Method and apparatus for simultaneous observation of three-degrees of vibrational freedom using single heterodyne beam

Abstract

A laboratory system has demonstrated the measurement of three degrees of vibrational freedom simultaneously using a single beam through heterodyne speckle imaging. The random interference pattern generated by the illumination of a rough surface with coherent light can be exploited to extract information about the surface motion. The optical speckle pattern is heterodyne mixed with a coherent reference. The recorded optical data is then processed to extract three dimensions of surface motion. Axial velocity is measured by demodulating the received time-varying intensity of high amplitude pixels. Tilt, a gradient of surface velocity, is calculated by measuring speckle translation following reconstruction of the speckle pattern from the mixed signal.

Claims

1. A heterodyne speckle imaging sensor system, comprising: a laser source emitting a linearly polarized laser; a first beam splitter to divide the linearly polarized laser from the laser source into a probe beam along a probe path and a reference beam along a reference path; a bi-convex probe lens in the probe path to provide focus adjustment for the probe beam; a first mirror in the probe path to reflect the probe beam as a redirected probe beam; a scattering source having a diffuse surface to scatter the redirected probe beam as a scattered radiation; bi-convex collecting lens to collect a portion of the scattered radiation as a collected radiation; a second mirror for redirecting the collected radiation as a propagated beam; plano-convex defocusing lens to defocus a field of the propagated beam; a third mirror to redirect the resulting defocused propagated beam; a polarizing filter to absorb horizontally polarized components of said propagating beam as a probe electric field towards an image plane; an arrangement of acousto-optic modulators to effect frequency offset of the electromagnetic field associated with the reference beam to result in a frequency offset reference beam; a reference mirror to redirect said frequency offset reference beam; a plano-convex reference lens to focus said redirected frequency offset reference beam as a focused reference beam; a reference spatial filter to spatial filter said focused reference beam to result in a diverging beam; a plano-convex collimating lens to collimate said diverging beam as a collimated reference beam; another polarizing filter to absorb horizontally polarized components of said collimated reference beam as a reference electric field towards said image plane; a second beam splitter to additively combine the probe and reference electric fields towards said image plane; and a focal plane array disposed along said image plane, wherein said probe and reference electric fields as additively combined are sensed by said focal plane array for detection of changes in the random scattered radiation.

2. The heterodyne speckle imaging sensor system recited in claim 1, wherein said arrangement of acousto-optic modulators is comprised of: a first acousto-optic modulator to upshift a frequency of the electromagnetic field associated with the reference beam; and a second acousto-optic modulator to effect downshift to the upshifted frequency of the electromagnetic field associated with the reference beam by an amount less than the upshift to result in said frequency offset reference beam.

3. The heterodyne speckle imaging sensor system recited in claim 1, wherein said focal plane array is a 6464 pixel detector.

4. The heterodyne speckle imaging sensor system recited in claim 1, further comprising: a trans impedance amplifier to convert charge from the focal plane array into a digital representation of irradiance as a detection output; and a signal processor to receive said detection output and compute random changes in the scattered radiation for display output.

5. The heterodyne speckle imaging sensor system recited in claim 1, wherein the focal plane array transduces irradiance of said probe and reference electric fields into an electrical charge proportional to the irradiance as a measurable magnitude of heterodyne irradiance.

6. The heterodyne speckle imaging sensor system recited in claim 5, wherein the magnitude of heterodyne irradiance shifts spatially in direct proportion to a surface tilt of the dynamic scattering source.

