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Estimation for spatial semi-functional partial linear regression model with missing response at random

  • Tawfik Benchikh EMAIL logo , Ibrahim M. Almanjahie , Omar Fetitah and Mohammed Kadi Attouch
Published/Copyright: March 13, 2025
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Abstract

The aim of this article is to study a semi-functional partial linear regression model (SFPLR) for spatial data with responses missing at random (MAR). The estimators are constructed using the kernel method, and some asymptotic properties, such as the probability convergence rates of the nonparametric component and the asymptotic distribution of the parametric and nonparametric components, are established under certain conditions. Next, the performance and superiority of these estimators are presented and examined through a study on simulated data, comparing our semi-functional partially linear model with the MAR estimator to the semi-functional partially linear model with the full-case estimator, and the functional nonparametric regression model estimator with MAR. The results indicate that the proposed estimators outperform traditional estimators as the amount of randomly missing data increases. Additionally, a study is conducted on real data regarding the modeling of pollution levels using our model, incorporating covariates such as average daily temperature as a functional variable, alongside maximum daily mixing height, total daily precipitation, and daily primary aerosol emission rates as explanatory variables.

MSC 2010: 62H12; 62G07; 62G35; 62G20

1 Introduction

Nowadays, statistical techniques are essential for the analysis of massive volumes of spatial data, particularly in fields such as environmental sciences, climate, geography, econometrics, medicine, biology, and other applied areas. For example, such data are commonly encountered in environmental and socioeconomic studies, where the goal is to assess the effect of environmental or other ecological parameters on the variability of biomass and the spatial distribution of species or groups of species in marine fauna [1]. These datasets are often sparse, high-dimensional, and include highly correlated responses. This is also the case in oil exploration, where the aim is to predict the physical parameters of oil layers while considering other available parameters from oil fields [2]. Additionally, research on hyperspatial image processing, as developed by [3], involves similar challenges. These data are collected continuously at different stations, and the goal is to understand the relationships between these multiple correlated responses. Consequently, high-dimensional data become functional data, which are then processed and analyzed using functional data analysis (FDA) methods. Such data are referred to as functional data with spatial correlation. Functional geostatistics is a field of application for this type of data. The theoretical and practical developments in this new branch of statistics have led to significant advancements in areas with geographic dependence (for recent reviews on the subject, see [4,5]).

FDA has experienced rapid growth in recent years, evolving from exploratory and descriptive data analysis to more sophisticated linear models and estimation techniques. This dynamic progression has contributed to theoretical and methodological improvements, as well as the expansion of applications across various fields (see, for example, [68] and recent bibliographic discussions such as [9,10]). One major area of research in this field is functional regression, which examines the influence of a functional random variable on a scalar variable. Among the key questions in this domain are semi-parametric functional regression models, which combine the flexibility of parametric regression models with the advantages of nonparametric approaches, without the sensitivity to dimensionality issues. For a comprehensive discussion on semi-parametric modeling in functional regression, readers are referred to the bibliographical surveys by [11].

Specifically, one of the most significant semi-parametric functional models is the partially linear regression model introduced by [12], known as the SFPLR model. This model has been widely studied and applied in various contexts. This model is expressed as

(1) Y = X T β + m ( Z ) + ε ,

where Y is the scalar response variable, X = ( X 1 , X 2 , , X p ) is a p -dimensional vector of explanatory variables, β is an unknown p -dimensional parameter vector, Z is a functional explanatory variable, m ( ) is an unknown smooth functional operator, and ε are identically distributed random errors satisfying E ( ε ) = 0 and unknown variance σ 2 ( ε ) < . We typically assume an additional condition of independence between the error variable ε and the random vector ( X , Z ) . The authors apply the classical kernel method (Nadaraya-Watson-type weighting method) to establish the asymptotic normality of β and the convergence rate of m . This model was later extended to dependent data by [13]. Furthermore, Aneiros-Pérez and Vieu [14] proposed a bootstrap procedure to approximate the distribution of these estimators, while Lian [15] generalized this model to the case where the linear component is also functional. More recently, Aneiros Pérez et al. [16] examined different bootstrapping procedures for this model under various dependency structures. Additionally, a procedure for testing linearity in partially linear functional models was proposed by Zhao and Zhang [17]. Other methods for estimating the parameters of the SFPLR model include the local linear approach by Feng and Xue [18], robust procedures considered by Boente and Vahnovan [19], the k -nearest neighbors ( k -NN) method used by Ling et al. [20], and Bayesian approaches proposed by Shang [21]. Moreover, Kedir et al. [22] introduced the local linear- k NN approach. For more recent advancements, we refer readers to the bibliographic reviews by previous studies [10,23].

Furthermore, only a few research works have addressed estimation in the SFPLR model for spatially dependent observations. We cite the work of Li and Ying [24] on the autoregressive semi-functional linear regression (SAR) model, which proposed an estimator based on the quasi-maximum-likelihood method and local linear estimation. Additionally, Benallou et al. [25] derived the asymptotic normality of the parametric component, as well as the convergence in probability with the rate of the nonparametric component. The complete analysis of the data is the subject of all the works listed. However, in many applications, this is unfortunately not the case, and we encounter missing data. Common causes of missing responses include faulty equipment, sample contamination, manufacturing defects, clinical study dropouts, climatic conditions, and inaccurate data entry. On the subject of missing data, imputation methods and the uncertainty associated with such imputations have been extensively studied in the multivariate case (see, for example, [26,27]). However, little research has been conducted on nonparametric functional regression with missing data. The first significant work was carried out by Ferraty et al. [28], who estimated the mean of a scalar response using an independent and identically distributed (i.i.d.) functional sample. In this study, the functional regressor is fully observed, but some responses are missing at random (MAR). They generalize the result obtained by Cheng [29] in the multivariate case. Meanwhile, Ling et al. [30] focused on estimating the regression function and established its asymptotic properties under the conditions of stationarity and ergodicity with MAR responses. On the other hand, Rachdi et al. [31] used the k -NN method in combination with the local linear method to estimate the regression function with a small number of randomly missing responses (MAR).

For semi-parametric partially linear multivariate models with randomly missing responses for i.i.d. data, we can cite previous studies [32,33]. The first results obtained for SFPLR models with MAR responses were established by Ling et al. [34], which generalizes those obtained by Wang et al. [32]. Later, Zou et al. [35] considered the partial functional linear model, a special case of the SFPLR model, where the covariate in the parametric component is measured with additive error and the responses are MAR. They used the least-squares method and empirical likelihood methods to construct the model’s estimators.

However, the handling of missing data in spatial data remains underdeveloped. We cite the work of [36] in the multivariate case, which estimates the regression function using the kernel method. The performance of the estimator obtained is compared with the k -NN method. Puranik et al. [37] explored multiple spatial regression models with missing data, using the regression-based imputation method to predict missing values and adding a normally distributed residual term to each predicted value. This approach restores the loss of variability and biases associated with regression imputation. For functional data, Alshahrani et al. [38] proposed studying the kernel estimation of the regression function when the data are spatially functional and MAR. They obtain the asymptotic properties of this estimator, particularly the probability convergence (with rates) and the asymptotic normality of the estimator under certain weak conditions.

