0.0032 0.2317 0.0024 0.1205 0.0034 0.1200 0.0013 0.1191
200, 150 λ 0.0022 0.1319 0.0010 0.0780 0.0022 0.0780 0.0045 0.0780
ϑ 0.0028 0.1134 0.0039 0.0690 0.0028 0.0689 0.0003 0.0687
ρ 0.0031 0.1957 0.0024 0.0939 0.0031 0.0938 0.0007 0.0937
(1.4, 3.5), (1.5, 4) 0.8 20, 15 λ 0.0104 0.4120 0.0272 0.2008 0.0101 0.1935 0.0231 0.1859
ϑ 0.0382 0.3738 0.0535 0.1499 0.0386 0.1887 0.0101 0.1738
ρ 0.0233 0.5195 0.0039 0.1259 0.0221 0.2486 0.0709 0.2445
50, 40 λ 0.0091 0.2390 0.0226 0.1234 0.0091 0.1312 0.0081 0.1275
ϑ 0.0138 0.2080 0.0205 0.1019 0.0138 0.1171 0.0007 0.1140
ρ 0.0066 0.3260 0.0037 0.1162 0.0064 0.1979 0.0323 0.1949
100, 120 λ 0.0046 0.1510 0.0066 0.0977 0.0045 0.0974 0.0043 0.0969
ϑ 0.0003 0.1465 0.0021 0.0896 0.0031 0.0894 0.0006 0.0892
ρ 0.0033 0.2368 0.0036 0.1124 0.0034 0.1236 0.0020 0.1231
200, 150 λ 0.0001 0.1101 0.0010 0.0726 0.0009 0.0726 0.0022 0.0724
ϑ 0.0002 0.1055 0.0010 0.0650 0.0019 0.0649 0.0004 0.0649
ρ 0.0004 0.1881 0.0021 0.0937 0.0007 0.0935 0.0018 0.0932
(1.8, 4), (1.9, 4.5) 0.8 20, 15 λ 0.0047 0.3412 0.0045 0.1337 0.0049 0.1303 0.0230 0.1293
ϑ 0.0228 0.3294 0.0313 0.1415 0.0229 0.1344 0.0069 0.1244
ρ 0.0471 0.4379 0.0336 0.1176 0.0464 0.1776 0.0703 0.1879
50, 40 λ 0.0007 0.2282 0.0045 0.1028 0.0046 0.1018 0.0112 0.1013
ϑ 0.0123 0.2068 0.0168 0.1032 0.0122 0.1010 0.0033 0.0979
ρ 0.0200 0.3188 0.0118 0.1052 0.0199 0.1503 0.0358 0.1507
100, 120 λ 0.0005 0.1461 0.0029 0.0915 0.0042 0.0915 0.0086 0.0914
ϑ 0.0020 0.1457 0.0038 0.0844 0.0020 0.0841 0.0015 0.0836
ρ 0.0077 0.2141 0.0053 0.1014 0.0077 0.1139 0.0124 0.1138
200, 150 λ 0.0001 0.1012 0.0023 0.0695 0.0013 0.0695 0.0008 0.0694
ϑ 0.0009 0.1006 0.0017 0.0630 0.0010 0.0630 0.0013 0.0630
ρ 0.0055 0.1784 0.0041 0.0893 0.0054 0.0894 0.0080 0.0895
Table 6

Intervals estimation by ML and Bayesian methods for parameters: λ = 2 , ϑ = 1.6 , ρ = 1.5

(T 11, T 12), (T 21, T 22) ML SLF LXF (q = −1.25) LXF (q = 1.25)
r/n n LACI CP LCCI CP LCCI CP LCCI CP
(1.4, 3.5), (1.5, 4) 0.6 20, 15 λ 0.5428 93.59% 0.5521 93.50% 0.5427 93.60% 0.5419 93.80%
ϑ 0.5613 93.09% 0.5877 93.10% 0.5612 93.10% 0.5204 92.60%
ρ 0.6734 92.09% 0.6840 92.80% 0.6731 92.10% 0.6748 92.10%
50, 40 λ 0.4875 93.89% 0.4921 94.20% 0.4873 93.90% 0.4810 94.70%
ϑ 0.4036 93.49% 0.4097 93.20% 0.4044 93.40% 0.3962 93.60%
ρ 0.6833 94.59% 0.6796 95.00% 0.6684 94.60% 0.6629 95.00%
100, 120 λ 0.3999 94.59% 0.4009 94.70% 0.4003 94.60% 0.3991 95.00%
ϑ 0.3551 95.10% 0.3562 95.30% 0.3550 95.10% 0.3525 95.20%
ρ 0.4701 95.50% 0.4722 95.50% 0.4704 95.50% 0.4671 95.30%
200, 150 λ 0.3058 95.29% 0.3059 95.30% 0.3057 94.93% 0.3054 94.30%
ϑ 0.2701 95.89% 0.2703 95.90% 0.2701 95.90% 0.2696 94.90%
ρ 0.3678 95.95% 0.3682 95.60% 0.3676 95.95% 0.3666 95.40%
(1.4, 3.5), (1.5, 4) 0.8 20, 15 λ 0.7570 94.19% 0.7801 94.50% 0.7577 94.20% 0.7236 94.70%
ϑ 0.7225 94.89% 0.7505 94.80% 0.7242 94.80% 0.6803 94.60%
ρ 0.9618 94.29% 1.0144 94.40% 0.9711 94.50% 0.9176 94.20%
50, 40 λ 0.5113 95.70% 0.5179 95.80% 0.5114 95.70% 0.5001 95.80%
ϑ 0.4562 94.69% 0.4613 94.80% 0.4559 94.70% 0.4470 94.50%
ρ 0.7755 94.59% 0.7896 94.50% 0.7757 94.60% 0.7537 94.60%
100, 120 λ 0.3815 94.69% 0.3823 94.70% 0.3815 94.70% 0.3801 94.60%
ϑ 0.3509 95.10% 0.3513 95.50% 0.3507 95.10% 0.3496 95.20%
ρ 0.4846 94.89% 0.4853 94.70% 0.4844 94.90% 0.4827 95.00%
200, 150 λ 0.2847 94.49% 0.2849 94.50% 0.2846 94.50% 0.2840 94.50%
ϑ 0.2543 96.10% 0.2547 96.10% 0.2545 96.10% 0.2541 96.00%
ρ 0.3658 95.20% 0.3673 95.10% 0.3667 95.20% 0.3655 95.20%
(1.8, 4), (1.9, 4.5) 0.8 20, 15 λ 0.5111 91.47% 0.5241 91.80% 0.5105 91.50% 0.4989 91.80%
ϑ 0.5198 92.47% 0.5413 92.90% 0.5192 92.50% 0.4870 92.10%
ρ 0.6695 93.07% 0.6785 93.20% 0.6722 93.10% 0.6834 93.10%
50, 40 λ 0.3993 93.19% 0.4027 93.40% 0.3991 93.20% 0.3950 93.40%
ϑ 0.3936 92.79% 0.3992 92.80% 0.3934 92.70% 0.3839 92.30%
ρ 0.5848 92.99% 0.5924 93.20% 0.5844 93.00% 0.5742 93.20%
100, 120 λ 0.3583 94.59% 0.3589 94.50% 0.3582 94.60% 0.3570 94.70%
ϑ 0.3298 94.69% 0.3307 94.70% 0.3297 94.70% 0.3279 94.50%
ρ 0.4460 94.39% 0.4472 94.40% 0.4458 94.40% 0.4435 94.60%
200, 150 λ 0.2725 94.79% 0.2726 94.80% 0.2724 94.80% 0.2721 94.70%
ϑ 0.2472 94.89% 0.2473 94.90% 0.2471 94.90% 0.2468 94.80%
ρ 0.3498 94.59% 0.3500 94.50% 0.3499 94.70% 0.3497 94.70%

