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Multiple structural breaks in cointegrating regressions: a model selection approach

  • Alexander Schmidt and Karsten Schweikert EMAIL logo

Abstract

In this paper, we propose a new approach to model structural change in cointegrating regressions using penalized regression techniques. First, we consider a setting with known breakpoint candidates and show that a modified adaptive lasso estimator can consistently estimate structural breaks in the intercept and slope coefficient of a cointegrating regression. Second, we extend our approach to a diverging number of breakpoint candidates and provide simulation evidence that timing and magnitude of structural breaks are consistently estimated. Third, we use the adaptive lasso estimation to design new tests for cointegration in the presence of multiple structural breaks, derive the asymptotic distribution of our test statistics and show that the proposed tests have power against the null of no cointegration. Finally, we use our new methodology to study the effects of structural breaks on the long-run PPP relationship.

JEL classification: C12; C22; C52
MSC classification: 62E20; 62J07; 91B84

Corresponding author: Karsten Schweikert, University of Hohenheim, Core Facility Hohenheim and Institute of Economics, Schloss Hohenheim 1 C, 70593 Stuttgart, Germany, E-mail:

Acknowledgements

We thank Robert Jung, Andrew Tremayne, and Jana Mareckova for valuable comments and suggestions. We are also grateful for the valuable remarks and suggestions by the editor, Bruce Mizrach, and an anonymous referee. We thank the organizers and participants of the Junior Research Seminar in Econometrics in Obermarchtal, Economics Brown Bag seminar at the University of Hohenheim, German Statistical Week in Linz, Conference on Decision Sciences in Konstanz, THE Christmas Workshop 2018 in Stuttgart, European Winter Meeting of the Econometric Society in Naples, 12th International Conference on Computational and Financial Econometrics in Pisa, and the 24th Spring Meeting of Young Economists in Brussels. Moreover, we thank Charles Engel and Chang-Jin Kim for making their data available and Daiki Maki for sending us his codes. Finally, we thank Maike Becker for excellent research assistance.

  1. Author contribution: All the authors have accepted responsibility for the entire content of this submitted manuscript and approved submission.

  2. Research funding: None declared.

  3. Conflict of interest statement: The authors declare no conflicts of interest regarding this article.

Appendix

Proof of Theorem 1

According to Assumption 1, the scalar partial sum process in Eq. (2) satisfies the functional central limit theorem (FCLT). For s ∈ [0, 1] and as T → ∞, it holds that

(21) x [ T s ] = T 1 / 2 t = 1 [ T s ] v t B ( s ) ,

where B(s) is a Brownian motion process with variance σ v 2 . This was shown by Herrndorf (1984) and extended to the vector case by Phillips and Durlauf (1986).

Next, we define the objective function V T ( b ) by

(22) V T ( b ) = t = 1 T ( u t b X t δ T 1 ) 2 u t 2 + λ T i = 2 p * + 1 w 1 i γ 1 | μ i * + b 1 i / T | + λ T j = 2 m * + 1 w 2 j γ 2 | β j * + b 2 j / T | ,

where b = ( b 1′, b 2′)′, δ T = diag ( T 1 / 2 I p * + 1 , T I m * + 1 ) and

(23) b ̂ = ( b ̂ 1 , b ̂ 2 ) = arg min V T ( b )

is the minimizer of V T with b ̂ 1 i = T ( μ ̂ T , i μ i * ) and b ̂ 2 j = T ( β ̂ T , j β j * ) .

First, we consider the asymptotic counterparts to the least squares terms

2 t = 1 T u t b X t δ T 1 + t = 1 T b X t δ T 1 δ T 1 X t b .

We use the decomposition X = ( X 1, X 2) to express the weak convergence result

(24) T 1 / 2 I m * + 1 X 2 , [ T s ] ( B ( s ) , B ( s ) φ τ 2,1 ( s ) , , B ( s ) φ τ 2 , m * ( s ) ) = B τ ( s ) ,

where

(25) φ τ k , l ( s ) 0 if s τ k , l 1 if s > τ k , l , k { 1,2 } , s [ 0,1 ] .

