Progress in Spectral-Spatial interferometry at
multi-THz frequencies - Potential applications
Peter Ade,
Amber Hornsby,
Enzo Pascale,
Rashmi Sudiwala
Roser Juanola-Parramon,
Nicola Baccichet,
Giorgio Savini∗
School of Physics and Astronomy
Cardiff Unviersity, Cardiff
Wales, UK
∗
Optical Science Laboraotory
Dept. of Physics and Astronomy
National University of Ireland Maynooth
University College London
Maynooth, Dublin
London, UK
Telephone: (800) 555–1212
Corresponding author. Email: g.savini@ucl.ac.uk
Fax: (888) 555–1212
Abstract—Spectral-spatial interferometry pioneered in a narrow band in the near infrared has not enjoyed much exploitation
as a technique. Proposed as a promising modulation method for
a potential Far-infrared future satellite, a period of study was
performed on two testbeds to improve and evolve this technique
in the laboratory in order to simplify some of the technical aspects
and the data analysis involved. Here we will present an update
on the successful upgrade of a previous wideband millimetric
(0.3-1.0 THz) testbed to a far-IR (11-14THz) one, as well as the
ongoing progress on a broadband setup for an imaging system
with a commercial thermal- or mid-IR (8 to 12 micron or 25-35
THz) camera currently working as imaging FTS. Source size,
coherence and technical issues are discussed.
I.
Colm Bracken,
Anthony Donohoe,
Anthony Murphy,
Credihe O’Sullivan
I NTRODUCTION
The first multi-Fourier transform experiments performed
by Mariotti and Ridgeway (MR88)[1] and Itoh and Ohtsuka
in similar fashion gave a glimpse of the possibilities that
Double-Fourier modulation (or spatial-spectral interferometry)
allow. MR88 focused on the application of this technique to
astronomy following in the pioneering footsteps of Michelson,
thus fuelling the interest in developing further concepts at
different wavelengths to improve angular resolution measurements while preserving wide band spectrophotometry.
modulation and spectral-spatial fringes in a laboratory environment [5].
Finally, in order to study other effects such as off-axis
corrections, imaging algorithms as well as the effect of the
thermal emission of the environment (critical for a spacebased mission) a third testbed was designed [6]. In the latter
(still in development phase) we aimed to study how variations
in the operational temperature of the optics affect the data
acquisition and the analysis as well as the added complexities
of an imaging system. To do this we elected to work in
the wavelength range where the peak of environment thermal
emission occurs and where large format detectors are relatively
”cheap” when compared to the sub-mm counterparts. The latter
testbed is in construction and has so far tested the phase
delay stage and detecting camera by working as an imaging
Fourier spectrometer while awaiting the final installation of a
large collimator to allow the re-assembly of the fore-optics to
resemble those of a spatial interferometer.
In the following section we will give a short description
of the latest work performed on both testbeds and how they
operate highlighting recent improvements while referring to
more details in previous respective works [5],[6].
The spectral spatial interferometry potential was immediately captured in the suggestion that this technique could be the
one of choice for the first Far-infrared interferometer in space
(SPIRIT [2] and FIRI-ESACDF [3] ). NASA [4] invested in
an optical scaled version of what the SPIRIT concept would
produce in order to reproduce the original experiment in a
fashion that would demonstrate intuitively through a simple
scaling the vast potential of this concept.
With the intention to reproduce the Mariotti and Ridgeway
experiment at longer wavelengths and to demonstrate and extend the feasibility of this technique to other frequency ranges
and broader frequency bands (and more importantly at those
frequencies which matter for the technology in question), a
first testbed in the Far Infrared (300GHz-1THz) was assembled
in a coordinated effort at Rutherford Appleton Laboratories.
Subsequently with the involvement of Cardiff University and
University College London, the testbed obtained its first double
Fig. 1. The Cardiff Far-infrared spectral-spatial testbed extends over 8m of
optical path (mostly collimated). The collimator is a 1m spherical segment and
the two telescopes are two pairs of off-axis parabolic mirrors which compress
the beam from the ∼ 7.5cm wide aperture to the 2.5 cm beam travelling on
the optical bench.
II.