The following procedure outlines how we’ll conduct the simulation study:

Step 1: Assign values for n 1, n 2, r 1, r 2, T 11, T 12, T 21, and T 22.

Step 2: Using the given prior parameters λ , ϑ , and ρ , generate λ , and ϑ from the gamma distributions ( a 1 , b 1 ) , and ( a 2 , b 2 ) while ρ has a truncated gamma distribution ρ 1 ∼ gamma ( a 3 , b 3 ) .

Step 3: Generate two random samples from the CDFs F 1(y) and F 2(y), as defined in Eqs. (2) and (4), and apply the GTII−HCS’s technique to obtain the two samples.

Step 4: Solve the nonlinear Eqs. (7) and (8) using the Newton-Raphson technique to obtain the MLEs of the parameters λ , ϑ , and ρ .

Step 5: Establish the Asy-CIs using asymptotic VC-M of the estimators.

Step 6: Use the MH algorithm to generate an iterative sequence of 11,000 random samples with N = 11,000 and M = 1,000.

Step 7: Calculate the BEs of λ , ϑ , and ρ based on the LXF and SLF.

Step 8: Repeat Steps 2 to 8 1,000 times for various sample sizes and censoring schemes and calculate the MSEs and Abias of all the estimates.

Tables 1, 3 and 5 present the MSEs and Abias of the MLEs and BEs for the parameters λ , ϑ , and ρ and are evaluated against the SLF and LXF (with varying q values) loss functions. Tables 2, 4 and 6 show the LCI and the corresponding 95% CPs derived from the asymptotic distributions of MLEs and the credible intervals. The prior parameters were determined using the elective hyperparameter method proposed by Dey et al. [41].

The analysis of data in Tables 16 reveals several trends regarding the performance of different estimation methods:

  1. Accuracy improves with sample size: As the number of samples (n) increases, the MSEs and Abias generally decrease for estimation methods. This indicates that larger datasets lead to more accurate estimates of the underlying parameters.

  2. Observed failure time matters: For a fixed sample size, using datasets with higher observed failure times results in lower MSEs and Abias for the estimated parameters. This suggests that data with more extreme values can improve estimation accuracy.

  3. Bayesian estimates with LXF: The BEs obtained using the LXF (with q = 1.25) consistently outperform other methods in terms of MSEs and Abias. This suggests that the LXF might be a particularly effective choice for this specific scenario.

  4. Credible intervals offer advantages: When comparing the LCI and CP of different CIs, credible intervals show smaller LCCI and CPs closer to the desired level (95%) compared to normal approximation CIs, which LACI and CP. This suggests that BCIs might be a more reliable choice for uncertainty quantification in this setting.

6 Data analysis

In this section, two real datasets for oil breakdown time analysis are introduced to show how the model using ML and Bayesian estimation methods works in practice based on real data from Nelson [4]. This study analyzes oil breakdown times for insulating fluid under different stress levels.

Dataset I: This dataset comprises breakdown times measured under various constant high voltage levels. For illustrative purposes, the data at 30 kV is assumed to represent normal use conditions, while the data at 32 kV is considered accelerated data. The 30 kV dataset is considered representative of normal stress conditions as follows: 7.74, 17.05, 20.46, 21.02, 22.66, 43.40, 47.30, 139.07, 144.12, 175.88, and 194.90. While the 32 kV dataset is considered representative accelerated stress conditions as follows: 0.27, 0.40, 0.69, 0.79, 2.75, 3.91, 9.88, 13.95, 15.93, 27.80, 53.24, 82.85, 89.29, 100.58, and 215.10.

Dataset II: This dataset focuses on breakdown times at two specific stress levels: 34 kV and 36 kV. The 34 kV dataset is considered representative of normal stress conditions as follows: 0.19, 0.78, 0.96, 1.31, 2.78, 3.16, 4.15, 4.67, 4.85, 6.50, 7.35, 8.01, 8.27, 12.06, 31.75, 32.52, 33.91, 36.71, and 72.89. While the 36 kV data is considered representative accelerated stress conditions as follows: 0.35, 0.59, 0.96, 0.99, 1.69, 1.97, 2.07, 2.58, 2.71, 2.9, 3.67, 3.99, 5.35, 13.77, and 25.5.

To analyze these datasets, the goodness-of-fit of the BIIID was initially assessed using the one-sample Kolmogorov–Smirnov (K-S) test. Table 7 presents the MLEs and their standard errors (StEr) under used and accelerated conditions. It also includes the K-S distance (KSD) with the corresponding p-value (PVKS) and some of the most famous statistical measures, such as Akaike’s information criterion (AIC), Bayesian information criterion (BIC), corrected AIC (CAIC), Hannan–Quinn information criterion (HQIC), Anderson–Darling (AD), and Cramer–von Mises (CVM) calculated based on the MLEs for each dataset. The goodness-of-fit test suggests that, irrespective of the estimator used, the BIIID is an appropriate life model for the analyzed datasets. Figures 14 illustrate the total time on test plots compared to the HF plot, the empirical CDF versus the fitted CDF, the histogram with the PDF line, as well as the quantile-quantile and probability-probability plots of the BIIID for each dataset, respectively.