Using (A.4) in Gregory and Hansen (1996a) and the continuous mapping theorem (CMT, see Billingsley (1999), Theorem 2.7), we observe that

t = 1 T b X t δ T 1 δ T 1 X t b b ϒ 0 0 0 1 B τ ( s ) B τ ( s ) d s b ,

where the weak convergence is uniform over the vector ( τ 1,1 , , τ 1 , p * , τ 2,1 , , τ 1 , m * ) T . Further, using (A.3) in Gregory and Hansen (1996a) and Theorem 3.1 in Hansen (1992), we have the weak convergence to a stochastic integral

t = 1 T u t b X t δ T 1 b U 0 1 B τ ( s ) d U ( s ) + b 0 0 Λ ( 1 τ 2,1 ) Λ ( 1 τ 2 , m * ) Λ ,

where UN(0, ϒσ 2) and Λ = t = 0 E ( v t u 0 ) .

Under Assumptions 2 and 3, the maximum number of breakpoints is limited and initial least squares estimates are available for the weights of the adaptive lasso estimator. We investigate the consistency of the individual coefficients and distinguish between the true coefficients being zero or nonzero:

  1. If μ i * 0 , we have

    (26) λ T w 1 i γ 1 | μ i * + b 1 i / T | | μ i * | = λ T T 1 μ ̂ I , i γ 1 T | μ i * + b 1 i / T | | μ i * | p 0 ,

    since (i) λ T T 0 , (ii) 1 μ ̂ I , i γ 1 p 1 μ i * γ 1 if the initial estimator is consistent and (iii) T | μ i * + b 1 i / T | | μ i * | p b 1 i sgn ( μ i * ) as in Zou (2006).

  2. If μ i * = 0 , we have

    λ T w 1 i γ 1 | μ i * + b 1 i / T | | μ i * | = λ T T 1 μ ̂ I , i γ 1 | b 1 i |

    (27) = λ T T 1 / 2 γ 1 / 2 1 T μ ̂ I , i γ 1 | b 1 i |

    if b 1 i 0 0 if b 1 i = 0 ,

    since (i) λ T T 1 / 2 γ 1 / 2 and (ii) the initial least squares estimator is tight and converges to a normal distribution, T μ ̂ I , i W 1 i N 0 , σ 2 τ 1 , i ( 1 τ 1 , i ) .

  3. If β j * 0 , we have

    (28) λ T w 2 j γ 2 | β j * + b 2 j / T | | β j * | = λ T T 1 β ̂ I , j γ 2 T | β j * + b 2 j / T | | β j * | p 0 ,

    since (i) λ T T 0 , (ii) 1 β ̂ I , j γ 2 p 1 β j * γ 2 if the initial estimator is consistent and (iii) T | β j * + b 2 j / T | | β j * | p b 2 j sgn ( β j * ) .

  4. If β j * = 0 , we have

    λ T w 2 j γ 2 | β j * + b 2 j / T | | β j * | = λ T T 1 β ̂ I , j γ 2 | b 2 j |

    (29) = λ T T 1 γ 2 1 T β ̂ I , j γ 2 | b 2 j |

    if b 2 j 0 0 if b 2 j = 0 ,

    since (i) λ T T 1 γ 2 , (ii) the least squares estimator is tight and has the following nonstandard distribution

    (30) T β ̂ I , j W 2 j = 0 1 B τ 2 , j ( s ) d U ( s ) + ( 1 τ 2 , j ) Λ 0 1 B τ 2 , j 2 ( s ) d s ,

    and (iii) P ( W 2 j = 0 ) a . s . 0 .

Thus, V T ( b ) ⇒ V( b ), where

(31) V ( b ) = b A b 2 b B 2 b C if b k = 0 for all k A c if b k 0 for some k A c

with

A = ϒ 0 0 0 1 B τ ( s ) B τ ( s ) d s ,

B = U 0 1 B τ ( s ) d U ( s ) , U N ( 0 , ϒ σ 2 ) ,

C = 0 , , 0 , Λ , ( 1 τ 2,1 ) Λ , , ( 1 τ 2 , m * ) Λ .

