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Open Journal of Statistics, 2011, 1, 185-198

doi:10.4236/ojs.2011.13022 Published Online October 2011 (http://www.SciRP.org/journal/ojs)

185

Double Autocorrelation in Two Way Error Component

Models

Jean Marcelin Bosson Brou1, Eugene Kouassi2, Kern O. Kymn3

1

Department of Economics, University of Cocody, Abidjan, Cote-dIvoire

2

Resource Economics, West Virginia University, Morgantown, USA

3

Division of Finance and Economics, West Virginia University, Morgantown, USA E-mail: [email protected]

Received September 15, 2011; revised October 16, 2011; revised October 30,2011

Abstract

In this paper, we extend the works by [1-5] accounting for autocorrelation both in the time specific effect as well as the remainder error term. Several transformations are proposed to circumvent the double autocorrela-tion problem in some specific cases. Estimaautocorrela-tion procedures are then derived.

Keywords:Two Way Random Effect Model, Double Autocorrelation, GLS, FGLS

1. Introduction

Following the works of [6], the regression model with error components or variance components has become a popular method for dealing with panel data. A summary of the main features of the model, together with a discus-sion of some applications, is available in [7-10] among others.

However, relatively little is known about the two way error component models in the presence of double auto-correlation, i.e, autocorrelation in the time specific effect

and in the remainder error term as well.

This paper extends the works by [2-5] on the one-way random effect model in the presence of serial autocorre-lation, and by [1] on the single autocorrelation two-way approach. It investigates some potential transformations to circumvent the double autocorrelation issue, along with some estimation procedures. In particular, we derive several transformations when the two disturbances fol-low various structures: from autoregressive and mov-ing-average processes of order 1 to a general case of double serial correlation. We deduce several GLS esti-mators as well as their asymptotic properties and provide a FGLS version.

The remainder of this paper is organized as follows: Section 2 considers simple transformations on the pres-ence of relatively manageable double autocorrelation structure. In Section 3, general transformations are con-sidered when the double autocorrelation is more complex. GLS estimators are derived in Section 4. Asymptotic

properties of the GLS estimators are considered in Sec-tion 5. SecSec-tion 6 provides a FGLS counterpart approach. Finally, some concluding remarks appear in Section 7.

2. Simple Transformations

To circumvent the double autocorrelation issue, we first need to transform the model based on the variance-co- variance matrix. The general regression model consid-ered is yit 0xituit, ;

where 0

1, ,

i  N t1, , T

 is the intercept and  is a vector of slope coefficients, it

1

k

x is a row vector of

ex-planatory variables which are uncorrelated with the usual two-way error components disturbances

1k

it i

u   t

it

 (see [7]). In matrix form, we writeyXu.

2.1. When the Errors Follow AR(1) Structures

If the time specific term follows an AR(1) structure, 1

tt t

    ,  1, with

0, 2 t IID

   , and the remainder error term also follow an AR(1) structure

, 1 iti t eit

    ,   1, with eit IID

0, e

2 

 , we

can define two transformation matrices of dimensions

T 2

 

T1

and

T 1

T respectively,

1 0 0

0 1

and 0

0 0 1

C

 

 

 

 

 

  

 

 

 

   

(2)

1

1 0 0

0 1

0

0 0

C

 

 

 

 

 

  

 

 

 

   

(1)

and since we have

3 2

, 1

e e

e e

i i

i

iT i T

C C

 

  

  

 

  

 

and

3 2

*

1

T T

C C

 

   

 

    

 

 

  

 

  (2)

the transformed errors * i

 and * follow two different MA(1) processes, of parameters  and  respective- ly. Thus, by applying the appropriate transformation ma-trices, the autoregressive error structure can be changed into a moving-average one. The only cost is the loss of the initial and first pseudo-differences, which has no se-rious consequence for a long time dimension. As a result, we focus on the MA(1) error structure.

