The VLT Interferometer - ESO
The VLT Interferometer - ESO
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 />
(1)