In this study, we propose to investigate SFPLR models for spatial data with missing responses. This article is organized as follows: in Section 2, the semi-functional partial linear model for spatial data is presented with these estimators, while the notations and hypotheses used in our work are postponed to Section 3. Section 4 is devoted to the asymptotic results. In Sections 5 and 6, a computer study on simulated and real data is carried out to demonstrate that the proposed estimators allow a nice improvement compared to the usual global approach. Finally, appendix gives some useful lemmas and the detailed proofs of our main results.

2 Model and its estimators

Let Z N be the integer lattice points in the N -dimensional Euclidean space, and let Λ i = { ( Y i , X i ( 1 ) , X i ( 2 ) , , X i ( p ) , Z i ) T , i = ( i 1 , , i N ) Z N } be a measurable strictly stationary spatial process defined over a probability space ( Ω , A , P ) and identically distributed as ( Y , X 1 , X 2 , , X p , Z ) T = ( Y , X , Z ) T R × R p × , where represents a functional semi-metric space equipped with a semi-metric d . The term site is used to designate a point i . As basic assumption in the non-parametric literature, we assume that the process can be observed in the rectangular domain n = { i = ( i 1 , , i N ) Z N , 1 i k n k , k = 1 , N } , with a sample size of n ^ = n 1 × × n N , where n = ( n 1 , , n N ) . Suppose, moreover that, for l = 1 , N , n l approaches infinity at the same rate: for any j k { 1 , , N } , we have C 1 < n j n k < C 2 for some 0 < C 1 < C 2 < , and we write that n if min k = 1 , N ( n k ) . This type of observation domain design is known as an asymptotically increasing domain, which allows this domain to expand, while keeping a minimum distance between observation sites. These data whose spatial locations are regular lattices in Z N are the analog of time series observed at equally spaced instances of time. Such data sets are frequently used in practice because the process under study is essentially discrete. To illustrate this last point, it often happens that in order to collect data, by orbiting satellites, on an agricultural surface, which is exploited in certain proportions (for example) by wheat, corn, soybeans, etc. and which must be estimated. These different crops have their reflectance properties, which, together with noise, are detected remotely. Then, the procedure is to divide the surface of this Earth into small rectangles called pixels. Thus, the data are received as a regular lattice in Z 2 and are identified with the centers of their respective pixels.

The main goal is to predict the spatial process ( Y i , i Z N ) in some unobserved locations, particularly at an unobserved site i 0 n under the information that can be drawn on ( X , Z ) i 0 and observations ( Λ i ) i ϑ , where ϑ is the observed spatial set of finite cardinality tending to as n + and contained in n , with i 0 ϑ .

As mentioned in Section 1, to meet this objective, we consider, in this work, the case where the response variable Y depends on a p -dimensional random vector X in a linear way but is related to functional variable Z in an indeterminate form through an SFPLR model:

(2) Y i = s = 1 p X i s β s + m ( Z i ) + ε i = X i T β + m ( Z i ) + ε i , i Z N ,

where X i = ( X i ( 1 ) , X i ( 2 ) , , X i ( p ) ) , β = ( β 1 , , β p ) T , m ( ) and ε are defined as before such that

E ( ε i X i ( 1 ) , X i ( 2 ) , , X i ( p ) , Z i ) = 0 and E ( ε i 2 X i ( 1 ) , X i ( 2 ) , , X i ( p ) , Z i ) < .

We denote by B ( Z , h ) = { Z such that d ( Z , Z ) h } the topological closed ball.

The kernel estimators of β n and m n (see [25]) are defined by

(3) β ^ n = i n X ˘ i ( X ˘ i ) T 1 i n X ˘ i Y ˘ i

and

(4) m ^ n ( t ) = i n w n ( z , Z i ) ( Y i X i T β ^ ) ,

where

Y ˘ i = Y i i n w n ( Z i , Z j ) Y i , X ˘ i = X i i n w n ( Z i , Z j ) X i ,

with

w n ( Z i , Z j ) = K ( d ( Z i , Z j ) b n 1 ) i n K ( d ( Z i , Z j ) b n 1 ) ,

where K denotes a real-valued kernel function and b n a decreasing sequence of bandwidths, which tends to zero as n tends to infinity.

In this article, we develop an estimation approach in which the values of the independent variables ( X and Z ) are all observed; however, some observations of the response variable ( Y values) are missing. We recall that we say that Y i is missing if Y i does not contain all of the required elements.

For this, we consider a real random variable denoted δ such that δ i = 1 if the value Y i is known, and δ i = 0 , otherwise. Thus, the study will be carried out on an incomplete sample of size n :

{ ( Y i , X i , Z i , δ i ) , i n } .

It is assumed that the random missing data mechanism satisfies the saving condition:

P ( δ i = 1 Y i = y , X i = x , Z i = z ) = P ( δ i = 1 X i = x , Z i = z ) = p ( x , z ) .

This conditional probability p ( x , z ) is generally unknown.

First, we note that

(5) δ i Y i = δ i X i T β + δ i m ( Z i ) + δ i ε i , i n .

From our assumption, by conditioning on Z i = z , it follows that

(6) E ( δ i Y i Z i = Z ) = E ( δ i X i Z i = Z ) T β + E ( δ i Z i = Z ) m ( Z i ) , i n ,

from where we have

(7) m ( Z ) = ( E ( δ i Y i Z i = Z ) E ( δ i X i Z i = Z ) T β ) E ( δ i Z i = Z ) .

In the following, we define m X ( z ) = E ( δ X Z = z ) E ( δ Z = z ) , m Y ( z ) = E ( δ Y Z = z ) E ( δ Z = z ) , and we write A 2 = A A T .

Then, by equations (5) and (6), we can write

δ i ( Y i m Y ( Z i ) ) = δ i ( X i m X ( Z i ) ) T β + δ i ε i .

Thus, if the functions m X ( Z ) and m Y ( Z ) are known, the least-squares estimator of β is given by

(8) β ˆ n = i n δ i ( X i m X ( Z i ) ) 2 1 i n δ i ( X i m X ( Z i ) ) ( Y i m Y ( Z i ) ) .

However, m X ( Z i ) and m Y ( Z i ) are generally unknown, and they must be estimated for using 8. Assuming that m X and m y are smooth functions of Z i , these can be estimated by using the nonparametric Nadaraya-Watson kernel estimator noted by m ˆ X ( Z ) and m ˆ Y ( Z ) and expressed by

m ˆ X,n ( Z ) = i n δ i w n ( Z , Z i ) X i , m ˆ y , n ( Z ) = i n δ i w n ( Z , Z i ) Y i ,

where

w n ( Z , Z i ) = K ( d ( Z , Z i ) h n ) j n δ j K ( d ( Z , Z j ) h n ) ,

with K being a real-valued kernel function and h n a decreasing sequence of bandwidths, which tends to zero as n tends to infinity.

Hence, an estimator of β n is given by

(9) β ˆ n = i n δ i X ˜ i ( X ˜ i ) T 1 i n δ i X ˜ i Y ˜ i ,

where

Y ˜ i = Y i j n δ j w n ( Z i , Z j ) Y j

and

X ˜ i = X i j n δ j w n ( Z i , Z j ) X j .