Table 7

The KS statistics and some statistical measures for the oil breakdown, assuming complete data

kV Estimates StEr AIC CAIC BIC HQIC CVM AD KSD PVKS
30 λ 1.0703 0.2388 121.0621 122.5621 121.8579 120.5604 0.0648 0.4582 0.2015 0.6925
ϑ 34.8903 25.6433
32 λ 0.0811 0.0836 137.4472 139.6290 139.5714 137.4246 0.0406 0.3104 0.1407 0.8885
ϑ 15.3974 14.0132
ρ 6737.773 65473.326
34 λ 0.8260 0.1332 143.0185 143.7685 144.9074 143.3382 0.0604 0.4150 0.1235 0.9002
ϑ 3.0668 0.7256
36 λ 1.0538 0.8830 77.4611 79.6429 79.5853 77.4385 0.0356 0.2168 0.1083 0.9864
ϑ 2.9483 2.3280
ρ 1.5475 2.5319
Figure 1 
               Some fitting plots of the BIIID for oil breakdown data with 30 kV.
Figure 1

Some fitting plots of the BIIID for oil breakdown data with 30 kV.

Figure 2 
               Some fitting plots of the BIIID for oil breakdown data with 32 kV.
Figure 2

Some fitting plots of the BIIID for oil breakdown data with 32 kV.

Figure 3 
               Some fitting plots of the BIIID for oil breakdown data with 34 kV.
Figure 3

Some fitting plots of the BIIID for oil breakdown data with 34 kV.

Figure 4 
               Some fitting plots of the BIIID for oil breakdown data with 36 kV.
Figure 4

Some fitting plots of the BIIID for oil breakdown data with 36 kV.

Table 8 discusses MLE and BE for dataset I, where normal use condition (30 kV) and accelerated stress condition (32 kV) with different values of times and different censored sizes. We are concluding that the BE has the smallest value of StEr and a smaller LCI than MLE. We estimated the D 1 , h 1 , D 2 , and D 2 GTII−HCS based on CSPALT. Figure 5 discusses likelihood profile plots for parameters with r 1 = 10, r 2 = 12, (T 11, T 12) = (50, 120), and (T 21, T 22) = (20, 60) to confirm the likelihood estimates have maximum and unique solutions.

Table 8

MLEs and BEs for Dataset I

r 1, r 2 (T 11, T 12), (T 21, T 22) Estimates StEr Lower Upper LCI D 1 , h 1 D 2 , h 2
7, 8 (40, 100), (12, 40) ML 0.4525 0.0871 0.2818 0.6233 0.3415 7, 47.3 8, 13.95
4.2424 0.9846 2.3126 6.1722 3.8596
2.0583 1.1426 −0.1812 4.2977 4.4789
Bayesian 0.4629 0.0831 0.3152 0.6382 0.3229
4.2653 0.8722 2.5826 6.0238 3.4412
1.9395 0.8465 0.5368 3.6748 3.1381
7, 12 (40, 100), (12, 40) ML 0.4464 0.0874 0.2752 0.6177 0.3425 7, 47.3 10, 40
4.0723 0.9138 2.2812 5.8634 3.5821
1.7981 0.9022 0.0299 3.5664 3.5366
Bayesian 0.4500 0.0840 0.2900 0.6124 0.3224
4.1798 0.8274 2.6655 5.9024 3.2369
1.9486 0.7603 0.6512 3.4412 2.7901
10, 12 (40, 100), (12, 40) ML 0.4218 0.0822 0.2608 0.5829 0.3221 7, 100 10, 40
4.1317 0.9222 2.3241 5.9392 3.6151
1.9832 1.0050 0.0133 3.9530 3.9396
Bayesian 0.4312 0.0785 0.2872 0.5991 0.3118
4.1480 0.8279 2.6167 5.8130 3.1962
2.0193 0.8072 0.6469 3.5833 2.9363
10, 12 (50, 120), (20, 60) ML 0.4161 0.0808 0.2578 0.5745 0.3166 7, 100 10, 40
4.1491 0.9089 2.3677 5.9305 3.5628
2.0343 0.9998 0.0747 3.9939 3.9192
Bayesian 0.4203 0.0747 0.2781 0.5677 0.2897
4.2227 0.8335 2.7154 5.9073 3.1919
2.1427 0.8283 0.7292 3.8388 3.1096
Figure 5 
               Likelihood profile plots for parameters: r
                  1 = 10, r
                  2 = 12, (T
                  11, T
                  12) = (50, 120), and (T
                  21, T
                  22) = (20, 60).
Figure 5

Likelihood profile plots for parameters: r 1 = 10, r 2 = 12, (T 11, T 12) = (50, 120), and (T 21, T 22) = (20, 60).

Table 9 discusses MLE and BE for dataset II, where normal use condition (34 kV) and accelerated stress condition (36 kV) with different values of times and different censored sizes. We are concluding that the BE has the smallest value of StEr and a smaller LCI than MLE. We estimated D 1 , h 1 , D 2 , and h 2 GTII−HCS based on CSPALT. Figure 6 discusses likelihood profile plots for parameters with r 1 = 10, r 2 = 10, (T 11, T 12) = (5, 8), and (T 21, T 22) = (2.5, 3.5) to confirm the likelihood estimates have maximum and unique solutions.

Table 9

MLE and BE for Dataset II

r 1, r 2 (T 11, T 12), (T 21, T 22) Estimates StEr Lower Upper LCI D 1 , h 1 D 2 , h 2
12, 10 (10, 21), (2.5, 4) ML 0.7775 0.1252 0.5320 1.0229 0.4910 14, 21 8, 4
3.1911 0.6394 1.9380 4.4442 2.5063
1.5007 0.7065 0.1160 2.8854 2.7694
Bayesian 0.7754 0.1211 0.5591 1.0322 0.4730
3.2650 0.5967 2.1395 4.4449 2.3054
1.6506 0.6704 0.4787 3.0498 2.5710
12, 10 (10, 15), (2.5, 3.5) ML 0.8035 0.1307 0.5474 1.0596 0.5122 14, 15 7, 3.5
3.1292 0.6362 1.8822 4.3762 2.4940
1.3326 0.6547 0.0494 2.6158 2.5664
Bayesian 0.7961 0.1239 0.5674 1.0421 0.4747
3.2614 0.6275 2.1560 4.5741 2.4181
1.5375 0.6494 0.3383 2.8957 2.5575
5, 5 (5, 8), (2.5, 3.5) ML 0.7962 0.1340 0.5336 1.0587 0.5251 11, 8 10, 3.5
3.3263 0.6435 2.0650 4.5877 2.5227
2.3940 1.1121 0.2144 4.5736 4.3593
Bayesian 0.7991 0.1308 0.5562 1.0614 0.5053
3.3603 0.6117 2.1467 4.5444 2.3976
2.4509 0.9853 0.8368 4.4390 3.6022
10, 10 (5, 8), (2.5, 3.5) ML 0.8074 0.1391 0.5348 1.0800 0.5451 10, 6.5 10, 2.9
3.4245 0.6650 2.1212 4.7279 2.6067
2.7017 1.2933 0.1669 5.2365 5.0696
Bayesian 0.8122 0.1363 0.5631 1.0908 0.5277
3.4904 0.6047 2.3413 4.6321 2.2908
2.8277 1.1439 0.8727 5.0707 4.1979
Figure 6 
               Likelihood profile plots for parameters: r
                  1 = 10, r
                  2 = 10, (T
                  11, T
                  12) = (5, 8), and (T
                  21, T
                  22) = (2.5, 3.5).
Figure 6

Likelihood profile plots for parameters: r 1 = 10, r 2 = 10, (T 11, T 12) = (5, 8), and (T 21, T 22) = (2.5, 3.5).