T HE FAR -IR CRYOGENIC TESTBED
The basic layout of the Far-IR testbed originally assembled
with a wide-band mm-wave beam-combiner working from
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300µm to 3mm can be seen in fig.1 of [5] and can be seen rearranged in the basic same configuration in Fig.1 of this paper.
The wide-band mm-wave beam combiner and cryostat optics
have been replaced to work at much shorter wavelength in the
21-27 µm atmospheric band. This band is well represented by
the maximum envelope of all the spectra plotted in Fig.2.
users) is present slightly both in size, but it is also apparent
in amplitude since the fast spatial modulation generated by
the two slits does not cancel down to zero implying a slight
unbalance of the two sources.
Atmospheric lines in the same Fig.2 can be seen ”invading”
the band of interest. These lines are useful in this measurement
as they serve as a consistency test between spectral measurements and as effective calibrators.
Fig. 3. Cosine transform of each spectral bin is performed and plotted vs
(baseline/wavelength). The different colours represent the varying wavelength
bin used. The black thin line, a preliminary analysis best fit of all the combined
cosine transforms and corresponds to the Fourier Transform of a double slit
source both measuring 1mm in width and positioned at 6.5mm from each
other (inset sketch).
Fig. 2. The spatial modulation of the overall spectral source (thick black
envelope) can be seen as the two-telescope baseline increases. The coloured
modulated spectra (from violet, to blue, green, yellow, red show the same
spectra modulated by the spatial interference as the two telescopes are moved
apart. The atmospheric telluric lines are well apparent in the 20-25 micron
range (12-15 THz).
In the Double-Fourier set-up, two small co-aligned telescopes receive the incoming collimated beam from a common
source scene at the focus of the collimator (in this case a
1m segment of a spherical mirror). The source and collimator
act as a sky simulator transforming spatial structure at the
collimator’s focal plane into angles of arrival at the telescopes
which depend on a combination of focal plane scale of the
collimator and the angle which its optical axis forms with
the telescope axes. The latter will dictate the portion of
spatial fringe sampled by the system as the baseline between
telescopes varies.
The inputs from the two telescopes are combined after
one of them is phase delayed as in the case of a classical
Fourier transform spectrometer. The resulting FT sets of data
(for each baseline length) is shown in different colours in
Fig.2. The spectra is effectively modulated by the spatial
interference induced by the combination of telescope separation and angle of arrival of the source. This modulation is
faster as the sources separate. If the observer were viewing a
mono-chromatic source, he would observe the corresponding
delta-function oscillating in amplitude to reflect the spatial
interference pattern as the baseline separates.
This reflects the way in which one can crudely analyse the
data, by considering spectral bins where sufficient signal is
present and plotting the integrated signal vs cycles (baseline/λ)
and doing this for each wavelength will produce the set
of points in Fig.3. These were then overlaid with a first
approximate best fit FT of the spatial structure generating
the spectral-spatial modulation observed as the thick black
line. The nature of the approximation lies in the symmetry
of the slit-source which was fourier transformed. In reality
more care and complexity could have been considered in using
an-asymmetrical source. Such an asymmetry (known to the
Further progress will be sought by adopting a 3 slit source
on a rotating mount in order to simulate a 2D interferometer
and test other reconstruction issues which could be ignored
given the one dimensional nature of the baselines.
III.
T HE MID -IR IMAGING TESTBED
In the previous section the testbed described can be modified accordingly and through the substitution of a few optical
elements (beam-combiner and filters) to work in a number of
different ranges spanning from 3mm up to 20 µm. Whilst the
technology required for this experiment relies on substantial
and complex technology heritage, one major advantage is
retained which is the fact that a single pixel is employed
with a substantial collecting area at the focus of the system (a
smooth walled conical horn in this specific case). Furthermore
given the long wavelength, we are generally in the RayleighJeans portion of the spectrum and temperature variations of
the environment and the optics have little to no impact on the
final measurements.
Fig. 4. The thermal-IR testbed setup initially assembled as an imaging FTS
to verify the alignment and performance of the translation stage.
For this reason the UCL testbed was initially set up:
the addition of imaging capability as well as the spectral
range shift to a region most sensitive to the peak thermal
emission of the optics used. Lessons learned in this testbed
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will prove valuable in future studies on space-based instrument
requirements.