Since V T is a convex function and V has a unique minimum, it follows from Knight and Fu (2000) that

(32) arg min V T ( b ) = b ̂ = T ( μ ̂ T μ * ) T ( β ̂ T β * ) arg min V ( b ) .

From these results, we can deduce that

(33) T ( μ ̂ T , A 1 c μ A 1 c * ) δ 0 | A 1 c | T ( μ ̂ T , A 1 μ A 1 * ) N ( 0 , Σ A 1 1 ϒ A 1 σ 2 ) ,

where δ 0 denotes the Dirac measure at 0. Correspondingly, we have

(34) T ( β ̂ T , A 2 c β A 2 c * ) δ 0 | A 2 c | T ( β ̂ T , A 2 β A 2 * ) 0 1 B τ , A 2 B τ , A 2 1 0 1 B τ , A 2 d U + C A 2 .

It remains to show that coefficients of inactive variables are set to zero with probability approaching one. We begin with a proof of P ( μ ̂ T , A 1 c = 0 ) 1 . Consider the event that μ ̂ T , i 0 although i A 1 c . We know from the Karush–Kuhn–Tucker (KKT) optimality conditions that the first order condition for a minimum is given by

(35) 2 φ τ 1 , i ( y x ( μ ̂ T , β ̂ T ) ) T = λ T w 1 i γ 1 sgn ( μ ̂ T , i ) T .

Note that

(36) λ T w 1 i γ 1 sgn ( μ ̂ T , i ) T = λ T T 1 / 2 γ 1 / 2 1 T μ ̂ I , i γ 1 ,

since (i) λ T T 1 / 2 γ 1 / 2 and (ii) T μ ̂ I , i is tight. The left hand side of the equation is equivalent to

(37) 2 φ τ 1 , i ( u x δ T 1 δ T ( μ ̂ T μ * , β ̂ T μ * ) ) T = 2 φ τ 1 , i u T 2 φ τ 1 , i x δ T 1 δ T ( μ ̂ T μ * , β ̂ T μ * ) T .

For the first term, we have the weak convergence

(38) φ τ 1 , i u T N ( 0 , σ 2 τ 1 , i )

and for the second term, we have the weak convergence of φ τ 1 , i x δ T 1 T , which depends on the timing of the break fraction τ 1,i relative to all other possible break fractions. Say τ 1 , i = τ 1 , p * > τ 2 , m * holds, then

(39) φ τ 1 , i x δ T 1 T 0 , , 0 , 0 1 B τ 2,1 ( s ) d s , , 0 1 B τ 2 , m * ( s ) d s .

Further, we have already shown the weak convergence of δ T ( μ ̂ T μ * , β ̂ T μ * ) . Hence, the distribution of the first term is tight and

(40) P ( μ ̂ T , i 0 ) P 2 φ τ 1 , i ( y x ( μ ̂ T , β ̂ T ) ) T λ T w 1 i γ 1 sgn ( μ ̂ T , i ) T = 0 0 .

Next, we show that P ( β ̂ T , A 2 c = 0 ) 1 . Again, we consider the event that β ̂ T , j 0 although j A 2 c . The KKT optimality condition in this case is given by

(41) 2 ( x φ τ 2 , j ) ( y x ( μ ̂ T , β ̂ T ) ) T = λ T w 2 j γ 2 sgn ( β ̂ T , j ) T ,

where the factor T substitutes the factor T in Eq. (35). For the right hand side of the equation, we observe that

(42) λ T w 2 j γ 2 sgn ( β ̂ T , j ) T = λ T T 1 γ 2 1 T β ̂ I , j γ 2 ,

since T β ̂ I , j is tight. For the left hand side,

(43) 2 ( x φ τ 2 , j ) u T 2 ( x φ τ 2 , j ) x δ T 1 δ T ( μ ̂ T μ * , β ̂ T μ * ) T ,

we have the weak convergence of the first term using

(44) ( x φ τ 2 , j ) u T 0 1 B τ 2 , j ( s ) d U ( s ) + ( 1 τ 2 , j ) Λ .

