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Springer Nature - PMC COVID-19 Collection logoLink to Springer Nature - PMC COVID-19 Collection
. 2022 Nov 21:1–19. Online ahead of print. doi: 10.1007/s11750-022-00649-x

Α new mixed δ-shock model with a change in shock distribution

Stathis Chadjiconstantinidis 1,, Altan Tuncel 2, Serkan Eryilmaz 3
PMCID: PMC9684896  PMID: 38625339

Abstract

In this paper, reliability properties of a system that is subject to a sequence of shocks are investigated under a particular new change point model. According to the model, a change in the distribution of the shock magnitudes occurs upon the occurrence of a shock that is above a certain critical level. The system fails when the time between successive shocks is less than a given threshold, or the magnitude of a single shock is above a critical threshold. The survival function of the system is studied under both cases when the times between shocks follow discrete distribution and when the times between shocks follow continuous distribution. Matrix-based expressions are obtained for matrix-geometric discrete intershock times and for matrix-exponential continuous intershock times, as well.

Keywords: Delta shock model, Mixed shock model, Matrix-geometric distributions, Matrix-exponential distributions, Reliability

Introduction

Although the event of system failure is defined through the magnitudes of random shocks in classical shock models, according to the delta shock model, the system fails if the length of the times between two successive shocks is less than a given fixed threshold. Such a model has been studied by Li (1984), Li and Kong (2007), Li and Zhao (2007) when the shocks occur according to a Poisson process, i.e. the interarrival times between shocks are exponentially distributed. Tuncel and Eryilmaz (2018) obtained the survival function and the mean time to failure of the system when intershock times follow proportional hazard rate model. Eryilmaz (2017) studied reliability properties of a system under the delta shock model when the shocks occur according to a Polya process. Under the assumption of Polya process, the interarrival times between successive shocks are no longer independent.

Various modifications and generalizations of delta shock (or simply, δ-shock) models have been introduced to represent real life systems and processes. Mallor and Santos (2003) studied a general shock model that generalizes the extreme, the cumulative and the run shock models. Wang and Zhang (2005) defined a mixed shock model. According to their model, the system fails if either the time between two successive shocks is less than a given threshold or the magnitude of a single shock exceeds a given threshold. This is a mixed model that combines delta and extreme shock models. See also Parvardeh and Balakrishnan (2015) for mixed shock models. Eryilmaz (2012) extended the delta shock model to the case when the system fails if a specified number of consecutive interarrival times are less than a threshold delta. Jiang (2020) defined and studied a generalized delta shock model with multi-failure thresholds. Goyal et al. (2022a) introduced a general δ-shock model when the recovery time depends on both the arrival times and the magnitudes of shocks. See also Lorvand et al. (2019), Poursaeed (2021), Goyal et al. (2022b) and Lorvard and Nematollahi (2022) for other types of extensions and generalizations of the delta shock model.

Shock models have wide applications for modeling various real-life processes and systems. The term shock is generic, and it can be replaced by an appropriate concept depending on the process under concern. For example, in a certain spare parts inventory management system, demands arrive randomly with random size. In this case, the interarrival times are the times between successive demands. The size of a demand coincides with the magnitude of a shock. In a certain portfolio of an insurance company, claims occur randomly over time. In this case, the interarrival times are the times between successive claims and the magnitudes of the shocks are the sizes of the claims.

In most real-life situations, after a shock that is above a certain level, the characteristics, e.g., distribution of the shocks may change. For example, if the shock is a kind of environmental effect, e.g., pressure, temperature, and wind, then a harsher environment might be available after the shock that is significantly different from the previous shocks. Eryilmaz and Kan (2021) studied reliability and optimal replacement policy for an extreme shock model when the distribution of the shock size changes after a random number of shocks following a particular distribution. In particular, for a sequence of shock sizes denoted by Y1, Y2, , they considered the case when Y1, Y2, , YM are independent and identically distributed (iid) with common distribution G1 and YM+1, YM+2, are iid with common distribution G2, where M is a positive discrete random variable independent of Yi’s and follows a particular distribution. Also, Eryilmaz and Kan (2021), studied the reliability of an extreme shock model when there is a change in the shock size distribution. According to their model, the change in shock size distribution occurs upon the occurrence of a shock that is above a fixed warning threshold. They assumed that the distribution of the magnitudes of shocks changes after the first shock of size at least d1 a given level. That is, if Nd1 denotes the number of shocks until the first shock of size at least d1, then it is assumed that Y1, Y2, , YNd1 have common distribution G1, and YNd1+1, YNd1+2, have another common distribution G2. In this case, the random variable Nd1 denotes the number of shocks until the change point depends on Y1, Y2, . Applications of this model to statistical control processes and wind turbines are given by Eryilmaz and Kan (2021).