We then insert β ˆ n in equation (7) to obtain

(10) m ^ n ( Z ) = m ˆ Y , n ( Z ) m ˆ X , n T ( Z ) β ˆ n .

3 Notations and hypotheses

Our main objective is to obtain the asymptotic normality of our estimator under the condition that the process Λ i is strictly stationary, which satisfies the following α -mixing condition [39]: there exists a real function φ ( t ) , which tends to 0 when t goes to , such that for finite cardinal subsets (Card ( ) < ) E , E Z N :

(11) α ( B ( E ) , B ( E ) ) = sup { ( A , B ) B ( E ) × B ( E ) } { P ( A B ) P ( A ) P ( B ) } φ ( d ( E , E ) ) ψ ( Card ( E ) , Card ( E ) ) ,

where d ( E , E ) denotes the Euclidean distance in Z N , B ( S ) = B ( Z i , i S ) , for S Z N , the σ -fields generated by a random variable Z i , and ψ : Z 2 R + is a symmetric positive function nondecreasing in each variable such that

(12) ( r , s ) Z 2 , ψ ( r , s ) C min ( r , s ) , for some C > 0 .

Moreover, as is often the case in spatial regression, we assume other conditions on the function φ :

(13) i = 1 i γ ( φ ( i ) ) < , for some γ > 0 .

Noting that both conditions (12) and (13) are satisfied by many spatial models (see, for example, the spatial linear process [40,41] for more details on the required conditions). It should be pointed out that if ψ = 1 , then the process Λ i is called a strong mixing process.

In the following, and in order to simplify the reading of the manuscript, we introduce the following notations.

Let ν ij = sup i j P [ ( Z i , Z j ) ( B ( z , h ) × B ( z , h ) ) ] the probabilistic joint distribution of Z i and Z j , and let ϕ z ( h n ) = P ( Z B ( z , h n ) ) called the small ball probability.

In addition, we note θ i ( s ) ( z ) = X i ( s ) E [ δ i X i ( s ) Z i = z ] , for s = 1 , , p , and θ i = ( θ i ( 1 ) , , θ i ( p ) ) T . Recall that the expressions of our estimators in (9) and (10) contain estimators of θ i . Now, in order to state the asymptotic properties of our estimators, we introduce the following assumptions.

(H1) We suppose that, z and i j Z N , there exist C > 0 such that

for some 1 < a < γ N 1 , sup i j ν ij C ( ϕ z ( h ) ) a + 1 a .

(H2) The kernel function K : R R + is assumed to be differentiable with support in the interval [ 0 , 1 ] such that there exist two constants C 3 and C 4 with

< C 3 < K ( t ) < C 4 < 0 , for t [ 0 , 1 ] .

(H3) We assume that any function f { m , θ i ( 1 ) ( z ) , , θ i ( p ) ( z ) } is smooth, i.e., there exists c > 0 such that for κ > 0 , we have

f ( u ) f ( v ) c d ( u , v ) κ , u , v .

(H4) We suppose that, z : ϕ z ( h n ) > 0 , there exists differentiable nonnegative functions τ and g such that

ϕ z ( h ) = g ( h ) × τ ( x ) + o ( g ( h ) ) .

(H5) For all t [ 0 , 1 ] , we have

lim h n 0 ϕ z ( t h n ) ϕ z ( h n ) = ι z ( t ) .

(H6) Let R i = θ i ε i and Σ = E [ p ( X 1 , Z 1 ) ( θ 1 ( θ 1 ) T ) ] , where 1 is the site spatial ( 1 , , 1 ) and we denote by 0 the site spatial ( 0 , , 0 ) .

  1. The matrix B = i n E [ p ( X i , Z i ) ( R 0 ( R i ) T ) ] is assumed to be positive definite.

  2. We assume that Σ is an invertible matrix.

(H7) We suppose that

  1. E ε 1 ρ + E θ 1 ( 1 ) ρ + + E θ 1 ( p ) ρ < , for some ρ 3 .

  2. For all i j , E [ Y i Y j ( Z i , Z j ) ] < .

  3. For all i j , max 1 s p E [ X i ( s ) X j ( s ) ( Z i , Z j ) ] < .

(H8) Let V 2 ( z ) = v a r ( Y i X i T β Z i = z ) and V s ( z ) = E [ Y i X i T β m ( z ) s Z i = z ] , with s > 2 .

  1. We suppose that the functions V 2 ( ) and V s ( ) are continuous functions near z , i.e., since h 0 , we have

    sup { z : d ( z , z ) h } V k ( z ) V k ( z ) = o ( 1 ) , k 2 .

  2. Let V ( z , z , z ) = E [ ( Y i X i T β m ( z ) ) ( Y j X j T β m ( z ) ) Z i = z , Z i = z ] , for i j .

We suppose that the function V is continuous in some neighborhood of ( z , z ) .

(H9) We also suppose that p 1 ( ) = P ( δ = 1 Z = z ) is continuous function near z , i.e.,

sup { u : d ( z , z ) h } p 1 ( z ) p 1 ( z ) = o ( 1 ) , as h 0 .

(H10) There exists 1 > ϑ > N γ such that ϕ z ( h ) n ^ ϑ 1 2 N + 1 .

Comments on the assumptions:

The asymptotic results obtained subsequently are based on Theorem 4.1 in [38]. It is, therefore, normal to impose the same hypotheses as in this theorem. More specifically, hypothesis ( H 1 ) measures the local dependence between observations, and such condition is necessary to reach the same rate of convergence as in the i . i . d . case. The assumption ( H 2 ) is also standard in this context of functional statistics. The conditions in these assumptions are satisfied by several kernels, which are traditionally used in practice such as Epanechnikov kernel, Parzen kernels, triangular kernel, and others. Hypothesis ( H 2 ) and hypothesis ( H 3 ) are used to control the bias of the estimator. The assumptions ( H 4 ) is known as the “concentration property” in the asymptotic theory of nonparametric functional statistics. It is a condition closely linked with the semi-metric d and such function ϕ z ( ) can be explicated for several continuous processes [8]. The information on the variability of the small-ball probability is given by hypothesis ( H 5 ) . This information is used to control the bias of the nonparametric estimators. Moreover, hypothesis ( H 5 ) is necessary to apply the central limit theorem to have asymptotic normality. It is well documented that this condition is not very restrictive and the function ι z ( t ) can be given explicitly for many classical stochastic processes [42]. Assumptions ( H 8 ) and ( H 10 ) present the continuous local conditions needed to establish the main results. In fact, the conditional expectation requires that V s and V are continuous. Assumption ( H 9 ) in FDA MAR models is typical (see, for example, [30,31]). The additional hypothesis ( H 6 ) is usual in the context of the SFPLR.

4 Theoretical results

We are now in a position to give our asymptotic results. The first one gives the asymptotic distribution of the estimator for the parametric component of the model ( β ^ n ).