7. A method for simultaneous observation of three-degrees of vibrational freedom based on a heterodyne speckle imaging sensor system, said method comprising the steps of: emitting a linearly polarized laser from a laser source; dividing by a first beam splitter the linearly polarized laser from the laser source into a probe beam and a reference beam; providing focus adjustment for the probe beam through a first lens; redirecting the probe beam by a first mirror towards an object dynamically disposed with respect to an object plane; scattering as a scattered radiation the redirected probe beam from a diffuse surface of the dynamic object moving in reference to the object plane, whereby an electric field resulting from the scattered radiation has a random spatial phase and amplitude; collecting a portion of the resulting scattered radiation through a collecting lens; redirecting the collected portion of the resulting scattered radiation using a second mirror; propagating the redirected collected portion as a propagated beam through a secondary optic which defocuses the resulting propagated beam relative to an image plane; redirecting the defocused propagated beam using an additional mirror through a dichroic polarizing probe filter where a horizontally polarized radiation is absorbed, resulting in a polarizer filtered beam; splitting the polarizer filtered beam using a second beam splitter, wherein a split portion of a radiation of the polarizer filtered beam is reflected from a first surface of the second beam splitter as a reflected filtered probe beam towards a focal plane array disposed along said image plane; following initial propagation through the first beam splitter, effecting frequency offset of the reference beam to result in a frequency offset reference beam; redirecting said frequency offset reference beam using a reference beam mirror to propagate toward and focus through a reference beam focusing lens to result in a focused reference beam; spatial filtering said focused reference beam using an aperture disposed at a focal point, resulting in a diverging beam; collimating the diverging beam using a collimating lens; filtering said collimated beam using a dichroic polarizing reference filter where a horizontally polarized radiation is absorbed and a filtered reference beam is transmitted; and directing the filtered reference beam towards a second surface of the second beam splitter, wherein a transmit portion of a radiation of the filtered reference beam is transmitted out the first surface of the second beam splitter as a transmitted filtered reference beam towards said focal plane array disposed along said image plane, whereby said reflected filtered probe beam and said transmitted filtered reference beam as additively combined allow focal plane array detection of changes in the random scattered radiation.

8. The method for simultaneous observation of three-degrees of vibrational freedom as recited in claim 7, wherein about half of a radiation of the polarizer filtered beam propagates through the first surface of the second splitter and a remaining portion of a radiation of the polarizer filtered beam is reflected from the first surface as the reflected filtered probe beam.

9. The method for simultaneous observation of three-degrees of vibrational freedom as recited in claim 7, wherein said effecting frequency offset of the reference beam is comprised of the steps of: upshifting a frequency of the electromagnetic field associated with the reference beam using a first acousto-optic modulator; and downshifting the upshifted frequency of the electromagnetic field associated with the reference beam using a second acousto-optic modulator by an amount less than the upshift to result in the frequency offset reference beam.

10. The method for simultaneous observation of three-degrees of vibrational freedom as recited in claim 7, wherein tilting and translating of said moving object imparts a phase shift due to an optical path change near the object plane, whereby a spatial shift corresponds to tilting of the diffuse surface of the dynamic object moving while the phase corresponds to an axial motion of the diffuse surface of the dynamic object moving.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) Additional advantages and features will become apparent as the subject invention becomes better understood by reference to the following detailed description when considered in conjunction with the accompanying drawings wherein:

(2) FIG. 1 shows an exemplary incident beam and moving surface geometry used to describe the three-dimensional vibration sensing method.

(3) FIG. 2 shows an exemplary heterodyne speckle imaging sensor system with a dynamic diffuse-scatterer for the target.

(4) FIG. 3 shows an exemplary method for simultaneous observation of three-degrees of vibrational freedom using a heterodyne beam, e.g., of a heterodyne speckle imaging sensor system shown in FIG. 2.

(5) FIG. 4 shows an exemplary process for signal processing a sensor observation of three-degrees of vibrational freedom using a heterodyne beam as exemplified in FIG. 3.

DETAILED DESCRIPTION

(6) Before entering into the detailed description of one embodiment of the present invention according to the accompanying Figures, the theory of the present invention will be explained hereinafter.

(7) FIG. 1 shows an exemplary incident beam and moving surface geometry 100 used to describe the three-dimensional vibration sensing method. The object plane, z=0, is allowed to rotate about a pivot {.sub.0,,0} and translate along the z-axis. An incident electromagnetic beam contacts {.sub.P,0,0} at angle before tilting. As the object plane rotates by angle , the incident electromagnetic beam impinges on a new spatial location, located distance d.sub.1 away along the axis of the beam. The image plane is located a sufficient distance from the object plane to be considered in the far field.