Figures 7 and 8 show the results of an MCMC simulation for estimating the posterior distribution of two parameters. The MCMC is a computational method used to sample from complex probability distributions. Top row: Presents trace plots for three parameters, visualizing the values generated by the MCMC simulation across iterations. Ideally, trace plots should display a lack of trend and reach stationarity (a stable distribution) after an initial “burn-in” period where the initial samples are discarded. Bottom row: Shows the posterior densities of the three parameters, illustrating the probability distribution of each parameter after incorporating the data and prior information into the MCMC analysis.

Figure 7 
               MCMC plots r
                  1 = 10, r
                  2 = 12, (T
                  11, T
                  12) = (50, 120), and (T
                  21, T
                  22) = (20, 60).
Figure 7

MCMC plots r 1 = 10, r 2 = 12, (T 11, T 12) = (50, 120), and (T 21, T 22) = (20, 60).

Figure 8 
               MCMC plots for r
                  1 = 10, r
                  2 = 10, (T
                  11, T
                  12) = (5, 8), and (T
                  21, T
                  22) = (2.5, 3.5).
Figure 8

MCMC plots for r 1 = 10, r 2 = 10, (T 11, T 12) = (5, 8), and (T 21, T 22) = (2.5, 3.5).

7 Concluding remarks

In order to reduce the testing length, units are subjected to more demanding conditions during ALTs. ALTs or PALTs are crucial for life testing research since they save money and time. PALTs are carried out in situations when the findings of ALT cannot be extended to regular conditions. The CSPALT proposed in this work is based on the premise that units’ lifespan under usage conditions follows the BIIID and is based on a GTII-HCS. Under typical use conditions, the ML approach is used to derive the estimates of the BIIID’s parameters and accelerated factor. Using the MCMC method, the Bayesian estimates are generated based on symmetric and asymmetric loss functions. Additionally, Asy-CIs and BCIs have been produced. To evaluate the proposed methodology, simulation studies with varying censoring strategies and sample sizes have been conducted. Our conclusion from the simulation dataset is that, in terms of MSEs and Abias, the BEs derived with the LXF (q = 1.25) regularly beat alternative approaches. It would appear from this that the LXF may be an especially good option in this case. Bayesian credible intervals display reduced average length and coverage probabilities nearer the intended level (95%) when compared with the corresponding Asy-CIs. In this context, it appears that BCIs might be a more reliable choice for quantifying uncertainty. Two data sets were then examined to demonstrate the effectiveness of the suggested strategies.

Acknowledgments

This research is supported by Ongoing Research Funding Program (ORF-2025-548), King Saud University, Riyadh, Saudi Arabia.

  1. Funding information: This research is supported by Ongoing Research Funding Program (ORF-2025-548), King Saud University, Riyadh, Saudi Arabia.

  2. Author contributions: All authors have accepted responsibility for the entire content of this manuscript and approved its submission.

  3. Conflict of interest: The authors state no conflict of interest.

  4. Data availability statement: All data generated or analysed during this study are included in this published article.

Appendix 1

The elements of the Fisher information matrix are given by:

2 l λ 2 = D 1 + D 2 λ 2 i = 1 D 1 ( ϑ + 1 ) y 1 i λ ( log y 1 i ) 2 ( 1 + y 1 i λ ) 2 i = 1 D 2 ( ϑ + 1 ) y 2 i λ ( log y 2 i ) 2 ( 1 + y 2 i λ ) 2 + i = 1 D 2 υ 1 ( λ ) ( ρ 1 ) υ 1 ( y 2 i , λ , ϑ ) i = 1 D 2 ( ρ 1 ) υ 1 ( λ ) 2 ( υ 1 ( y 2 i , λ , ϑ ) ) 2 + ( n 1 D 1 ) υ 2 ( λ ) υ 2 ( h 1 , λ , ϑ ) ( n 1 D 1 ) υ 2 ( λ ) 2 ( υ 2 ( h 1 , λ , ϑ ) ) 2 ( n 2 D 2 ) υ 3 ( λ ) 2 ( υ 3 ( h 2 , λ , ϑ ) ) 2 + ( n 2 D 2 ) υ 3 ( λ ) υ 3 ( h 2 , λ , ϑ ) ,

2 l ϑ 2 = D 1 + D 2 ϑ 2 i = 1 D 2 ( ρ 1 ) ( 1 + y 2 i λ ) ϑ ( log ( 1 + y 2 i λ ) ) 2 υ 1 ( y 2 i , λ , ϑ ) ( n 1 D 1 ) ( 1 + h 1 λ ) ϑ ( log ( 1 + h 1 λ ) ) 2 υ 2 ( h 1 , λ , ϑ ) i = 1 D 2 ( ρ 1 ) υ 1 ( ϑ ) 2 ( υ 1 ( y 2 i , λ , ϑ ) ) 2 ( n 1 D 1 ) υ 2 ( ϑ ) 2 υ 2 ( h 1 , λ , ϑ ) ( n 2 D 2 ) ( 1 + h 2 λ ) ϑ ( log ( 1 + h 2 λ ) ) 2 υ 3 ( h 2 , λ , ϑ ) ( n 2 D 2 ) υ 3 ( ϑ ) 2 υ 3 ( h 2 , λ , ϑ ) ,