In this paper, we study a new mixed shock model that combines extreme and delta shock models under the change point model proposed by Eryilmaz and Kan (2021). Such a model is useful for modeling various real-life systems or processes. In general, this proposed new change point setup is useful to model the situation when there is a change in behavior of the system/process upon the occurrence of an unexpected event, e.g., a sudden change in environmental condition, a large claim due to an extreme event, an enormous demand shock for health care systems and ventilators due to COVID-19. Such changes ensure the change in probability distribution of the shock/claim/demand. Also, this model is useful for insurance portfolio management. Consider a heterogeneous portfolio of losses and/or payments of an insurance company. Expected losses are defined by a threshold, say d1, and are such that the loss sizes do not exceed the threshold d1. An unexpected future loss, (with loss size exceeding the value of the threshold) could be used as a warning for an approaching high-risk situation for the portfolio since the distribution of the claim sizes may change after an unexpected loss. This may occur if the portfolio is affected by a random event such as explosion, breakdown that influence all policies. A plausible criterion to confer that a high-risk situation is approaching for the insurance company would be to observe at least two unexpected losses that are very close to each other or more generally to observe least two unexpected losses which are separated by at most δ expected losses (this corresponds to the classical δ-shock model) as well as the size of a unexpected catastrophic loss is at least d>d1 (this corresponds to the extreme shock model).

The findings of the paper can be summarized as follows:

  • The probability generating function (Laplace-Stieltjes transform) of the system’s lifetime is obtained when the times between shocks follow discrete (continuous) distribution

  • The matrix-based expressions for the survival function of the system are obtained when the times between shocks follow discrete matrix-geometric (continuous matrix-exponential) distribution.

In mixed shock models, system failure results from the competing failure criteria. Indeed, in most real-life processes, the system failure occurs with respect to the occurrence of two or more different events. The novelty of the present paper lies in combining the mixed shock model previously studied in the literature with the change point-based model. Such a combined model is flexible and can be used in a more general setting.

The paper is organized as follows. In Sect. 2, the model is described, and some preliminary results are presented. In Sect. 3, the reliability properties of the system are investigated under both cases when the interarrival times between successive shocks follow discrete and continuous probability distributions. Section 4 contains numerical illustrations.

Description of the model and preliminary results

We consider a system that is subject to random shocks. Let X1, X2, be the interarrival times between successive shocks, with common distribution function (df) Fx=1-F¯x=PrXx, where X denotes a generic random variable of Xi s. Also, let Y1, Y2, be the random magnitudes of the shocks. It is assumed that the distribution of the magnitudes of shocks changes after the first shock of size at least d1>0. That is, the random shock magnitudes Y1, Y2, , YNd1 have common df G1, and YNd1+1, YNd1+2, have common df G2, where Nd1 denotes the random number of shocks until the first shock of size at least d1. The system fails when the time between successive shocks is less than a given threshold δ>0, or the magnitude of a single shock is at least d, where d>d1. Let also Nd denotes the number of shocks for which the time between successive shocks is less than a given threshold δ, or the magnitude of a single shock is at least d. Then, the lifetime of the system is T=i=1NdXi, Hence, T is a random sum and has a compound distribution.

For simplicity, let us denote by:

p1=G1d1: the probability that the magnitude of a shock before the change in shock size distribution is below d1,

p2=G1d: the probability that the magnitude of a shock before the change in shock size distribution is below d,

p3=G2d: the probability that the magnitude of a shock after the change in shock size distribution is below d.

It should be noted that the mixed shock model considered in the present paper coincides with the model studied by Eryilmaz and Kan (2021) when δ0.

In the following Lemma 1 we obtain the joint probability mass function (pmf) of the random vector (Nd1, Nd).

Lemma 1.

The joint pmf of the random variables Nd1 and Nd is

Pr(Nd1=m,Nd=n)=p2-p1p1m-1p3n-m-1F¯n-1δ1-p3F¯δ,n>mp1n-1F¯n-1δ1-p2F¯δ,n=m. 1

Proof.

