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Article

Regression Analysis of Dependent Current Status Data with Left Truncation

1
Center for Applied Statistical Research, School of Mathematics, Jilin University, Changchun 130012, China
2
School of Mathematical Sciences, Capital Normal University, Beijing 100048, China
3
Key Laboratory of Applied Statistics of MOE, School of Mathematics and Statistics, Northeast Normal University, Changchun 130024, China
4
Department of Statistics, University of Missouri, Columbia, MO 65211, USA
*
Author to whom correspondence should be addressed.
Mathematics 2023, 11(16), 3539; https://doi.org/10.3390/math11163539
Submission received: 11 July 2023 / Revised: 2 August 2023 / Accepted: 15 August 2023 / Published: 16 August 2023
(This article belongs to the Special Issue Computational Statistics and Data Analysis, 2nd Edition)

Abstract

:
Current status data are encountered in a wide range of applications, including tumorigenic experiments and demographic studies. In this case, each subject has one observation, and the only information obtained is whether the event of interest happened at the moment of observation. In addition to censoring, truncating is also very common in practice. This paper examines the regression analysis of current status data with informative censoring times, considering the presence of left truncation. In addition, we propose an inference approach based on sieve maximum likelihood estimation (SMLE). A copula-based approach is used to describe the relationship between the failure time of interest and the censoring time. The spline function is employed to approximate the unknown nonparametric function. We have established the asymptotic properties of the proposed estimator. Simulation studies suggest that the developed procedure works well in practice. We also applied the developed method to a real dataset derived from an AIDS cohort research.

1. Introduction

Current status data generally arise in demographic, tumorigenic, and epidemiological fields [1,2,3]. One significant feature of the current status data is that the failure time cannot be accurately observed. On the contrary, it is known that the failure time is less than or greater than the observation or examination time. One common feature of studies that produce such data is that participants are only observed once, perhaps due to the limitation of resources. In this manuscript, we consider the semiparametric regression analysis of current status data with left truncation and informative censoring. In addition, an SMLE method is proposed.
Several methods have been developed to study the current status data. For example, under the proportional hazards (PH) model, ref. [1] considered the efficiency problem and established asymptotic properties of maximum likelihood estimators of regression parameters and baseline cumulative hazard functions. Ref. [4] studied this problem under the additive hazard model and proposed an estimation equation approach to estimate the regression coefficient. Ref. [5] discussed the regression analysis problem under the proportional odds model.
Note that all the literature above assume that the failure time is independent of the examination or observation time. When the two are not independent, the data obtained are generally referred to as current status data with informative observation times or dependent current status data. Currently, some literature studies have discussed the regression analysis of current status data under the assumption of informative censoring. For example, ref. [2] discusses the regression analysis of the current status with informative examination times under the additive hazards regression model. Ref. [6] developed a class of semiparametric transformation models for dependent current status data. The above literature studies introduced frailty to depict the correlation between failure time and examination time. It is well-known that this method needs to assume the specific distribution of the latent variable, which makes the application of this method limited. An alternative way to describe the correlation between the failure time and the examination time is by introducing the copula function. For example, ref. [7] employed this method and discussed the regression analysis of current status data under the PH model. Note that the copula method has been applied in many types of dependent data analyses [8,9,10].
In addition to censoring, truncation is another statistical phenomenon that arises in various fields, including survival analysis, astronomy, epidemiology, and economics [11,12,13,14,15]. Subjects whose failure times were truncated were unable to provide any information to researchers. When only the data of individuals whose event times exceeded a certain random time (i.e., left truncation time) are recorded, left truncation will occur. Under left truncation, individuals with smaller event times are less likely to be observed, leading to bias in the research sample toward larger event times. Currently, some literature studies have developed regression analyses of current status data with left truncation [16,17]. In the following, we will discuss the regression analyses of current status data with left truncation and informative censoring.
The remainder of the article is structured as follows: We introduce the models and assumptions in Section 2. In Section 3, we introduce the SMLE method, including the estimation procedure and asymptotic properties. In Section 4, we conduct simulation studies to evaluate the practical performance of the developed approach. In Section 5, we apply the established approaches to a real dataset. Our discussions and concluding remarks are presented in Section 6.

