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Claims  |
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What is claimed is:
1. An in-line interferometric time integrating correlator comprising:
(a) a first reference signal acousto-optic (AO) cell together with a first
signal source for injecting a first reference signal therein at a first
terminal portion thereof and propagating through said AO cell in a first
direction;
(b) a second AO cell together with a second signal source at a second
terminal portion thereof, opposite said first terminal portion, for
injecting a second signal therein, to be correlated with said first
reference signal, and counter-propogating within said second AO cell with
respect to the direction of propagation of said first reference signal;
(c) a source of coherent light for directing a light beam along an optical
axis and intersecting the first AO cell for producing an undiffracted beam
emerging therefrom and a first plus one diffracted order beam exiting said
first AO cell;
(d) first imaging means for projecting the first plus one order diffracted
beam from the first AO cell upon the second AO cell along with said
undiffracted beam for producing second and third overlapping plus one
diffracted order beams exiting said second AO cell;
(e) a light integrating photodetector array means;
(f) a second imaging means for imaging the second and third overlapping
plus one diffracted order beams upon said photodetector array means,
enabling the resulting interference to be integrated by said photodetector
array means with respect to a user-defined integration time; and
(g) Dove prism means, positioned within said first imaging means, in the
path of said first plus one diffracted order beam, for causing the second
and third plus one diffracted order beams to overlap upon exiting the
second AO cell and scan in opposite directions at the photodetector array.
2. The correlator of claim 1 including a plano-cylindrical lens positioned
between said source of coherent light and said first AO cell for focusing
a collimated beam into a line at a central portion of said first AO cell.
3. The correlator of claim 1 including means for translating said Dove
prism in a direction transverse to said optical axis thereby to change the
angle of said overlap of said second and third plus one diffracted order
beams.
4. The correlator of claim 2 including means for translating said Dove
prism in a direction transverse to said optical axis thereby to change the
angle of said overlap of the second and third plus one diffracted order
beams.
5. The correlator of claim 1 including a spatial filter positioned within
said second imaging system for preventing undiffracted light from reaching
said photodetector array.
6. The correlator of claim 2 including a spatial filter positioned within
said second imaging system for preventing undiffracted light from reaching
said photodetector array.
7. The correlator of claim 3 including a spatial filter positioned within
said second imaging system for preventing undiffracted light from reaching
said photodetector array.
8. The correlator of claim 4 including a spatial filter positioned within
said second imaging system for preventing undiffracted light from reaching
said photodetector array.
9. An in-line interferometric time integrating correlator comprising:
(a) a first signal acousto-optic (AO) cell together with a first signal
source for injecting a first signal therein;
(b) a second AO cell together with a second signal source for injecting a
second signal therein, to be correlated with said first signal;
(c) a source of coherent light for directing a light beam along an optical
axis and intersecting the first AO cell for producing an undiffracted beam
emerging therefrom and a first plus one order diffracted beam exiting said
first AO cell;
(d) first imaging means for projecting the first plus one order diffracted
beam from the first AO cell upon the second AO cell along with said
undiffracted beam for producing second and third overlapping plus one
diffracted order beams exiting said second AO cell;
(e) a light integrating photodetector array means;
(f) a second imaging means for imaging the second and third overlapping
plus one diffracted first order beams upon said photodetector array means,
enabling the resulting interference to be integrated by said photodetector
array means with respect to a user-defined integration time; and
(g) Dove prism means, positioned in the path of said first plus one
diffracted order beam and co-acting with said first and second imaging
means, for causing the second and third plus one diffracted order beams to
overlap upon exiting the second AO cell and scan in opposite directions at
the photodetector array.
10. The correlator of claim 9 including a plano-cylindrical lens positioned
between said source of coherent light and said first AO cell for focusing
a collimated beam into a line at a central portion of said first AO cell.