2 l ϑ λ = 2 l λ ϑ = i = 1 D 1 log y 1 i 1 + y 1 i λ + i = 1 D 2 log y 2 i 1 + y 2 i λ + i = 1 D 2 ( ρ 1 ) υ 1 ( ϑ λ ) υ 1 ( y 2 i , λ , ϑ ) i = 1 D 2 ( ρ 1 ) υ 1 ( λ ) υ 1 ( ϑ ) ( υ 1 ( y 2 i , λ , ϑ ) ) 2 + ( n 1 D 1 ) υ 2 ( ϑ λ ) υ 2 ( h 1 , λ , ϑ ) ( n 1 D 1 ) υ 2 ( λ ) υ 2 ( ϑ ) υ 2 ( h 1 , λ , ϑ ) + ( n 2 D 2 ) ρ υ 3 ( ϑ λ ) υ 3 ( h 2 , λ , ϑ ) ( n 2 D 2 ) υ 3 ( λ ) υ 3 ( ϑ ) υ 3 ( h 2 , λ , ϑ ) ,

2 l ρ λ = 2 l λ ρ = i = 1 D 2 υ 1 ( λ ) [ υ 1 ( y 2 i , λ , ϑ ) ] + ( n 2 D 2 ) υ 3 ( λ ) υ 3 ( h 2 , λ , ϑ ) , 2 l ρ ϑ = 2 l ϑ ρ = i = 1 D 2 υ 1 ( ϑ ) [ υ 1 ( y 2 i , λ , ϑ ) ] + ( n 2 D 2 ) υ 3 ( ϑ ) υ 3 ( h 2 , λ , ϑ ) ,

2 l ρ 2 = D 2 ρ 2 , υ 1 ( λ ) = υ 1 ( λ ) λ = ϑ ( log y 2 i ) 2 y 2 i λ [ ( 1 + y 2 i λ ) ϑ 1 ( ϑ + 1 ) y 2 i λ ( 1 + y 2 i λ ) ϑ 2 ] ,

υ 2 ( λ ) = υ 2 ( λ ) λ = ϑ ( log h 1 ) 2 h 1 λ [ ( 1 + h 1 λ ) ϑ 1 ( ϑ + 1 ) h 1 λ ( 1 + h 1 λ ) ϑ 2 ] , υ 3 ( λ ) = υ 3 ( λ ) λ = ϑ ( log h 2 ) 2 h 2 λ [ ( 1 + h 2 λ ) ϑ 1 ( ϑ + 1 ) h 2 λ ( 1 + h 2 λ ) ϑ 2 ] ,

υ 1 ( ϑ λ ) = υ 1 ( ϑ ) λ = y 2 i λ log y 2 i ( 1 + y 2 i λ ) ϑ 1 [ ϑ log ( 1 + y 2 i λ ) 1 ] ,

υ 2 ( ϑ λ ) = υ 2 ( ϑ ) λ = h 1 λ log h 1 ( 1 + h 1 λ ) ϑ 1 [ ϑ log ( 1 + h 1 λ ) 1 ] ,

and

υ 3 ( ϑ λ ) = υ 3 ( ϑ ) λ = h 2 λ log h 2 ( 1 + h 2 λ ) ϑ 1 [ ϑ log ( 1 + h 2 λ ) 1 ] .

References

[1] Epstein B. Truncated life tests in exponential case. Ann Math Stat. 1954;25:555–64.10.1214/aoms/1177728723Search in Google Scholar

[2] Childs A, Chandrasekar B, Balakrishnan N, Kundu D. Exact likelihood inference based on Type-I and Type-II hybrid censored samples from the exponential distribution. Ann Inst Stat Math. 2003;55:319–30.10.1007/BF02530502Search in Google Scholar

[3] Chandrasekar B, Childs A, Balakrishnan N. Exact likelihood inference for the exponential distribution under generalized type-I and type-II hybrid censoring. Nav Res Logist. 2004;51:994–1004.10.1002/nav.20038Search in Google Scholar

[4] Nelson W. Accelerated testing: Statistical models, test plans and data analysis. New York: John Wiley; 1990.10.1002/9780470316795Search in Google Scholar

[5] Bai DS, Chung SW. Optimal design of partially accelerated life tests for the exponential distribution under type-I censoring. IEEE Trans Reliab. 1992;41(3):400–6.10.1109/24.159807Search in Google Scholar

[6] Bai DS, Chung SW, Chun YR. Optimal design of partially accelerated life tests for the lognormal distribution under type-I censoring. Reliab Eng Syst Saf. 1993;40(1):85–92. 10.1016/0951-8320(93)90122-F.Search in Google Scholar

[7] Abd-Elfattah AM, Hassan AS, Nassr SG. Estimation in step-stress partially accelerated life tests for the Burr Type XII distribution using type I censoring. Stat Methodol. 2008;5(6):502–14.10.1016/j.stamet.2007.12.001Search in Google Scholar

[8] Hassan A, Hagag AE, Metwally N, Sery O. Statistical analysis of inverse Weibull based on step-stress partially accelerated life tests with unified hybrid censoring data. Comput J Math Stat Sci. 2025;4(1):162–85. 10.21608/cjmss.2024.319502.1072.Search in Google Scholar

[9] Ismail AA, Abdel-Ghaly AA, El-Khodary EH. Optimum constant-stress life test plans for Pareto distribution under type-I censoring. J Stat Comput Simul. 2011;81(12):1835–45. 10.1080/00949655.2010.506440.Search in Google Scholar

[10] Abushal TA, Soliman AA. Estimating the Pareto parameters under progressive censoring data for constant partially accelerated life tests. J Stat Comput Simul. 2015;85(5):917–34.10.1080/00949655.2013.853768Search in Google Scholar

[11] Hassan AS, Assar MS, Zaky AN. Constant-stress partially accelerated life tests for inverted Weibull distribution with multiple censored data. Int J Adv Stat Probability. 2015;3(1):72–82.10.14419/ijasp.v3i1.4418Search in Google Scholar

[12] Li X, Zheng H. Estimation and optimum constant-stress partially accelerated life test plans for Gompertz distribution with Type-I censoring. Commun Stat-Theory Methods. 2015. 10.1080/03610926.2013.839041.Search in Google Scholar

[13] Lone SA, Panahi H, Shah I. Bayesian prediction interval for a constant-stress partially accelerated life test model under censored data. J Taibah Univ Sci. 2021;15(1):1178–87. 10.1080/16583655.2021.2023847.Search in Google Scholar

[14] Hassan AS, Pramanik S, Maiti S, Nassr SG. Estimation in constant stress partially accelerated life tests for Weibull distribution based on censored competing risks data. Ann Data Sci. 2020;7(1):45–62.10.1007/s40745-019-00226-3Search in Google Scholar

[15] Almalki SJ, Farghal AA, Rastogi MK, Abd-Elmougod GA. Partially constant-stress accelerated life tests model for parameters estimation of Kumaraswamy distribution under adaptive type-II progressive censoring. Alex Eng J. 2022;61(7):5133–43.10.1016/j.aej.2021.10.035Search in Google Scholar