2. Notation, Assumptions, and Models

Suppose that a failure time study consists of n independent subjects. For subject i, let T i represent the failure time and Z i be the p-dimensional vector of the covariate associated with the subject. As mentioned above, truncation is also very common in practice. For this, assume that, for every subject, there exists a left truncation time A i , such that A i T i . The examination time is denoted by Y i . It is possible that Y is dependent on the failure time T i . Define δ i = I ( T i Y i ) . The observed data can be represented as follows: { D i = ( A i , δ i , Y i , Z i ) , i = 1 , 2 , . . . , n } . In other words, for the failure time T i , we only have current status data with the left truncation available.
We assume that T i follows a Cox model given by
h ( t | Z ) = h 10 ( t ) exp ( α Z ) ,
where h ( t | Z ) is the hazard function of T i given Z i , h 10 ( t ) denotes an unspecified baseline hazard function, and α denotes a p × 1 vector of regression coefficients.
In practice, the covariate may also affect the observation time Y i . So, we suppose that the hazard function of Y i has the following form
h ( y | Z ) = h 20 ( y ) exp ( η Z ) ,
where h 20 ( y ) represents an unknown baseline hazard function, and η represents the regression parameter.
To show the correlation between T i and Y i , we next introduce the Copula function. Let F ( · , · ) represent the joint distribution function of T i and Y i given Z i . Thus, according to Theorem 2.3.3 in [9], there exists a copula function C μ ( u , v ) , satisfying
F ( t , y ) = C μ ( F T ( t ) , F Y ( y ) ) ,
where F T ( · ) and F Y ( · ) denote the marginal distribution function of T i and Y i , respectively, μ is the association parameter representing the correlation between T i and Y i . C μ ( u , v ) satisfies C μ ( u , 0 ) = C μ ( 0 , v ) = 0 , C μ ( u , 1 ) = u , and C μ ( 1 , v ) = v . We then have the conditional distribution function of T i given Y i and Z i , as follows:
P ( T t | Y = y , Z ) = C μ ( u , v ) v | u = F T ( t ) , v = F Y ( y ) = m μ ( F T ( t ) , F Y ( y ) ) .
Let H 10 ( t ) = 0 t h 10 ( s ) d s , H 20 ( y ) = 0 y h 20 ( s ) d s and θ = ( α , η , H 1 , H 2 ) . We define f Y ( · ) to be the marginal density function of Y i , given the covariate, so we can obtain
F T ( t ) = 1 exp H 10 ( t ) exp ( α Z ) ,
F Y ( y ) = 1 exp H 20 ( y ) exp ( η Z ) ,
and
f Y ( y ) = exp H 20 ( y ) exp ( η Z ) h 20 ( y ) exp ( η Z ) .
When δ = 1 , we have
P ( δ = 1 , Y | T A , Y A , Z ) = P ( A T Y , Y | Z ) P ( T A , Y A | Z ) = f Y ( Y ) m μ ( F T ( Y ) , F Y ( Y ) ) m μ ( F T ( A ) , F Y ( Y ) ) 1 F T ( A ) F Y ( A ) C μ ( F T ( A ) , F Y ( A ) ) .
For δ = 0 , we have
P ( δ = 0 , Y | T A , Y A , Z ) = P ( T > Y , Y | Z ) P ( T A , Y A | Z ) = f Y ( Y ) 1 m μ ( F T ( Y ) , F Y ( Y ) ) 1 F T ( A ) F Y ( A ) C μ ( F T ( A ) , F Y ( A ) ) .
Therefore, the likelihood function based on ( A , δ , Y , Z ) is
f Y ( Y ) m μ ( F T ( Y ) , F Y ( Y ) ) m μ ( F T ( A ) , F Y ( Y ) ) δ 1 m μ ( F T ( Y ) , F Y ( Y ) ) 1 δ 1 F T ( A ) F Y ( A ) C μ ( F T ( A ) , F Y ( A ) ) .
Thus, the full likelihood function based on the i.i.d. sample ( A i , δ i , Y i , Z i ) has the following form
L n ( θ ) = i = 1 n f Y ( Y i ) m μ ( F T ( Y i ) , F Y ( Y i ) ) m μ ( F T ( A i ) , F Y ( Y i ) ) δ i 1 m μ ( F T ( Y i ) , F Y ( Y i ) ) 1 δ i 1 F T ( A i ) F Y ( A i ) C μ ( F T ( A i ) , F Y ( A i ) ) .
In the next part, we will consider the maximization of the above likelihood function. It should be noted that, as mentioned by [3], given a specified parametric copula family, the associated parameter μ cannot be identified without prior or additional information. Hence, in the next section, we assume that both the copula functions and the associated parameters are necessary.

3. Maximum Likelihood Estimation

Now, we discuss how to maximize the full likelihood function L n ( θ ) . In fact, it is difficult to directly maximize the likelihood function because this likelihood function contains not only finite-dimensional parameters but also infinite-dimensional parameter functions, H 1 ( · ) and H 2 ( · ) . In order to maximize the likelihood function, we intend to approximate H 1 ( · ) and H 2 ( · ) by linear combinations of some basic functions. Specifically, we intend to use the I-spline function to accomplish this task [18]. Let I d ( t ) d = 1 k + m n represent the I-spline base function, where k and m n are the order of the spline and the number of interior knots, respectively. Additionally, m n = o ( n ν ) and 0 < ν < 0.5 . Then, we define
G n j = H j n : H j n ( s ) = d = 1 k + m n ϕ j d I d ( t ) , ϕ j d 0 , d = 1 , 2 , . . . , k + m n , s [ l , u ]
as the sieve space, j = 1 , 2 , and [ l , u ] denote the range of A i , Y i , i = 1 , 2 , . . . , n . Thus, the functions in G n j are all non-negative and non-decreasing on the interval [ l , u ] [18]. Therefore, we can employ H j n ( · ) to approximate or replace H j ( · ) in the likelihood function, and estimate the regression parameters α , η and coefficients ϕ j = { ϕ j d } d = 1 k + m n simultaneously by maximizing the L n ( θ ) subject to ϕ j d 0 , j = 1 , 2 .
One issue when using splines is how to choose k and m n . An easy way to do this for a given problem is to try several different values for k and m n and compare the results. Furthermore, we can employ the Bayesian information criteria (BIC) to choose k and m n , which give the smallest BIC values.
Let θ ^ n = ( α ^ n , η ^ n , H ^ 1 n ( · ) , H ^ 2 n ( · ) ) represent the estimator of θ described above and θ 0 = ( α 0 , η 0 , H 10 ( · ) , H 20 ( · ) ) be the true value of θ . To establish the asymptotic properties, we need to describe the regularity conditions first.
(C1)
The copula functions are differentiable and the partial derivatives satisfy the Lipschitz condition.
(C2)
The covariate Z has bounded support in R p .
(C3)
(i) If a constant ϵ 0 and the constant vector ζ 0 satisfy ζ 0 T Z = c 0 almost surely, then ϵ 0 = 0 and ζ 0 = 0 . (ii) Assume that for any open set B in [ 0 , 1 ] × [ 0 , 1 ] , ω C ( B ) > 0 , where ω C represents the probability measure generated by the copula function C .
(C4)
For ϑ = ( α , η ) , suppose that the Fisher matrix E ( S ϑ S ϑ ) is positive-definite, where S ϑ is defined in Appendix A.
(C5)
Let H j ( k ) ( · ) denote the kth derivative of H j ( · ) , j = 1 , 2 . Assume they are Holder-continuous with exponent ω . In other words, there exists a positive constant K and some η ( 0 , 1 ] , such that | H j ( k ) ( t 1 ) H j ( k ) ( t 2 ) | K | t 1 t 2 | ω for all t 1 , t 2 ( l , u ) . In the following, let r = k + ω .
According to [19,20], the aforementioned conditions are typically moderate and meet in practical situations. The following theorems provide the large sample properties of the estimators. Here, for function g, let g ( X ) 2 = ( | g ( X ) | 2 d P ) 1 / 2 , where P is the probability measure generated by X.
Theorem 1.
Assume that the regularity conditions C1–C4 are satisfied. Then,
α ^ n 0 , η ^ n 0 ,
H ^ 1 n H 10 2 0 , H ^ 2 n H 20 2 0
almost surely.
Theorem 2.
Assume that the regularity conditions C1–C4 are satisfied. Then
H ^ 1 n H 10 2 + H ^ 2 n H 20 2 = O p ( n ( 1 ν ) / 2 + n r ν ) .
Theorem 3.
Assume that conditions C1–C5 are satisfied and r > 2 . Then, as n , we have n ( ( α ^ n α 0 ) , ( η ^ n η 0 ) ) d N ( 0 , Σ ) ; the definition of Σ is in Appendix A.
We provide the proof of the above theorems in the appendix. In order to estimate the covariance matrix, we recommend a common and direct method based on the sieve likelihood function, i.e., using the inverse of the observed information matrix. The observed information may be poorly conditioned or high-dimensional, so this method might be computationally demanding. Nevertheless, the simulation results shown in the following section suggest that it typically performs effectively, particularly when k and m n are not very big.

