Patent Document

FIELD OF THE INVENTION  
       [0001]     The present invention is related to a system for optical coherence tomographic imaging of turbid (i.e., scattering) materials utilizing multiple channels of information. The multiple channels of information may be comprised and encompass spatial, angle, spectral and polarization domains. More specifically, the present invention is related to methods and apparatus utilizing optical sources, systems or receivers capable of providing (source), processing (system) or recording (receiver) a multiplicity of channels of spectral information for optical coherence tomographic imaging of turbid materials. In these methods and apparatus the multiplicity of channels of spectral information that can be provided by the source, processed by the system, or recorded by the receiver are used to convey simultaneously spatial, spectral or polarimetric information relating to the turbid material being imaged tomographically.  
         [0002]     The multichannel optical coherence tomographic methods can be incorporated into an endoscopic probe for imaging a patient. The endoscope comprises an optical fiber array and can comprise a plurality of optical fibers adapted to be disposed in the patient. The optical fiber array transmits the light from the light source into the patient, and transmits the light reflected by the patient out of the patient. The plurality of optical fibers in the array are in optical communication with the light source. The multichannel optical coherence tomography system comprises a detector for receiving the light from the array and analyzing the light. The methods and apparatus may be applied for imaging a vessel, biliary, GU and/or GI tract of a patient.  
       BACKGROUND OF THE INVENTION  
       [0003]     Myocardial infarction or heart attack remains the leading cause of death in our society. Unfortunately, most of us can identify a family member or close friend that has suffered from a myocardial infarction. Until recently many investigators believed that coronary arteries critically blocked with atherosclerotic plaque that subsequently progressed to total occlusion was the primary mechanism for myocardial infarction. Recent evidence from many investigational studies, however, clearly indicate that most infarctions are due to sudden rupture of non-critically stenosed coronary arteries due to sudden plaque rupture. For example, Little and coworkers (Little, W C, Downes, T R, Applegate, R J. The underlying coronary lesion in myocardial infarction: implications for coronary angiography.  Clin Cardiol  1991; 14: 868-874, incorporated by reference herein) observed that approximately 70% of patients suffering from an acute plaque rupture were initiated on plaques that were less than 50% occluded as revealed by previous coronary angiography. This and similar observations have been confirmed by other investigators (Nissen, S. Coronary angiography and intravascular ultrasound.  Am J Cardiol  2001; 87 (suppl): 15A -20A, incorporated by reference herein).  
         [0004]     The development of technologies to identify these unstable plaques holds the potential to decrease substantially the incidence of acute coronary syndromes that often lead to premature death. Unfortunately, no methods are currently available to the cardiologist that may be applied to specify which coronary plaques are vulnerable and thus prone to rupture. Although treadmill testing has been used for decades to identify patients at greater cardiovascular risk, this approach does not have the specificity to differentiate between stable and vulnerable plaques that are prone to rupture and frequently result in myocardial infarction. Inasmuch as a great deal of information exists regarding the pathology of unstable plaques (determined at autopsy) technologies based upon identifying the well described pathologic appearance of the vulnerable plaque offers a promising long term strategy to solve this problem.  
         [0005]     The unstable plaque was first identified and characterized by pathologists in the early 1980&#39;s. Davis and coworkers noted that with the reconstruction of serial histological sections in patients with acute myocardial infarctions associated with death, a rupture or fissuring of atheromatous plaque was evident (Davis M J, Thomas A C. Plaque fissuring: the cause of acute myocardial infarction, sudden death, and crescendo angina.  Br Heart J  1985; 53: 363-373, incorporated by reference herein). Ulcerated plaques were further characterized as having a thin fibrous cap, increased macrophages with decreased smooth muscle cells and an increased lipid core when compared to non-ulcerated atherosclerotic plaques in human aortas (Davis M J, Richardson P D, Woolf N, Katz D R, Mann J. Risk of thrombosis in human atherosclerotic plaques: role of extracellular lipid, macrophage, and smooth muscle cell content, incorporated by reference herein). Furthermore, no correlation in size of lipid pool and percent stenosis was observed when imaging by coronary angiography. In fact, most cardiologists agree that unstable plaques progress to more stenotic yet stable plaques through progression via rupture with the formation of a mural thrombus and plaque remodeling, but without complete luminal occlusion (Topol E J, Rabbaic R. Strategies to achieve coronary arterial plaque stabilization.  Cardiovasc Res  1999; 41: 402-417, incorporated by reference herein). Neo-vascularization with intra-plaque hemorrhage may also play a role in this progression from small lesions (&lt;50% occluded) to larger significant plaques. Yet, if the unique features of unstable plaque could be recognized by the cardiologist and then stabilized, a dramatic decrease may be realized in both acute myocardial infarction and unstable angina syndromes, and in the sudden progression of coronary artery disease.  
         [0006]     The present invention uses depth-resolved light reflection or Optical Coherence Tomography (OCT) to identify the pathological features that have been identified in the vulnerable plaque. In OCT, light from a broad band light source or tunable laser source is input into an interferometer with a portion of light directed to the vessel wall and the other portion directed to a reference surface. The distal end of the optical fiber is interfaced with a catheter for interrogation of the coronary artery during a heart catheterization procedure. The reflected light from the plaque is recombined with the signal from the reference surface forming interference fringes (measured by an photovoltaic detector) allowing precise depth-resolved imaging of the plaque on a micron scale.  
         [0007]     OCT uses narrow linewidth tunable laser source or a superluminescent diode source emitting light over a broad bandwidth (distribution of wave length) to make in situ tomographic images with axial resolution of 10-20 μm and tissue penetration of 2-3 mm. OCT has the potential to image tissues at the level of a single cell. In fact, the inventors have recently utilized broader band width optical sources such as femto-second pulsed lasers, so that axial resolution is improved to 4 microns or less. With such resolution, OCT can be applied to visualize intimal caps, their thickness, and details of structure including fissures, the size and extent of the underlying lipid pool and the presence of inflammatory cells. Moreover, near infrared light sources used in OCT instrumentation can penetrate into heavily calcified tissue regions characteristic of advanced coronary artery disease. With cellular resolution, application of OCT may be used to identify other details of the vulnerable plaque such as infiltration of monocytes and macrophages. In short, application of OCT can provide detailed images of a pathologic specimen without cutting or disturbing the tissue.  