(8) The variation in path length P due to tilt and translation is a combination of the incoming and outgoing light. The incoming light is assumed to be coherent and planar at an angle relative to the surface plane. The image plane is assumed to be sufficiently far such that outgoing light is orthogonal to the surface plane. The path variation is geometrically determined,
P=d.sub.1+d.sub.2d.sub.3d.sub.4
P=(.sub.0)[sin()(1cos())+(1+cos())sin()]d.sub.4(1+cos())
where is angular change due to the tilting surface to which a small angle assumption is applied sin(),

(9) $\cos \left(\right)1-\frac{{}^2}{2},$
and .sup.2<<. This assumption leads to a simplified path length.
P(.sub.0)(1+cos())d.sub.4(1+cos())

(10) In the description below the direction of illumination, and hence the Doppler velocity, are assumed to be aligned with the z-axis, =0.
P(.sub.0)2 sin()2d.sub.4
If we maintained the cos() term through the subsequent equations, the velocity would be measured along an axis that is acute with the plane. This increases the utility of the method to horizontal translation as well as pistoning.

DETAILED DESCRIPTION OF THE INVENTION

(11) An exemplary heterodyne speckle imaging system is represented in FIG. 2. Such an exemplary heterodyne speckle imaging sensor system 200 is shown comprising a laser source 201; a beam splitter 202; 750 mm bi-convex lens 203; a first mirror 204; a dynamic diffuse scatterer 205; 500 mm bi-convex lens 206; a second mirror 207; 250 mm plano-convex lens 208; a third mirror 209; a polarizing filter 210; a first acousto-optic modulator AOM1 211, 80.01 MHz upshift; a second acousto-optic modulator AOM2 (212), 80 MHz downshift; a fourth mirror 213; 50 mm plano-convex lens 214; 50 m diameter spatial filter 215; 250 mm plano-convex lens 216; another polarizing filter 217; another beam splitter 218; 6464 pixel detector 219; a trans impedance amplifier 220 sampling at 30 kHz; and a signal processor and data display 221.

(12) FIG. 3 shows an exemplary method for simultaneous observation of three-degrees of vibrational freedom 300 using a heterodyne beam, e.g., of a heterodyne speckle imaging sensor system shown in FIG. 2. Referring now to FIGS. 2 and 3, the source 201 is a linearly polarized laser 301. A splitter 202 divides the source into a probe and reference beams 302. In the probe beam path, a single lens provides focus adjustment for 303 the beam 203 and mirror 204 redirects the beam to a dynamic object 205; the object has a diffuse surface. The electric field scatters 305 from the moving object 205 and now has a random spatial phase or amplitude. The purpose of the invention is to determine changes to the surface's position by tracking changes in the random, scattered electric field. As the object is tilted and translated, a phase shift is imparted due to the optical path change near the object plane 205. Thus, the optical field at the object is modified by a phase associated with the new position of the object.

(13) $\begin{array}{cc}{u}_O\left(,\right).fwdarw.u_O\left(,\right){}^{\frac{\mathrm{j2}P}{}}& \left(1\right)\end{array}$
Where is the optical wavelength.

(14) Some of the resulting scattered radiation is collected 306 by a single lens 206. The radiation is redirected 307 using a mirror 207 and propagates through a secondary optic 208 which defocuses 308 the field relative to the image plane 219. An additional mirror 209 redirects the beam 309 through a dichroic polarizing filter 210 where the horizontally polarized radiation is absorbed 310. The radiation from the probe beam propagates to a second beam splitter 218 where half the radiation propagates through the splitter and half is redirected towards the focal plane array 219. The probe-leg electric field at the image plane 219 can be described as U.sub.P(x,y,t.sub.1), at one time, and U.sub.P(x,y,t.sub.2) at a later time. Where U.sub.P(x,y,t.sub.2) is a phase modified version of U.sub.P(x,y,t.sub.1), the field at a previous frame. The relationship between the these fields is

(15) $\begin{array}{cc}{U}_p\left(x,y,t_2\right)={}^{\frac{\mathrm{j4}\left({}_O+d_4\right)}{}}{}^{-\mathrm{j2}\mathrm{kx}}{}^{j2\mathrm{kz}{}^2}{U}_p\left(x-2z,y-2z,t_1\right)& \left(2\right)\end{array}$
Where k is the optical wavenumber. The invention makes use of this shifted and phase modified version of the original field to determine the object's motion; the spatial shift corresponds to tilting of the surface 205 while the phase corresponds to the axial motion of the surface 205.