For n>m we have

{Nd1=m,Nd=n}={X1>δ,Y1<d1,,Xm-1>δ,Ym-1<d1,Xm>δ,d1Ym<d,Xm+1>δ,Ym+1<d,,Xn-1>δ,Yn-1<d,Xnδ}{X1>δ,Y1<d1,,Xm-1>δ,Ym-1<d1,Xm>δ,d1Ym<d,Xm+1>δ,Ym+1<d,,Xn-1>δ,Yn-1<d,Xn>δ,Ynd}

and

Pr(Nd1=m,Nd=n)=F¯n-1δG1m-1d1G1d-G1d1G2n-m-1dFδ+F¯nδG1m-1d1G1d-G1d1G2n-m-1d1-G2d=F¯n-1δp1m-1p2-p1p3n-m-1Fδ+F¯nδp1m-1p2-p1p3n-m-11-p3=p2-p1p1m-1p3n-m-1F¯n-1δ1-p3F¯δ.

For n=m we have

{Nd1=n,Nd=n}={X1>δ,Y1<d1,,Xn-1>δ,Yn-1<d1,Xnδ}{X1>δ,Y1<d1,,Xn-1>δ,Yn-1<d1,Xn>δ,Ynd}

and

Pr(Nd1=n,Nd=n)=F¯n-1δG1n-1d1Fδ+F¯nδG1n-1d11-G1d=F¯n-1δp1n-1Fδ+F¯nδp1n-11-p2=p1n-1F¯n-1δ1-p2F¯δ

Using Lemma 1, we can easily obtain the marginal pmfs of the random variables Nd1 and Nd, given in the following:

Corollary 1.

(i) The marginal pmf of Nd1 is given by.

PrNd1=m=1-p1F¯δp1m-1F¯m-1δ 2

(ii) The marginal pmf of Nd is given by

PrNd=n=p3-p2p3-p1p1F¯δn-11-p1F¯δ+p2-p1p3-p1p3F¯δn-11-p3F¯δ, 3

for p1p3, and

PrNd=n=p2-p3F¯δ1-p3F¯δn-1p3F¯δn-21-p3F¯δ2+1-p2F¯δ1-p3F¯δp3F¯δn-11-p3F¯δ 4

for p1=p3.

Proof.

(i) Using (1) we get

PrNd1=m=Pr(Nd1=m,Nd=m)+n=m+1PrNd1=m,Nd=n=p1m-1F¯m-1δ1-p2F¯δ+p2-p1p1m-11-p3F¯δn=m+1p3n-m-1F¯n-1δ=p1m-1F¯m-1δ1-p2F¯δ+p2-p1p1m-1F¯mδ=1-p1F¯δp1m-1F¯m-1δ.

(ii) Similarly, from (1) we obtain

PrNd=n=m=1n-1PrNd1=m,Nd=n+PrNd1=n,Nd=n=p2-p1F¯n-1δ1-p3F¯δm=1n-1p1m-1p3n-m-1+p1n-1F¯n-1δ1-p2F¯δ=p2-p1F¯n-1δ1-p3F¯δp3n-2m=0n-2p1p3m+p1n-1F¯n-1δ1-p2F¯δ.

Now, the result follows immediately, since

m=0n-2p1p3m=p3p3-p11-p1p3n-1n-1,ifp1=p3,ifp1p3.

Remark 1. (i) From Eq. (2), we have that the random variable Nd1 follows the geometric distribution with parameter 1-p1F¯δ.

(ii) Let p1p3.

Let also

ω=p3-p2p3-p1and1-ω=p2-p1p3-p1 5

and consider the geometric random variables W1 and W2 having probability mass functions

PrW1=n=p1F¯δn-11-p1F¯δ,n=1,2, 6

and

PrW2=n=p3F¯δn-11-p3F¯δ,n=1,2, 7

respectively. Note that W1Nd1, where the symbol means equality in distribution.

Then Eq. (3) can be rewritten as

PrNd=n=ωPrW1=n+1-ωPrW2=n,n=1,2, 8

Therefore, the distribution of the random variable Nd is a mixture of two geometric distributions. It should be noted that the weights ω and 1-ω may take negative values and hence, Eq. (8) is a generalized mixture of two geometric distributions.