         [0008]     One concern regarding application of this technology to image atherosclerotic plaques within the arterial lumen is the strong scattering of light due to the presence of red blood cells. Once a catheter system is positioned in a coronary artery, the blood flow between the OCT optical fiber and artery can obscure light penetration into the vessel wall. One proposed solution is the use of saline flushes. Saline use is limited in duration, however, since myocardial ischemia eventually occurs in the distal myocardium. The inventors have proposed the use of artificial hemoglobin in the place of saline. Artificial hemoglobin is non-particulate and therefore does not scatter light. Moreover, artificial hemoglobin is about to be approved by the United States Food and Drug Administration as a blood substitute and can carry oxygen necessary to prevent myocardial ischemia. Recently, the inventors demonstrated the viability of using artificial hemoglobin to reduce light scattering by blood in mouse myocardium coronary arteries (Villard J W, Feldman M D, Kim Jeehyun, Milner T E, Freeman G L. Use of a blood substitute to determine instantaneous murine right ventricular thickening with optical coherence tomography.  Circulation  2002; Volume 105: Pages 1843-1849, incorporated by reference herein).  
         [0009]     The first prototype of an OCT catheter to image coronary plaques has been built and is currently being tested by investigators in Boston at Harvard-MIT (Jang I K, Bouma B E, Kang D H, et al. Visualization of coronary atherosclerotic plaques in patients using optical coherence tomography: comparison with intravascular ultrasound.  JACC  2002; 39: 604-609, incorporated by reference herein) in association with Light Lab Co. The prototype catheter consists of a single light source and is able to image over a 360 degree arc of a coronary arterial lumen by rotating a shaft that spins the optical fiber. Because the rotating shaft is housed outside of the body, the spinning rod in the catheter must rotate with uniform angular velocity so that the light can be focused for equal intervals of time on each angular segment of the coronary artery. Mechanical drag in the rotating shaft can produce significant distortion and artifacts in recorded OCT images of the coronary artery. Unfortunately, because the catheter will always be forced to make several bends between the entry point in the femoral artery to the coronary artery (e.g., the 180 degree turn around the aortic arch), uneven mechanical drag will result in OCT image artifacts. As the application of OCT is shifted from imaging gross anatomical structures of the coronary artery to its capability to image at the level of a single cell, non-uniform rotation of the single fiber OCT prototype will become an increasingly problematic source of distortion and image artifact.  
         [0010]     Essentially, current endoscope type single channel OCT systems developed by Light Lab Co. suffers by non-constant rotating speed that forms irregular images of a vessel target. See U.S. Pat. No. 6,134,003, incorporated by reference herein. Their approach of a rotary shaft to spin a single mode fiber is prone to produce artifact. The catheter will always be forced to make several bends from its entry in the femoral artery, to the 180 degree turn around the aortic arch, to its final destination in the coronary artery. All these bends will cause uneven friction on the rotary shaft, and uneven time distribution of the light on the entire 360 degree arch of the coronary artery. As the application of OCT is shifted from gross anatomical structures of the coronary artery to its capability to image at the level of a single cell, then non-uniform rotation of the single fiber OCT will become even a greater source of greater artifact.  
         [0011]     The present invention solves rotational distortion and related artifactual problems by developing a multiphase array OCT catheter. By incorporating 10-60 individual OCT fibers within a single catheter, rotation of the optical fiber or similar element (e.g., micro-motor driven mirror) and associated image distortion and artifacts are eliminated and spatial resolution may be improved. The catheter will allow 10-60 individual sources of light to independently image the 360 degree arc of the coronary arterial lumen. An additional advantage of the multiphase array is provision of greater spatial resolution of the object being interrogated in comparison to single fiber designs. Many investigators recognize that a single rotating fiber or micro-motor driven mirrors utilized in current designs will not allow imaging at the level of a single cell while the multiphase array approach can provide cellular resolution.  
         [0012]     The construction of a multiphase array OCT catheter requires resolution of a number of problems using innovative design solutions. Successful design and demonstration of the catheter requires the development of an optical channel containing 10-60 individual fibers in a 1.5 mm diameter. Each fiber requires a lens to focus the light, and a mirror fabricated using nanotechnology to redirect light from each fiber by 90 degrees from the catheter to the luminal surface of the coronary artery. Further, each of the 10-60 light paths has to be split again for both reference and artery paths. The present invention provides design solutions to both the catheter and multichannel interferometer.  
       SUMMARY OF THE INVENTION  
       [0013]     The present invention pertains to an endoscope for a patient. The endoscope comprises a light producing means, such as a light source. The endoscope comprises an optical fiber array comprising a plurality of optical fibers adapted to be disposed in the patient. The optical fiber array transmits the light from the light producing means into the patient, and transmits the light reflected by the patient out of the patient. The plurality of the optical fibers of the array in optical communication with the light producing means. The endoscope comprises a detector for receiving the light from the array and analyzing the light. The plurality of the optical fibers of the array in optical communication with the detector.  
         [0014]     The present invention pertains to a method for imaging a patient. The method comprises the steps of transmitting light from a light source into an optical fiber array comprising a plurality of optical fibers in the patient. There is the step of transmitting the light reflected by the patient out of the patient. There is the step of receiving the light from the array at a detector. There is the step of analyzing the light with the detector.  
         [0015]     The present invention pertains to an apparatus for studying an object. The apparatus comprises means for producing light. The apparatus comprises means for analyzing the light that has reflected from the object based on polarization, space, position or angle.  
         [0016]     The present invention pertains to an apparatus for studying an object. The apparatus comprises means for producing light. The apparatus comprises means for analyzing the light that has reflected from the object based on polarization.  
         [0017]     The present invention pertains to an apparatus for studying an object. The apparatus comprises means for producing light. The apparatus comprises means for analyzing the light that has reflected from the object based on space.  
         [0018]     The present invention pertains to an apparatus for studying an object. The apparatus comprises means for producing light. The apparatus comprises means for analyzing the light that has reflected from the object based on angle.  
         [0019]     The present invention pertains to a method for studying an object. The method comprises the steps of producing light. The method comprises the steps of analyzing the light that has reflected from the object based on polarization, space, position or angle.  
         [0020]     The present invention pertains to a method for studying an object. The method comprises the steps of producing light. The method comprises the steps of analyzing the light that has reflected from the object based on polarization.  
         [0021]     The present invention pertains to a method for studying an object. The method comprises the steps of producing light. The method comprises the steps of analyzing the light that has reflected from the object based on space.  
         [0022]     The present invention pertains to a method for studying an object. The method comprises the steps of producing light. The method comprises the steps of analyzing the light that has reflected from the object based on angle. 
     
    
     BRIEF DESCRIPTION OF THE DRAWINGS  
       [0023]     In the accompanying drawings, the preferred embodiment of the invention and preferred methods of practicing the invention are illustrated in which:  
         [0024]      FIG. 1  is a schematic representation of an overview of the present invention.  
         [0025]      FIG. 2  is a top view of an input arm (light source) of the present invention.  
         [0026]      FIG. 3  is a schematic representation of a side view of the input arm (light source).  