Theorem 4.1

When the assumptions (H1)–(H10) and (11)–(13) hold, if additionally, the bandwidth parameter h n and the function ϕ z ( h n ) satisfy n ^ ϕ z ( h n ) log ( n ^ ) and n ^ h n κ ϕ ( h n ) log ( n ^ ) 0 , as n , we have

(14) ( n ^ ) 1 2 ( β ^ n β ) d N ( 0 , Σ 1 B ( Σ 1 ) T ) ,

where d stands for convergence in distribution.

The following results give the probability convergence and the asymptotic normality of the estimator of the non-parametric part.

Theorem 4.2

Under the conditions of Theorem 4.1, we have

(15) m ^ n ( z ) m ( z ) p 0 ,

where p stands for convergence in probability.

Theorem 4.3

Under the conditions of Theorem 4.1, and if, in addition, n ^ h n 2 κ ( ϕ x ( h n ) ) 0 as n , we have

(16) ( n ^ ϕ z ( h n ) ) 1 2 m ^ n ( z ) m ( z ) d N ( 0 , σ 2 ( z ) ) ,

where σ 2 ( z ) = ι 2 ι 1 2 V 2 ( z ) p 1 ( z ) τ ( z ) , with ι k = 0 1 ι z ( t ) ( K k ) ( t ) d t , for k = 1 , 2 .

We note that these results obtained extend those that are established in the case of complete data [25].

5 Computational study

In this section, we are interested in the behavior of the estimators proposed on samples of finite size, with particular attention to the influence of spatial correlation and the effect of MAR on the efficiency of the estimators. To do that, we conducted simulations based on observations denoted as ( X i , Z i , Y i , δ i ) with i = ( i 1 , i 2 ) , 1 i 1 n 1 , 1 i 2 n 2 , and we generate the SFPLR model with MAR as follows:

(17) δ i Y i = δ i r ( Z i , X i ) + δ i ε i = δ i X i T β + δ i m ( Z i ) + δ i ε i ,

where β = ( 1 , 2 ) T , X i j Exponential ( 0.5 ) , j = 1 , 2 , and take the nonparametric operator m as follows:

m ( z ) = 1 0 1 1 + z ( t ) d t .

The curves Z i ( t ) are defined as follows: Z i ( t ) = B i t sin ( t A i ) + ν i ( t ) , for t [ 0 , 1 ] .

For simulating the curves Z i , we take ν i ( t ) N ( 0 , 0.2 ) , A = D * sin G 2 + 0.5 , with G = G R F ( 0 , 5 , 3 ) , B = G R F ( 2.5 , 5 , 3 ) , and ε = G R F ( 0 , 0.1 , 5 ) , where the function G R F ( μ , σ 2 , s ) denotes a stationary Gaussian random field with mean μ and covariance function defined by C ( l ) = σ 2 exp l s 2 , l R 2 and s > 0 . And the function D is defined by

D i = 1 n 1 × n 2 j exp i j a i.e. D i = 1 n 1 × n 2 1 j 1 n 1 1 j 2 n 2 exp ( i 1 , i 2 ) ( j 1 , j 2 ) a .

The curves, following the values of a , are displayed in Figure 1. Note that we consider the same curves as in [43], where the function D is used to control the spatial mixing condition. Therefore, these observations are a mixture of independent and dependent data points, as illustrated in Figure 2 (for more details, see [43]).

Figure 1 
               Curves 
                     
                        
                        
                           
                              
                                 Z
                              
                              
                                 i
                              
                           
                           ,
                           t
                           ∈
                           
                              [
                              
                                 0
                                 ,
                                 1
                              
                              ]
                           
                        
                        {Z}_{{\bf{i}}},t\in \left[0,1]
                     
                   for 
                     
                        
                        
                           a
                           =
                           5
                        
                        a=5
                     
                  , 20, and 50.
Figure 1

Curves Z i , t [ 0 , 1 ] for a = 5 , 20, and 50.

Figure 2 
               Simulations of the random field were generated for different values of 
                     
                        
                        
                           a
                        
                        a
                     
                  , specifically 
                     
                        
                        
                           a
                           =
                           5
                        
                        a=5
                     
                  , 20, and 50.
Figure 2

Simulations of the random field were generated for different values of a , specifically a = 5 , 20, and 50.

To reduce the level of independence in the data, it is sufficient to decrease the value of a . For our analysis, we have employed a value of σ 2 = 5 and s = 5 . Moreover, similar to that described in [34], we adopted the following missing data mechanism:

p ( X = ( x 1 , x 2 ) , z ) = P ( δ = 1 X 1 = x 1 , X 2 = x 2 , Z = z ) = expit 2 α j = 1 2 x j + 0 1 z 2 ( t ) d t ,

where expit ( u ) = e u ( 1 + e u ) , for all u R , and we will take for α the following values: α = 0.05 , 0.5, and 5.

Let us remember that the degree of dependence between the functional variable Z and the variable δ is controlled by the parameter α , and to check the value of p ( x ) , we compute δ ¯ = 1 1 n 1 × n 2 i 1 = 1 n 1 i 2 = 1 n 2 δ ( i 1 , i 2 ) for different values of α to measure the missing rate.

In order to calculate our estimators, we use the class of semi-metrics based on the principal component analysis (PCA) metric, which is best suited to the treatment of this type of data (discontinuous functional variable). Furthermore, we have chosen the standard kernel function defined as follows: K ( u ) = 3 2 ( 1 u 2 ) 1 [ 0 , 1 ] ( u ) .

The objective of this computer study is to conduct a comparison between our semi-partially linear model with MAR estimator (SFPLRM), semi-partially linear model estimator r ˜ n in the complete case (SFPLRC) (see [25]), and the nonparametric functional model estimator with MAR (FNPM).

Recall that the FNPM model is defined as

Y = r ( Z ) + ε ,

and the estimator of operator regression r [38] is given by

r ^ n ( z ) = j n δ j Y j K ( d ( z , Z j ) h n ) j n δ j K ( d ( z , Z j ) h n ) .

For that purpose, we conducted a random split of our data, denoted as ( X i , Z i , Y i , δ i ) i , into two subsets: a test sample ( X i , Z i , Y i ) i I (consisting of data without missing values) and training sample ( X i , Z i , Y i , δ i ) i I that they will be used to select the optimal smoothing parameters h opt . The training sample was used to choose the smoothing parameter ( h opt ). The h o p t is the data-driven bandwidth obtained by a cross-validation procedure:

h o p t = arg min h C V ( h ) , where C V ( h ) = i I δ i [ Y i ( m ^ n ( i ) ( Z i ) + X i T β ^ n ) ] 2 ,

with m ^ n ( i ) ( ) being the estimator of m ( ) based on the leave-one-out method calculated without observation ( X i , Z i ) after estimating β n (see [14,44] for more details).

To evaluate the precision of the estimators of the three models (SFPLRM, SFPLRC, and FNPM), we use the square and mean square errors, denoted mean squared error (MSE):

MSE FNPM = 1 # ( I ) i I ( r ^ n ( Z i ) Y i ) 2 , MSE S F P L R C = 1 # ( I ) i I ( r ˜ n ( Z i , X i ) Y i ) 2 , MSE S F P L R M = 1 # ( I ) i I ( r ^ n ( Z i , X i ) Y i ) 2 ,

where # ( I ) represents the size of the testing sample I . The experiment was replicated M = 100 times, which allows us to compute M values for MSE and display their distribution through a boxplot. The results obtained (the prediction values compared with the true values) are presented in Figure 3 for the three models with different values of a . Figure 4 displays the boxplots constructed from MSE obtained for the three models.