(iii) Let p1=p3.

Then, Eq. (4) can also be rewritten as

PrNd=n=θPrU1=n+1-θPrW2=n,n=1,2, 9

where

θ=p2-p3F¯δ1-p3F¯δ,1-θ=1-p2F¯δ1-p3F¯δ 10

PrW2=n is given by (7), and the random variable U1 has the negative binomial distribution with probability mass function

PrU1=n=n-1p3F¯δn-21-p3F¯δ2,n=2,3,. 11

Therefore, since the weights θ and 1-θ may take negative values, Eq. (9) is a generalized mixture of negative binomial and geometric distributions.

Reliability of the system

For our system, the following two dependent lifetime random variables are of interest

T1=i=1Nd1Xi,T=i=1NdXi.

Note that T1 and T are compound random variables (or random sums), T1 denotes the time until the first shock is of size at least d1, i.e., it is the time until the change point and the random variable T denotes the lifetime of the system.

In the sequel, we examine two cases according to which the interarrival times X1, X2, between successive shocks have a discrete or a continuous distribution.

The discrete case

Suppose that the interarrival times X1, X2, between successive shocks have a discrete distribution with an arbitrary common df F. Let ft=Pr(X=t) be the pmf of X and fTt=Pr(T=t) be the pmf of the lifetime T. Define the probability generating functions (pgf) of the conditional random variables XXδ and XX>δ by

PX,δu=EuX|Xδ

and

P¯X,δu=EuX|X>δ.

Then, we have the following.

Theorem 1.

Let PT1,Tu1,u=Eu11uT be the joint pgf of the random vector T1,T. Then, it holds.

PT1,Tu1,u=PX,δuFδp2-p1P¯X,δu1uF¯δ+P¯X,δup2-p11-p3P¯X,δu1u(F¯δ)21-p3F¯δP¯X,δu1-p1F¯δP¯X,δu1u+PX,δu1uFδ+P¯X,δu1uF¯δ1-p21-p1F¯δP¯X,δu1u.

Proof.

By conditioning on Nd1,Nd we get

PT1,Tu1,u=m=1n=m+1Eu1i=1Nd1Xiui=1NdXiNd1=m,Nd=nPr(Nd1=m,Nd=n)+n=1Eu1i=1Nd1Xiui=1NdXiNd1=n,Nd=nPr(Nd1=n,Nd=n)

The result follows using the details in the proof of Lemma 1.

By letting u=1and u1=1 in Theorem 1 we obtain the marginal pgfs of the lifetimes T1and T, respectively. Thus, we have the following:

Corollary 2.

(i) The pgf PT1u=EuT1 of the lifetime random variable T1is.

PT1u=Fδp2-p1P¯X,δuF¯δ+p2-p11-p3P¯X,δu(F¯δ)21-p3F¯δ1-p1F¯δP¯X,δu+PX,δuFδ+P¯X,δuF¯δ1-p21-p1F¯δP¯X,δu. 12

(ii) The pgf PTu=EuT of the lifetime random variable T is

PTu=PX,δuFδp2-p1P¯X,δuF¯δ+P¯X,δup2-p11-p3P¯X,δu(F¯δ)21-p3F¯δP¯X,δu1-p1F¯δP¯X,δu+PX,δuFδ+P¯X,δuF¯δ1-p21-p1F¯δP¯X,δu. 13

Using that ET1=PT11 and ET=PT1 and Corollary 2, we can obtain the means of the random variables T1 and T. Thus, we have the following:

Corollary 3.

The mean of T1 is

ET1=11-p1F¯δEX

and the mean time to failure (MTTF) of the system is

ET=1+p2-p1-p3F¯δ1-p1F¯δ1-p3F¯δEX.

For some specific distributions of the random variable X we can obtain analytical results for the evaluation of the distributions of the lifetime random variables T1 and T.

At first, we consider the particular case when the interarrival times between successive shocks follow the geometric distribution with common pmf

ft=p1-pt-1,t=1,2, 14

and we represent the random variables T1 and T as matrix-geometric distributions.

