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The VLT Interferometer - ESO

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in Table I for incidence angles 9 equal to 45 and 60 degrees (a quarter<br />

wave retardation corresponds to 90 0 retardation). Also shown in Table I<br />

are the measurements for a silver over chrome coating of interest for<br />

astronomical interferometry3.<br />

Both polarization and retardation vary approximately as 9 3 for small<br />

incidence angles. At visible wavelengths the polarization /retardation<br />

effects are substantial especially when one considers the presence of<br />

a number of these reflections in the beam. At infrared wavelengths the<br />

effects are minor. Since the magnitude of the effects sharply increase<br />

wi th e it is important to keep the incidence angles as small as<br />

possible. More complex multilayer coatings in which the reflectivity is<br />

optimized will reduce the amount of polarization but the retardance will<br />

stay in general high.<br />

3. FORMALISM FOR ANALYZING FRINGE CONTRAST AND PHASE EFFECTS<br />

Sections 3.1 and 3.2 will summarize the part of the Jones calculus<br />

of interest for the current application. Section 3.3 will then derive<br />

the formalisms specific to astronomical interferometry.<br />

3.1 <strong>The</strong> Jones vector : J<br />

In Jones Calculus the state of polarized light is expressed by a<br />

vector J which has the form:<br />

J =<br />

Aqexp (iEq)<br />

where (p,q) are a set of predefined linear orthogonal coordinates, where<br />

Ap and Aq are the amplitudes of the electromagnetic waves, and where Ep<br />

and Eq are their phases (in radians) .<br />

TABLE II<br />

Jones Vectors for Assumed Incident Polarization States<br />

State Type: Ap Aq Ep Eq<br />

I Linear (0.=0) 1 0 0 0<br />

II Linear (0.=90) 0 1 0 0<br />

III Linear (0.=45) 1.5 1.5 0 0<br />

IV Linear (0.=-45) 1.5 -1.5 0 0<br />

V Right Circular 1.5 1.5 -rr/2 0<br />

VI Left Circular 1.5 1.5 rr/2 0<br />

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