Figure 3 
               Predictions of the three models for 
                     
                        
                        
                           a
                           =
                           5
                           ,
                           20
                        
                        a=5,20
                     
                  , and 50.
Figure 3

Predictions of the three models for a = 5 , 20 , and 50.

Figure 4 
               Boxplot MSE of the three models for 
                     
                        
                        
                           α
                           =
                           0.05
                        
                        \alpha =0.05
                     
                  , 0.5, and 5.
Figure 4

Boxplot MSE of the three models for α = 0.05 , 0.5, and 5.

In Figure 4, we observe that the SFPLRM estimator shows better prediction effects than the FNPM in comparison with the SFPLRC estimator.

In Table 1, which presents the MSE for FNPM, SFPLRM, and SFPLRC under various conditions defined by combinations of n 1 , n 2 , and α , it becomes evident that the SFPLRM estimator consistently shows superior predictive accuracy when compared to the FNPM estimator across a range of settings. This is notably evident as the MSE values for the SFPLRM estimator consistently remain lower across the majority of combinations of n 1 , n 2 , and α . Furthermore, a notable observation is that higher values of α (e.g., α = 5 ) tend to correspond with lower MSE values, indicating enhanced predictive performance for the SFPLRM estimator. It is also worth mentioning that as the number of samples ( n 1 × n 2 ) increases, the results suggest that the MAR mechanism has little to no discernible effect on the prediction of MSE. This observation implies that the SFPLRM estimator maintains consistent performance regardless of the presence of missing data, mainly when dealing with larger sample sizes.

Table 1

MSE for FNPM, SFPLRM, and SFPLRC

FNPM SFPLRM FNPM SFPLRM FNPM SFPLRM SFPLRC
n 1 n 2 α = 0.05 α = 0.05 α = 0.5 α = 0.5 α = 5 α = 5 Complete
δ ¯ = 30.71 % δ ¯ = 30.71 % δ ¯ = 18.20 % δ ¯ = 18.20 % δ ¯ = 05.84 % δ ¯ = 05.84 % δ ¯ = 00 %
10 10 22.29 6.562 21.64 3.782 21.13 2.611 2.504
10 20 26.29 5.869 24.88 3.329 25.06 1.232 1.228
10 50 22.62 5.132 21.89 2.929 21.71 1.105 1.098
20 10 22.98 4.865 21.62 3.079 21.37 1.282 1.253
20 20 20.00 4.539 19.22 2.845 18.82 0.991 0.987
20 50 21.63 4.518 21.18 2.428 21.03 0.763 0.755
50 10 20.14 4.578 20.19 2.973 19.51 1.642 1.624
50 20 22.27 3.817 21.83 2.285 21.93 0.631 0.630
50 50 20.64 3.892 20.37 2.246 20.29 0.491 0.488

Now, we aim to examine the bias in the estimation of β and its associated square error (ASE), which is defined as

ASE = β ^ n β 2 .

The results are presented in Table 2.

Table 2

Square error ASE for β ^

SFPLRM SFPLRM SFPLRM SFPLRM SFPLRM SFPLRM SFPLRC SFPLRC
β ^ n 1 β ^ n 2 β ^ n 1 β ^ n 2 β ^ n 1 β ^ n 2 β ^ n 1 β ^ n 2
n 1 n 2 α = 0.05 α = 0.05 α = 0.5 α = 0.5 α = 5 α = 5 Complete Complete
δ ¯ = 30.71 % δ ¯ = 30.71 % δ ¯ = 18.20 % δ ¯ = 18.20 % δ ¯ = 05.84 % δ ¯ = 05.84 % δ ¯ = 00 % δ ¯ = 00 %
10 10 0.504 1.148 0.477 0.807 0.574 0.475 0.463 0.456
10 20 0.479 1.309 0.471 1.025 0.280 0.491 0.331 0.475
10 50 0.485 1.415 0.472 1.144 0.337 0.492 0.287 0.479
20 10 0.485 1.488 0.464 1.086 0.348 0.510 0.320 0.471
20 20 0.488 1.597 0.477 1.163 0.311 0.488 0.275 0.478
20 50 0.469 1.432 0.463 1.029 0.317 0.488 0.258 0.482
50 10 0.491 1.534 0.475 1.048 0.274 0.516 0.322 0.498
50 20 0.489 1.426 0.479 1.096 0.237 0.481 0.271 0.472
50 50 0.477 1.463 0.468 1.106 0.290 0.487 0.246 0.480

The results from Table 2 suggest that the SFPLRM estimator displays good accuracy in estimating the parameters β ^ n , with relatively small square error values. This implies that the estimator provides reasonably accurate estimates of the true parameters, even in cases with missing data and varying degrees of dependence. The theoretical conclusions of Theorems 3.1 and 3.2 are consistent with such a numerical outcome.

Remark 5.1

Note that it is possible to extend the scope of this contribution to other domains using continuous-time spatial processes, in particular to the spatiotemporal process. Indeed, by following the same approach for the prediction of continuous-time processes (see [13] for time series), we can apply the estimation of our parameters of the spatial SFPLR model to the prediction of a continuous random field (see, for example, [45] for more details). In our application, we used spatiotemporal data, but we made the prediction for each time s . Alternatively, we could have treated time as a spatial index, as they did in [46], which would allow for a unified spatial-temporal approach, where both space and time are treated on equal footing.

6 Real data application

The objective of this part is to compare, on a set of real data consisting of particle pollution indices, the effectiveness of the SFPLR model by our estimators when the data are MAR. The source of these data is the AriaWeb information system, managed by CSI Piemonte and Regione Piemonte, and our analysis is obtained from 34 monitoring sites using gravimetric instruments recorded during the winter season from October 2005 to March 2006 (daily measurements including T = 182 days). This involves analyzing the levels of pollution, which allowed us to detect higher levels of pollution in the plains closer to urban centers, while lower concentrations of this index are observed near the Alps (for more detailed information about the data, we recommend referring to the publication by [47]).

To select the appropriate covariates, a preliminary regression analysis was carried out, and the following covariates were selected:

  1. X 1 = HMIX : maximum daily mixing height (in m),

  2. X 2 = EMI ( s ) : daily primary aerosol emission rates (in g/s),

  3. X 3 = PREC ( s ) : total daily precipitation (in mm),

  4. Z = TEMP : the average daily temperature (in Kelvin K ).

To implement the theoretical conclusions of the previous section on real data, we will analyze the effectiveness of our estimators built with MAR data in the context of spatial functional prediction, which highlights the importance of considering spatial locations. Specifically, we assume that the observations are linked via an SFPLR model (17), where the response variable is Y = PM 10 ( s ) (in μ g/m3) (for each s = 1 , , 182 ) represents pollution levels, the functional predictor Z i ( t ) represents the daily mean temperature curve recorded at the i th station, with its precise location determined by the coordinates i = ( UTMX ; UTMY ) , Z = T E M P ( t ) ; t = 1 , , 182 , and the parametric part are X = ( X 1 , X 2 , X 3 ) , (for 182 days). δ = 1 if PM 10 ( s ) is observed and δ = 0 otherwise. Note that our data have some missing values (473 NaN of PM 10 ( s ) for each s = 1 , , 182 and each station, about 7.64% missing data).