2.2. When the Errors Follow MA(1) Structures

Here, the time specific term t follows an MA(1)

struc-ture,  t  t   t1 ,  1 with

2 0,

t IID

  

while the remainder error term, it also follows an MA

(1) structure, i t, eitei t, 1 ,  1 with

it

2 e

e IID 0, . For convergence purpose and assuming normality, the initial values are defined

2 2

0 0, 1 e

i N  

2

     

and

2 2

0 N 0,  1  2

     

The variance-covariance matrix of the three components error term is given by,

2 2 ' 2 '

e IN   IN i iT Ti iN N

  

         (3)

where   

 

and   

 

are positive defi-nite matrices of order T and where

 

.

xx,0, ,0

is defined by . The exact inverse of such matrices suggested by [11] and [1] does not involve the parameters

 

xToeplitz 1 2,

 and . Following [11], let be the Pesaran orthogonal matrix whose t-th row is given by,

P

2 π 2π

sin ,sin , ,sin

1 1 1

t

t t Tt

L

T T T T

 π

1

     

 

           

where

'

PP  ,  diag

1, , T

,

2

12cos π 1

t

t T

 

 

 , and

' PPD

1, , t

g dd

Ddia with 2  cos π 1

t T

 

 

1 2

t

d

  .

Pre-multiplying the model by

INP

of *

u

yields the fol-lowing variance-covariance matrix

INP u

,

'

* 2 2

I D I i i 

  2

'

e N N T Ti iN N

        (4)

where .

eral T

sformations

eral case of double

T T

i Pi

. Gen

ran

3

e are now in the context of a gen W

autocorrelation issue and lead to a suitable error covari-ance matrix similar to Equation (4) and its inverse.

.1. First Transformation 3

et P

L

tri

denote the matrix such that ' . Such

T

P  PI

a ma x does exist for  and is efinite matrix. Transformation of the initial model

a positive-d yXu by

INP

yields

P

y Xu

* N

yI   *  * (5)

and the variance-covariance of the transformed errors is

 

* * *' 2 '

N

2 ' ' 2 '

E u u I P P

N T T N N T

I P i i P i i I

   

 

   

   

    

(6)

This transformation has removed the autocorrelation in the time-specific effect t. Unfortunately, by doing

so it has infected the its a worsened the initial cor-

relation in the remaind disturbances. An additional “treatment” is therefore needed.

.2. Second Transformation

nd er

3

e now consider an orthogona

W l matrix P and a

di-P

agonal matrix D such that P P

  P'

'D (di-agonalization of '

P  P ). Thu cond

transformation

s, applying a se

INP

yields,

*

y** INP yX**u** (7) The underlying variance-covariance matrix of the errors is,

** **'

2

'

'

N

(3)

J. M. B. BROU ET AL. 187

'

2 ' ' ' 2 '

N T T N N

I P P i i P P i i P

   

 

    P (8a)

or,

** ** **' 2

1 2

2 ' 2 '

2 3

1

N

N T T N N

E u u I D

I i i  i i

 

 

   

   

(8b)

where iT PP iT ,

 

 ,  PP', P P

P P'

' D     2

2 2

1 

 

 ,

2 2

2 2

  

 , and

2

2 2

3

2 2 1 2 1  

  

    ,

if 2 2 2 2

  

    .

Here, because of the choice of matrices P and end up with

P,

we  IT

elemen

since is an or tri

ng the procedure de-ra, one gets

P

to

thogo eed

nal ma-x. Generally speaking,  and D just n to have zero off-diagonal ts, i.e., be diagonal matrices.

The double autocorrelatio structure is thus absorbed, and one can easily accommodate with the non-spherical form of ** by means of an accurate inversion process.

3.3. Computing the Inverse

n

The inverse of ** is obtained usi eloped by [1]. After a bit of algeb v

 

** 1

2 2

1

1 1 1

N T N T

E K E L J S

d N

 

      NT

(9) where

' 1

2 2

2 1

T T

di D i     , JNi iN N' ,

N

N N

J

E I

N

  , 1

T T

KD L ,

1 ' 1

T D i iT T

 

  ,

' 1 1

T T

L

i D  

D

i

2 2

4 2

1N 1 i

 

 

' 2

1

1

T T T

S S Si i S

  

 

 

 

and

s with

2 ' 2 T SiT

   

1

g s, , T

dia S

2 1

2 2

1 3

T

t t

N s

d N

 

  .