A discrete random variable W with zero pmf at zero that has a probability generating function in the form

EuW=c1u++cmum1+d1u++dmum 15

for some m1 and real constants c1,,cm and d1,,dm, is said to have a matrix-geometric distribution (see, e.g. Bladt and Nielsen (2017)). In this case, the probability mass function and the survival function of the random variable Tδ can be represented, respectively, as

PW=n=πQn-1u 16

and

PWn=πQnIm-Q-1u, 17

where π=1,0,,0 is a 1×m row vector, Im is the identity matrix of order m, and the m×m matrix Q and the m×1 column vector u are given by

Q=-d10001-dm0000-dm-11000-dm-20100-d20010,u=c1cmcm-1cm-2c2. 18

We write WMGmQ,u, to represent that the random variable W has matrix-geometric distribution.

Theorem 2.

Let the interarrival times between successive shocks follow the geometric distribution with common pmf given by (14). Then

(i) The random variable T1MGδ+1Q,u, where Q:δ+1× δ+1 and u:δ+1×1 are given by (18) with

c1=p;ci=0,2iδ;cδ+1=-p1pqδ;d1=-q,di=0,2iδ;dδ+1=-p1pqδ.

(ii) The random variable TMG2δ+2Q,u, where Q:2δ+1×2δ+1 and u:2δ+1×1 are given by (18) with

c1=p;c2=-pq;ci=0;2<iδ;cδ+1=-p2pqδ;cδ+2=p2p2qδ-p1p2qδ+p2pqδ+1-p3p2qδ;ci=0,δ+2<i2δ+1;c2δ+2=p1p3p2q2δ;d1=-2q;d2=q2;di=0;2<iδ;dδ+1=-p1pqδ+p3pqδ;dδ+2=p1pqδ+1+p3pqδ+1;di=0,δ+3<i2δ+1;d2δ+2=p1p3p2q2δ.

Proof.

Under the assumptions of the Theorem,

PX,δu=EuX|Xδ=pu1-quδ1-qu1-qδ,

and

P¯X,δu=EuX|X>δ=1qδpu1-qu-PX,δu1-qδ.

(i) Using Eq. (12), the pgf of T1 is obtained as

PT1u=pu-p1pqδuδ+11-qu-p1pqδuδ+1,

and hence the result follows directly from (15).

(ii) Using Eq, (13), the pgf of T can be written as

PTu=i=12δ+1ciui/1+i=12δ+1diui,

where the coefficients ci and di are as given in the theorem. Since PTu is of the form of Eq. (15), the result follows immediately.

The continuous case

Now suppose that the interarrival times X1, X2, between successive shocks have a continuous distribution with an arbitrary common df Ft=PrXt and let ft=Ft denotes its common probability density function (pdf). Also, let f^u=Ee-uX=0e-utftdt be the Laplace–Stieltjes transform (LST) of X. Similar to the proof of Theorem 2, we can obtain the joint LST f^T1,Tu1,u=Ee-u1T1-uT of the random vector T1,T given in the following Theorem 3. Define the LSTs of the random variables XXδ and XX>δ by

f^X,δu=Ee-uX|Xδ

and

g^X,δu=Ee-uX|X>δ,

respectively, then we have the next.

Theorem 3.

The joint LST f^T1,Tu1,u=Ee-u1T1-uT of the random vector T1,T is.

f^T1,Tu1,u=f^X,δuFδp2-p1g^X,δu1+uF¯δ+g^X,δup2-p11-p3g^X,δu1+u(F¯δ)21-p3F¯δg^X,δu1-p1F¯δg^X,δu1+u+f^X,δu1+uFδ+g^X,δu1+uF¯δ1-p21-p1F¯δg^X,δu.

Using the LST of Theorem 3, we get the marginal LSTs f^T1u=Ee-uT1 and f^Tu=Ee-uT of the random variables T1 and T.

Corollary 4.

The marginal LSTs corresponding to T1 and T are given, respectively, by.

f^T1u=Fδp2-p1g^X,δuF¯δ+p2-p11-p3g^X,δu(F¯δ)21-p3F¯δ1-p1F¯δg^X,δu+f^X,δuFδ+g^X,δuF¯δ1-p21-p1F¯δg^X,δu.

and

f^Tu=f^X,δuFδp2-p1g^X,δuF¯δ+g^X,δup2-p11-p3g^X,δu(F¯δ)21-p3F¯δg^X,δu1-p1F¯δg^X,δu+f^X,δuFδ+g^X,δuF¯δ1-p21-p1F¯δg^X,δu.