4. Simulation Study

In this section, simulation studies are conducted to evaluate the performance of the developed procedure. We suppose that the Z i covariates are Bernoulli (0.5). We first generate the left truncation time A i from the exponential distribution with parameters a, where constant a is selected to provide a suitable percentage of the left truncation. We set H 10 ( t ) = t , and T i is generated from model (1). To generate the examination time Y i , we consider the following three copula models:
C μ ( u , v ) = u v + μ u v ( 1 u ) ( 1 v ) , 1 μ 1 , log μ 1 ( 1 μ u ) ( 1 μ v ) 1 μ , μ > 0 , μ 1 , exp [ ( log u ) μ + ( log v ) μ ] 1 / μ , μ 1 .
They are the FGM, Frank, and Gumbel models, respectively. As mentioned above, the association parameter μ here indicates the correlation between T and Y. Since the range of μ in the above three copula models are not the same, one needs a uniform measure of association between T and Y, such as Kendall’s τ . For the FGM model, τ = 2 μ / 9 , and τ = 1 + 4 h 1 B 1 ( h ) 1 for the Frank model, h = log μ and B 1 ( h ) = h 1 0 h x ( e x 1 ) 1 d x . Under the Gumbel model, the relationship is τ = 1 1 / μ .
Based on a fixed copula function, we set H 20 ( y ) = y , then the examination time Y i is generated from the conditional distribution, given T i . Specifically, we first generate a random number b U ( 0 , 1 ) ; given T i = t i and b, we can solve the following equation for Y i = y i ,
P ( Y i y i | T = t i , Z i ) = C μ ( u , v ) u | u = F T ( t i ) , v = F Y ( y i ) = b .
For the spline functions, we employ the quadratic splines with the 1 / 4 , 1 / 2 , 3 / 4 quantiles of the pooled set of all A i ’s and Y i ’s as three interior knots. The results shown below are based on 1000 replications.
Table 1 and Table 2 report the simulation results under the FGM model with sample sizes n = 200 and 400. The results show the estimated bias (bias, empirical average of the parameter estimator minus the true value), the standard error of the parameter estimator (SSE), the empirical average of the standard error estimator (SEE), and the empirical coverage percentage of the 95% confidence interval (CP). Figure 1 presents the boxplots of estimators of α and η with α 0 = 0.4 and η 0 = 0.4 under the FGM copula. It can be seen that the estimators have a slight bias, and the bias becomes smaller as n increases. The true variabilities are accurately reflected by the variance estimators, and the confidence intervals have proper coverage probabilities, i.e., the normal approximation to the distribution of the estimated regression parameters seems reasonable. The estimation results based on the Frank and Gumbel copulas are presented in Table 3, Table 4, Table 5 and Table 6; they yield comparable conclusions to those given in Table 1.
Regarding model misspecification, Table 7 shows the estimation results of the simulated data generated under the Frank model but obtained from the FGM model. In the table, τ E presents Kendall’s τ for the estimation. This table suggests that the estimator of α may be biased when copula is specified correctly but τ is specified wrong. When τ is specified correctly but the copula model is misspecified, the estimator seems relatively reasonable. In addition, the estimator of η seems to be less sensitive to the choice of the association parameter τ or the copula model. We attempted other set-ups and acquired comparable conclusions.