Proof: (see the A

4.

ition of the estimator followed ghted average property.

The GLS estimator is,

ppendix)

GLS Estimation

We begin with the defin y its interpretation and wei b

4.1. The GLS Estimator

Proposition 1:

 

**' ** 1 **

1 **'

 

** 1 **

GLS X X X y

 

   (10)

Proof: (Straightforward)

4.

ression models, [12,13] provide n interpretation of the GLS estimator, which is

appeal-2. Interpretation

In classical two-way reg a

ing in view of the sources of variation in sample data. In the straight line of their work, the GLS estimator may be viewed as obtained by pooling three uncorrelated esti-mators: the covariance estimator (or within estimator), the between-individual estimator and the within-indi- vidual estimator. They are the same as those suggested by [1] except for the last one which was labeled be-tween-time estimator. We have,

1) The covariance estimator,

**' **

1 C

'

** ** 1

X A X

  X A y1 ,

where A1

ENKT

;

2) The between-indivi ual estimator, d

**' **

1 **' *

2 2

B

*

X A X X A y

   ,

2 2

1

N T

A J S

N

 

where and,

e within-individual or,

3) Th estimat

**' **

1 **'

3 T

** 3

X A X X A

   y ,

where A3 

ENLT

.

It is im

from so on

portant to note that these estimators are obtained me transformati s of the regression Equation (7),

i.e.,

** ' * ** **

yINP yX u .

The covariance estimator, C

y

is obtained when Equa- tion (7) is pre-multiplied b M1

ENKT

A1; the tra

ones in the matrix o nsformation annihilates the individual- and time-ef- fects as well as the column of f ex-planatory variables. It is equivalent to the within estima-tor in the classical two-way error component model (see [1-7]).

The between-individual estimator B comes from the

(4)

'

2

1

N T

M i I

N

  . This is equivalent to averaging

indi-r each time peindi-riod. ividual estimator T

vidual equations fo

The within-ind  is derived when Equation (7) is transformed byM3

ENLT

A3. The presence of the idempotent matrix EN indicates that

this transformation wipes out th ell as the time specific error term t

e constant term as w

 . Howe , the individual effect i

ver

 remains.

4.3. GLS as a Weighted Average Estimator

ge of e three estimators defined above.

As in [14], the GLS estimator is a weighted avera th

Proposition 2:

C C B B

F F F

GLS T T

       (11) with,

 

**' ** 1 **

1 **' **

1 2

1 1

C

F X X X A

 

  ,

 

**' ** 1 **

1 **' **

2 B

X

F X X X A X

 

  ,

and

 

**' ** 1 **

1 **' **

3

1

T C B

F X X X A X I F F

d

 

    

Proof:

From Equation (10), it comes that

 

 

X**' ** 1y** X**' ** 1X** GLS

with

 

1

**' ** ** **' ** **' **

1 2

2 1

**' ** 3

1

1

X y X A y X A

X A y d

 

  

y

By definition, the estimators C, B and T are

re-spectively such that

**' ** **' *

X A y1X A1X * C,

**' ** **' **

2 2 B

X A yX A X  ,

and

**' ** **' **

3 3 T

X A yX A X  .