(16) Following initial propagation through the beam splitter 202, the reference beam propagates through two acousto-optic modulators AOM1 (211) and AOM2 (212). AOM1 211 upshifts the frequency of the electromagnetic field 311 by a specified amount AOM2 212 downshift the frequency 312 by an amount less than the upshift producing a modest frequency offset of the reference field. A mirror 213 redirects the reference beam 313 where it propagates through a focusing lens 214 to focus the beam 314. An aperture 215 is placed at the focal point of 214, acting as a spatial filter to spatial filter the beam 315. The diverging beam propagates to another lens 216 which collimates the expanded beam 316. The resulting electromagnetic radiation propagates through a dichroic polarizing filter 217 where the horizontally polarized radiation is absorbed 317. The reference field propagates to the beam splitter 218 where half the radiation transmits through the splitter.

(17) The device uses the same propagation distance, the distance between splitter mirror 202 and beam splitter 218, on both probe and reference fields. The beam splitter 218 additively combines the probe and reference electric fields 318 in the region between splitter 218 and the focal plane array 219. The total field U.sub.t at the image plane is the superposition of the probe and reference fields.
U.sub.t(x,y,t)=U.sub.r(x,y,t)+U.sub.p(x,y,t)(3)
The focal plane array 219 transduces the irradiance of these two fields 319 into an electrical charge proportional to the irradiance.
I(x,y,t)=U.sub.tU.sub.t*=U.sub.rU.sub.r*+U.sub.mU.sub.m*+U.sub.rU.sub.m*+U.sub.r*U.sub.m(4)

(18) $\begin{array}{cc}I\left(x,y,t\right)=\frac{1}{{}^2{z}^2}[R^2+{.Math.P.Math.}^2+2R.Math.P.Math.\cos \left({}_{\mathrm{LO}}t+\frac{4}{}\left(\left(t\right){}_0+\left(t\right){}_0+d_4\left(t\right)\right)-{}_p\right]& \left(5\right)\end{array}$
Where R and |P| are the magnitudes of the reference and probe field respectively. The combined irradiance is the sum of three terms: 1) irradiance of the reference R.sup.2, 2) irradiance of the probe |P|.sup.2 and 3) the mix term R|P|.

(19) The system relies on a heterodyne component where the reference field strength amplifies the probe field. This is possible since the reference field is frequency shifted at a frequency equal to .sub.LO, the difference frequency of AOM1 211 and AOM2 212. The magnitude 2R|P| of the heterodyne irradiance shifts spatially in direct proportion to the surface tilt 205. The phase terms associated with cos(.sub.LOt+) contain sufficient information to compute the z-axis velocity of the surface. This phase term modulates the local oscillator frequency, .sub.LO. The phase is

(20) $\begin{array}{cc}\left(t\right)=\frac{4}{}\left(\left(t\right){}_O+\left(t\right){}_O+d_4\left(t\right)\right)-{}_p& \left(6\right)\end{array}$
where the term containing d.sub.4 is the Doppler shift due to translation of the object in the z dimension. The terms containing and are Doppler shift due to the tilting motion. It occurs in this expression because the pivots do not intersect the origin and the illumination is assumed to be centered at the origin. In other words, this term represents motion in the z direction based on the amount of tilt and the relative distance between the pivot point and the center of illumination. The two terms just described do not depend on spatial position on the image plane. In contrast .sub.p(x,y) is the phase of the probe speckle pattern and will shift in a manner similar to the magnitude of the speckle pattern.

(21) A trans-impedance amplifier circuit 220 converts charge from the focal plane array 219 into a digital representation 320 of the irradiance on a computer 221. The acquisition is repeated sequentially in time at a frame rate sufficient to observe the intermediate carrier frequency resulting from the upshift and downshift from the acousto-optic modulators 211 and 212. The focal plane array also has sufficient pixels to observe speckles caused by light reflected from a diffuse target.