5. An Application

Now, we apply our method to an AIDS cohort study of hemophiliacs, as analyzed by [21], among others. This study included 257 hemophilia patients receiving treatment at medical centers in France since 1978. Due to the potential contamination of blood factors used for treatment, these patients were in danger of contracting HIV-1. In this study, the failure time represents the duration from HIV-1 infection to the AIDS diagnosis. Patients were divided into two groups—heavily and lightly treated groups—based on the blood volume they received. Here, the primary objective was to evaluate the effect of the treatment on the total time to HIV diagnosis from the beginning of the treatment.
HIV-1 contraction and the time of AIDS diagnosis cannot be accurately observed since the patients were only examined regularly; only the time intervals that include HIV-1 contraction and AIDS diagnosis can be observed. Here, the left truncation time is taken as the midpoint of the examination interval for HIV-1 infection, and the observation time is taken as the right endpoint of the examination interval for AIDS diagnosis [21]. For our analysis, we focus on the 188 patients identified as HIV-1-infected during the study. Of these, 41 had been diagnosed with AIDS.
Let the covariate Z i be 1 if the ith subject is in the heavily treated groups, and 0, otherwise. Following the simulation part, we still use the quadratic spline functions with m n = 3 , 4 , 5 , 6 , 7 , or 8 for approximation, and use FGM, Frank, and Gumbel copulas for dependent censoring. In the following, the BIC values were calculated to find the smallest one, which is given by the FGM copula model with m n = 7 and τ = 0.2 . We present the results obtained under the FGM model in Table 8 with m n = 6 and 7, and several τ values. The table shows the estimated treatment effect α ^ n , the estimated effect on the examination time η ^ n , the estimated standard error (SE), and the p-value for testing the absence of treatment effects. The results indicate that the patients in the heavily treated group had a higher hazard of being diagnosed with AIDS, which is similar to the conclusions presented in [16].

6. Discussion and Concluding Remarks

In the previous sections, we discussed the regression analysis of dependent current status data with left truncation and developed an SMLE method for inference. The developed procedure uses the copula function to depict the correlation between the failure time and the examination time, and the spline function is used to approximate the known nonparametric function in the model. Simulation studies suggest that the considered approach works well in practice.
For the presented approach, one may consider other statistical models, like the linear transformation model and accelerated failure model, and develop comparable estimation procedures. In our approach, we applied the copula model to construct the joint distribution. One future study direction will be to apply the frailty methods to describe the connection between the two and establish corresponding statistical methods. Furthermore, in our method, while we adopted the I-splines to approximate unknown functions in our approach, other basis functions can also be utilized, such as monotone B-splines, Bernstein polynomials, and even step functions.

Author Contributions

Methodology, T.H.; Software, M.Z. and D.X.; Writing—original draft, D.X.; Writing—review & editing, J.S.; Supervision, J.S.; Project administration, S.Z.; Funding acquisition, D.X. All authors have read and agreed to the published version of the manuscript.

Funding

Xu’s work was partially supported by the National Natural Science Foundation of China (NSFC) (12001093) and the National Key Research and Development Program of China (no. 2020YFA0714102). Zhao’s work was partially supported by the National Natural Science Foundation of China (NSFC) (12071176).

Data Availability Statement

Not applicable.

Conflicts of Interest

The authors declare no conflict of interest.