[16] Eliwa MS, Ahmed EA. Reliability analysis of constant partially accelerated life tests under progressive first failure type-II censored data from Lomax model: EM and MCMC algorithms. AIMS Math. 2022;8(1):29–60. 10.3934/math.2023002.Search in Google Scholar

[17] Mahmoud MAW, Ghazal MGM, Radwan HMM. Constant-partially accelerated life tests for three parameter distribution: Bayes inference using progressive type-II censoring. J Stat Appl Probab. 2022;11(1):15–28.10.18576/jsap/110102Search in Google Scholar

[18] Bantan R, Hassan AS, Almetwally E, Elgarhy M, Jamal F, Chesneau C, et al. Bayesian analysis in partially accelerated life tests for weighted Lomax Distribution. Comput Mater Continua. 2021;68(3):2859. 10.32604/cmc.2021.015422.Search in Google Scholar

[19] Ahmad HH, Ramadan DA, Almetwally EM. Tampered random variable analysis in step-stress testing: Modeling, inference, and applications. Mathematics. 2024;12(8):1248.10.3390/math12081248Search in Google Scholar

[20] Yousef MM, Fayomi A, Almetwally EM. Simulation techniques for strength component partially accelerated to analyze stress–strength model. Symmetry. 2023;15(6):1183.10.3390/sym15061183Search in Google Scholar

[21] El-Sherpieny ESA, Muhammed HZ, Almetwally EM. Accelerated life testing for bivariate distributions based on progressive censored samples with random removal. J Stat Appl Probab. 2022;11(2):203–23.10.18576/jsap/110228Search in Google Scholar

[22] Alomani GA, Hassan AS, Al-Omari AI, Almetwally EM. Different estimation techniques and data analysis for constant-partially accelerated life tests for power half-logistic distribution. Sci Rep. 2024;14:20865. 10.1038/s41598-024-71498-w.Search in Google Scholar PubMed PubMed Central

[23] Alrashidi A, Rabie A, Mahmoud AA, Nasr SG, Mustafa MS, Al Mutairi A, et al. Exponentiated gamma constant-stress partially accelerated life tests with unified hybrid censored data: Statistical inferences. Alex Eng J. 2024;88:268–75. 10.1016/j.aej.2023.12.066.Search in Google Scholar

[24] Burr IW. Cumulative frequency function. Ann Math Stat. 1942;1:215–32.10.1214/aoms/1177731607Search in Google Scholar

[25] Gove JH, Ducey MJ, Leak WB, Zhang L. Rotated sigmoid structures in managed uneven-aged northern hardwood stands: A look at the Burr Type III distribution. Forestry. 2008;81:21–36.10.1093/forestry/cpm025Search in Google Scholar

[26] Nadarajah S, Kotz S. On the alternative to the Weibull function. Eng Fract Mech. 2007;74:451–6.10.1016/j.engfracmech.2006.06.007Search in Google Scholar

[27] Klugman SA, Panjer HH, Willmot GE. Loss models. New York: Wiley; 1998. MR1490300.Search in Google Scholar

[28] Mielke PW. Another family of distributions for describing and analyzing precipitation data. J Appl Meteorol. 1973;12:275–80.10.1175/1520-0450(1973)012<0275:AFODFD>2.0.CO;2Search in Google Scholar

[29] Mokhlis NA. Reliability of a stress-strength model with Burr type III distributions. Commun Stat – Theory Methods. 2005;34:1643–57. MR2168516.10.1081/STA-200063183Search in Google Scholar

[30] Elbatal I, Hassan AS, Diab LS, Ben Ghorbal A, Elgarhy M, El-Saeed AR. Stress–strength reliability analysis for different distributions using progressive type-II censoring with Binomial removal. Axioms. 2023;12:1054. 10.3390/ axioms12111054.Search in Google Scholar

[31] Chernobai AS, Fabozzi FJ, Rachev ST. Operational risk: a guide to Basel II capital requirements, models, and analysis. New York: John Wiley & Sons; 2007.Search in Google Scholar

[32] Abd-Elfattah AM, Alharbey AH. Bayesian estimation for Burr distribution type III based on trimmed samples. ISRN Appl Math. 2012;2012:250393.10.5402/2012/250393Search in Google Scholar

[33] Kim C, Kim W. Estimation of the parameters of Burr Type III distribution based on dual generalized order statistics. Sci World J. 2014;2014:512039. 10.1155/2014/512039.Search in Google Scholar PubMed PubMed Central

[34] Altindag O, Cankaya MN, Yalcinkaya A, Aydogdu H. Statistical inference for the burr type III distribution under type II censored data. Commun Fac Sci Univ Ank Ser A1 Math Stat. 2017;66(2):297–310.10.1501/Commua1_0000000820Search in Google Scholar

[35] Gamchi FV, Alma ÖG, Belagh RA. Classical and Bayesian inference for Burr type-III distribution based on progressive type-II hybrid censored data. Math Sci. 2019;13:79–95. 10.1007/s40096-019-0281-9.Search in Google Scholar

[36] Panahi H. Estimation of the Burr type III distribution with application in unified hybrid censored sample of fracture toughness. J Appl Stat. 2017;44:2575–92.10.1080/02664763.2016.1258549Search in Google Scholar

[37] Hassan AS, Selmy AS, Assar SM. Assessing the lifetime performance index of Burr Type III distribution under progressive type II censoring. Pak J Stat Oper Res. 2021;17(3):633–47.10.18187/pjsor.v17i3.3635Search in Google Scholar

[38] Dutta S, Kayal S. Estimation and prediction for Burr type III distribution based on unified progressive hybrid censoring scheme. J Appl Stat. 2022;51(1):1–33. 10.1080/02664763.2022.2113865.Search in Google Scholar PubMed PubMed Central

[39] Hassan AS, Elsherpieny EA, Aghel WE. Statistical inference of the Burr Type III distribution under joint progressively Type-II censoring. Sci Afr. 2023;21:e01770. 10.1016/j.sciaf.2023.e01770.Search in Google Scholar

[40] DeGroot MH, Goel PK. Bayesian estimation and optimal designs in partially accelerated life testing. Nav Res Logist Q. 1979;26(2):223–35.10.1002/nav.3800260204Search in Google Scholar

[41] Dey S, Ali S, Park C. Weighted exponential distribution: properties and different methods of estimation. J Stat Comput Simul. 2015;85:3641–61.10.1080/00949655.2014.992346Search in Google Scholar

[42] Kundu D, Howlader H. Bayesian inference and prediction of the inverse Weibull distribution for type-II censored data. Comput Stat Data Anal. 2010;54:1547–58.10.1016/j.csda.2010.01.003Search in Google Scholar

Received: 2024-07-22
Revised: 2025-04-30
Accepted: 2025-05-06
Published Online: 2025-07-21

© 2025 the author(s), published by De Gruyter

This work is licensed under the Creative Commons Attribution 4.0 International License.