11. The correlator of claim 9 including means for translating said Dove
prism in a direction transverse to said optical axis thereby to change the
angle of said overlap of said second and third plus one diffracted order
beams.
12. The correlator of claim 10 including means for translating said Dove
prism in a direction transverse to said optical axis thereby to change the
angle of said overlap of the second and third plus one diffracted order
beams.
13. The correlator of claim 9 including a spatial filter positioned within
said second imaging system for preventing undiffracted light from reaching
said photodetector array.
14. The correlator of claim 10 including a spatial filter positioned within
said second imaging system for preventing undiffracted light from reaching
said photodetector array.
15. The correlator of claim 11 including a spatial filter positioned within
said second imaging system for preventing undiffracted light from reaching
said photodetector array.
16. The correlator of claim 12 including a spatial filter positioned within
said second imaging system for preventing undiffracted light from reaching
said photodetector array.
17. An in-line interferometric time integrating correlator comprising:
a) a first signal acousto-optic (AO) cell together with a first RF signal
source for injecting a first RF signal therein;
(b) a second AO cell together with a second RF signal source for injecting
a second RF signal therein, to be correlated with said first RF signal;
(c) a source of coherent light for directing a coherent light beam at the
first AO cell for producing an undiffracted beam emerging therefrom and a
first plus one order diffracted beam exiting said first AO cell;
(d) first imaging means for projecting the first plus one order diffracted
beam from the first AO cell upon the second AO cell along with said
undiffracted beam for producing second and third overlapping plus one
diffracted order beams exiting said second AO cell;
(e) a light integrating photodetector array means;
(f) a second imaging means for imaging the second and third overlapping
plus one diffracted first order beams upon said photodetector array means,
enabling the resulting interference to be integrated by said photodetector
array means with respect to a user-defined integration time; and
g) Dove prism means, positioned in the path of said first plus one
diffracted order beam and co-acting with said first and second imaging
means, for causing the second and third plus one diffracted order beams to
overlap upon exiting the second AO cell and scan in opposite directions at
the photodetector array.
18. The correlator of claim 17 including a plano-cylindrical lens
positioned between said source of coherent light and said first AO cell
for focusing a collimated beam into a line at a central portion of said
first AO cell.
19. The correlator of claim 17 including means for translating said Dove
prism in a direction transverse to said optical axis thereby to change the
angle of said overlap of said second and third plus one diffracted order
beams.
20. The correlator of claim 18 including means for translating said Dove
prism in a direction transverse to said optical axis thereby to change the
angle of said overlap of the second and third plus one diffracted order
beams. |
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Claims  |
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Description  |
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BACKGROUND OF THE INVENTION
Spectrum analysis is a widely used signal processing technique for gaining
information about unknown signals. For programmability and accuracy,
digital processing techniques are preferred over analog methods. However
for real-time processing of large instantaneous bandwidth signals, analog
systems are required for the computationally intensive operations of
spectrum analysis. Acousto-optic (AO) based correlators or spectrum
correlators are considered to be attractive analog techniques because of
their parallel processing capability. Many forms of AO spectrum analyzers
have been developed for analog signal processing applications. The
different approaches include the AO power spectrum analyzer; the AO
in-line time integrating correlator; the interferometric AO spectrum
analyzer; and the cascaded AO interferometric architecture.
The major limitation of the power spectrum analyzer is a limited dynamic
range of 25-30 dB due to the squaring operation of the instantaneous
spectrum of the input waveform at the photodetector array. The in-line
time integrating correlator overcomes the dynamic range problems by using
a hetrodyne technique at the photodetector array by which provides an
output proportional to the magnitude spectrum of the input waveform. The
major disadvantage of the in-line correlator architecture is that the
spatial frequency of the correlation is fixed with respect to the center
frequency of the input signal. The pitch requirement for the photodetector
array limits the useful input signal bandwidth of the in-line
architecture. The interferometric AO spectrum analyzer uses a spatially
and temporally modulated reference beam for generating a fixed spatial
frequency at the detector plane while maintaining a high dynamic range for
spectrum analysis. The spatial frequency is set by varying the
recombination paths between the reference and unknown signal AO inputs in
the Mach-Zehnder architecture. The major limitation of this system is that
the reference and unknown signals follow widely varying paths in reaching
the detector. Thus, the system is extremely sensitive to vibration.