Figure 5 provides the curves of the functional variable Z i , and Figure 6 represents the spatial position of the 34 monitoring stations in the Piemonte region (northern Italy).

Figure 5 
               Temperature curves 
                     
                        
                        
                           Z
                        
                        Z
                     
                  .
Figure 5

Temperature curves Z .

Figure 6 
               Locations of the stations in Piemonte (northern Italy).
Figure 6

Locations of the stations in Piemonte (northern Italy).

However, implementing this spatial modeling approach requires preliminary data preparation to validate the stationarity assumption that handles spatial heterogeneity resulting from variations in the effects of space on sampled units. To answer this, we will use an “detrending step” introduced by [48], which is designed for the multivariate case of the three variables (response, functional, and vectorial explanatory). This algorithm is defined by the following regression:

X ˜ i = m 1 ( i ) + X i , Z ˜ i = m 2 ( i ) + Z i , and Y ˜ i = m 3 ( i ) + Y i .

Thus, instead of the initial observations ( X i , Z i , Y i , δ i ) i , we compute the SFPLRM estimator from the statistics ( X ^ i , Z ^ i , Y ^ i , δ i ) i (Figure 7). The latter are obtained by

X ^ i = X ˜ i m ^ 1 ( i ) , Z ^ i = Z ˜ i m ^ 2 ( i ) , and Y ^ i = Y ˜ i m ^ 3 ( i ) ,

and m ^ 1 ( ) , m ^ 2 , and m ^ 3 are the kernel estimators of the regression functions m 1 ( ) , m 2 ( ) , and m 3 ( ) , which are expressed by

m ^ 1 ( i 0 ) = i n δ i X i H 1 ( i 0 i h n 1 ) i n δ i H 1 ( i 0 i h n 1 ) , m ^ 2 ( i 0 ) = i n δ i Z i H 2 ( i 0 i h n 2 ) i n δ i H 2 ( i 0 i h n 2 )

and m ^ 3 ( i 0 ) = i n δ i Y i H 3 ( i 0 i h n 3 ) i n δ i H 3 ( i 0 i h n 3 ) ,

where the functions H j , j = 1 , 2 , 3 represent the kernel functions, while h n j , j = 1 , 2 , 3 are the bandwidth parameters associated with the actual regression. To illustrate the practical implications of this detrending step on our dataset, we will examine its impact by performing a comparative analysis of the performance of the SFPLRM regression in the two cases, one with detrending and the other without this one.

Figure 7 
               No detrending observations 
                     
                        
                        
                           
                              
                                 PM
                              
                              
                                 10
                              
                           
                           
                              (
                              
                                 s
                              
                              )
                           
                        
                        {{\rm{PM}}}_{10}\left(s)
                     
                   (
                     
                        
                        
                           Y
                        
                        Y
                     
                  ) versus detrending observations 
                     
                        
                        
                           
                              
                                 PM
                              
                              
                                 10
                              
                           
                           
                              (
                              
                                 s
                              
                              )
                           
                        
                        {{\rm{PM}}}_{10}\left(s)
                     
                   (
                     
                        
                        
                           
                              
                                 Y
                              
                              
                                 ^
                              
                           
                        
                        \widehat{Y}
                     
                  ).
Figure 7

No detrending observations PM 10 ( s ) ( Y ) versus detrending observations PM 10 ( s ) ( Y ^ ).

To conduct this analysis, we employ the same methodology as employed in the simulation example for the selection of the estimator’s parameters. Specifically, we use the quadratic kernel on the interval ( 0 , 1 ) in combination with the PCA metric and the cross-validation (CV) criterion to determine the smoothing parameter h n . For the real regressions m 1 ( ) , m 2 ( ) , and m 3 ( ) , we use the npreg routine in the R-package np, with K = H 1 = H 2 = H 3 .

To assess the feasibility of this approach, we randomly split the data sample multiple times (precisely 100 times). The data are divided into two subsets: a learning sample consisting of 24 observations and a test sample containing 10 observations. We then evaluate the significance of the proposed detrending procedure by examining the MSE, as used in the simulation example. This analysis allows us to determine the impact of detrending on the performance of the estimators in practice.

The results in Figure 8 reveal a significant enhancement in model accuracy with the inclusion of the detrending step. The MSE values are substantially reduced when detrending is applied, indicating a clear advantage of this data preprocessing technique. As illustrated in Figure 9, it becomes apparent that the detrending step consistently outperforms the non-detrending, clearly showcasing its superior capability to accurately capture the underlying functional relationships. These results underscore the pivotal role of detrending in enhancing model performance and underscore the inherent advantages of the SFPLRM estimator in the realm of non-parametric spatial data analysis.

Figure 8 
               Boxplot of MSE values: detrending vs no detrending.
Figure 8

Boxplot of MSE values: detrending vs no detrending.

Figure 9 
               Prediction of the testing sample of the 
                     
                        
                        
                           
                              
                                 PM
                              
                              
                                 10
                              
                           
                        
                        {{\rm{PM}}}_{10}
                     
                   for 
                     
                        
                        
                           s
                           =
                           150
                           ,
                           
                              …
                           
                           ,
                           182
                        
                        s=150,\ldots ,182
                     
                   in 10 stations: (a) zone 1, (b) zone 2, (c) zone 3, (d) zone 4, (e) zone 5, (f) zone 6, (g) zone 7, (h) zone 8, (i) zone 9, and (j) zone 10.
Figure 9

Prediction of the testing sample of the PM 10 for s = 150 , , 182 in 10 stations: (a) zone 1, (b) zone 2, (c) zone 3, (d) zone 4, (e) zone 5, (f) zone 6, (g) zone 7, (h) zone 8, (i) zone 9, and (j) zone 10.

7 Conclusion

This article addresses the issue of a SFPLR model for spatial data, assuming that the missing responses occur randomly. The construction of the estimator encompasses both the linear and nonparametric components of the model. One crucial aspect of this study involves the demonstration of the asymptotic normality of the best estimators. This is achieved by imposing certain mild constraints and establishing the probability convergence of the nonparametric component. Furthermore, the use of both simulated and real data in the analysis highlights the potential viability and adaptability of the proposed model, along with its associated estimators, in predictive tasks. This is achieved through a comparative analysis using a non-parametric estimator. It is essential to highlight that significant emphasis was placed on the absence of a missing mechanism that is MAR within the domain of functional data statistics. In future analyses, it would be interesting to explore the extension of our framework in alternative directions. One such avenue involves expanding the framework from MAR data to censored data, which would require the use of advanced mathematical techniques.

Acknowledgement

The authors would like to appreciate the Editor in Chief and the two referees for their valuable comments and suggestions that are very helpful for them to improve the quality and presentation of this article significantly.