Appendix A. Proofs of Theorems 1–3

In the following proofs, let P g = g ( x ) d P ( x ) and P n g = 1 n i = 1 n g ( D i ) represent the empirical process of g ( D ) . Let
Θ n = θ n = ( α , η , H 1 n , H 2 n ) B H n 1 H n 2
be the sieve space for θ , where B = ( α , η ) R 2 p , α + η H , and H be a positive number. In the following, let K , H , H n , C represent constants whose values may vary at different locations.
Proof of Theorem 1.
Let ( θ , D ) represent the log-likelihood of one observation D = ( δ , A , C , Z ) . For consistency, let L n = { ( θ , D ) : θ Θ n } .
According to Lemma A.1 in [22], the covering number satisfies
N ϵ , L n , L 1 ( P n ) K H 2 p H n 2 ( k + m n ) ϵ p m ,
where p k = 2 p + 2 ( k + m n ) . In addition, by inequality (31) in [23], we acquire
sup θ Θ n | P n ( θ , D ) P ( θ , D ) | a . s . 0 .
Let Q ( θ , D ) = ( θ , D ) , ξ 1 n = sup θ Θ n | P n Q ( θ , D ) P Q ( θ , D ) | , ξ 2 n = P n Q ( θ 0 , D ) P Q ( θ 0 , D ) , and K ϵ = { θ : d ( θ , θ 0 ) ϵ , θ Θ n } . Hence, we have
inf K ϵ P Q ( θ , D ) = inf K ϵ P Q ( θ , D ) P n Q ( θ , D ) + P n Q ( θ , D )
ξ 1 n + inf K ϵ P n Q ( θ , D ) .
If θ ^ n K ϵ , then
inf K ϵ P n Q ( θ , D ) = P n Q ( θ ^ n , D ) P n Q ( θ 0 , D ) = ξ 2 n + P Q ( θ 0 , D ) .
Thus, by condition (C3), we have inf K ϵ P H ( θ , D ) P H ( θ 0 , D ) = ρ ϵ > 0 . Combining (A2) and (A3), we can obtain inf K ϵ P H ( θ , D ) ξ 1 n + ξ 2 n + P Q ( θ 0 , D ) = ξ n + P Q ( θ 0 , D ) with ξ n = ξ 1 n + ξ 2 n . Thus, ξ n ρ ϵ and { θ ^ n K ϵ } { ξ n ρ ϵ } . Therefore, by (A1), we have ξ 1 n a . s . 0 and ξ 2 n a . s . 0 . Finally, we conclude that i = 1 n = i { θ ^ n K ϵ } i = 1 n = i { ξ n ρ ϵ } . □
Proof of Theorem 2.
In order to prove Theorem 2, for any κ > 0 , define F κ = { ( θ n 0 , D ) ( θ , D ) : θ Θ n , d ( θ , θ n 0 ) κ } with θ n 0 = ( α 0 , η 0 , H 1 n 0 , H 2 n 0 ) . According to [24], it can be shown that log N [ ] ( ε , F κ , · 2 ) M N log ( κ / ε ) , where N = 2 ( k + m n ) . After a little bit of algebra, we can obtain ( θ n 0 , D ) ( θ , D ) 2 2 M κ 2 for any ( θ n 0 , D ) ( θ , D ) F κ .
Hence, based on Lemma 3.4.2 in [25], we have that
E P n 1 / 2 ( P n P ) F κ M J κ ( ε , F κ , · 2 ) { 1 + J κ ( ε , F κ , · 2 ) κ 2 n 1 / 2 } ,
where J κ ( ε , F κ , · 2 ) = 0 κ { 1 + log N [ ] ( ε , F κ , · 2 ) } 1 / 2 d ε M N 1 / 2 κ . Therefore, we have φ n ( κ ) = M ( N 1 / 2 κ + N / n 1 / 2 ) , and φ n ( κ ) / κ decreases with κ . In addition, we also have r n 2 φ n ( 1 / r n ) = r n N 1 / 2 + r n 2 N / n 1 / 2 < 2 n 1 / 2 , here, r n = n 1 / 2 / N 1 / 2 = n ( 1 ν ) / 2 with 0 < ν < 0.5 . Based on Theorem 3.2.5 in [25], we obtain n ( 1 ν ) / 2 d ( θ ^ , θ n 0 ) = O P ( 1 ) . Then, according to Lemma A1 in [26], we can obtain d ( θ ^ , θ 0 ) = O p ( n ( 1 ν ) / 2 + n r ν ) . □
Proof of Theorem 3.
First, let θ 0 represent the true value of θ , and let V represent the linear span of Θ θ 0 . Define σ n = n r / ( 1 + 2 r ) . For any θ { θ Θ 0 : θ θ 0 = O ( σ n ) } , denote
˙ ( θ , D ) [ ζ ] = d ( θ + s ζ , D ) d s | s = 0
to be the directional derivative of l ( θ , D ) at the direction ζ W . Define
< ζ , ζ ˜ > = P ˙ ( θ , D ) [ ζ ] ˙ ( θ , D ) [ ζ ˜ ]
the Fisher inner product on W, and the corresponding norm ζ 1 / 2 = < ζ , ζ > . Let W ¯ denote the closure of W under the Fisher norm. Therefore, ( W ¯ , < · , · > ) is a Hilbert space.
Let
η ( θ ) = c 1 α + c 2 η ,
where c = ( c 1 , c 2 ) is a vector with c 1 . So, η ( θ ) is a linear function on W ¯ . For ζ W , let
η ˙ ( θ 0 ) [ ζ ] = d η ( θ 0 + s ζ ) d s | s = 0 .
Then we have η ( θ ) η ( θ 0 ) = η ˙ ( θ 0 ) [ θ θ 0 ] . Based on the Riesz theorem, there exists ζ * W ¯ , so that η ˙ ( θ 0 ) [ ζ ] = < ζ * , ζ > for all ζ W ¯ with ζ * 2 = η ˙ ( θ 0 ) .
Since c ( ( α ^ α 0 ) , ( η ^ η 0 ) ) = η ( θ ^ ) η ( θ 0 ) = η ˙ ( θ 0 ) [ θ ^ θ 0 ] = < θ ^ θ 0 , ζ * > , by the Cram é r–Wold device, in order to prove Theorem 3, it suffices to show
n < θ ^ θ 0 , ζ * > d N ( 0 , b Σ b ) .
Recall that ϑ = ( α T , η T ) T . For each component, ϑ q , q = 1 , 2 , , 2 p , let ψ q * = ( c 1 q * , c 2 q * ) be the minimizer of
E ϑ · e q c 1 [ c 1 q ] c 2 [ c 2 q ] 2 ,
where ϑ = ( α , η ) , e q is a 2 p -dimensional vector whose qth element is 1 and all other elements are 0. c 1 [ c 1 ] and c 2 [ c 1 ] denote the directional derivatives with respect to H T and H C , respectively. Then, according to a similar method by [27], we can obtain ζ * 2 = η ˙ ( θ 0 ) = sup ζ W ¯ : ζ > 0 | η ˙ ( θ 0 ) [ ζ ] | ζ = b Σ b , where Σ = [ E ( S ϑ S ϑ ) ] 1 , S ϑ = { ϑ c 1 * [ c 1 * ] c 2 * [ c 2 * ] } . This completes the proof of Theorem 3. □