         [0027]      FIG. 4  is a schematic representation of a fiber based solution for the input arm.  
         [0028]      FIG. 5  is a schematic representation of a side view of the sample arm.  
         [0029]      FIG. 6  is a schematic representation of an axial view of the sample arm.  
         [0030]      FIG. 7  is a schematic representation of a top view of an axicon lens.  
         [0031]      FIG. 8  is a schematic representation of an optical fiber array of the sample arm.  
         [0032]      FIG. 9  is a schematic representation of a perspective view of a probe tip of the sample arm emphasing the mirrors to refocus the light on the tissue of interest.  
         [0033]      FIG. 10  is a schematic representation of a side view of a groove of the tip with an attached fiber ending with a 45° angled mirror (reflection).  
         [0034]      FIG. 11  is a schematic representation of a top view of the tip with an attached fiber.  
         [0035]      FIG. 12  is a schematic representation of a first step of manufacture of each fiber lens of the sample arm.  
         [0036]      FIG. 13  is a schematic representation of a second step in the manufacture of each fiber lens of the sample arm.  
         [0037]      FIG. 14  is a schematic representation of a reference arm of the present invention.  
         [0038]      FIG. 15  is a schematic representation of a top view of a detection arm of the present invention.  
         [0039]      FIG. 16  is a schematic representation of a side view of the detection arm.  
         [0040]      FIG. 17  is an alternative schematic representation of a scanning probe of the sample arm.  
         [0041]      FIGS. 18   a  and  18   b  are schematic representations of an hydraulic mechanism.  
         [0042]      FIGS. 19   a  and  19   b  are schematic representations of exploded views of the hydraulic mechanism.  
         [0043]      FIGS. 20   a - 20   d  are schematic representations of different views of a twisted shaft of the hydraulic mechanism.  
         [0044]      FIGS. 21   a  and  21   b  are schematic representations of the fiber-shaft holder.  
         [0045]      FIGS. 22   a - 22   c  are schematic representations of fiber grooves.  
         [0046]      FIG. 23  is a side view of the micro-mirror.  
         [0047]      FIG. 24  is a perspective view of the micro-mirror.  
         [0048]      FIG. 25  is a perspective view of the micro-mirror with a portion irradiated by the laser beam.  
         [0049]      FIG. 26  is a perspective view of the micro-mirror having a deformation generated from being irradiated by a laser beam as shown in  FIG. 25 .  
         [0050]      FIG. 27  is a schematic representation of the micro-mirror being continuously heated by a laser beam shining on different locations of the micro-mirror.  
         [0051]      FIG. 28  is a schematic representation of the resulting changing of the tilting direction of the micro-mirror because of the changing location of the laser beam on the micro-mirror.  
         [0052]      FIG. 29  is a schematic representation of the micro-mirror in the probe cover relative to the fibers.  
         [0053]      FIG. 30  is a schematic representation of the micro-mirror movement relative to the fiber.  
         [0054]      FIG. 31  is a schematic diagram of single channel fiber-based polarization sensitive spectral domain optical coherence tomography with a fiber optic spectral polarimetry instrument (FOSPI).  
         [0055]      FIG. 32  is a schematic representation of a fiber-based spatially multiplexed swept source optical coherence tomography.  
         [0056]      FIG. 33  is a schematic representation of a multi-fiber angle-domain OCT.  
         [0057]      FIGS. 34 and 35  are images recorded with a spatially multiplexed OCT system.  
         [0058]      FIGS. 36 and 37  are phase retardation due to birefringence and fast-axis angle, respectively. 
     
    
     DETAILED DESCRIPTION  
       [0059]     Referring now to the drawings wherein like reference numerals refer to similar or identical parts throughout the several views, and more specifically to  FIGS. 1-5 ,  15  and  16  thereof, there is shown an endoscope  10  for a patient. The endoscope  10  comprises means  102  for producing light, such as a light source  51 . The endoscope  10  comprises an optical fiber array  28  comprising a plurality of optical fibers  8  adapted to be disposed in the patient. The optical fiber array 28 transmits the light from the producing means, preferably including a light source  51 , into the patient, and transmits the light reflected by the patient out of the patient. The plurality of the optical fibers  8  of the array  28  is in optical communication with the light producing means  102 . The endoscope  10  comprises a detector D for receiving the light from the array  28  and analyzing the light. The plurality of the optical fibers  8  of the array  28  is in optical communication with the detector D.  
         [0060]     Preferably, the endoscope  10  includes a tube  53  about which the plurality of optical fibers  8  are disposed. The tube  53  preferably has grooves  54  that extend longitudinally along the tube  53 , as shown in  FIG. 10 . One of the plurality of optical fibers  8  is disposed in each of the grooves  54 . Preferably, the endoscope  10  includes a probe tip  55 , as shown in  FIG. 11 , having a reflector  56  disposed in each groove which reflects light from the optical fiber  8  in the groove when the reflector  56  is in the patient and reflects light from the patient to the optical fiber  8  when the array  28  is in the patient.  
         [0061]     The light source  51  preferably includes a coherent light source  51  and means  57  for guiding the light from the light source  51  to the plurality of optical fibers  8  of the array  28 . Preferably, the optical fiber  8  is single mode, has a core  118  with cladding  120  disposed about the core  118 , and has a lens  122  at its tip which focuses the light from the core  118  to the reflector  56  and light from the reflector  56  to the core  118 , as shown in  FIGS. 12 and 13 . The array  28  preferably includes a transparent cover  7 .  
         [0062]     Preferably, the light source  51  comprises an input arm  58 , the array  28  comprises a sample arm  59 , the detector D comprises a reference arm  60  and a detector arm  61 ; and the input arm  58 , the detector arm  61 , the sample arm  59  and the reference arm  60  together form an interferometer. The reference arm  60  preferably uses RSOD to introduce depth scanning and dispersion compensation to the interferometer.  
         [0063]     Preferably, the endoscope  10  includes an opto-coupler  62  which optically couples corresponding optical fibers  8  of the input arm  58 , sample arm  59 , reference arm  60  and detecting arm together. The detector D preferably determines structural information about the patient from the intensity of an interference signal from reflected light from corresponding fibers of the sample arm  59  and the reference arm  60  having a same bypass length.  
         [0064]     Preferably, the probe tip  55  includes a scanning head  1  which holds N optical fibers  8 , where N is greater than or equal to 2 and is an integer, as shown in  FIGS. 17-22   c . The N optical fibers  8  are preferably arranged around the scanning head  1  in parallel and equal spacing. Preferably, the probe tip  55  includes a mechanism  134  for moving the scanning head  1  so each of the optical fibers  8  scan an angular range of N/360 degrees. The moving mechanism  134  preferably includes a mechanism  9  for linear motion which causes the scanning head  1  to rotate.  