To verify the basic functionality of the testbed elements
(detector camera and moving stage) the testbed was initially
set up and aligned in an FTS configuration (Fig.4) where the
FTS stage can be seen on the left and the source is at the far
top right corner of the picture.
Fig. 6. Crude average FT of the pixels lying in one line coincident with the
printed electronic strip (black) compared to the normalized average FT of all
the interferograms of the pixels where a ZPD was detected above a threshold
of 5σ of the noise level of the IG acquired. A small but obvious shift can be
noted between the two thermal emission envelopes. No black-body fit has been
attempted due to the complex convolution of the camera specific sensitivity
as well as the camera lens specific transmission.
spherical collimator to be mounted at the edge of the optical
bench.
Fig. 5. Top: Setup of the weak thermal source (a heated printed electronics
circuit line) which acted as spatial structure for the thermal IR camera. Below
the picture of the electronic print is the Temperature data in rainbow colour
(25-45◦ C), below that the standard deviation of the timeline acquired as a
function of the optical delay stage (used as a proxy for the identification of
fringe visibility (arbitrary units), and at the bottom, the position of the ZPD
as a function of time for each of the pixels of the image. With the ZPD first
appearing at the far right of the image and travelling to the left end of the
strip.
The source used was a weak spatial thermal source obtained via Joule heating a single printed electronic strip (on a
polypropylene substrate),to a maximum of 45 degrees Celsius.
As the FTS was scanned the max recorded value was registered
as shown below the strip picture in Fig.5. A proxy of fringe
visibility for the spectrometer was taken by looking at the
standard deviation of the interferogram (after noting that
the average S/N ratio of the biggest IG signals was ∼30).
Additionally, the position of the ZPD for each scan was noted
and colour coded to verify how the ZPD would temporally
move across the image (typical of the case where the image
plane of the scene presented is not exactly orthogonal to the
optical axis of the spectrometer).
By placing a temperature threshold on the thermal image
the hottest (35-45◦ C) and warm (25-35◦ C) pixels were identified, Fourier transformed and co-added to create to spectra
which were then normalized and compared. A non-negligible
shift in the peak of this recovered thermal emission spectra
can be observed in Fig.6 and is expected. No attempt to fit
an actual black-body curve was performed due to the added
complexity of the camera spectral sensitivity as well as the lens
transmission in addition to this being beyond the scope of this
test. The IR testbed has now been re-assembled to employ
a single beam-combiner and two parallel output ports which
will impact on the lower portion of a large (81 cm) diameter
Fig. 7. The same testbed shown in Fig.4 is now modified to have two outgoing
beams which join at the beam combiner from two adjacent optical ports. The
collimator will be installed at the far end of the optical bench with a folded
path (given its size) maintained on a plane above the testbed.
IV.
D ISCUSSION
We have shown ongoing progress in the development of
the Cardiff Far-Infrared testbed which demonstrates further the
capability of adapting to a particular wavelength range of operation while maintaining the main opto-mechanical features.
There remain substantial complexities in the alignment of both
systems where qualitative measurements can be performed
trivially but which for precise quantitative analysis additional
metrology on most of their optical components is required. It
is also worth mentioning that the sources in question play a
significant role in the demonstration of such systems. The Farinfrared system relies on a bright Hg-arc lamp viewed through
machined slits of a size which given the magnification of the
system is tailored to view a few spatial fringes. The imaging
camera testbed on the other hand requires careful planning
of the source which if not magnified (as is the plan with the
collimator) and will require image-matching at pixel level to
preserve coherency which can be quite challenging given the
few-micron size of its pixels.
As is the case for classical interferometers, knowledge of
what is the desired physical scale to which the instrument
should be sensitive will help the user in designing the range of
baselines available. This reduces the practicality and uses of
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such a system compared to a direct imaging or a spectral system, but should be considered for more specific, high-angular
resolution applications, albeit possibly remaining confined to
either space applications due to the absence of atmosphericinduced coherence issues or near-field applications.
ACKNOWLEDGMENT
The research leading to these results has received funding
from the European Unions Seventh Framework Programme
(FP7/2007-2013) under FISICA grant agreement n 312818.
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