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Figure 1. Boxplots for the estimators of α and η with α 0 = 0.4 and η 0 = 0.4 under the FGM copula.
Figure 1. Boxplots for the estimators of α and η with α 0 = 0.4 and η 0 = 0.4 under the FGM copula.
Mathematics 11 03539 g001
Table 1. Simulation results under the FGM model with n = 200 .
Table 1. Simulation results under the FGM model with n = 200 .
α ^     η ^    
α 0 η 0 τ 0   Bias    SSE    SEE    CP    Bias    SSE    SEE    CP  
0−0.4−0.2−0.00340.23220.22840.952−0.02020.16050.15760.936
−0.1−0.01410.21190.21450.953−0.00770.15650.15080.953
0−0.01350.20610.20560.964-0.00870.14180.14520.960
0.1−0.00010.20020.19800.9460.00320.14420.14200.954
0.20.00450.19220.19010.9500.00230.13590.13980.952
0−0.20.02060.23400.22810.952−0.00520.15870.15500.940
−0.1−0.01080.21620.21480.9510.00130.14850.14760.945
0−0.01000.20300.20340.9520.00900.14130.14260.966
0.1−0.00870.21060.19440.9120.00140.14490.13900.948
0.2−0.00220.19060.18640.951−0.00410.14110.13610.943
0.4−0.20.00660.26120.23630.9320.00930.16170.15800.946
−0.10.01200.22820.22090.9340.01810.15140.15050.966
00.01580.21600.20970.9420.01120.14980.14540.952
0.10.00770.20440.20160.9380.00100.15090.14210.934
0.20.01960.20250.19190.9370.01380.14470.13990.951
0.4−0.4−0.2−0.00660.22740.22230.949−0.01010.16640.16130.947
−0.10.02190.22240.21590.958−0.01130.15450.15210.942
00.01130.21700.21090.949−0.00240.15510.14530.935
0.10.03530.22630.20600.9360.00120.14970.14230.938
0.20.01220.20580.20040.9490.00200.14240.14130.959
0−0.20.02180.23150.22420.9460.00520.16140.15810.938
−0.10.02130.22990.21530.938−0.00890.15530.14880.952
00.03140.20960.20670.938−0.00160.14950.14290.934
0.10.02220.20910.19890.9450.00020.14730.13890.935
0.20.03660.19650.19150.9410.00520.13310.13570.961
0.4−0.20.02500.25420.23450.9330.00420.16820.15970.947
−0.10.03730.24070.22120.9260.00790.15040.15120.954
00.02690.20810.21090.9500.00740.13660.14540.964
0.10.00100.20090.20170.9570.01470.14170.14160.955
0.20.01480.19410.19530.9370.00760.13880.13880.949
Table 2. Simulation results under the FGM model with n = 400 .
Table 2. Simulation results under the FGM model with n = 400 .
α ^     η ^    
α 0 η 0 τ 0   Bias    SSE    SEE    CP    Bias    SSE    SEE    CP  
0−0.4−0.20.00990.16430.15890.945−0.01580.11910.11060.929
−0.1−0.01040.15860.14980.940−0.01540.10270.10580.950
0−0.00200.14320.14300.958−0.00470.10560.10230.942
0.10.00740.13760.13720.9630.00370.09790.10020.955
0.20.01910.14440.13220.9190.00690.10170.09850.937
0−0.20.00780.16550.15940.941−0.00800.10700.10860.945
−0.10.00130.15020.14930.943−0.00440.10000.10370.957
00.00010.14440.14160.944−0.00420.09560.10040.960
0.10.00160.13990.13490.940−0.00110.09860.09800.952
0.20.00010.13290.12900.9550.00840.09640.09610.951
0.4−0.20.01180.16550.16370.956−0.00100.11000.11040.952
−0.10.01630.16430.15370.9340.00340.10930.10570.942
00.00120.14880.14600.9420.00600.10570.10230.944
0.10.01190.14080.14010.9370.01000.09890.10030.955
0.20.00550.13870.13410.933−0.00230.09400.09860.957
0.4−0.4−0.20.00190.16320.15510.930−0.01390.11750.11290.938
−0.1−0.01440.15360.14940.949−0.00660.10720.10680.953
00.01180.15260.14490.942−0.00180.10290.10230.958
0.10.01330.14700.14110.941−0.00170.10440.10070.937
0.20.00270.14360.13760.9310.00470.09570.09980.957
0−0.20.02980.15740.15650.949−0.01420.11770.11020.927
−0.10.01310.14460.14910.963−0.00630.10910.10470.935
00.01270.14910.14340.9440.00520.09540.10060.966
0.10.01250.13790.13770.9580.00470.10320.09810.932
0.20.00470.14140.13300.950−0.00460.10150.09620.934
0.4−0.20.02630.16870.16380.938−0.00010.11320.11190.948
−0.10.02050.16020.15420.9280.00620.10680.10640.952
00.01310.15380.14670.9500.01060.10320.10260.938
0.10.00140.14580.14070.9370.00270.10520.09990.943
0.20.00010.12860.13510.9550.00880.09370.09780.965
Table 3. Simulation results under the Frank model with n = 200 .
Table 3. Simulation results under the Frank model with n = 200 .
α ^     η ^    
α 0 η 0 τ 0   Bias    SSE    SEE    CP    Bias    SSE    SEE    CP  
0−0.4−0.25−0.00360.23130.22620.945−0.00340.16420.16180.941
−0.1−0.01090.22870.21420.948−0.02020.15450.15100.942
−0.05−0.01360.20980.20930.942−0.01550.15600.14750.942
0.050.00530.21020.20140.934−0.00780.14560.14330.938
0.10.00800.19310.19680.951−0.01730.14820.14210.941
0.250.00280.19400.18660.935−0.00750.13550.13970.961
0−0.250.01040.24270.22600.9310.00510.16400.15870.943
−0.10.00840.22610.21310.9360.00170.14790.14760.958
−0.050.00080.22310.20830.924−0.00930.14140.14480.954