The expression of the weak convergence result for the second term depends on the timing of the break fraction τ 2,j . Say τ 2 , j = τ 1 , m * > τ 1 , p * holds, we have

(45) ( x φ τ 2 , j ) x δ T 1 T 0 1 B τ 2 , j ( s ) d s , 0 1 B τ 1,1 ( s ) d s , , 0 1 B τ 2 , p * ( s ) d s , 0 1 B τ 2 , j 2 ( s ) d s , 0 1 B τ 1,1 2 ( s ) d s , , 0 1 B τ 2 , m * 2 ( s ) d s ,

and as before δ T ( μ ̂ T μ * , β ̂ T μ * ) is tight. Finally, we have shown that

(46) P ( β ̂ T , j 0 ) P 2 ( x φ τ 2 , j ) ( y x ( μ ̂ T , β ̂ T ) ) T λ T w 2 j γ 2 sgn ( β ̂ T , j ) T = 0 0

and this completes the proof. □

Proof of Theorem 2

For ease of exposition, we assume that the maximum number of breaks is m* = 2 and the true intercept is known to be μ t = 0 for all t. In this case, we obtain three possible model selection outcomes regarding the number of breaks for the post-lasso regressions:

  1. All coefficients of break indicator regressors are shrunk to zero

    (47) y t = β 1 x t + e t τ 0 .

  2. One structural break is (falsely) detected

    (48) y t = β 1 x t + β 2 x t φ t , τ 2,1 + e t τ 1 .

  3. Two structural breaks are (falsely) detected

    (49) y t = β 1 x t + β 2 x t φ t , τ 2,1 + β 3 x t φ t , τ 2,2 + e t τ 2 .

Note that the specification of indicator terms in Eqs. (48) and (49), i.e., the timing of (falsely) detected breaks, depends on the tuning parameter λ. We continue the proof for the bias-corrected test statistic, Z 2, corresponding to the case of two (falsely) detected structural breaks with unknown timing. The asymptotic distribution of the test statistics for the two remaining cases can be easily deduced from our derivations. We decompose the cumulative sum into S t = (S 1t , S 2t )′. Further, we define the break fraction vector τ 2 = (τ 2,1, τ 2,2)′ as a compact set on (0, 1) × (0, 1) and define the matrix X t τ 2 = ( S t , S 2 t φ t , τ 2,1 , S 2 t φ t , τ 2,2 ) = ( S 1 t , X 2 t τ 2 ) .

Using the result

(50) T 1 / 2 S [ τ 2 , i T ] B ( τ 2 , i )

and the CMT yields the weak convergence of

(51) 1 T 2 t = [ τ 2 , i T ] T S t S t = τ 2 , i 1 B B .

Further, (50) and Theorem 4.1 of Hansen (1992) yield the weak convergence of

(52) 1 T t = [ τ 2 , i T ] T S t 1 u t = τ 2 , i 1 B d B + ( 1 τ 2 , i ) Λ .

The result in (51) can straightforwardly be extended to

(53) 1 T 2 t = 1 T X t τ 2 X t τ 2 = 0 1 X τ 2 X τ 2 ,

where X τ 2 = ( B 1 , B 2 , B 2 φ τ 2,1 , B 2 φ τ 2,2 ) = ( B 1 , X 2 τ 2 ) and

(54) φ τ 2 , i ( s ) = 0 if s τ 2 , i 1 if s > τ 2 , i , s [ 0,1 ] , i { 1,2 } .

Define β ̂ τ 2 = ( β ̂ 1 , β ̂ 2 , β ̂ 3 ) as the post-lasso least squares estimator and set η ̂ τ 2 = ( 1 , β ̂ τ 2 ) so that

(55) η ̂ τ 2 1 0 1 X 2 τ 2 X 2 τ 2 1 0 1 X 2 τ 2 B 1 = η τ 2 .

We partition

(56) Λ = Λ 11 Λ 12 Λ 21 Λ 22 Ω = Ω 11 Ω 12 Ω 21 Ω 22

in conformity with S t and define Λ2⋅ = (Λ21, Λ22) and Λ⋅2 = (Λ12, Λ22)′.