It should be noted that using the relations ET1=-f^T10, ET=-f^T0 and Corollary 4, we can obtain the means of the random variables T1 and T. Their expressions are the same with those given in Corollary 3 for the discrete case.

As in the discrete case, by considering specific distributions of the random variable X, we can obtain analytical results for the evaluation of the distributions of the lifetime random variables T1 and T. We consider the particular case when the interarrival times between successive shocks follow the exponential distribution with common pdf

ft=λe-λt,t0,λ0.

In this case, we have

f^X,δu=Ee-uX|Xδ=11-e-λδλu+λ1-e-u+λδ,

and

g^X,δu=Ee-uX|X>δ=λu+λe-δu.

Using Corollary 3, the LSTs of the random variables T1 and T are found to be

f^T1u=λ1-p1e-u+λδ-p3e-λδ+p1p3e-u+2λδλ+u-λp1e-u+λδ-λ+up3e-λδ+λp1p3e-u+2λδ, 19

and

f^Tu=λλ+u1-p2e-u+λδ+λ2p1p3e-2u+λδ+λ2(p2-p1-p3)e-u+λδλ+u2-λλ+up3e-u+λδ-λλ+up1e-u+λδ+λ2p1p3e-2u+λδ. 20

Corollary 5

Let Xi have the exponential distribution with parameter λ>0. If δ, then the distribution of the random variables T1 and T approaches the exponential distribution with parameter λ, that is.

limδT1>t=limδT>t=e-λt.

Proof.

The result follows immediately from (19) and (20), since

limδf^T1u=λλ+uandlimδf^Tu=λλ+uλ+u2=λλ+u,

and λ/λ+u is the LST of the exponential distribution with parameter λ.

A continuous random variable W is said to have a matrix-exponential distribution, if its distribution function is given by

FWt=PrWt=1-F¯Wt=1+aTexpStS-1s, 21

where a is a p×1 vector, S is a p×p matrix (which is called a companion matrix) and s is a p×1 vector. We write WMEp(a,S,s), to present that the random variable W has a matrix-exponential distribution with parameters (a,S,s). The common probability density function is computed from fWt=aTexpSts. If f^Wu=Ee-uX=0e-utftdt denotes the Laplace–Stieltjes transform of X, then f^Wu can be computed from

f^Wu=aTuIp-S-1s,

where Ip is the identity matrix of order p.

The non-centralized moments of W can be computed from

EWn=n!aT-S-n+1s.

Asmussen and Bladt (1997) showed that if WMEp(a, S, s), then the LST f^Wu is rational and can be written as

f^Wu=b1+b2u++bpup-1a1+a2u++apup-1+up, 22

where ai, bi, 1in are real numbers. It should be noted that Eq. (22) holds true when there is no point mass at zero. Then, the representation (a, S, s) is given by

aT=(b1,b2,,bp),S=01000001000001000001-a1-a2-a3-a4-ap,s=00001. 23

For a comprehensive review of matrix-exponential distributions and their sub-class of phase-type distributions, we refer to Bladt and Nielsen (2017).

As it is clear from (19) and (20), the LSTs of the random variables T1 and T are not in the form of (22). That is, the numerator and denominator are not polynomial functions. Therefore, the random variables T1 and T do not have matrix-exponential distributions. However, using the Taylor expansion for the exponential terms involved in (19) and (20), the LSTs and hence the survival functions of T1 and T can be approximated by matrix-exponential distributions. Such a method has been used by Kus et al. (2022) and Chadjiconstantinidis and Eryilmaz (2022). To obtain the approximated values of the survival functions, we first represent (19) and (20) in the form of (22) via Taylor expansion of the exponential terms and then use (23).

For illustration purposes, let us consider the LST of the random variables T1. Multiplying both the numerator and the denominator of the right-hand side of (19) by euδ, we get

f^T1u=-λp1e-λδ+eδu-λp1e-λδ+λeδu+ueδu.

For sufficiently large q, using the Taylor expansion i=0q-1δuii! for the term eδu the LST of T1 can be approximated by the rational LST

f^T~1u=b1+b2u++bquq-1a1+a2u++aquq-1+uq,

where

b1=1-λp1e-λδq-1!δq-1;bi=q-1!/δq-ii-1!,2iq-1
a1=λ1-p1e-λδq-1!δq-1;ai=λi-1!+1δi-2!q-1!δq-i,2iq.

