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          August 31, 2006
                         3:8
 JWBK119-23
                             Detecting Outliers and Level Shifts             357
                                                          (d)
      If we let y t = [φ(B)/θ(B)]Y t and x t = [φ(B)ω(B)/θ(B)δ(B)]ξ t  , we have
        y t = ω 0 x t + ε t ,
      which is just a simple linear regression equation. Thus, the impact parameter ω 0 can
      be estimated using
               T                           2
               t=1  y t x t              σ    ,
                T   2    with Var( ˆω 0 ) =   T  2
        ˆ ω 0 =
                t=1  x t                 t=1  x t
      where T representsthesamplesize.Usingtheseequations,wecanobtainthefollowing
      estimates of ω 0 for the three types of disturbance mentioned above:

                           T−t
               ⎧

               ⎨ 2
                 ρ     y t −  π i y t+i  t = 1, 2,..., T − 1,
        ˆ ω AO,t =  AO,t                                                   (23.4)
                           i=1          t = T,
               ⎩
                 y t
         ˆ ω IO,t = y t                 t = 1, 2,..., T,                   (23.5)
               ⎧
                          T−t

               ⎨ 2
                 ρ    y t −  η i y t+i  t = 1, 2,..., T − 1,
         ˆ ω LS,t =  LS,t                                                  (23.6)
                          i=1
               ⎩                        t = T,
                 y t
                                 −1                                −1
      where ρ 2  = 1 +    T−t  π 2  , ρ 2  = 1, and ρ 2  = 1 +    T−t  η 2
             AO,t         i=1  i    IO,t        LS,t        i=1  i  . The π i and η i
                                                               2
                          i
      are the coefficients of B in the polynomials π(B) = 1 − π 1 B − π 2 B − ... = φ(B)/θ(B)
                              2
      and η(B) = 1 − η 1 B − η 2 B − ... = π(B)/(1 − B), respectively. The π weights are
      found by multiplying both sides of the definition of π(B)by θ(B)toget θ(B)(1 −
               2
      π 1 B − π 2 B − ...) = φ(B). For example, for an ARMA(1,1) process we have
                                      2
        1 − φB = (1 − θ B)(1 − π 1 B − π 2 B − ...)
                                         2
                                                       3
               = 1 − (π 1 + θ)B − (π 2 − θπ 1 )B − (π 3 − θπ 2 )B − ....
      Equating the coefficients of like powers of B, we have π 1 = φ − θ, π 2 = θπ 1 , and
      π j = θπ j−1 = θ  j−1 π 1 for j > 1. A similar approach can also be used in calculating
      the η weights. One can easily verify that for an ARMA(1,1) model the corresponding
      η weights are η 1 = φ − θ − 1 and η j = η j−1 + θ  j−1 π 1 for j > 1. Thus, for an AR(1)
                    j
      process, π j = φ and η j = φ − 1 for j ≥ 1.
        Using the above results, we can construct the following test statistic for testing the
      existence of AO, IO, and LS at time point d:
                  ˆ ω j,d    ˆ ω j,d
        λ j,d =           =      ,    j = AO, IO, LS.                      (23.7)
              [Var( ˆω j,d )] 1/2  ρ j,d σ
      Under the null hypothesis of no outliers or level shifts, and assuming that both time
      d and the parameters of the ARMA model in equation (23.1) are known, the statistics
      λ AO,t , λ IO,t and λ LS,t are asymptotically distributed as N(0,1). In practice, the time series
      parameters for this statistic are usually unknown and must therefore be replaced by
      some consistent estimates. 33,34
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