For each element of S 2 t τ 2 = ( S 2 t φ t , τ 2,1 , S 2 t φ t , τ 2,2 ) it holds that

(57) Δ S 2 t φ t , τ 2 , i = Δ S 2 t φ t , τ 2 , i + S 2 t 1 Δ φ t , τ 2 , i

and Δ φ t , τ 2 , i = φ t , τ 2 , i φ t 1 , τ 2 , i = 1 { t = [ τ 2 , i T ] } . Since φ t 1 , τ 2 , i Δ φ t , τ 2 , i = 0 and

(58) d ( B 2 ( s ) φ τ 2 , i ( s ) ) = d B 2 ( s ) φ τ 2 , i ( s ) + d φ τ 2 , i ( s ) B 2 ( s )

for the asymptotic counterpart, we have the identities

(59) 0 1 B d B 2 ( s ) φ τ 2 , i ( s ) = τ 2 , i 1 B d B 2 ( s ) + B ( τ 2 , i ) B 2 ( τ 2 , i )

and

(60) 0 1 B 2 φ τ 2 , i d B 2 ( s ) φ τ 2 , i ( s ) = τ 2 , i 1 B 2 φ τ 2 , i d B 2 ( s ) = τ 2 , i 1 B 2 d B 2 ( s ) .

Consequently, we can state the following important weak convergence results

(61) 1 T t = 2 T X t 1 τ 2 Δ S 2 t τ 2 0 1 X τ 2 d B 2 τ 2 + ( 1 τ 2,1 ) Λ 21 ( 1 τ 2,2 ) Λ 12 ( 1 τ 2,1 ) Λ 22 ( 1 τ 2,2 ) Λ 22 ( 1 τ 2,1 ) Λ 21 ( 1 τ 2,2 ) Λ 22 ( 1 τ 2,2 ) Λ 21 ( 1 τ 2,2 ) Λ 22 ,

where d B 2 τ 2 = ( d ( B 2 ( s ) φ τ 2,1 ( s ) ) , d ( B 2 ( s ) φ τ 2,2 ( s ) ) ) and

(62) 1 T t = 2 T X t 1 τ 2 Δ X t τ 2 0 1 X τ 2 d X τ 2 + Λ τ 2 ,

where

(63) Λ τ 2 = Λ 11 Λ 12 ( 1 τ 2,1 ) Λ 12 ( 1 τ 2,2 ) Λ 12 Λ 21 Λ 22 ( 1 τ 2,1 ) Λ 22 ( 1 τ 2,2 ) Λ 22 ( 1 τ 2,1 ) Λ 12 ( 1 τ 2,1 ) Λ 22 ( 1 τ 2,1 ) Λ 21 ( 1 τ 2,2 ) Λ 22 ( 1 τ 2,2 ) Λ 12 ( 1 τ 2,2 ) Λ 22 ( 1 τ 2,2 ) Λ 21 ( 1 τ 2,2 ) Λ 22 .

Under the null hypothesis, the cointegration residuals can be written as e ̂ t τ 2 = η ̂ τ 2 X t τ 2 and we can show weak convergence of the sample moments. It holds that

(64) 1 T 2 t = 1 T e ̂ t τ 2 2 = η ̂ τ 2 1 T 2 t = 1 T X t τ 2 X t τ 2 η ̂ τ 2 η τ 2 0 1 X τ 2 X τ 2 η τ 2 = σ 2 0 1 W τ 2 2 ,

where W τ 2 ( s ) = W 1 ( s ) 0 1 W 1 W 2 τ 2 0 1 W 2 τ 2 W 2 τ 2 1 W 2 τ 2 and

(65) 1 T t = 2 T e ̂ t 1 τ 2 Δ e ̂ t τ 2 = η ̂ τ 2 1 T t = 2 T X t 1 τ 2 Δ X t τ 2 η ̂ τ η τ 2 0 1 X τ 2 d X τ 2 + Λ τ 2 η τ 2 = σ 2 0 1 W τ 2 W τ 2 + η τ Λ τ η τ .

Next, we consider the bias-correction term for the first-order serial correlation coefficient. We denote the kernel weights as w(j/M) = w j and can show that

(66) ψ ̂ τ 2 = j = 1 M w j 1 T t Δ e ̂ t j τ 2 Δ e ̂ t τ 2 + o p ( 1 ) .