         [0065]     Preferably, the linear motion mechanism  9  includes a fiber shaft holder having a shaft channel  31  extending axially along the holder, and N fiber channels  32  are arranged around the holder in parallel with the shaft channel  31 , and a twisting shaft that fits in and conforms with the shaft channel  31 , as the shaft moves in the channel, the holder rotates.  
         [0066]     The scanning head  1  preferably has a socket head that conforms with the shaft and causes the scanning head  1  to rotate. Preferably, the probe tip  55  includes a guide wire holder  2  disposed on the scanning probe  50  which receives and follows a guide wire when the guard wire is in a blood vessel, biliary tract, and possible GU tract. A guide wire is not necessary in the GI tract. Preferably, the endoscope  10  includes a spring disposed between the scanning head  1  and the fiber shaft holder which forces the shaft back after the shaft has moved forward.  
         [0067]     The present invention pertains to a method for imaging a vessel, GU, GI or biliary tract of a patient. The method comprises the steps of transmitting light from a light source  51  into an optical fiber array  28  comprising a plurality of optical fibers  8  in the patient. There is the step of transmitting the light reflected by the patient out of the patient. There is the step of receiving the light from the array  28  at a detector D. There is the step of analyzing the light with the detector D.  
         [0068]     Preferably, there are the steps of reflecting light from each optical fiber  8  with a corresponding reflector  56  associated with the fiber, and reflecting light from the patient to the associated fiber with a reflector  56 . There is preferably the step of moving each of N optical fibers  8  comprising the optical fiber array  28  an angular range of N/360 degrees. Preferably, there is the step of applying a linear motion to cause each of the N optical fibers  8  of the optical fiber array  28  to move the angular range.  
         [0069]     The step of applying the linear motion preferably includes the step of moving axially forward in parallel with the N optical fibers  8  a twisting shaft through a shaft channel  31  extending axially along a fiber shaft holder having N fiber channels  32  arranged around the holder in parallel with the shaft channel  31  which causes the holder to rotate. Each of the N optical fibers  8  is disposed in a respective fiber channel  32  of the N fiber channels  32 . The twisting shaft fits in and conforms with the shaft channel  31 , as the shaft moves in the channel. Preferably, there is the step of guiding the optical fiber array  28  along a guide wire which is received by a guide wire holder  2  when the guide wire is in a blood vessel, biliary tract, and possibly GU system, but not in the GI tract.  
         [0070]     The present invention pertains to an apparatus for studying an object. The apparatus comprises means for producing light. The apparatus comprises means for analyzing the light that has reflected from the object based on polarization, space, position or angle.  
         [0071]     The means for analyzing is preferably described in the figures, where polarization is found in  FIG. 31 , position in  FIGS. 1-30 , space in  FIG. 32 , and angle in  FIG. 33 .  
         [0072]     The present invention pertains to an apparatus for studying an object. The apparatus comprises means for producing light. The apparatus comprises means for analyzing the light that has reflected from the object based on polarization.  
         [0073]     The present invention pertains to an apparatus for studying an object. The apparatus comprises means for producing light. The apparatus comprises means for analyzing the light that has reflected from the object based on space.  
         [0074]     The present invention pertains to an apparatus for studying an object. The apparatus comprises means for producing light. The apparatus comprises means for analyzing the light that has reflected from the object based on angle.  
         [0075]     The present invention pertains to a method for studying an object. The method comprises the steps of producing light. The method comprises the steps of analyzing the light that has reflected from the object based on polarization, space, position or angle.  
         [0076]     The present invention pertains to a method for studying an object. The method comprises the steps of producing light. The method comprises the steps of analyzing the light that has reflected from the object based on polarization.  
         [0077]     The present invention pertains to a method for studying an object. The method comprises the steps of producing light. The method comprises the steps of analyzing the light that has reflected from the object based on space.  
         [0078]     The present invention pertains to a method for studying an object. The method comprises the steps of producing light. The method comprises the steps of analyzing the light that has reflected from the object based on angle.  
         [0079]     In the operation of the invention, a near infrared broadband light source  51  sends a light beam into the input arm  58  of the array  28  type interferometer. The beam profile from the light source  51  is a circular gaussion. The optics before connector  1  makes the beam profile linear and focuses it into the connector  1 . The array  28  type interferometer consists of multiple fiber-based interferometer that has four fiber arms connected to an opto-coupler  62 . Incoming light into the input arm  58  is divided to the sample and reference arms  59 ,  60 , respectively. In the sample arm  59 , optical fibers  8  are distributed like an annular ring, and light will be focused at the target vessel perpendicular to the optical axis. In the reference arm  60 , RSOD introduces depth scanning and dispersion compensation. When the reflected light from both arms have the same light path length, strictly speaking within a coherence length, interference occurs. The intensity of the interference signal represents the structural information of a sample.  
         [0080]     More specifically, in regard to the input arm  58 , and referring to  FIGS. 1, 2  and  3 , a single beam comes out of S 1  and will be collimated by L 1 . At this point, the beam diameter is big enough to project across all of C 1 &#39;s area, but the beam is still circular. CL 1  and CL 2 , circular lenses, change the beam profile to a linear shape, which means that the beam is not circular anymore, but it looks narrow from  FIG. 2  and the same shape with the beam after L 1  on  FIG. 3 . ML 1  focuses all light onto C 1 .  
         [0081]     This is known as an open optic solution: 
        Light source S 1  has a fiber tip from which light departs into air.     L 1  is a collimating lens  122 , so the fiber tip of the light source  51  should be located at the back of the focal point of L 1  in order to collimate the light.     CL 1 ,  2  are cylindrical lenses. Separation between two is the sum of each cylindrical lens  122  focal length. They work as a telescope which decrease beam size only in one direction. In other words, the size of the beam does not change from  FIG. 3 .     ML 1  is a micro lens array  28 , which has a lot of small lenses. Each of the small lenses is positioned to have a focal point at each fiber entrance of C 1 . C 1  should be located at the focal point of ML 1 . All micro lenses have same focal length. C 1  is a linear fiber array  28 .        
 
         [0086]     In an alternative embodiment of the input arm  58 , as shown in  FIG. 4 , known as a fiber based solution: 
        Light source S 1  is connected to a single mode fiber, which is connected to fiber splitter (50:50), S 1 .     The first fiber splitter is 1 by 2. Each output end of the 1*2 fiber splitter is connected to 1*4 splitter, SP 1 .     Each output end of the 1*4 splitter, 2 nd  layer, is connected to another 1*4 splitter, 3 rd  layer, SP 2 .     At the output of the 3 rd  layer, the number of fiber is 32. 32 fiber comprises a linear fiber array  28 , SP 3 . 