0.05−0.00700.19390.19860.964−0.00610.14040.14060.964
0.10.01080.20890.19320.9340.00860.13790.13900.954
0.250.01220.19210.17960.9300.01280.13580.13500.946
0.4−0.250.00520.23740.23330.9450.02160.17080.16150.937
−0.10.01630.22990.22000.9520.02320.15490.15040.936
−0.050.00730.22260.21480.9470.00660.15290.14760.945
0.050.00500.21490.20390.9270.00360.14940.14340.945
0.10.00100.20180.19910.9530.01400.14160.14210.949
0.250.00210.20100.18480.921−0.00550.13850.13940.953
0.4−0.4−0.25−0.00890.21830.22340.962−0.00980.16460.16570.946
−0.10.00870.22260.21460.935−0.01630.15270.15170.947
−0.05−0.00120.21280.21180.964−0.00670.14690.14800.948
0.050.03490.22210.20880.942−0.01260.15290.14360.928
0.10.03890.20980.20500.956−0.00180.14450.14240.950
0.250.02170.20190.20070.9530.00650.14330.14300.931
0−0.250.02710.22690.22410.939−0.00390.17030.16140.937
−0.10.04080.22060.21440.9460.00200.15180.14870.942
−0.050.03550.22140.21170.941−0.00740.14610.14550.939
0.050.01890.21160.20240.9340.00820.14040.14070.946
0.10.01930.21090.19960.9520.00270.14050.13890.954
0.250.02590.20090.18880.9430.01200.13770.13540.945
0.4−0.250.03220.24500.23530.937−0.00120.16050.16430.953
−0.10.03150.22780.22050.9350.00820.14830.15090.959
−0.050.03450.21050.21600.9440.00570.15370.14820.940
0.050.02410.20620.20640.9560.01180.14400.14340.934
0.10.03870.19900.20170.9530.00760.15330.14180.927
0.250.00590.20110.18980.9350.00010.13980.13750.951
Table 4. Simulation results under the Frank model with n = 400 .
Table 4. Simulation results under the Frank model with n = 400 .
α ^     η ^    
α 0 η 0 τ 0   Bias    SSE    SEE    CP    Bias    SSE    SEE    CP  
0−0.4−0.25−0.00310.16170.15850.942−0.01470.11800.11280.932
−0.1−0.00700.15430.14950.948−0.00910.10210.10560.956
−0.05−0.00660.14590.14610.956−0.01210.10580.10390.938
0.050.00270.14120.13970.956−0.00020.10080.10110.952
0.10.00330.13820.13690.9390.00220.09790.10000.957
0.250.01150.12410.13040.9610.00070.09740.09970.951
0−0.25−0.00870.16540.15750.9350.00630.11200.11060.947
−0.10.01000.15760.14850.928−0.00770.10900.10370.930
−0.050.00110.14990.14500.9400.00150.10470.10190.946
0.050.00530.14200.13800.949−0.01020.09630.09920.959
0.1−0.00220.14090.13440.9360.00050.09270.09800.962
0.250.00790.12500.12420.9580.00080.09460.09550.954
0.4−0.250.01800.16050.16230.9460.00740.11560.11300.950
−0.10.02630.15420.15300.9380.00150.10810.10540.950
−0.050.00790.15760.14970.9260.00740.10590.10390.934
0.050.00350.14340.14240.9480.00690.10550.10110.938
0.10.00340.14080.13890.9480.00460.10150.10020.946
0.250.00970.13030.12900.942−0.00050.10260.09850.938
0.4−0.4−0.250.00300.16350.15440.933−0.01110.10950.11590.959
−0.10.01090.15150.14910.956−0.00760.10270.10650.958
−0.050.01000.15420.14690.946−0.00490.10350.10430.960
0.050.00630.13910.14310.9520.00040.10340.10120.952
0.10.01530.14040.14180.951−0.00030.10420.10070.951
0.250.01190.14030.13860.9390.00130.10400.10190.949
0−0.250.01120.16490.15630.942−0.00150.12830.11330.918
−0.10.01140.14040.14900.958−0.01040.10790.10450.938
−0.050.00970.14680.14610.9540.00060.10030.10230.946
0.050.01990.13740.14050.9520.00100.09860.09910.954
0.10.01550.14240.13780.9360.00400.09620.09800.952
0.250.01460.13660.13050.9320.00480.09930.09540.932
0.4−0.250.02730.17960.16260.9110.00330.11470.11470.943
−0.10.03810.15250.15410.9440.00050.11000.10620.946
−0.050.00940.15320.15000.9440.00080.10580.10420.946
0.050.01210.14070.14340.9420.00160.09800.10110.962
0.10.01380.13730.14010.9590.00870.10480.09990.931
0.25−0.00190.12830.13070.9580.00470.10180.09740.948
Table 5. Simulation results under the Gumbel model with n = 200 .
Table 5. Simulation results under the Gumbel model with n = 200 .
α ^     η ^    
α 0 η 0 τ 0   Bias    SSE    SEE    CP    Bias    SSE    SEE    CP  
0−0.40.050.00540.20640.19800.944−0.01350.15060.14470.946
0.10.00250.20730.19140.938−0.00800.15060.14390.958
0.25−0.01230.18330.17270.943−0.00370.15390.14240.931
00.05−0.00520.19740.19650.9580.01580.14500.14170.954
0.10.00720.19470.18940.9390.00280.14230.14090.953
0.250.01130.18140.17190.937−0.00160.14720.13850.941
0.40.050.02480.20060.20380.9480.01080.14090.14450.964
0.10.01820.20380.19870.9310.00070.15160.14380.939
0.250.03580.19080.18430.9330.01300.14890.14270.941
0.4−0.40.050.01030.21160.20300.9490.00310.14570.14580.953
0.10.02110.21190.20010.9320.00240.14410.14710.954
0.25-0.04060.19050.18450.9270.01140.15470.14890.943
00.050.02620.21490.19910.9350.01760.14940.14260.937
0.10.02050.19380.19130.9500.01520.14260.14280.956
0.250.00790.17570.17360.9480.02200.14380.14190.938