The cascaded interferometric AO architecture overcomes the vibration
limitations of the interferometric AO spectrum analyzer by cascading the
AO cells such that the reference and signal beam travel along a common
path. The interferometric properties of the system are obtained by using
two Bragg cells with different acoustic velocities or by interposing a
birefringent prism between the two AO cells. The major disadvantage of
this approach is the development and use of AO cells with different
acoustic velocities or the placement of a prism between the two closely
spaced AO cells.
BRIEF SUMMARY OF THE INVENTION
An in-line interferometric time integrating correlator is provided which
employs a Dove prism to ensure that the signals to be correlated are
counter-propagating in the correlation plane, and which provides a means
to control the spatial frequency at the detector array so that the spatial
frequency of the interferometric correlation can be matched to the spatial
frequency of the photodetector array elements.
BRIEF DESCRIPTION OF THE DRAWINGS
Other features and advantages of the present invention will become apparent
upon study of the following description taken in conjunction with the
drawings in which:
FIG. 1 illustrates a preferred embodiment of the invention;
FIG. 2 illustrates use of the Dove prism to cause linear shift of the
diffracted order and to invert the scan direction of the optical beam
after the focal point; and
FIGS. 3-5 illustrate waveforms useful in the further understanding of the
invention.
DETAILED DESCRIPTION OF EMBODIMENTS OF THE INVENTION
The features of the in-line, interferometric, time integrating correlator
are shown in FIG. 1. The apparatus is made up of a coherent light source
10, collimator 12, cylindrical lens 18, the reference signal AO cell 16,
dove prism 28, signal AO cell 30, and the photodetector array 44. Coherent
light source 10 accesses the delay window of the reference AO cell 16
which is oriented at the Bragg angle with respect to the light 14
propagated along optical axis 13. The time integrating correlator aspect
of the invention consists of imaging the plus one diffracted order 20 from
the reference cell 16 onto a second AO cell 30, which is driven by the
unknown RF signal 32. Signal AO cell 30 is oriented to satisfy the Bragg
condition for the undiffracted light 14 from the reference AO cell 16. The
imaging process between the two AO cells ensures that the plus one
diffractive order from reference cell 16 overlaps the plus one diffractive
order from the signal AO cell 30. These overlapped beams are then imaged
onto the photodetector array 44 where the resulting interference is
integrated with respect to time. If the unknown RF signal 32 correlates
with the reference RF signal 48, then the counter-propagating beams will
pass through each other at the same detector elements on array 44 during
each cycle of the RF signals. The detector elements in the array collect
light for a user defined integration time, during which the consecutive
cycling of the correlated RF signals build up light intensity at the array
locations where the beams repeatedly overlap each other. If the signals do
not correlate with one other, then they will not repeatedly overlap at the
same location on array 44 during the integration time, and the detector
array will not register increased light intensity at any location without
correlation.
Because the photodetector array's element-to-element spacing limits the
resolution, the RF signal correlation needs to be imposed on a stationary
pattern of interference fringes called a spatial carrier. The interference
fringes are created by the constructive and destructive interference of
the two plane waves of light from diffracted beams 20 and 34. The spatial
separation of the interference fringes, which is a function of the angular
separation of the two beams, must be at least twice the detector element
spacing of array 44 to ensure that the fringes are resolvable.