Hence, we have the weak convergence result

(67) ψ ̂ τ 2 = η ̂ τ 2 j = 1 M w j 1 T t Δ X t j τ 2 Δ X t τ 2 η ̂ τ 2 + o p ( 1 ) η τ 2 Λ τ 2 η τ 2 .

For the long-run variance, we obtain the result

(68) σ ̂ τ 2 2 η τ 2 Ω τ 2 η τ 2 ,

where

Ω τ 2 = σ 2 Ω 12 ( 1 τ 2,1 ) Ω 12 ( 1 τ 2,2 ) Ω 12 Ω 21 Ω 22 ( 1 τ 2,1 ) Ω 22 ( 1 τ 2,2 ) Ω 22 ( 1 τ 2,1 ) Ω 12 ( 1 τ 2,1 ) Ω 22 ( 1 τ 2,1 ) Ω 21 ( 1 τ 2,2 ) Ω 22 ( 1 τ 2,2 ) Ω 12 ( 1 τ 2,2 ) Ω 22 ( 1 τ 2,2 ) Ω 21 ( 1 τ 2,2 ) Ω 22

(69) = 1 , κ τ 2 1 0 0 D τ 2 1 κ τ 2 = σ 2 ( 1 + κ τ 2 D τ 2 κ τ 2 )

and

(70) D τ 2 = 1 ( 1 τ 2,1 ) ( 1 τ 2,2 ) ( 1 τ 2,1 ) ( 1 τ 2,1 ) ( 1 τ 2,2 ) ( 1 τ 2,2 ) ( 1 τ 2,2 ) ( 1 τ 2,2 ) .

Now, we use the CMT to show that

(71) Z 2 = 1 T 2 t = 2 T e ̂ t 1 τ 2 Δ e ̂ t τ 2 ψ ̂ τ 2 1 T 2 t = 2 T e ̂ t 1 τ 2 2 × 1 σ ̂ τ 2 T 2 t = 2 T e ̂ t 1 τ 2 2 1 / 2 σ 2 0 1 W τ 2 d W τ 2 + η τ 2 Λ τ 2 η τ 2 η τ 2 Λ τ 2 η τ 2 σ 2 0 1 W τ 2 2 × 1 σ 2 ( 1 + κ τ 2 D τ 2 κ τ 2 ) σ 2 0 1 W τ 2 2 1 / 2 = 0 1 W τ 2 d W τ 2 0 1 W τ 2 2 1 / 2 1 + κ τ 2 D τ 2 κ τ 2 1 / 2

for each configuration of τ 2. Correspondingly, the test statistics for the remaining model selection outcomes have the asymptotic distributions

(72) Z 1 0 1 W τ 1 d W τ 1 / 0 1 W τ 1 2 1 / 2 1 + κ τ 1 D τ 1 κ τ 1 1 / 2 ,

W τ 1 = W 1 ( s ) 0 1 W 1 W 2 τ 1 0 1 W 2 τ 1 W 2 τ 1 1 W 2 τ 1 ( s ) ,

κ τ 1 = 0 1 W 2 τ 1 W 2 τ 1 1 0 1 W 2 τ 1 W 1 ,

W 2 τ 1 = W 2 ( s ) , W 2 ( s ) φ τ 2,1 ( s ) ,

and

(73) Z 0 0 1 W τ 0 d W τ 0 / 0 1 W τ 0 2 1 / 2 ,

W τ 0 = W 1 ( s ) 0 1 W 1 W 2 0 1 W 2 2 1 W 2 ( s ) ,

respectively. Naturally, the distributions of Z 2 and Z 1 depend on the timing of the breakpoint. Finally, selecting the infimum statistic over all potential model selection outcomes is a continuous transformation so that we can use the CMT to complete the proof. □

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Supplementary Material

The online version of this article offers supplementary material (https://doi.org/10.1515/snde-2020-0063).


Received: 2020-06-01
Revised: 2021-02-06
Accepted: 2021-03-20
Published Online: 2021-04-09

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