It is often convenient to introduce the proper reference frame of the detector with coordinates . Because the motion of this frame with respect to the SSB is non-relativistic, we can assume that the transformation between the SSB-related coordinates and the detector’s proper reference frame coordinates has the form

where the functions describe the motion of the origin of the proper reference frame with respect to the SSB, and the functions account for the different orientations of the spatial axes of the two reference frames. One can compute some of the quantities entering Eqs. (12) in the detector’s coordinates rather than in the TT coordinates. For instance, the matrix of the wave-induced spatial metric perturbation in the detector’s coordinates is related to the matrix of the spatial metric perturbation produced by the wave in the TT coordinate system through equation where the matrix has elements . If the transformation matrix is orthogonal, then , and Eq. (19) simplifies to See [31, 54, 68, 78] for more details.For a ground-based laser-interferometric detector, the long-wavelength approximation can be employed (however, see [27, 115, 114] for a discussion of importance of high-frequency corrections, which modify the interferometer response function computed within the long-wavelength approximation). In the case of an interferometer in a standard Michelson and equal-arm configuration (such configurations can be represented by Figure 1 with the particle 1 corresponding to the corner station of the interferometer and with ), the observed relative frequency shift is equal to the difference of the round-trip frequency shifts in the two detector’s arms [136]:

Let be the components (with respect to the TT coordinate system) of the 3-vector connecting the origin of the TT coordinate system with the corner station of the interferometer. Then , , and, making use of Eq. (17), the relative frequency shift (21) can be written as The difference of the phase fluctuations measured, say, by a photo detector, is related to the corresponding relative frequency fluctuations by One can integrate Eq. (22) to write the phase change as where the dimensionless function , is the response function of the interferometric detector to a plane gravitational wave in the long-wavelength approximation. To get Eqs. (24) – (25) directly from Eqs. (22) – (23) one should assume that the quantities , , and [entering Eq. (22)] do not depend on time . But the formulae (24) – (25) can also be used in the case when those quantities are time dependent, provided the velocities of the detector’s parts with respect to the SSB are non-relativistic. The error we make in such cases is on the order of , where is a typical value of the velocities . Thus, the response function of the Earth-based interferometric detector equals where all quantities here are computed in the SSB-related TT coordinate system. The same response function can be written in terms of a detector’s proper-reference-frame quantities as follows where the matrices and are related to each other by means of formula (20). In Eq. (27) the proper-reference-frame components and of the unit vectors directed along the interferometer arms can be treated as constant (i.e., time independent) quantities.From Eqs. (26) and (3) it follows that the response function is a linear combination of the two wave polarizations and , so it can be written as

The functions and are the interferometric beam-pattern functions. They depend on the location of the detector on Earth, the position of the gravitational-wave source in the sky, and the polarization angle of the wave (this angle describes the orientation, with respect to the detector, of the axes relative to which the plus and cross polarizations of the wave are defined, see, e.g., Figure 9.2 in [135]). Derivation of the explicit formulae for the interferometric beam patterns and can be found, e.g., in Appendix C of [66].In the long-wavelength approximation, the response function of the interferometric detector can be derived directly from the equation of geodesic deviation [126]. Then the response is defined as the relative difference between the wave-induced changes of the proper lengths of the two arms, i.e., , where and are the instantaneous values of the proper lengths of the interferometer’s arms and is the unperturbed proper length of these arms.

In the case of an Earth-based resonant-bar detector the long-wavelength approximation is very accurate and the dimensionless detector’s response function can be defined as , where is the wave-induced change of the proper length of the bar. The response function can be computed in terms of the detector’s proper-reference-frame quantities from the formula (see, e.g., Section 9.5.2 in [135])

where the column matrix consists of the components (computed in the proper reference frame of the detector) of the unit vector directed along the symmetry axis of the bar. The response function (29) can be written as a linear combination of the wave polarizations and , i.e., the formula (28) is also valid for the resonant-bar response function but with some bar-pattern functions and different from the interferometric beam-pattern functions. Derivation of the explicit form of the bar patterns can be found, e.g., in Appendix C of [66].
Living Rev. Relativity 15, (2012), 4
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