Therefore,

 

1

**' ** ** **' **

1 2 1

**' ** **' **

2 3

1

1

C

B T

X y X A X

X A X X A X

d

 

 

 

Or,

 

1

**' ** ** **' **

1 2 1

**' ** **' **

2 3

1

1

GLS C

B T

X X X A X

X A X X A X

d

 

 

 

 

Thus,

 

 

 

1 1

**' ** ** **' **

1 2

1

1 1

**' ** ** **' **

2 1 1

**' ** ** **' **

3 1

1

GLS C

B

T

C C B B T T

X X X A X

X X X A X

X X X A X

d

F F F

 

  

 

 

 

 

 

 

  

with FC, FB and FT

no

defined according to Equation 11). ld also te that the three estimators

(

We shou C, B

and T are uncorrelated. In fact,

2

** 1

1 2 N N T T 0

A A E J K DS

N

   

and

** 2

1 3 1 N T T 0

AA  EK DL

because K iT T 0 EN N  0

i , while A2**A3 0 since

N N

J E  . As a result,

cov  C, B cov C, T cov  B, T 0 (12)

Moreover, following [1], the fact that

 

1

rank M r M

 



2

ank rank

1 1 1

N T T N N

      

3 M

T (13)

le information gives evidence on the use of all availab

from the sample. The estimators C, B and T

to-gether use up the entire set of to GLS estimator

information build the

GLS

 with no loss at

rs o tor, say

all.

5. Asymptotic Properties

Under regular assumptions, the GLS and the three pseudo estimato f the coefficient vec GLS,

C

 , B and T are all consistent and asympto

the one obtain lassical two-way error component model (see [15]).

tically ed in the equivalent. It is a result similar to

c

5.1. Assumptions

We assume that the x sit are weakly non-stochastic, i.e.

(5)

189 J. M. B. BROU ET AL.

 

' '

** X A X

 ** ** **

1

plim plim X EN KT X

a

 

 

 

  

1

NT NT

   

   

for the first transformation;

 

'

' ** **

** ** 2

2 1

1

plim plim

N T

X J S X

X A X N

b

T T

   

   

 

 

  

   

 

 

for the second transformation; and

 

'

' ** **

** **

3

1 plim plim

N T

X E L X

X A X c

NT NT

 

 

 

  

   

   

more, in the straight for the third transformation. Further

line of [1], we also assume that,

 

'

' ** **

** ** 1

2 plim plim 0

N T

X E K u

X A u a

NT NT

 

 

 

   

   

   

for the first transformation;

 

'

'

** ** 2 2

** **

2

plim X

N

 

 

plim

1

0

N T

X A u b

T

J S u

T

 

 

 

 

   

 

 

 

 

for the second transformation;

 

'

' ** **

** ** 3

2 plim plim 0

N T

X E L u

X A u c

NT NT

  

   

  

  

   

addition,

the variance-components for the third transformation. In

' 1

lim i D iT  T   , so that T

quantity ' 1

T T

i D i 

2 2

2 1

 

. The lim and N 

symptotic 

infinite as T   taken as T  

garding the error v sures the a

denotes by remains its and pro lities a

, ss tions

re-ptotic erty of

The covariance estimator

d

babi

. All along this section ump

re

following [1], we consider the “usual” a ector **

u , as stated in [16] and [17],

which en normality.

5.2. Asym Prop the Covariance

Estimator

Proposition 3:

C

 is consistent.

T Proof:

Since,

**' **

1 **'

**

C X EN KT X X EN K u

     

Hence,

1

**' K X**

   

**' **

plim

plim 0

N T

C

N T

X E

NT

X E K u

NT

 

 

 

 

 

  

plim

 

 

Making use of assumptions (a1) and (a2), we establish the consistency of the covariance estimator, plim

 

C .

Proposition 4:

The covariance estimator C has an asymptotic nor-mal distribution given by,

1

**' **

2 1

1

, plim N T

a

C N

NT NT

 



X E K X

  

1 ation, we have

(14)

Proof:

Under the M -transform

**

 

** 0

N T N T

E EK uEK E u  .

Moreover its variance is given by

** 2

1

N T N

V EK u EK

eq

T and its inverse is

ual to 12

END

while assumption (a2) states t 1

he

absence of correlation between regressors and istur-. We have

d bances under the M1 transformation

**' **

* 2

N T d

N T

X E K u

NT

X



 *' **

1

0, plim E K X

N

NT

 

 

(15)

and,

1

**' ** **' **

C

N T N T

NT

X E K X X E

NT NT

 

    

    

   

hich we deduce that

K u

from w

1

**' **

2 1

0, plim

d C

N T

NT

X E K X

N

NT

 

 

 

   

 

.