 
 Linear fiber array  28 : 
    Each fiber is a single mode fiber, which can have a different cutoff frequency. The cutoff frequency is dependent on the center wavelength of the light source  51 . Usually, 850 nm or 1300 nm of center wavelength for the light source  51  are used.     Each fiber is attached to another so that all together they form a linear fiber array  28 .        
 
         [0093]     C 1  is connected to multiple interferometers. Each interferometer consists of four fiber arms and opto-coupler  62 . At each end of each arm, there is a linear array  28  fiber connector (C 1 , C 2 , C 3  C 4 ). Incoming light will be divided by the opto-coupler  62  into the sample and reference arms  59 ,  60 , respectively.  
         [0094]     With respect to the sample arm  59 , this sample arm  59 , as shown in  FIGS. 5, 6 ,  7 ,  8  and  17 , goes into the target vessel. C 2  is connected to a linear fiber array  28  which is of an annular shape at the other end. The total length of the arm will be around 2˜3 m. When the light leaves the annular tip F, it will be collimated by L 1  and then reflected by L 2  outward from the probe.  
         [0095]     Reflected light from tissue will follow back to L 2  and L 1  and be gathered by the fiber tip. Later, two reflected lights from the sample and reference arms  59 ,  60 , respectively, will make interference, which will be detected by the array  28  detector D at the detection arm.  
         [0096]     The sample arm  59  is supposed to go through a target vessel, GI, GU or biliary tract. C 2  is connected to a linear fiber array  28  which has an annular shape at the other end (probe tip  55 ) ( FIG. 8 ). Total length of the sample arm  59  is about 1.5 m. The fiber array  28  will be molded by a transparent cover  7  material (ex: silicon resin or polymers).  
         [0097]     At the annular probe tip F shown in  FIG. 9 , each fiber is glued at a groove of a cylindrical polymer tube  53 . The shape of each groove is shown at  FIGS. 10 and 11 . Each groove end has a reflector  56  which is 45° oblique to axial direction. The groove will be made by micro fabrication technique. Each fiber has a lens  122  at the tip, which can be manufactured by splicing a multimode fiber with the same diameter of the cladding  120  of the single mode fiber and then melting the end of multimode fiber in order to get curvature ( FIGS. 12 and 13 ). When the light leaves the fiber tip, the light will be reflected outward by the reflector  56  at the end of the groove, and then will be focused at the target tissue area. Reflected light from the tissue will follow back the same path as the incoming light, and go to the detection arm.  
         [0098]     Micromachining or micro-electro-mechanical systems (MEMS) and nanotechnology are becoming increasingly popular for the development of improved biomaterials and devices (Macilwain C., “US plans large funding boost to support nanotechnology boom,”  Nature , 1999; 400:95, incorporated by reference herein). Similar to manufacturing methods used for computer microchips, MEMS processes combine etching and/or material deposition and photolithographic-patterning techniques to develop ultrasmall devices (Madou, M., “Fundamentals of microfabrication,”  CRC Press: Boca Raton , 2002, incorporated by reference herein). MEMS has been proven promising in medicine for its small mass and volume, low cost, and high functionality. Successful MEMS devices in medicine include smart sensor for cataract removal, silicon neurowells, microneedles for gene and drug delivery, and DNA arrays (Polla, D. L., Erdman, A. G., Robbins, W. P., Markus, D. T., Diaz-Diaz, J., Rizq, R., Nam, Y., Brickner, H. T., Wang, A., Krulevitch, P., “Microdevices in Medicine,”  Annu. Rev. Biomed. Eng ., 2000; 02:551-76; McAllister et al., 2000, both of which are incorporated by reference herein). However, most of the MEMS processes are planar in nature for two-dimension (2D) micro-features and primary for processing silicon material. Other micromachining processes include laser beam micromachining (LBM), micro-electrical discharge machine (micro-EDM), and electron beam machining (EBM) (Madou, M., “Fundamentals of microfabrication,”  CRC Press: Boca Raton , 2002), incorporated by reference herein. Micro-fabrication and micro-device development using metals, metal alloys, silicon, glass, and polymers are described in the following. (Chen, S. C., Cahill, D. G., and Grigoropoulos, C. P., “Transient Melting and Deformation in Pulsed Laser Surface Micro-modification of Ni-P Disks,”  J. Heat Transfer , vol. 122 (no. 1), pp. 107-12, 2000; Kancharla, V. and Chen, S. C., “Fabrication of Biodegradable Microdevices by Laser Micromachining of Biodegradable Polymers,”  Biomedical Microdevices , 2002, Vol. 4(2): 105-109; Chen, S. C., Kancharla, V., and Lu, Y., “Laser-based Microscale Patterning of Biodegradable Polymers for Biomedical Applications,” in press,  International J. Nano Technology , 2002; Zheng, W. and Chen, S. C., “Continuous Flow, nano-liter Scale Polymerase Chain Reaction System,”  Transactions of NAMRC/SME , Vol. 30, pp. 551-555, 2002; Chen, S. C., “Design and Analysis of a Heat Conduction-based, Continuous Flow, Nano-liter Scale Polymerase Chain Reaction System,”  BECON , 2002, all of which are incorporated by reference herein).  
         [0099]     For the array  28 , a stainless steel cylinder is chosen with a diameter of 1.5 mm as the base material. The diameter is 1.0 mmm for vascular applications, larger for GU, GI and biliary applications, up to 3.0 mm, if desired. Both the micro-grooves  54  (or micro-channels of 200 microns wide) and the reflecting surfaces are machined by micro-electrical discharge machining (micro-EDM) or micro-milling using focused ion machined tool. To enhance the reflectivity of the reflecting surface, the stainless steel cylinder are coated with evaporated aluminum using electron-beam evaporation.  
         [0100]     In regard to the reference arm  60 , shown in  FIG. 14 , light is collimated by L 1  after leaving connector C 4 , and be spectrally distributed by a grating (G 1 ) and will be focused to a mirror (GA 1 ). By vibrating GA 1 , the light path length will be changed in order to achieve depth scanning.  
         [0101]     There are many options to build the reference arm  60  applying existing techniques. A very simple form of the reference arm  60  has just a mirror attached onto a voice coil that is driven by a function generator with sine wave. The light reflects back by the mirror and the mirror position changes the light path length. This path length change provides depth scanning of the target tissue because interference occurs only when both arms have the same light path length. Preferably, the reference arm  60  is more complicated than the simple one. That is called Rapid-Scanning Optical Delay (RSOD) which can provide fast depth scanning and dispersion compensation.  