(22) The sequence of image frames captured on the computer 221 undergoes a process on the same computer 321 to calculate tilt in the x and y directions, and respectively, as well as axial velocity in the z direction. The process is outlined in FIG. 4, with two process sequences.

(23) FIG. 4 shows an exemplary process 400 for signal processing a sensor observation of three-degrees of vibrational freedom using a heterodyne beam. The process to produce two dimensions of tilt is based on sequential estimates of the probe leg's speckle pattern amplitude. First, the image data stored on the computer 221 is accessed 401. The heterodyne signal is isolated from the complete measurement by high-pass filtering 402 each pixel independently. This filter removes R.sup.2 and |P|.sup.2 from the camera's representation of the optical field, equation 5. The filter 402 outputs the heterodyne information at the local oscillator frequency .sub.LO. A temporal Hilbert transform 403 extracts the envelope 2R|P| at each pixel. The output of 403 is a speckle pattern that shifts spatially for each subsequent frame. Each frame is cross-correlated 404 with its prior time frame producing a sequence of new data frames each containing a spatial peak. A peak's position relative to center of the frame corresponds to the number of pixels shifted between two image frames. A peak's location is estimated using a two dimensional parabolic spatial fit 405 on a cross correlation frame. In this way the peak location can capture sub-pixel shifts in the image pairs and consequently small amplitudes of tilt. The output of the parabolic fit 405 is a temporal sequence of peak locations applied in two dimensions, in other words, two temporal sequences of spatial shifts s.sub.x and s.sub.y between subsequent image frames. The spatial shifts are converted 406 to units of object tilt difference and between subsequent image frames,
=s.sub.x/2z(7a)
=s.sub.y/2z.(7b)
The tilt can then be displayed as two time sequences on a data display device 407.

(24) A parallel sequence of the processing is used to calculate z-axis velocity. This demodulation process uses a standard arctangent demodulation for Doppler shifted heterodyne signals applied to each pixel. (See, e.g., B. K. Park, O. Boric-Lubecke, and V. M. Lubecke, Arctangent demodulation with DC offset compensation in quadrature Doppler radar receiver systems, IEEE Trans. Microw. Theory Tech., vol. 55, no. 5, pp. 1073-1079, May 2007, incorporated herein by reference.) The output of filter 402 provides the heterodyne information at the local oscillator frequency .sub.LO necessary to begin the demodulation. In-phase and quadrature 408 are calculated by multiplying each pixel by the sine and cosine of the local oscillator frequency .sub.LO. The resulting in-phase I.sub.demod and quadrature Q.sub.demod time sequences are low pass filtered 409 to remove unwanted components at frequencies greater than .sub.LO.
Q.sub.demod(t)=LP[HP[I(t)] sin(.sub.LOt)](8)
I.sub.demod(t)=LP[HP[I(t)] cos(.sub.LOt)](9)
The in-phase and quadrature terms are then processed in block 410 that contains mathematical equation 10 and produces an estimate of the Doppler phase at each pixel

(25) $\begin{array}{cc}\mathrm{unwrap}\left[{\tan }^{-1}\left(\frac{Q_{\mathrm{demod}}\left(t\right)}{I_{\mathrm{demod}}\left(t\right)}\right)\right].& \left(10\right)\end{array}$
The velocity for each pixel is then estimated 411 using the Doppler phase.

(26) $\begin{array}{cc}v=\frac{}{4}\left(\frac{{}_2-{}_1}{t_2-t_1}\right).& \left(11\right)\end{array}$
The optical component 208 produces defocused images, as a result, estimates of velocity at each pixel should be equal. However, destructive interference from the diffuse scattering source 205 produces some low amplitude field strengths from the probe that are not accurately captured with the camera 219 and 220. The velocity estimates associated with low amplitude pixels will not produce accurate estimates of velocity. Process step 412 removes low signal strength pixels. The remaining pixels are averaged 413 to reduce noise. The output is displayed 414 as a single velocity time series representing axial velocity in the z direction.

(27) It is obvious that many modifications and variations of the present invention are possible in light of the above teachings. It is therefore to be understood that within the scope of the appended claims, the invention may be practiced otherwise than as described.