Thus, the asymptotic normality of the covariance esti-mator immediately follows,

1

**' **

2 1 1

, plim N T

a C

X E K X

N

NT NT

 



 

(6)

5.3. Asymptotic Property of the Between-Time Estimator

Proposition 5:

The between time estimator B is consistent. Proof:

Since,

**' **

1 **' **

2 2

B X A X X A u

   

Hence, according to assumptions (b1) and (b2),

1

**' **

plim

N

J

X S X

  2

**' **

2

plim

plim 0

T

B

N T

N T

J

X S u

N T

    

    

     

 

  

   

 

 

 

 

 

the consistency of the between time estimator,

 

 

Making use of assumptions (b1) and (b2), we establish

 

plim B .

Proposition 6:

The between-time estimator B has an asymptotic

normal distribution given by,

1

**' **

2 1 1

, lim

N T

a B

X J S X

N

N p

T T

 

       

      

 

  

 

Proof:

nsformation, we get

  

 

(16)

Under the M2-tra

 

' '

**

N N

T

i i

E I u

N N

    

 

   ** 0

T

I E u



    

 

The variance of this error term is written as

' 2

** 2 1 2 '

1 N

T T

i

V I u S i

N N

 

  

  

  



  

  iT

Its inverse is Again, ption (b2) states the ab-se rrelation between regressors and disturbances un

T

S . assum nce of co

der the M2 transformation. We get

**' **

2 N

T

d

J

X S u

N T

 

  

**' **

2 0, plim

N T

J

    

X S X

N N

T

   

  

  

  

 

In addition, we have

1

**' **

2

**' **

2

N T

B

N T

J

X S X

N T

T

J

X S u

N

T

 

   

   

 

 

 

 

 

 

   

   

 

 

 

 

 

that from which we deduce

1

**' **

2 0, plim

d B

N T

T

J

X S X

N N

T

 

 

 

 

Thus, the asymptotic normality of the between-time es-timator immediately follows,

1

**' **

2 1 1

, plim

N T

a B

X

J S X

N N

T T

 

 

 

 

 

 

 

 

.

5.4. Asymptotic Property of the Within-Individual Estimator

ator

Proposition 7:

The within individual estim T is a consistent

estimator.

Proof:

Since,

**' **

1 **' **

3 3

T X A X X A u

   

Hence,

1 **'

plim plim N

T

X E

NT

   

 

**

**' **

T

L X

X E L u

T

 

 

  

plim N T 0 N

 

(7)

J. M. B. BROU ET AL. 191

f assumptions (c1) and (c2), we establish the consistency of the covariance estimator,

Making use o

 

plim T 

Proposition 8:

thin individual estimator

The wi T has an

asymp-totic normal distribution given by,

1

**' **

, plim N T

a T

X E L X

d N

NT NT

 



 

 

(17)

Th is obtained as

Proof:

Under the M3-transformation, we obtain

**

 

** 0

N T N T

E EL uEL E u

e variance of

**

N T

EL u

**

N T

V EL ud ENLT

The inverse of this matrix is 1

EN LT

d  . Assumption (c2) states the absence of correlation between regressors and disturbances under the M3 transformation. We have

**' **

**' **

0, plim

N T d

N T

X E L u

NT 

X E L X

N d

   

 

 

and,

NT

 

 

1

**' **

N T

X E L X

NT

  

 

from which we deduce that

**' **

T

N T

NT

X E L u

NT

   

 

  



1

**' **

0, plim

d T

N T

NT

X E L X

N d

NT

 

 



  

 

Thus, the asymptotic normality of the within individual estimator immediately follows,



1

**' **

, plim N T

a T

X E L X

d N

NT NT

 



 

 

 

 

of the GLS Estimator

Proposition 9:

The GLS estimator

5.5. Asymptotic Property

GLS

ator

is asymptotically equivalent to the covariance estim C and therefore,

1

**' **

2

1

, lim X EN KT X

N p

NT

 



 

 

(18)

1 a GLS

NT

 

  

 

 

 

Proof:

From Equation (10), we get

 

 

1

1 1

**' ** ** **' ** **

X X X u

 

 

   

GLS

NT

NT NT

     

   

   

On the one hand, we have

 

1

**' ** ** **' **

2 1

**' ** **' **

2 1

1 1

N T

N T N T

X X X E K X

NT NT

X E L X X J S X

d NT N N T

 

 

 

 

here

' 1

2 2

2 1

T T

di D i     

w 

om assumption (a1), we find

, as .

There-fore, fr that

T 

** 1

wise

' **

0

N T

X E L X

d NT

 , when N T,  . Like ,

assumption (a2) leads us to

**'

X J **

1

0

X

N  ,

when . Hence,

2 N ST

N T

,

N T  

 

1

**' ** ** **' **

2 1 1

plim X X plim X EN KT X

NTNT

 

 

 

 

 

On the other hand, we can write

 

1

**' ** ** **' **

** **

1 N T

X u X E K u

NT

2 1

**' **'

2

1 1

N T N T

NT

X E L u X J S u

N NT

 

 

the M1 and mations, we get

d NT

 

.

Under M2 transfor

**' **

**' **

1 plim

1

2

plim 0

N T

N T

X E L u

d NT

X J S u

T

  

 

 

 

  

N N



 

(8)

leading to

 

1

**' ** ** **' **

2 1

1

plim X u plim X EN KT u

NTNT

 

   

  

 

.

As a result,

1

**' **

**' **

plim

plim

plim

GLS

N T

N T

NT

X E K X

NT

X E K u

NT

 

 

  

 

 

 

  



 

 

i.e.,

plim NTGLS plim NTC 

Finally, NT

GLS 

has the same limiting distribu-tion as NT

C

of the two

. This shows the asymptotic equivalence estimators GLS and C. We then deduce that,

1

**' **

2 1 1

, plim N T

a GLS

X E K X

N

NT NT

 



 

.

Thus, the GLS estimator suggested under the double au- ation error structure has the desired asymptotic ies.

6. FGLS Estimation

the

variance-n it i

approach is required. The method used consists in removing the time specific effect to ob-tain a one-way error component model where only tocorrel

propert

In practice, covariance matrix is unknown, as well as all the parameters involved i s determ nation. Therefore, a FGLS

it

his carries the serial correlation (see [18] and [3]). T method has been directly applied to AR(1) and MA(1) processes in separate subsections.

6.1. Feasible Double AR(1) Model

We assume that it   i, 1t eit, t  t1t,

1 

  , 1,

2

e e IID 0

it

   , , 0, 2

t IID

   .

The within error term is,

 

 

 

N T N T N T T

uEI uE iEI    i  (19) The associated variance-covariance matrix is,

 

 ' 2

'

2

N T T N

E uu E i i E

       (20)

Since it follows an AR(1) process of parameter ,

we define the matrix C as the famili mation matrix with parameter

ar [19] transfor-

 . This matrix is su ch that,

2

'

2

2 2 e

1 T T

C C    I  I

r is given by The resulting GLS estimato

*' *

1 *' *

W X X X y

   (21)

where *

N

yIC y and X*

INC X

. us The covariance matrix of *

N

uIC u, ing [20] trick, is

* 2 2 2 2

e e

1 d EN JT EN ET

    

      

(22) where

 



'

' 

1

1 1

1

1 1 1 1

T T

i Ci

i

 

 1

T

 

 

  

  

   

   

 

' 2

1

T T T

J i i

d

 

, 

T

T T

E IJ 

and

2

2 ' '

2 2 2 2

1

1 1 1

T T T T

d i i i i

T d

   

 

  

  

  

 

     

Following [21], another GLS estimator can be derived. We label this estimator the within-type estimator and is given by