Therefore, the approximated random variable T~1 of T1 has a matrix-exponential distribution, and hence, using these coefficients, the survival function of T1 can be approximated by

PrT~1>t=-aTexpStS-1s,

where

aT=(b1,b2bq),S=01000001000001000001-a1-a2-a3-a4-aq,s=00001,q×1,

and bi’s, ai’s are given as above.

By a similar way, using (20) we can approximate the LST of T by a rational LST, and hence we can approximate the distribution of T by a matrix-exponential distribution. Using Corollary 4, this approach can be easily applied and for the more general case when the interarrival times between successive shocks have a matrix-exponential distribution. The details are omitted (see, for example in Kus et al. (2022) and Chajiconstantinidis and Eryilmaz (2022)).

Numerical illustrations

In this section, we present some illustrative computational results. First, consider the case when the intershock times follow the geometric distribution with mean 1p and when δ=2 and p1=0.7,p2=0.9,p3=0.6. In Table 1, we present the survival functions of T1 and T for selected values of t. Clearly, the survival functions are decreasing in p since we expect more frequent shocks with an increase in p.

Table 1.

Survival functions when the intershock times have geometric distribution

p t PrT1>t PrT>t
0.1 5 0.7283 0.7676
10 0.5979 0.6772
15 0.4910 0.5931
20 0.4032 0.5162
0.2 5 0.4997 0.5489
10 0.3093 0.3802
15 0.1915 0.2586
20 0.1185 0.1735

Table 2 contains approximated values of the survival functions when the intershock times have exponential distribution with mean 1λ when p2=0.9,p3=0.6 and δ=2. As expected, an increase in λ leads to a decrease in survival probabilities.

Table 2.

Survival functions when the intershock times have exponential distribution

λ p1 t PrT1>t PrT>t
0.1 0.7 5 0.7324 0.7746
10 0.6061 0.6810
15 0.5016 0.6033
20 0.4153 0.5256
0.8 5 0.7546 0.7715
10 0.6454 0.6871
15 0.5560 0.6078
20 0.4818 0.5366
0.2 0.7 5 0.5263 0.5744
10 0.3384 0.4107
15 0.2170 0.2895
20 0.1390 0.2019
0.8 5 0.5469 0.5711
10 0.3765 0.4147
15 0.2564 0.2965
20 0.1790 0.2096

Reliability application

Kus et al. (2022) used the mixed δ-shock model to represent a repairable system consisting of active and cold standby components. As noted by Kus et al. (2022), at time t = 0, both of the components are new, and component 1 starts operation first, while component 2 is in a cold standby state. The standby component is switched into operation when the active component (component 1) fails, and a repair action is immediately taken for component 1. Suppose that the repair time for a failed component is fixed as δ, and the component is as good as new after repair. A damage of random size occurs upon the failure of a component. Let Yi+1 denote the magnitude of the damage for the component who livesXi, i = 0, 1, 2, …. If the size of the damage is above d, then the unit cannot be repaired and hence the system fails after the failure of the standby component. Such a repairable system fails either if one of Xi s is less than or equal to δ or the size of the damage for a failed component is above d. The lifetime of the system is then represented as

T=i=0NdXi.

Under the change point setup considered in the present paper, the random variable Nd1 denotes the number of component failures until the first damage that is at least d1. Assume that the size of the damage is determined by a certain environmental factor. Thus, the probabilistic law of the damage size changes after the damage above the threshold d1.

Suppose that there is a desired level for the mean time to failure (MTTF) of the system. If the MTTF of the system is below a given specified level, then an additional standby component may be added to increase the performance of the system. The MTTF of the system can be computed from

ET=1+1+p2-p1-p3F¯δ1-p1F¯δ1-p3F¯δEX,

where Fx=Pr(Xx) is the time to failure distribution of the component. The distribution Fx may be either discrete or continuous depending on the system. If the lifetime of the component corresponds to the number of cycles, then Fx should be modeled as discrete. For example, the lifetimes of batteries may be measured in terms of how many times their charge–discharge processes have been repeated. In this case, a cycle is one complete use of the battery to store power and release it (Willis and Scott (2000)).