         [0102]     Linear array type beam launches from C 4 , and is collimated by L 1 . A mirror (M 1 ) reflects the beam to a grating (G 1 ) which spectrally distributes the broadband source light. Spectrally distributed light will be focused on a Galvono-scanning mirror (GA 1 ) by a lens (L 2 ). Separation between G 1  and L 2  determines the amount of chromatic dispersion degree so any material dispersion can be compensated for usually caused by fibers. The beam offset from the scanning mirror center determines the fringe frequency that will show up after interfering two reflected lights. The reflected light from the GA 1  goes to L 2 , G 1 , and to M 2 . And then the light reflected following back incoming path and will be coupled back to C 4 .  
         [0103]     Referring to the detection arm, as shown in  FIGS. 15 and 16 , light is collimated by L 1  after leaving connector C 3 , and is circular. Combination of CL 1  and CL 2  makes the beam look linear in one plane (horizontal). Micro-lens array ML 1  makes the light focus on the array  28  detector D.  
         [0104]     As shown in  FIGS. 17, 19   a , and  19   b , the scanning probe  50  is comprised of a scanning head  1 , a fiber-shaft holder  3 , a twisted shaft  4 , a transparent cover  7 , a guide wire holder  2 , and a mechanism  9  for linear motion. In this embodiment, the scanning head  1  is adapted to hold a fiber bunch that contain  20  optical fibers  8 , which are arranged around the scanning head  1  in parallel and equal spacing. In operation, each of the fibers is set to scan an angular range of 18 degrees (360°÷20 =18°). Reflective surfaces  11  are formed on the scanning head  1  and are oriented 45° degrees to the central axis of each respective optical fibers  8 , such that they would guide the light from the fiber bunch and direct the light through the transparent cover  7 .  
         [0105]     The scanning head 1 is designed to provide an 18 degrees&#39; back-and-forth rotation. The back-and-forth rotation realizes the scanning function required by the OCT system. The mechanism of this back-and forth rotation is described below.  
         [0106]     The fiber-shaft holder is substantially a multi-tubular structure. It is formed with one shaft channel  31  extending along the central axis of the fiber-shaft holder and  20  fiber channels  32  arranged around the fiber-shaft holder  3  in parallel. The optical fibers  8  extend through respective fiber channels  32 . The shaft channel  31  has a round cross-sectional area. At the upper end of the shaft channel  31 , the shaft channel  31  is an opening, but the geometry of the opening is reduced from the round cross-sectional area to a rectangular cross-sectional hole  311 . The reason for this structural design will be described along with the description of the twisted shaft  4 .  
         [0107]     The twisted shaft  4  has a rectangular cross-section area, which is identical in geometry to the rectangular cross-sectional hole of the fiber-shaft holder  3 . Indicated by its name, the shaft  4  is partially twisted along the shaft central axis and can be divided into a non-twisted part  41  and a twisted part  42 . In assembly, the shaft  4  is passed through the rectangular cross-sectional hole of the fiber-shaft holder  3 , and it is enabled to slide back-and-forth via the rectangular cross-sectional hole. The relative motion of the surfaces of the rectangular cross-sectional hole and the twisted shaft  4  form the mechanism that realizes a back-and-forth rotation. The reason is that when the twisted part  42  of the shaft  4  slides through the rectangular cross-sectional hole, the shaft  4  itself is forced to rotate along the shaft central axis to fit the matching of both the surfaces of the rectangular cross-sectional hole and the twisted shaft  4 . Particularly, the shaft  4  and the holder  3  compose a mechanism  9  that can transmit a linear motion into a rotational motion.  
         [0108]     The description is now focused on the scanning head  1 . The scanning head  1  has a rectangular socket  12 , which has a cross-section area identical to that of the twisted shaft  4 . The rectangular socket  12  provides a channel covering the non-twisted part  41  of the twisted shaft  4  and lets the non-twisted part  41  exert the back-and forth motion inside the rectangular socket  12 . The moving range of the shaft  4  is constrained such that the twisted part  42  does not pass into the scanning head&#39;s rectangular socket  12  (that will result in a geometric mismatch), but the twisted part  42  only interacts with the fiber-shaft holder&#39;s rectangular cross-sectional hole. According to the description above, the motion of the shaft  4  is comprised of a linear component (V) and an angular component (ω). Referring to the geometry of the rectangular socket  12  and non-twisted part  41  of the shaft  4 , the shaft motion&#39;s linear component (V) would not contribute to the motion of the scanning head  1  (regardless of the friction between the surfaces), but the angular component (ω) does. The scanning head  1  rotates back and forth with the rotational motion of the twisted shaft  4 , which in turn results from the twisted shaft&#39;s linear back-and-forth movement relative to the fiber-shaft holder  3 . As a result, the scanning head  1  provides a back-and-forth rotational motion transmitted from the back and forth linear motion provided by the twisted shaft  4 .  
         [0109]     A guide wire holder  2  is a module used to guide the scanning probe  50  toward the investigated section of the detected blood vessel, biliary duct, and possibly GU application. For the GI tract, a guide wire is generally not used. In operation, a guide wire  01 , or “guide tissue”, is previously disposed along a specific route of human vessels, such that a track for the scanning probe  50  of the OCT system can be formed. The guide wire holder  2  constrains the scanning probe  50  such that it can only slide along the track formed by the guide wire  01 . The scanning probe  50  is therefore guided to the patient section to be investigated.  
         [0110]     Guide wire holder  2  and holder  5  function as bearings of the scanning head  1 . They constrain the movement of the scanning head  1  and stabilize it. As well, a compressive spring  6  is disposed between the scanning head  1  and the fiber-shaft holder  3 . The spring  6  is mildly compressed in assembly, such that it pushes the scanning head  1  against the holder  5  and eliminates any potential axial movement of the scanning head  1  that may result in axial positioning errors (Δd). It is preferable that the spring  6  supplies torque between the scanning head  1  and the fiber-shaft holder  3 . The spring  6  has its both ends, respectively, fixed on the scanning head  1  and the fiber-shaft holder  3 . The spring  6  is mildly twisted in assembly. By this means, the spring can provide a torque to the back-and-forth rotational mechanism, such that the backlash (resulting from, for example, the tolerance between the rectangular cross-sectional hole and the shaft) of the rotational mechanism, as well as the resultant angular positioning errors (Δθ), are eliminated.  
         [0111]     Note that, the cross-section geometry of the shaft channel  31  is circular. With respect to the shaft channel  31 , the twisted shaft  4  is formed with a cylinder part  43  at its end of the twisted part  42 . The cylinder part  43  and the shaft channel  31  performs a motion like a piston. In an upward movement of the twisted shaft  4 , due to the geometric difference, the cylinder part  43  would be blocked at the edge  33  of the rectangular cross-sectional hole of the fiber-shaft holder  3  and provide an upper stopper for the twisted shaft  4 . On the other hand, a lower stopper  34  is placed to block the cylinder part  43  in a downward movement. The function of the upper and lower stoppers is helpful in controlling the movement of the twisted shaft  4 , as well as controlling the angular motion of the scanning head  1 .  