**' **

1 **' ** WGLS X X X y

   (23)

with   1 *

** 2 *

y  y

  and  

1 *

** 2 *

X  X

  . In order to get the estimates of numerous parameters involved in the we first need an estimate of the correlation coef-model,

ficient . The autocorrelation function of the error term u is given by

 

 

2 2

, 1

for 0,1, ,

N

h t

h it i t h

N

h E u u   

        

We deduce from it that

 

 

(24)

 

 

 

 

1 2

0 1

 

 

 

(9)

J. M. B. BROU ET AL. 193

to a convergent estimator of  (see [7]), i.e.,

 

 



 



 



 

1 2

0 1

  

where 

 

   

 ,

1 1

1 N T

it i t h i t h

h u u

N T h

 

   

 

with uit

de-fined s the OLS ra esiduals of the within equation

  

yXu. Hence, we get

 

 1

1 

  

  

2 e BQU estimate of

 (25a)

(25b)

Furthermore, th and

1

1

d     T

2

2

 

 

2 e

 is also avail-able as

 



*' *

2 e

1 1

N T

u E E u

N T

 

   

 (26)

u being the OLS estimate of u*. As a consequence, we get

*

 2e

1

2

2 

  

 (27a)

and

 

1

 

2 2

0

N N

 

  

W

 

  (27b)

e now need to find 2 and . Th autocovariance function of the initial error term u is gi n

e ve

 

2 2 2 

 

2

1

h h N h

h h

N

      

       

 

for

0,1, , h  t. It comes that,

2 

 

0 

 

0

 

2 2

0 1

N N

  

     

  (28)

We immediately deduce a c erge second correlation coefficient, ,

onv

i.e.

nt estimator of the

 

 



 



 

 

 



 



 

1 2 1 2

1

0 1 0 1

1 N N

N

N

 

 

where 

 

   

   

 

   

 

(29)

1

 

N T

u

 

 

it i t h, with

N Th i1t h1 

h u

  

de-

noting the OLS residuals of yXu. The varian s

it

u

ce 2

e

 is estimated by,

2

 

2 2

1

e

   

ators mention ch as the within

(30)

addition to the GLS estim ed in Se r GLS estimators su estimator In

othe

ction 4,

W

and the within-type estimator WGLS can all be

per-formed as well. Actually, the knowledge of the AR(1) parameters  and 

termin

entitles us to bu

n of

 

** 1ild the ma lved in e de atio , say ma

trices trices invo

C

th

, C, C, P, , D, KT, LT, S

, 1

e ei t

and

6.2. Feasible Double MA(1) Model

state that

T.

S

We now itit  , with  1 and

2

e

eitIID 0, . Again, deviations from individual means lead to the model

yXu with    it i

u   it

trix of u . The

Equ

variance-covariance ma ation (20), with now

is still given by

2

Toeplitz 1, ,0, ,0 1

r

 

 

  

    

   (31)

Here, we set CCT, CT denoting the correlation

cor-rection matr s defi by [8] in their orthogonalizing algorithm. We then transform th hin model by

i

e wit x a ned

IN C

riance

 . The ew ern ha the fo win atrix,

ror term s llo g

m

* u cova

* 2 2 2 2

T

N EN ET

d E J 

     (32)

Because of the

  

    

moving average nature of the process, linear estimation of the correlation parameter  is not

easily obtainable. Instead, 2 1

r 

   

 proves useful.

The autocorrelation function of the within error term uit

is given by,

 

 

2

 

h

, 1

it i t h

N

h E u u

N  

         

  (33)

for h0,1, , t

with 

 

h denoting the autocovariance function of

it

 . As a consequence, 2  

 

1

N j N

 

  for some

and 2

j

2 

 



 

2

0 N 0

1

N

   

 (34)

(10)

where 

 

 , 1

1 N T

it i t h i t h

h u u

N T h

 

  

 

1 is the pirical em

autocovariance function and u sit are the OLS residuals

of the within equation. We also get, for some j2,



 



 

2 1

1

N r

N

 

j

 

 

(35)

We then apply the [8] matrix to the data (for in-stance to the within transformed dependent vector T

C

y).

r,

to get estim of the

Moreove CT will be applied to the vector of constants

t

ates  s. W , in the straight e

of

Ste pute

e have lin

[8], the following steps:

p 1: Com

* 1

1 ,1 i i

y y

g

 and

 *

, 1

, 1 *

, i t it

t it

t

r y y

g y

g

 

for t2, ,T

where  2 ,t 1

r

g   

for t 2, ,T

, 1t

g 

  .