  1. Funding information: The authors thank and extend their appreciation to the funder of this work. This work was supported by the Deanship of Scientific Research and Graduate Studies at King Khalid University through the Large Research Groups Project under Grant Number R.G.P. 2/338/45.

  2. Author contributions: The authors contributed approximately equally to this work. All authors have read and agreed to the final version of the manuscript. Formal analysis, Tawfik Benchikh; validation, Omar Fetitah; writing – review and editing, Ibrahim M. Almanjahie and Mohammad Kadi Attouch.

  3. Conflict of interest: Authors state no conflict of interest.

Appendix

This section is devoted to the proof of our main result. The notation introduced earlier will continue to be used throughout the following discussion. For the remainder of this article, we set K i = K ( h n 1 d ( x , X i ) ) , for all i n .

First, we need to state some preliminary results. We denote λ i ( z ) = ϕ z ( h ) E ( K 1 ) [ δ i ( Y i X i T β m ( z ) ) K i ] , and we define the random variable W i ( z ) as W i ( z ) = λ i ( z ) E ( λ i ( z ) ) .

Lemma A.1

Under the hypotheses of Theorem 4.1, we have

(A1) ( n ^ ) 1 Var i n W i ( z ) V ( z ) = p 1 ( z ) V 2 ( z ) ι 2 ι 1 2 τ ( z ) a s n .

Proof

Before proceeding further, note that

(A2) Var i n W i ( z ) = i n Var ( W i ( z ) ) + i j Cov ( W i ( z ) , W j ( z ) ) = I n ( z ) + R n ( z ) .

First, we have Var ( W i ( z ) ) = E ( λ i 2 ( z ) ) E 2 ( λ i ( z ) ) . Conditioning on Z i and using MAR assumption, we obtain

E ( λ i ( z ) ) = ϕ z ( h ) ( m ( z i ) m ( z ) ) E ( K i ) E ( K 1 ) ,

then, ( H3 ) and ( H9 ) imply

E ( λ i ( z ) ) ϕ z ( h ) h κ ( p 1 ( z ) + o ( 1 ) ) E ( K i ) E ( K 1 ) .

Similarly, conditioning on Z i and using MAR assumption, we have

E ( λ i 2 ( x ) ) = ϕ z ( h ) E p 1 ( z i ) ( m ( z i ) m ( z ) ) 2 K i 2 E 2 ( K 1 ) + ϕ x ( h ) E p 1 ( z i ) V 2 ( z i ) K i 2 E 2 ( K 1 ) .

It follows, from ( H8 ) ( i ) and ( H9 ) , that

E p ( z i ) V 2 ( z i ) K i 2 E 2 ( K 1 ) = ( p 1 ( z ) + o ( 1 ) ) ( V 2 ( z ) + o ( 1 ) ) E ( K i 2 ) E 2 ( K 1 ) .

Similarly, using ( H3 ) and ( H9 ) , we obtain

E p 1 ( z i ) ( m ( z i ) m ( z ) ) 2 K i 2 E 2 ( K 1 ) ( p 1 ( z ) + o ( 1 ) ) h 2 κ E ( K i 2 ) E 2 ( K 1 ) .

Therefore, we have

E ( λ i 2 ( z ) ) ϕ z ( h ) ( p 1 ( z ) + o ( 1 ) ) [ ( V 2 ( z ) + o ( 1 ) ) + h 2 κ ] E ( K i 2 ) E 2 ( K 1 ) ,

which implies that

(A3) E ( W i ( z ) 2 ) ϕ z ( h ) ( p 1 ( z ) + o ( 1 ) ) ( V 2 ( z ) + o ( 1 ) ) E ( K i 2 ) E 2 ( K 1 ) + h 2 κ ϕ z ( h ) ( p 1 ( z ) + o ( 1 ) ) E ( K i 2 ) E 2 ( K 1 ) + h 2 κ ϕ x ( h ) ( p 1 ( z ) + o ( 1 ) ) E 2 ( K i ) E 2 ( K 1 ) .

Thus, we have

I n ( x ) n ^ ϕ z ( h ) ( p 1 ( z ) + o ( 1 ) ) ( V 2 ( z ) + o ( 1 ) ) E ( K i 2 ) E 2 ( K 1 ) + n ^ h 2 κ ( p 1 ( z ) + o ( 1 ) ) E ( K i 2 ) E 2 ( K 1 ) + n ^ h 2 κ ϕ z ( h ) ( p 1 ( z ) + o ( 1 ) ) E 2 ( K i ) E 2 ( K 1 ) .

On the other hand, using (H1)–(H2), (H4)–(H5), we deduce that

( τ ( z ) ϕ z ( h ) ) 1 E ( K i j ) ι j , j = 1 , 2 ,

Consequently, we obtain

(A4) 1 n ^ I n ( z ) = 1 n ^ i n E ( W i ( z ) 2 ) V ( z ) = ι 2 ι 1 2 p 1 ( z ) V 2 ( z ) τ ( z ) , as n .

For the covariance term R n ( z ) , taking into account that

i j C o v ( W i ( z ) , W j ( z ) ) = i j E ( W i ( z ) W j ( z ) ) ,

then, by some argument as above, we obtain

(A5) i≠j E ( W i ( z ) W j ( z ) ) 1 E 2 ( K 1 ) h 2 κ ϕ z ( h ) ( p 1 ( z ) + o ( 1 ) ) 2 i≠j ( E ( K i K j ) E ( K i ) E ( K i ) ) .

In the following, we introduce the following sets E 1 = { i j n such that i j c n } , and E 2 = { i j n such that i j > c n } , where c n is a real sequence that tends to + as n , which will be specified later. We denote

R n 1 = E 1 E ( K i K j ) E ( K i ) E ( K j ) and R n 2 = E 2 E ( K i K j ) E ( K i ) E ( K j ) .

On the one hand, by assumption ( H1 ) , we have

(A6) R n 1 C n ^ c n N 1 E 2 ( K 1 ) h 2 κ ϕ z ( h ) ( p 1 ( z ) + o ( 1 ) ) i j ϕ z ( h ) 1 + 1 a .

On the other hand, by Lemma (3.3) in [39] and using the fact that the random variables K i are bounded, we deduce that

E ( K i K j ) E ( K i ) E ( K j ) C φ ( i j ) .

Consequently, we obtain

(A7) R n 2 1 E 2 ( K 1 ) C h 2 κ ϕ z ( h ) ( p 1 ( z ) + o ( 1 ) ) i,j E 2 φ ( i j ) 1 E 2 ( K 1 ) C n ^ h 2 κ ϕ z ( h ) ( p 1 ( z ) + o ( 1 ) ) i : i c n φ ( i ) 1 E 2 ( K 1 ) C n ^ h 2 κ ϕ z ( h ) ( p 1 ( z ) + o ( 1 ) ) c n N a i j i : i c n i N a φ ( i ) .

Then, using condition (13), if we set c n = ( ϕ z ( h ) ) 1 N a , we have

(A8) R n = R n 1 + R n 2 C n ^ 1 E 2 ( K 1 ) h 2 κ ϕ z ( h ) ( p 1 ( z ) + o ( 1 ) ) .