         [0112]     There are many methods in the prior art that are able to provide the power for the mechanism to push and pull the twisted shaft  4  to generate the linear movement. However, hydraulic force, particularly fluidic pressure, is preferred due to the following advantages: 
        1. Electricity is not required to be transmitted into the scanning head  1  to energize a hydraulic linear mechanism  9 . Some of the mechanisms, such as electromagnetic systems (or more particularly, some micro-motors), require not only electricity to be energized, but also additional components, e.g., coils or magnets, installed to the scanning head  1  to transform the electrical energy into mechanical momentum. The use of electricity is not preferable for medical issues; and the requirement of additional components would increase the technical difficulty in manufacturing and the complexity of the whole system. Some of the other mechanisms, like those comprising piezoelectric materials, can be composed with little space and simple structure, but they still need to receive a large voltage to generate the required momentum.     2. A hydraulic mechanism  9  takes little space.        
 
         [0115]     The structure of the hydraulic mechanism  9  is illustrated in  FIGS. 18   a  and  18   b . The hydraulic mechanism  9  can be simply a liquid conduit that guides liquid, such as water, to push or pull the piston system comprised of the cylinder part  43  and the shaft channel  31 . Considering that leakage through the gap of a piston system may result in undesirable problems, the hydraulic mechanism  9  is, preferably, comprised of a micro-balloon  91  made by a polymeric thin film. As shown in  FIGS. 18   a  and  18   b , the twisted shaft  4  is in its lower position when the balloon  91  is flat ( FIG. 18   a ). As water is pumped into the piston system, the balloon  91  becomes turgid, and the twisted shaft  4  is pushed toward its upper position with an 18 degree spin ( FIG. 18   b ). The required back-and forth motion can be generated by switching the flat and turgid states of the micro-balloon  91 .  
         [0116]     For a single fiber OCT system, a scan rate of 6 rev/sec (6 Hz) is satisfactory [Andrew M. Rollins et al., “Real-time in vivo imaging of human gastrointestinal ultrastructure by use of endoscopic optical coherence tomography with a novel efficient interferometer design”, OPTICS LETTERS, Vol. 24, No. 19, Oct. 1, 1999, incorporated by reference herein]. That means in one second the OCT system should be able to provide at least 6 pictures illustrating the cross-sectional data of the vessel. The scanning probe  50  has 20 fibers, so the satisfactory scan rate can be reduced to 0.3 Hz (6÷20=0.3), which is much slower and much easier to be realized by the hydraulic actuating system. Ideally, 15 pictures/sec. is required for optimal image resolution.  
         [0117]     Rather than continuous rotation, the scanning probe  50  operates in a back-and-forth manner, so that the angular speed of the scanning head  1  will not be constant even when the whole system reaches its steady state. During operation, therefore, detecting the angle of the scanning head  1 , as well as figuring out the angular position that the scanned data belongs to, are important issues. The angle of the scanning head  1  can be simply approximated by comparing the output effort of the pumping system with a reference curve obtained from previous experiments. More precise detection can be reached by the analysis of the feedback of the optical signals. For example, analyzing the Light Doppler Effect [Volker Westphal at al., “Real-time, high velocity-resolution color Doppler optical coherence tomography”, OPTICS LETTERS, Vol. 27, No. 1, Jan 1, 2002, incorporated by reference herein] of the feedback signals is another method.  
         [0118]     The twisted shaft  4  can be formed by precise CNC machining that is well known in the industry. A thin round shaft, minimum diameter 1.0 mm, may be used as the intrinsic material before the machining. For production, two ends of the round shaft are clamped, its central portion is precisely milled and four orthogonal planes on the central portion are generated. The planes define the rectangular cross-section of the twisted shaft  4  (forming a long shaft in this step), as shown in  FIG. 20   a . Following the milling, one of the two clamps holding the shaft is rotated relative to the other clamp to twist the shaft a specific angle about its central axis. The twisted part of the twisted shaft  4  being formed.  
         [0119]     Following the twisting step, the rotated clamp is released to free the elastic distortion of the shaft (with its plastic distortion remaining), and then the clamp is tightened again. At the next step, as shown by  FIG. 20   b , the shaft is milled again at one side of its still-round portion, thereby generating another rectangular portion that is untwisted.  
         [0120]     The cylindrical portion (serves as a piston) is formed from the round portion of the shaft. A precise lathering could further be used to fix the central axis and diameter of the cylindrical part. As shown in  FIG. 20   c , only a short portion of the shaft is required. The excess portion of the shaft part is cut off.  
         [0121]     As shown in  FIG. 21   a , the fiber-shaft holder  3  can be combined with two parts, A and B. The part A is actually the body of the catheter. The cross-section of the catheter is shown in  FIG. 21   b ; the catheter could be manufactured by the cable extrusion technique that generally is applied in fiber optics industry [Refer to the homepage of Optical Cable Corporation.] Note that the central channel of the catheter is used to be the conduit for the guidance of actuating liquid mentioned previously. There are also several conduits used to guide air flowing in and out the probing tip to balance the air pressure inside the OCT system (during operation, the free volume inside the probing tip changes while the twisted shaft  4  is moving). The diameter of the conduit is equal to that of the cylinder part  43  of the twisted shaft  4 .  
         [0122]     Part B in  FIG. 21   a  is simply a plate having fiber holding edges (B 1 ) and a rectangular central opening (B 2 ). This part could be made from metal by using punching technology as is commonly applied in the industry. In assembly, Part A and Part B are connected with glue such as epoxy. The lower stopper, which is required to constrain the twisted shaft  4  at its lower position, is formed together with the formation of the micro-balloon.  
         [0123]     Micro-molding with polymeric material (such as SBS) could be used to fabricate the scanning head  1 . The process of micro-molding requires a set of micro-molds. In this case, the fiber grooves  54  and the reflective surface  11  at the end of the fiber grooves  54  can be realized by a set of micro-molds comprised of 18 edges ( FIG. 22   a ), each of which has the geometry shown in  FIG. 6   b . As well, the central rectangular channel could be molded by a rectangular shaft made by the equipment for the fabrication of the twisted shaft  4 . For the convenience of assembly, the scanning head  1  could be previously provided with the geometry shown in  FIG. 22   c . The excess parts of the scanning head  1  would provide guidance and help with the alignment for the optical fibers  8 . UV glue could be used to fix the position of the optical fibers  8 . The excess portion of the scanning head  1  could be cut off after the assembly of the optical fibers  8 .  