Step 2: Compute   1 *

** 2 *

y  y

  knowing that

'

1 2

T T T T

i C i     . The estimates of the tsare

obtained as  1 1 and

 

, 1 ,

1 r

g

 

t

t

g

 

fo ,T.

We then obtain the estimate of

t

  r t2,

2

d as 2 2

1 T

t t

d 

.

 of the initial pirical counterpart The autocovariance function

2

 

h E u u

it i t h,

 

h

   

composite error term u and its em

 

h   

 

 ,

it i

h u u

1 1

T

h

1 N

t h i t

N Th

 

 

 , (it b

del)

u

mo

eing the OLS

residuals of the in -way mation of

itial two permit the esti-2

 and r,

2 

 

2 2

0

  

    and

(36a)

 

 2 2 2 1 r

r   

  

 

 

(

The within estimator

36b)

W

 and the within-type one

WGLS

GLS

are now obtainable. However, the GLS estimator

 can be estimated, provided the MA(1) parameters 

 and  2

are known, especially under the conditions 1 4r 0

     and    1 4r2 0. In other words, the estimates r and r should b h lie e open interval

ot inside th 1 1,

2 2

 

  as a

GLS

pre-requisite to a direct

estimation of  , C, Band T.

7. Final Remarks

au dealt with some

par-simonious models, especially the AR(1) and MA(1) ones, as well as the general framework. T

a of the variance-covariance matrix of the errors, rived the GLS estimator and related asymptotic properties. An investigation of the FGLS

ered in the paper.

8.

[1]

la

[2] B. H. Baltagi . Li, “A Transform e Problem

Component Model,” Journal of Econometric, Vol. 48, No.

-393.

This paper has considered a complex but realistic corre-lation structure in the two-way error component model: the double tocorrelation case. It

hrough a precise formul

we de

is also

References

N. S. Revankar, “Error Component Models with Serial Corre ted Time Effects,” Journal of the Indian Statisti-cal Association, Vol. 17, 1979, pp. 137-160.

and Q ation that will Cir-cumvent th of Autocorrelation in an Error 3, 1991, pp. 385 doi:10.1016/0304-4076(91)90070-T

[3] B. H. Balt d Q. L Predic in

ror Component Model with Seragi an i, “ ial Correlation,” tion the One-Way Er-Journal of Forecasting, Vol. 11, No. 6, 1992, pp. 561-567.

0110605 doi:10.1002/for.398

] B. H. Baltagi and Q. Li, “Estimating Error Component [4

Models with General MA(q) Disturbances,” Econometric Theory, Vol. 10, No. 2, 1994, pp. 396-408.

doi:10.1017/S026646660000846X

[5] J. W. Galbraith and V. Zinde-Walsh, “Transforming the Error Component Model for Estimation with general ARMA Disturbances,” Journal of Econometrics, Vol. 66, No. 1-2, 1995, pp. 349-355.

doi:10.1016/0304-4076(94)01621-6

[6] P. Balestra and M. Nerlove, “Pooling Cross-Section and Time-Series Data in the Estimation of a Dynamic Model: for Natural Gas,” Econometrica, Vol. 34,

. 585-612.doi:10.2307/1909771

The Demand No. 3, 1966, pp

[7] B. H. Baltagi, “Econometric Analysis of Panel Data,” 3rd Edition, John Wiley and Sons, New York, 2008.

[8] C. Hsiao, “Analysis of Panel Data,” Cambridge Univer-sity Press, Cambridge, 2003.

References

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