Thus, from equations (A5)–(A7), we deduce that

(A9) i , j C o v ( W i ( z ) , W j ( z ) ) = o ( n ^ ) .

The proof follows from (A2), (A4), and (A9).□

Second, we recall the following results (Theorem 4.1 in [38]), which will be used in the proofs of our results.

Lemma A.2

Under hypotheses (H1)–(H10) and conditions (11)–(13), if, in addition the bandwidth parameter h n and the function ϕ z ( h n ) satisfy n ^ ϕ z ( h n ) log ( n ^ ) and n ^ h n κ ϕ z ( h n ) log ( n ^ ) 0 , when n , then

n ^ ( ϕ x ( h n ) log ( n ^ ) ) m ^ X ( z ) m X ( z ) p 0 . n ^ ( ϕ x ( h n ) log ( n ^ ) ) m ^ Y ( z ) m Y ( z ) p 0 .

Finally, using Lemma A.1 and the same reasoning as in the proof of Theorem 4.2. in [38] (with the same notations), we prove the following result.

Lemma A.3

Under hypotheses (H1)–(H10), if the bandwidth parameter h n and the function ϕ z ( h n ) satisfy n ^ ϕ z ( h n ) and n ^ h n 2 κ ϕ z ( h n ) 0 , as n + , then, we have

(A10) n ^ ϕ z ( h n ) m ^ n ( z ) m ( z ) D N ( 0 , σ 2 ( z ) ) ,

with σ 2 ( z ) = ι 2 ι 1 2 V 2 ( z ) p 1 ( z ) τ ( z ) .

Now, to establish our main results, we present the following lemma.

Lemma A.4

Under hypotheses (H1) through (H10), if, in addition, n ^ ϕ z ( h n ) log ( n ^ ) and n ^ h n κ ϕ z ( h n ) log ( n ^ ) 0 , when n tend to ∞, then we have:

(A11) 1 n ^ i n δ i X ˜ i ( X ˜ i ) T p Σ .

Proof

Taking into account that the ( r , s ) th element of 1 n ^ i n δ i X ˜ i ( X ˜ i ) T is

(A12) 1 n ^ i n δ i X ˜ i ( X ˜ i ) T r s = 1 n ^ i n δ i θ i ( r ) θ i ( s ) + 1 n ^ i n δ i Δ i ( r ) θ i ( s ) + 1 n ^ i n δ i Δ i ( s ) θ i ( r ) + 1 n ^ i n δ i Δ i ( r ) Δ i ( s ) ,

where

Δ i ( s ) ( z ) = E [ δ i X i ( s ) Z i = z ] i n δ j w n ( Z i , Z j ) X j ( s ) , s = 1 , , p .

Then, by the strong law of large numbers and the MAR assumption, we have

(A13) 1 n ^ i n δ i θ i ( r ) θ i ( s ) p E [ p ( X 1 , Z 1 ) θ 1 ( r ) θ 1 ( s ) ] = Σ r s .

On the other hand, by Lemma A.2 and the strong law of large numbers, we have

(A14) 1 n ^ i n δ i Δ i ( r ) θ i ( s ) max i n max 1 r p Δ i ( r ) 1 n ^ i n δ i θ i ( s ) p 0 ,

(A15) 1 n ^ i n δ i Δ i ( s ) θ i ( r ) max i n max 1 s p Δ i ( s ) 1 n ^ i n δ i θ i ( r ) p 0 ,

and

(A16) 1 n ^ i n δ i Δ i ( r ) Δ i ( s ) max i n max 1 r , s p Δ i ( r ) Δ i ( s ) 1 n ^ i n δ i p 0 .

Thus, we conclude the proof of Lemma A.4 using (A13)–(A16).□

Proof of Theorem 4.1

Let us use the following decomposition:

(A17) ( n ^ ) 1 2 ( β ^ n β ) = 1 n ^ i n δ i X ˜ i ( X ˜ i ) T 1 1 n ^ i n δ i R i + i n δ i θ i ( Δ i ( 0 ) Δ i T β ) + i n δ i Δ i ε i + i n δ i Δ i ( Δ i ( 0 ) Δ i T β ) ,

where

Δ i ( 0 ) = E [ δ i Y i Z i ] i n δ i w n ( Z i , Z j ) Y i .

So, using (A14)–(A15) and the Cauchy-Schwartz inequality, we obtain

(A18) 1 n ^ i n δ i θ i ( Δ i ( 0 ) Δ i T β ) + 1 n ^ i n δ i Δ i ε i + 1 n ^ i n δ i Δ i ( Δ i ( 0 ) Δ i T β ) = o P ( 1 ) .

This implies, using Lemma A.4, that

(A19) β ^ n β ( Σ 1 + o ( 1 ) ) 1 n ^ i n δ i R i + o ( 1 ) , in probability .

Then, according to condition (H6) (ii) and by applying Theorem 6.1.1 in [49] to { δ i R i , i Z 2 } , we obtain:

(A20) ( n ^ ) 1 2 i n δ i R i D N ( 0 , B ) .

The proof follows from (A14), (A19), (A20), and Lemma A.4.□

Proof of Theorem 4.2

It suffices to see that

(A21) m ^ n ( z ) m ( t ) = ( m ˆ y , n ( Z ) m y , n ( Z ) ) ( m ˆ X , n ( Z ) ( β ^ n β ) ) = S 1 S 2 .

Then, we have

(A22) n ^ ( ϕ z ( h n ) log ( n ^ ) ) m ^ n ( z ) m ( z ) n ^ ( ϕ z ( h n ) log ( n ^ ) ) S 1 + n ^ ( ϕ z ( h n ) log ( n ^ ) ) S 2 .

By Lemma A.2, we have

(A23) n ^ ( ϕ z ( h n ) log ( n ^ ) ) S 1 p 0 .

On the other hand, we can write

S 2 β ^ β E ( δ i X i Z i = z ) + i n δ i w n ( t , Z i ) X i E ( δ i X i Z i = z ) .

Then, by Theorem 4.1, β ^ n β converge in probability to 0, and according to (H7), we have E ( δ i X i Z i = z ) < . Moreover, by Lemma A.2, we have

n ^ ( ϕ z ( h n ) log ( n ^ ) ) i n δ i w n ( z , Z i ) X i E ( δ i X i Z i = z ) p 0 ,

which implies

(A24) n ^ ( ϕ z ( h n ) log ( n ^ ) ) S 2 p 0 .

Thus, from (A22)–(A24), the proof is complete.□

Proof of Theorem 4.3

From (A21), we have

(A25) n ^ ϕ z ( h n ) ( m ^ n ( z ) m ( t ) ) = n ^ ϕ z ( h n ) ( m ˆ y , n ( Z ) m y , n ( Z ) ) n ^ ϕ z ( h n ) ( m ˆ X , n ( Z ) ( β ^ β ) ) = S 3 S 4 .

Now, by Lemma A.3, we have

(A26) S 3 D N ( 0 , σ 2 ( z ) ) ,

and by Theorem 4.1, we have S 4 p 0 .

Then, from (A25) to (A26), the proof is complete.□

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Received: 2024-04-25
Revised: 2024-12-11
Accepted: 2025-02-17
Published Online: 2025-03-13

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

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

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