0.40.050.02600.20410.20250.9410.01690.14740.14500.947
0.10.02790.20610.19490.9390.02590.15540.14480.931
0.250.01150.17130.17350.9650.01170.14290.14160.955
Table 6. Simulation results under the Gumbel model with n = 400 .
Table 6. Simulation results under the Gumbel model with n = 400 .
α ^     η ^    
α 0 η 0 τ 0   Bias    SSE    SEE    CP    Bias    SSE    SEE    CP  
0−0.40.05−0.00330.14640.13720.9280.00370.09990.10150.944
0.1−0.01830.14160.13310.9330.00210.11270.10080.929
0.25−0.01400.12460.12140.9440.01420.10180.10040.950
00.05−0.00540.14030.13690.945−0.00650.10270.09970.943
0.1−0.00470.13450.13240.944−0.00870.10230.09890.940
0.250.00430.12820.12050.9360.01790.10500.09710.922
0.40.050.00010.14490.14270.9440.00110.10270.10160.952
0.10.01360.13760.13870.9520.00230.10750.10100.946
0.250.03080.13820.12830.921−0.00190.11340.09970.908
0.4−0.40.050.01040.15020.14120.9430.00240.10510.10220.957
0.1−0.01510.15180.13710.9210.00100.09670.10270.969
0.25−0.02460.13530.12790.9270.02460.11170.10420.927
00.050.00960.13580.13740.9500.00540.09850.10020.952
0.1−0.00320.12660.13240.9530.01030.10340.09980.941
0.25−0.00480.13370.12080.9190.00990.10360.09900.935
0.40.050.01270.14070.14090.9480.01250.10280.10210.940
0.10.00550.12560.13480.9710.02140.09820.10130.953
0.250.00970.11970.12190.9530.00540.10350.09960.933
Table 7. Simulation results for model misspecification.
Table 7. Simulation results for model misspecification.
α ^ η ^
α 0 η 0 τ 0 τ E   Bias    SSE    SEE    CP    Bias    SSE    SEE    CP  
000.1−0.2−0.00490.22280.20460.9300.00190.16680.16270.946
−0.10.00580.20690.20180.9520.01010.15460.14970.950
0.10.00390.18670.19420.9540.00880.13890.13880.940
0.20.02870.20350.18840.9250.00760.14060.13700.949
0.2−0.20.00760.21270.19810.936−0.01540.16120.16390.962
−0.10.00920.20830.19740.9360.00640.14480.15050.960
0.1−0.00340.19460.18980.9390.01150.13520.13860.953
0.20.00210.18600.18350.932−0.00290.13760.13590.940
0.40.1-0.2−0.10600.21690.21120.8910.05330.16290.16630.937
−0.1−0.05840.21310.20870.9320.02830.14280.15240.964
0.10.00800.21130.20100.939−0.00230.14860.14190.935
0.20.04380.19500.19380.933−0.00250.14340.14040.937
0.2−0.2−0.14740.22180.20620.8810.10550.17740.16820.893
−0.1−0.12130.21570.20350.8860.04950.15330.15390.942
0.1−0.05710.19730.19600.9440.01080.14470.14140.944
0.2−0.00520.18950.19350.9430.01220.15090.14050.917
0.400.1−0.20.02030.22240.20290.926−0.05460.16410.16620.928
−0.10.04310.21360.20320.942−0.03700.14810.15080.948
0.10.02190.20440.19850.9500.01350.14370.13780.938
0.20.00670.19660.19500.9540.01470.13230.13680.960
0.2−0.20.01880.20700.19740.936−0.08120.17000.16420.920
−0.10.05370.20780.19840.935−0.03220.15780.15180.929
0.10.03820.19590.19480.9540.00340.14530.13830.942
0.20.02890.20830.19040.9330.00930.13460.13610.951
0.40.1−0.2−0.07430.22860.20720.909−0.01030.17240.16660.951
−0.1−0.03950.21840.20520.936−0.00420.15450.15320.954
0.10.02400.21110.20230.9300.02010.14120.14160.952
0.20.03830.20650.19850.9540.01930.14310.14000.944
0.2−0.2−0.06880.22220.20000.898−0.00250.17060.16760.956
−0.1−0.04520.21340.20110.9120.00990.14730.15450.960
0.1−0.01620.19970.19680.9490.01800.14630.14110.931
0.20.00460.19080.19170.9590.00630.13680.13880.949
Table 8. Estimation results for the AIDS data.
Table 8. Estimation results for the AIDS data.
τ α ^ SEp-Value η ^ SEp-ValueBIC
m n = 6
−0.20.22390.29680.45060.05380.14680.71391049
−0.10.57070.31760.07240.29410.15980.06571052
00.82180.33350.01370.10940.14620.45441025
0.10.38910.31220.21270.18170.12460.14491002
0.20.91030.33780.00710.07480.11220.5053982
m n = 7
−0.20.28980.29530.32650.24970.14800.09151015
−0.10.59880.32090.06210.33710.17400.05271022
00.67360.32930.04080.32850.14690.02541000
0.10.24000.45740.59980.08380.12590.5055972
0.20.53620.22890.01910.13860.11260.2185956
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Zhang, M.; Zhao, S.; Hu, T.; Xu, D.; Sun, J. Regression Analysis of Dependent Current Status Data with Left Truncation. Mathematics 2023, 11, 3539. https://doi.org/10.3390/math11163539

AMA Style

Zhang M, Zhao S, Hu T, Xu D, Sun J. Regression Analysis of Dependent Current Status Data with Left Truncation. Mathematics. 2023; 11(16):3539. https://doi.org/10.3390/math11163539

Chicago/Turabian Style

Zhang, Mengyue, Shishun Zhao, Tao Hu, Da Xu, and Jianguo Sun. 2023. "Regression Analysis of Dependent Current Status Data with Left Truncation" Mathematics 11, no. 16: 3539. https://doi.org/10.3390/math11163539

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