Note that the two AO cell light beam deflector signals are
counter-propagating due to the RF reference signal input 48 being on the
lower portion of reference AO cell 16 and the unknown signal input 32
being on the upper portion of the signal AO cell 30. A first 1:1 imaging
lens system 22 comprising lenses 24 and 26, images the aperture of the
reference AO cell 16 into AO cell 30 driven by the unknown signal. The
first 1:1 imaging system inverts the scan direction of the scanning spot
from the first AO cell 16, effectively negating the counter-propogating
layout of the two AO cells 16 and 32. However, within this first imaging
system, Dove prism 28, placed in the beam path of the plus one diffracted
order, performs two critical functions: it inverts the scan direction of
beam 20 and provides an angular shift of the same beam.
Dove prism 28 inverts the scan direction of the scanning spot from the
first AO cell 16. This function, which is a unique aspect of the present
invention, is necessary in order for the scanning spots from the two AO
cells to counter-propagate at the photodetector array 44. The scan
directions of these two beams must be opposite to one another at the
photodetector array 44 in order to mathematically perform the correlation
operation. If the propagation of each scan is in the same direction, then
all array elements 44 will effectively see the same light intensity which
indicates no correlation. The Dove prism 28 inverts the scan direction of
beam 20 upon reflection at the lower face of the prism as shown in FIG. 2.
This reflection effectively inverts the image inversion about the focal
point of beam 20, also as shown in FIG. 2. The DC beam 14 satisfies the
Bragg condition for the second AO cell 30. A second lens system comprising
lenses 31 and 33, images the plus one diffracted orders from the first and
second AO cells upon the photodetector array 44 which could be part of a
line scan camera. Spatial filter 42 blocks the undiffracted light. Thus
with the Dove prism in the optical system, beams 20 and 34 scan in
opposite directions at the photodetector array 44, which mathematically
performs the correlation operation.
The second function of the Dove prism 28 is to cause a spatial displacement
in the aforesaid y direction of the plus one diffracted order 20 of the
first AO cell without affecting the undiffracted order 14. This
displacement causes the diffracted order 20 to recombine with the plus one
diffracted order 34 at the second AO cell at a slight angular displacement
at the photodetector 44. The angular displacement caused by the Dove prism
produces linear interference fringes at the photodetector in the same
manner as interference fringes are caused by the angular recombination of
two coherent plane waves of light. The spatial frequency of the fringes
will vary by changing the angular displacement of the two light sources
(diffracted orders). The spacing of these fringes can be optimized for the
photodetector spacing (optimum sampling of the correlation) by varying the
recombination angle of beam 20. The spatial frequency of these fringes can
be tuned by translating the prism by means of drive mechanism 21 in a
direction transverse to the optical axis 13, thereby changing the
recombination angle of the plus one orders at the photodetector. The
correlation is formed as the photodetectors integrate the
counter-propogating scanning spots over time.
A combination of three mirrors placed in the path of the plus one
diffracted order can theoretically perform the same scan direction
inversion performed by the Dove prism without changing the direction of
the beam as it exits the mirror arrangement. Additionally, an optical
wedge inserted in the plus one diffracted order 20 could produce angular
displacement. The great advantage of the Dove prism over this approach is
the simplicity of providing both functions in one device. Also, mirrors
tend to be vibrationally sensitive which reduces the inherent stability
advantages of the interferometric design.
Our novel design demonstrates improved vibrational stability, system light
efficiency, and dynamic range over a dual-path interferometric correlator.
The resulting tunable spatial frequency represents an advantage over the
in-line interferometric correlator. We designed and built an optical
system to demonstrate the invention. Coherent light source 10 was a ten
mWatt HeNe laser at 632.8 nm which was spatially filtered and collimated
to 20 mm diameter by beamforming optics 12. A 300 mm plano-cylindrical
lens 18 focused the light into AO cell 16 to improve system diffraction
efficiency. AO cells 16 and 30, manufactured by the IntraAction
Corporation, have a 40 MHz center frequency, a 20 MHz 3 dB bandwidth, a 22
mm spatial aperture, and a five microsecond time aperture. The first 1:1
imaging system consisted of two plano-convex lenses of 300 mm focal
length. The first lens 24 has a two inch diameter, and the second lens 26
has a three inch diameter. The DC light 14 and plus one diffractive order
20, generated by reference RF signal 48 on a 40 MHz RF carrier, are
focussed into two vertical lines at the focal plane of the first imaging
lens 24. At this point, the plus one order 20 passes through Dove prism
28, mounted on translation drive stage 21. The prism base is 0.7 inches in
length with a height of 0.5 inches.