Summary and conclusions

In this paper, a mixed shock model that combines extreme and delta shock models has been studied when there is a change in shock size distribution. Computationally efficient matrix-based expressions were obtained for the survival function and mean time to failure of the system. The results extend and generalize the previous results mainly in two directions. First, the model of Eryilmaz and Kan (2021) has been extended to a mixed model. Second, discrete intershock times have also been considered for reliability evaluation of the system. The latter one is also new for the extreme shock model with a change point studied in Eryilmaz and Kan (2021). As a future work, more general models and extensions can be considered. For example, a mixed model that combines run and delta shock models can be studied. The dependence between shock magnitude and the intershock time may be considered as well. The consideration of the change point in the interarrival times is also worthy to investigate since it is applicable to real life systems.

Acknowledgements

The authors thank the anonymous referees for their helpful comments and suggestions, which were useful in improving the paper.

Footnotes

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References

  1. Asmussen S, Bladt M (1997) Renewal theory and queueing algorithms for matrix-exponen-tial distributions. In: Alfa A, Chakravarthy SR (eds) Matrix-analytic methods in stochastic models. Taylor and Francis, Boca Raton, pp 313–341 [Google Scholar]
  2. Bladt M, Nielsen BF (2017) Matrix-exponential Distributions in Applied Probability. Springer, New York [Google Scholar]
  3. Chadjiconstantinidis S, Eryilmaz S (2022) Reliability assessment for censored δ-shock Models. Methodol Comput Appl Probab. 10.1007/s11009-022-09972-z [Google Scholar]
  4. Eryilmaz S (2012) Generalized δ-shock model via runs. Stat Probab Lett 82:326–331 [Google Scholar]
  5. Eryilmaz S (2017) δ-shock model based on Polya process and its optimal replacement policy. Eur J Oper Res 263:690–697 [Google Scholar]
  6. Eryilmaz S, Kan C (2021) A new shock model with a change in shock size distribution. Probab Eng Inf Sci 35:381–395 [Google Scholar]
  7. Goyal D, Hazra NK, Finkelstein M (2022a) On the general δ-shock model. TEST. 10.1007/s11749-022-00810-5 [Google Scholar]
  8. Goyal D, Hazra NK, Finkelstein M (2022b) On the time-dependent delta-shock model governed by the generalized Polya process. Methodol Comput Appl Probab 24:1627–1650 [Google Scholar]
  9. Jiang Y (2020) A new δ-shock model for systems subject to multiple failure types and its optimal order-replacement policy. Proce Instit Mechan Eng Part O J Risk Reliab 234:138–150 [Google Scholar]
  10. Kus C, Tuncel A, Eryilmaz S (2022) Assessment of shock models for a particular class of intershock time distributions. Methodol Comput Appl Probab 24:213–231 [Google Scholar]
  11. Li ZH (1984) Some distributions related to Poisson processes and their application in solving the problem of traffic jam. J Lanzhou Univ Nat Sci 20:127–136 [Google Scholar]
  12. Li ZH, Kong XB (2007) Life behavior of δ-shock model. Statist Probab Lett 77:577–587 [Google Scholar]
  13. Li ZH, Zhao P (2007) Analysis on the δ-shock model of complex systems. IEEE Trans Reliab 56:340–348 [Google Scholar]
  14. Lorvand H, Nematollahi AR, Poursaeed MH (2019) Life distribution properties of a new delta-shock model. Commun Statist Theory Methods 49:3010–3025 [Google Scholar]
  15. Lorvard H, Nematollahi AR (2022) Generalized mixed delta-shock models with random interarrival times and magnitude of shocks. J Comput Appl Math 403:112832 [Google Scholar]
  16. Mallor F, Santos J (2003) Reliability of systems subject to shocks with a stochastic dependence for the damages. TEST 12:427–444 [Google Scholar]
  17. Parvardeh A, Balakrishnan N (2015) On mixed δ-shock models. Statist Probab Lett 102:51–60 [Google Scholar]
  18. Poursaeed MH (2021) Reliability analysis of an extended shock model. Proce Instit Mech Eng Part O J Risk Reliab 235:845–852 [Google Scholar]
  19. Tuncel A, Eryilmaz S (2018) System reliability under shock model. Commun Statist Theory Methods 47:4872–4880 [Google Scholar]
  20. Wang GJ, Zhang YL (2005) A shock model with two-type failures and optimal replacement policy. Int J Syst Sci 36:209–214 [Google Scholar]
  21. Willis HL, Scott WG (2000) Distributed power generation Planning and Evaluation. CRC Press, Taylor & Francis Group

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