Articles in the same Issue

  1. Research Articles
  2. Single-step fabrication of Ag2S/poly-2-mercaptoaniline nanoribbon photocathodes for green hydrogen generation from artificial and natural red-sea water
  3. Abundant new interaction solutions and nonlinear dynamics for the (3+1)-dimensional Hirota–Satsuma–Ito-like equation
  4. A novel gold and SiO2 material based planar 5-element high HPBW end-fire antenna array for 300 GHz applications
  5. Explicit exact solutions and bifurcation analysis for the mZK equation with truncated M-fractional derivatives utilizing two reliable methods
  6. Optical and laser damage resistance: Role of periodic cylindrical surfaces
  7. Numerical study of flow and heat transfer in the air-side metal foam partially filled channels of panel-type radiator under forced convection
  8. Water-based hybrid nanofluid flow containing CNT nanoparticles over an extending surface with velocity slips, thermal convective, and zero-mass flux conditions
  9. Dynamical wave structures for some diffusion--reaction equations with quadratic and quartic nonlinearities
  10. Solving an isotropic grey matter tumour model via a heat transfer equation
  11. Study on the penetration protection of a fiber-reinforced composite structure with CNTs/GFP clip STF/3DKevlar
  12. Influence of Hall current and acoustic pressure on nanostructured DPL thermoelastic plates under ramp heating in a double-temperature model
  13. Applications of the Belousov–Zhabotinsky reaction–diffusion system: Analytical and numerical approaches
  14. AC electroosmotic flow of Maxwell fluid in a pH-regulated parallel-plate silica nanochannel
  15. Interpreting optical effects with relativistic transformations adopting one-way synchronization to conserve simultaneity and space–time continuity
  16. Modeling and analysis of quantum communication channel in airborne platforms with boundary layer effects
  17. Theoretical and numerical investigation of a memristor system with a piecewise memductance under fractal–fractional derivatives
  18. Tuning the structure and electro-optical properties of α-Cr2O3 films by heat treatment/La doping for optoelectronic applications
  19. High-speed multi-spectral explosion temperature measurement using golden-section accelerated Pearson correlation algorithm
  20. Dynamic behavior and modulation instability of the generalized coupled fractional nonlinear Helmholtz equation with cubic–quintic term
  21. Study on the duration of laser-induced air plasma flash near thin film surface
  22. Exploring the dynamics of fractional-order nonlinear dispersive wave system through homotopy technique
  23. The mechanism of carbon monoxide fluorescence inside a femtosecond laser-induced plasma
  24. Numerical solution of a nonconstant coefficient advection diffusion equation in an irregular domain and analyses of numerical dispersion and dissipation
  25. Numerical examination of the chemically reactive MHD flow of hybrid nanofluids over a two-dimensional stretching surface with the Cattaneo–Christov model and slip conditions
  26. Impacts of sinusoidal heat flux and embraced heated rectangular cavity on natural convection within a square enclosure partially filled with porous medium and Casson-hybrid nanofluid
  27. Stability analysis of unsteady ternary nanofluid flow past a stretching/shrinking wedge
  28. Solitonic wave solutions of a Hamiltonian nonlinear atom chain model through the Hirota bilinear transformation method
  29. Bilinear form and soltion solutions for (3+1)-dimensional negative-order KdV-CBS equation
  30. Solitary chirp pulses and soliton control for variable coefficients cubic–quintic nonlinear Schrödinger equation in nonuniform management system
  31. Influence of decaying heat source and temperature-dependent thermal conductivity on photo-hydro-elasto semiconductor media
  32. Dissipative disorder optimization in the radiative thin film flow of partially ionized non-Newtonian hybrid nanofluid with second-order slip condition
  33. Bifurcation, chaotic behavior, and traveling wave solutions for the fractional (4+1)-dimensional Davey–Stewartson–Kadomtsev–Petviashvili model
  34. New investigation on soliton solutions of two nonlinear PDEs in mathematical physics with a dynamical property: Bifurcation analysis
  35. Mathematical analysis of nanoparticle type and volume fraction on heat transfer efficiency of nanofluids
  36. Creation of single-wing Lorenz-like attractors via a ten-ninths-degree term
  37. Optical soliton solutions, bifurcation analysis, chaotic behaviors of nonlinear Schrödinger equation and modulation instability in optical fiber
  38. Chaotic dynamics and some solutions for the (n + 1)-dimensional modified Zakharov–Kuznetsov equation in plasma physics
  39. Fractal formation and chaotic soliton phenomena in nonlinear conformable Heisenberg ferromagnetic spin chain equation
  40. Single-step fabrication of Mn(iv) oxide-Mn(ii) sulfide/poly-2-mercaptoaniline porous network nanocomposite for pseudo-supercapacitors and charge storage
  41. Novel constructed dynamical analytical solutions and conserved quantities of the new (2+1)-dimensional KdV model describing acoustic wave propagation
  42. Tavis–Cummings model in the presence of a deformed field and time-dependent coupling
  43. Spinning dynamics of stress-dependent viscosity of generalized Cross-nonlinear materials affected by gravitationally swirling disk
  44. Design and prediction of high optical density photovoltaic polymers using machine learning-DFT studies
  45. Robust control and preservation of quantum steering, nonlocality, and coherence in open atomic systems
  46. Coating thickness and process efficiency of reverse roll coating using a magnetized hybrid nanomaterial flow
  47. Dynamic analysis, circuit realization, and its synchronization of a new chaotic hyperjerk system
  48. Decoherence of steerability and coherence dynamics induced by nonlinear qubit–cavity interactions
  49. Finite element analysis of turbulent thermal enhancement in grooved channels with flat- and plus-shaped fins
  50. Modulational instability and associated ion-acoustic modulated envelope solitons in a quantum plasma having ion beams
  51. Statistical inference of constant-stress partially accelerated life tests under type II generalized hybrid censored data from Burr III distribution
  52. On solutions of the Dirac equation for 1D hydrogenic atoms or ions
  53. Entropy optimization for chemically reactive magnetized unsteady thin film hybrid nanofluid flow on inclined surface subject to nonlinear mixed convection and variable temperature
  54. Stability analysis, circuit simulation, and color image encryption of a novel four-dimensional hyperchaotic model with hidden and self-excited attractors
  55. A high-accuracy exponential time integration scheme for the Darcy–Forchheimer Williamson fluid flow with temperature-dependent conductivity
  56. Novel analysis of fractional regularized long-wave equation in plasma dynamics