Since the Dove prism 28 is placed in the focal plane of imaging lens 26,
the spatial displacement induced by the prism results in an angular
displacement of the plus one order 20 when it is imaged into the signal AO
cell 30. Cell 30 is oriented so as to satisfy the Bragg condition for the
incident DC light 14. The RF input into the signal AO cell 30 on a 40 MHz
RF carrier produces plus one diffracted order 34 which propogates at a
slight angle to the diffracted order 20 from the reference AO cell 16. The
undiffracted light from the signal AO cell 30 is blocked by spatial filter
42 at the focal point of the imaging system 36.
Plano-cylindrical lens 18 performs several useful functions. It focuses the
collimated beam 14 into a horizontally compresses line at the center of
the AO cell 16, thereby improving system diffraction efficiency. As shown
in FIG. 1, lens 18 essentially maintains collimation of beam 14
perpendicular to the optical axis as indicated by arrow labelled y, but
focuses this beam in the horizontal x direction extending into the plane
of the paper, as indicated by the symbol x, thus producing a vertical line
in the y direction at the focal plane of lens 24, intersecting the Dove
prism. This facilitates the passage of beam 20 through the Dove prism,
which is a fairly small optical element. Similarly, beams 14, 20 and 34
focus to a vertical line at the focal plane of lens 37, which facilitates
separating beam 14 from 20 and 34 and blocking this beam with the spatial
filter 42. Finally, the net effect of lens 18 and the two imaging systems
is to image the horizontally compressed beam within AO cell 16 onto the
photodetector array 44.
The second 1:1 imaging system 36, consisting of two 2" inch diameter
plano-convex lenses 31 and 33 of 150 mm focal length, images the two
diffracted beams onto the photodetector array 44. The plano-cylindrical
lens 18 causes the light to focus into a horizontal line at the detector
plane. Array 44 was an EG&G Reticon LC1901 modular line scan camera with
512 pixels, 26 micrometer pitch. The camera was interfaced to a PC via a
Reticon RS 1910 camera controller and a Girard 3197 8-bit interface board.
As an initial test signal, we mixed a one MHz sinusoidal modulation with a
40 MHz suppressed carrier. This test signal was used as an input to both
AO cells. We expected the autocorrelation to be a 2 MHz modulation (the
beat frequency between 39 and 41 MHz sidelobes of the amplitude
modulation) of the interferometrically produced spatial frequency. The
resulting autocorrelation produced by the linescan camera output is shown
in FIG. 3. This data agrees with the expected result. As can be seen there
are about eleven repetitions over a five microsecond window which
corresponds to two MHz (11 cycles/5.5 microseconds). The sinusoidal
modulation was decreased to 500 KHz. Therefore we expected a one MHz
modulation of the spatial carrier. The optically computed autocorrelation,
shown in FIG. 4, agrees with the expected result.
The third test signal used was a one microsecond rectangular pulse
modulation at a five microsecond pulse repetition, of a 40 MHz suppressed
carrier. We expect the autocorrelation of a one microsecond RECT function
to be a TRI function of total width 2 microseconds. The optically computed
autocorrelation of this signal, which agrees with the expected result, is
shown in FIG. 5.
Other embodiments of the invention will become readily apparent to the
skilled workers in the art, and thus the scope of the invention is to be
limited solely by the terms of the following claims and art recognized
equivalents thereof.
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Description  |
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