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Subsections

2 Description of a single-mode interferometer

 

  
\begin{figure}
\begin{center}
\leavevmode
 
\includegraphics [angle=-90,width=0.9\textwidth]{functdiag.ps}
 \end{center}\end{figure} Figure 1: Functional diagram of a single-mode interferometer. The dark underlying box merges the interferometric functions that can be integrated on a single optical chip. The numbers at the right bottom refer to the corresponding paragraph numbers

To understand where and how integrated optics can play a role in astronomical interferometry, we review the different optical functions present within an interferometer (see Fig. 1). This comes after a summary of stellar interferometry principles. All interferometers but GI2T being single-mode beam combiners (the field is limited to the diffraction pattern of each aperture), we limit our study to the single-mode field, the most appropriate mode for integrated optics.

A two-telescope stellar interferometer provides the measure of interference fringes between two beams at the spatial frequency $B/\lambda$, where $\lambda$ is the wavelength, and B the projection of the baseline vector $\vec{B}$ defined by the two telescopes along $\vec{s}$ the unit vector pointing to the source. The complex visibility of these fringes is proportional to the Fourier transform of the object intensity distribution (Van-Cittert Zernike theorem). Hereafter we call visibility V the modulus of the degree of coherence at the spatial frequency $B/\lambda$ normalized to the value at the zero frequency,  
 \begin{displaymath}
 V =\frac{\vert\tilde{I}(B/\lambda)\vert}{\vert\tilde{I}(0)\vert},\end{displaymath} (1)
and phase $\phi$ its argument. The phase is related to the position of the photo-centroid of the source $\vec{s}$ by the relation:  
 \begin{displaymath}
 \phi =2\pi\frac{\vec{B}.\vec{s}}{\lambda}.\end{displaymath} (2)
For ground-based interferometers, the source phase is corrupted by atmospheric turbulence. This prevents an absolute measurement of the source phase. However it is possible to measure the difference in source phase between two wavelengths[*].

2.1 Light collecting

The stellar light is collected by each individual aperture. These apertures can be either siderostats (e.g. Mark III, PTI, IOTA) or telescopes (e.g. GI2T, VLTI, Keck Interferometer). The coverage of the spatial frequencies is usually done by carefully locating the apertures in order to take advantage of the earth rotation which induces a variation of the length and orientation of the projected baselines (super-synthesis effect). If the structure of the object does not depend on wavelength, then observing at different wavelengths is equivalent to observing at different spatial frequencies. When the apertures are movable (GI2T, IOTA, SUSI), the interferometer can cover many different baselines with different geometrical configurations.

2.2 Beam transportation

The beams coming out from each telescope must be directed toward the beam combination table. Two different techniques can achieve this transportation:

2.3 Optical path delay (OPD)

The optical path from the beam combiner upward to the stellar source are not identical for each beam. The interferometer must equalize the pathlength at the micron-level accuracy. Furthermore the path lengths change with time and the interferometer must take into account the sidereal motion. This optical function is performed with delay lines.

The classical solution consists in a retro-reflector based on a moving chart [Colavita et al. (1991)]. The retro-reflector can be either a cat's eye or a corner cube. [Reynaud & Delaire (1994),Zhao et al. (1995)] have proposed to stretch optical fibers to delay the optical path. Laboratory experiments showed that this type of delay lines can achieve more than 2 m continuous delay with 100 m silica fibers [Simohamed & Reynaud (1996)], and about 0.4 mm continuous delay with 3.4 m fluoride fibers [Zhao et al. (1995)]. However in the latter case, the maximum optical path delay is somewhat limited since the fiber length is restricted to the maximal accepted stretch: [Zhao et al. (1995),Mariotti et al. (1996)] proposed multi-stage delay lines which perform short continuous delays by fiber stretching and long delays by switching between fiber arms of different lengths. However the differential dispersion in fibers of different length still remains a limiting factor of this technology.

Optical path modulation using silica fibers has been implemented in the ESO prototype fringe sensor unit [Rabbia et al. (1996)].

2.4 Beam quality control

  The control of the beam quality is essential to maintain the intrinsic contrast of the interferometer.

2.5 Photometric calibration

  The interference signal which is measured in stellar interferometry is directly proportional to each incoming beam intensity. These intensities fluctuates because of the atmospheric turbulence. The estimation of the fringe contrast is improved when these intensities are monitored as suggested by [Connes et al. (1984)] and validated by [Coudé du Foresto (1996)]. Photometric calibration combined with spatial filtering leads to visibility accuracies better than 0.3% [Coudé du Foresto et al. (1996)].

2.6 Beam combination

 
  
\begin{figure}
\begin{center}
 \leavevmode
 
\includegraphics [angle=-90,width=0.95\columnwidth]{recomb_bulk.ps}
 \end{center}\end{figure} Figure 2: The different types of beam combination in classical optics with the profile of the output intensity

[Mariotti et al. (1992)] have classified the different types of beam combinations. In the single-mode case, there are two types of beam combination:

In bulk optics, the co-axial combination is performed with a beam splitter whereas the multi-axial combination is done by focusing the different beams on the same spot. In the case of multi-axial combination, the differential tilt between the beams produces fringes on the point spread function. The co-axial combination can be regarded as a particular case of the multi-axial mode where all the beams are superposed without tilts: the fringes disappears and the amplitude of the resulting spot depends on the phase difference between the two beams.

The fringe encoding is achieved, in the co-axial case, by modulating the optical path difference between the two beams which results in an intensity modulation, or, in the multi-axial case, by sampling the spatial fringes with a detector matrix[*]. Usually if the fringes are coded in one direction, the other direction is compressed to reduce the number of pixels.

2.7 Spectral information

  This function is not always implemented in existing instruments, although it is useful for two objectives: to estimate the physical parameters of the source (temperature, kinematics, ...), and, to determine the position of the central fringe at zero OPD. The distance between the fringes being directly proportional to the wavelength, one can derotate the fringe phase like in Mark III and PTI [Shao et al. (1988)] or to measure the group-delay like in GI2T [Koechlin et al. (1996)].

The spectral information can be obtained by dispersing the fringes with a dispersive element (GI2T, PTI). Mariotti & Ridgway (1988) also suggested to apply the concept of Fourier transform spectrography to interferometry by performing double Fourier transform interferometry.

2.8 Detection

In the visible, the detectors are either CCDs or photon-counting cameras. In the infrared, for long mono-pixel InSb detectors have been used, but with the availability of array detectors with low read-out noise, interferometers started to use detector matrices.


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