  57. Development of a photoelectrode based on a bismuth(iii) oxyiodide/intercalated iodide-poly(1H-pyrrole) rough spherical nanocomposite for green hydrogen generation
  58. Investigation of solar radiation effects on the energy performance of the (Al2O3–CuO–Cu)/H2O ternary nanofluidic system through a convectively heated cylinder
  59. Quantum resources for a system of two atoms interacting with a deformed field in the presence of intensity-dependent coupling
  60. Studying bifurcations and chaotic dynamics in the generalized hyperelastic-rod wave equation through Hamiltonian mechanics
  61. A new numerical technique for the solution of time-fractional nonlinear Klein–Gordon equation involving Atangana–Baleanu derivative using cubic B-spline functions
  62. Interaction solutions of high-order breathers and lumps for a (3+1)-dimensional conformable fractional potential-YTSF-like model
  63. Hydraulic fracturing radioactive source tracing technology based on hydraulic fracturing tracing mechanics model
  64. Numerical solution and stability analysis of non-Newtonian hybrid nanofluid flow subject to exponential heat source/sink over a Riga sheet
  65. Numerical investigation of mixed convection and viscous dissipation in couple stress nanofluid flow: A merged Adomian decomposition method and Mohand transform
  66. Effectual quintic B-spline functions for solving the time fractional coupled Boussinesq–Burgers equation arising in shallow water waves
  67. Analysis of MHD hybrid nanofluid flow over cone and wedge with exponential and thermal heat source and activation energy
  68. Solitons and travelling waves structure for M-fractional Kairat-II equation using three explicit methods
  69. Impact of nanoparticle shapes on the heat transfer properties of Cu and CuO nanofluids flowing over a stretching surface with slip effects: A computational study
  70. Computational simulation of heat transfer and nanofluid flow for two-sided lid-driven square cavity under the influence of magnetic field
  71. Irreversibility analysis of a bioconvective two-phase nanofluid in a Maxwell (non-Newtonian) flow induced by a rotating disk with thermal radiation
  72. Hydrodynamic and sensitivity analysis of a polymeric calendering process for non-Newtonian fluids with temperature-dependent viscosity
  73. Exploring the peakon solitons molecules and solitary wave structure to the nonlinear damped Kortewege–de Vries equation through efficient technique
  74. Modeling and heat transfer analysis of magnetized hybrid micropolar blood-based nanofluid flow in Darcy–Forchheimer porous stenosis narrow arteries
  75. Activation energy and cross-diffusion effects on 3D rotating nanofluid flow in a Darcy–Forchheimer porous medium with radiation and convective heating
  76. Insights into chemical reactions occurring in generalized nanomaterials due to spinning surface with melting constraints
  77. Influence of a magnetic field on double-porosity photo-thermoelastic materials under Lord–Shulman theory
  78. Soliton-like solutions for a nonlinear doubly dispersive equation in an elastic Murnaghan's rod via Hirota's bilinear method
  79. Analytical and numerical investigation of exact wave patterns and chaotic dynamics in the extended improved Boussinesq equation
  80. Nonclassical correlation dynamics of Heisenberg XYZ states with (x, y)-spin--orbit interaction, x-magnetic field, and intrinsic decoherence effects
  81. Exact traveling wave and soliton solutions for chemotaxis model and (3+1)-dimensional Boiti–Leon–Manna–Pempinelli equation
  82. Unveiling the transformative role of samarium in ZnO: Exploring structural and optical modifications for advanced functional applications
  83. On the derivation of solitary wave solutions for the time-fractional Rosenau equation through two analytical techniques
  84. Analyzing the role of length and radius of MWCNTs in a nanofluid flow influenced by variable thermal conductivity and viscosity considering Marangoni convection
  85. Advanced mathematical analysis of heat and mass transfer in oscillatory micropolar bio-nanofluid flows via peristaltic waves and electroosmotic effects
  86. Exact bound state solutions of the radial Schrödinger equation for the Coulomb potential by conformable Nikiforov–Uvarov approach
  87. Some anisotropic and perfect fluid plane symmetric solutions of Einstein's field equations using killing symmetries
  88. Nonlinear dynamics of the dissipative ion-acoustic solitary waves in anisotropic rotating magnetoplasmas
  89. Curves in multiplicative equiaffine plane
  90. Exact solution of the three-dimensional (3D) Z2 lattice gauge theory
  91. Propagation properties of Airyprime pulses in relaxing nonlinear media
  92. Symbolic computation: Analytical solutions and dynamics of a shallow water wave equation in coastal engineering
  93. Wave propagation in nonlocal piezo-photo-hygrothermoelastic semiconductors subjected to heat and moisture flux
  94. Comparative reaction dynamics in rotating nanofluid systems: Quartic and cubic kinetics under MHD influence
  95. Laplace transform technique and probabilistic analysis-based hypothesis testing in medical and engineering applications
  96. Physical properties of ternary chloro-perovskites KTCl3 (T = Ge, Al) for optoelectronic applications
  97. Gravitational length stretching: Curvature-induced modulation of quantum probability densities
  98. The search for the cosmological cold dark matter axion – A new refined narrow mass window and detection scheme
  99. A comparative study of quantum resources in bipartite Lipkin–Meshkov–Glick model under DM interaction and Zeeman splitting
  100. PbO-doped K2O–BaO–Al2O3–B2O3–TeO2-glasses: Mechanical and shielding efficacy
  101. Review Article
  102. Examination of the gamma radiation shielding properties of different clay and sand materials in the Adrar region
  103. Special Issue on Fundamental Physics from Atoms to Cosmos - Part II
  104. Possible explanation for the neutron lifetime puzzle
  105. Special Issue on Nanomaterial utilization and structural optimization - Part III
  106. Numerical investigation on fluid-thermal-electric performance of a thermoelectric-integrated helically coiled tube heat exchanger for coal mine air cooling
  107. Special Issue on Nonlinear Dynamics and Chaos in Physical Systems
  108. Analysis of the fractional relativistic isothermal gas sphere with application to neutron stars
  109. Abundant wave symmetries in the (3+1)-dimensional Chafee–Infante equation through the Hirota bilinear transformation technique
  110. Successive midpoint method for fractional differential equations with nonlocal kernels: Error analysis, stability, and applications
  111. Novel exact solitons to the fractional modified mixed-Korteweg--de Vries model with a stability analysis
Downloaded on 4.11.2025 from https://www.degruyterbrill.com/document/doi/10.1515/phys-2025-0161/html
Scroll to top button