         [0124]     In another embodiment, laser beams heat at least three different locations on the surface of the micro-mirror  210 , which is shown as a disk in  FIGS. 23-25 , successively. The micro-mirror  210  will provide a wabling corresponding to this kind of un-symmetric heating process, and an incident light (other than the heating laser) can be redirected in a swaying manner.  
         [0125]     The heating process corresponds to the rotation period of the micro-mirror  210  as required.  
         [0126]     The micro-mirror  210  comprises two layers: a first layer  212  and a second layer  214  ( FIG. 23 ). At least one of the two layers can generate structural deformation (contraction or expansion) by the application of laser light. If the case is that both of the layers are deformable by laser light, the sensitivities of the two layers to a same laser light would be set different to each others.  FIG. 24  shows the perspective view of the micro-mirror  210 .  
         [0127]     When the micro-mirror  210  is irradiated with a laser beam, there will be expansion or contraction in the layers. Because the expansion or contraction within the layers is of different degrees (only one layer is deformed or the two layers are deformed with different degrees), the structure of the whole micro-mirror  210  will be twisted.  
         [0128]     For example, in  FIG. 25 , when the section marked with the pie is irradiated with a laser beam, there is a deformation generated as shown in  FIG. 26 .  
         [0129]     The material of the first and second layers  212 ,  214  could be metals or photosensitive polymers.  
         [0130]     In the case of metal layers, for example, the first layer  212  is poly-silicon and the second layer  214  is gold. The mechanism of the expansion or contraction within the layers is thermal expansion. The metals will absorb the energy of a laser beam and be heated. Due to different thermal expansion coefficients of the two layers, the structure will be twisted or bent. This will result in turning the mirror, as shown in  FIG. 26 .  
         [0131]     In the case of photosensitive polymers, for example, liquid crystal materials, the mechanism of the expansion or contraction inside the layers is a phase change of the materials. Under the irradiation of a laser beam, the molecules of the polymeric materials will undergo phase change, wherein the chemical structures of the materials are deformed, and a structural deformation occurs. Next, similar to the case of metal layers, the degrees of deformation of the two layers are different, and there will be a twisting or bending effect in the structure of the micro-mirror  210 , and the effect in  FIG. 26  is reached.  
         [0132]     When the structure is twisted or bent by the application of laser energy, the surface of the mirror, shown in  FIG. 24 , can be tiled to a specific direction. Therefore, one can control the direction of the micro-mirror  210  by controlling the laser energy input.  
         [0133]     The way to control the application of the laser light is to select the location on the micro-mirror  210  to be irradiated by the laser beam, and control the intensity of the laser. By controlling the location, one can control the tilting direction of the mirror; and by controlling the intensity, one can control the tilting angle of the micro-mirror  210 .  
         [0134]     Referring to  FIG. 25  and  FIG. 26 , by continuously changing the laser-shining location ( FIG. 27 ), the tilting direction of the micro-mirror  210  can be continuously changed ( FIG. 28 ). That is, the micro-mirror  210  could be rotated by changing the location of the laser-shining.  
         [0135]     This is the mechanism for the rotation of the laser-actuated micro-mirror  210 .  
         [0136]     As to the assembly of the whole OCT system ( FIG. 29 ), the micro-mirror  210  is mounted on a base  21   b  connected to the tip end of the probe cover. There is no object between the fibers and the mirror. Fiber  1 , which is used to guide the detecting light, is the same fiber used in other embodiments of the OCT probe. The detecting light is redirected by the tilting surface of the micro-mirror  210 , such that it can scan around by means of the tilting and rotating mirror. The fibers  2  are used to guide the actuating-laser light. As shown, at least three fibers  2  are needed. The fibers  2  fire lasers in turns, such that they can generate continuous tilting effect as shown in  FIG. 27  and  FIG. 28 .  
         [0137]     The other features of the laser-actuating OCT probe are the same as those described in other embodiments. For instance, the fiber, and fibers  2  are disposed in a fiber shaft holder  3 .  
         [0138]     After the fabrication by semiconductor technique, which is well known by those skillful in the art, the mirror is formed on a substrate (usually silicon substrate). The substrate material forms the base. Then a small piece is cut from the base that carries the mirror from the substrate with a dicer. The small piece is mounted on to the tip&#39;s end by glue (EPOXY, for example).  
         [0139]     Only one fiber  1  is enough to transmit the detecting light in this embodiment. During operation, a circular scanning profile of the detecting laser is realized. In this embodiment, illustrated in  FIG. 30 , the detecting laser is not centered to the mirror&#39;s center. Instead, the following remain constant: (1) d, the distance between the mirror center and the axis of the detecting light. (2) alfa, the angle between the mirror surface and the axis of the detecting light. An open-loop system is used for position feedback to properly arrange the periodical change of the laser powers from the three fibers  2  to realize the constant alfa and d.  
         [0140]     The position control is more complex than single-fiber  2  actuation. Particularly, the micro-mirror  210  needs a period of time to respond mechanically to the laser energy coming from the fiber  2 . Even though it is known when and which of the fibers  2  are firing the laser power, the exact direction of the mirror surface information cannot be assured.  
         [0141]     The absolute position of the mirror is actually not necessary. Instead, speed-control is used to control the rotation of the scanning mirror. For example, in the case of the mirror driven by a transmission cable rotated from outside, the exact position of the mirror (which may be affected by a delay of cable transmission due to the cable&#39;s compliance) is not of concern; the rotation period of the mirror is controlled so that the “relative position” of the mirror is known. After receiving a continuous data stream from the reflected detecting laser, the cross-section image of the vessel is constructed by simply matching the data series to the rotating period.  
         [0142]     In this embodiment, the operation will be similar. What is different is that the micro-mirror  210  is not actuated by a rotator but by three bimorph heat-deformable cantilever beams. This makes the control more complex. If only one of the fiber  2  fires at one time, it will be very different if not impossible for the mirror to scan a circular profile needed. Instead, the three fibers  2  are needed to fire together, with different powers, to bend the three cantilevers at different status at one time to match a circular scanning profile. The three cantilevers are actuated individually by the three fibers  2  such that they cooperate with specific bending patterns that realize a circular scanning profile on the wall of the vessel.  
         [0143]     In an alternative embodiment regarding the micro-mirror  210 , the fibers  1  and the fibers  2  are reversed so healing energy comes from a single fiber  2  disposed preferably along the central axis of the tube. The plurality of fibers  1  are disposed about the circumference of the tube. When the micro-mirror  210  is irradiated by the laser beam from the fiber  2 , the laser energy causes the mirror to bend. By changing the intensity of the laser or pulsing the laser, motion can be imported to the micro-mirror  210  which wires the probe tip to which it is attached, to move back and forth, and thus the plurality of fibers  1  for scanning the interior of the area of the patient in question.  
         [0144]     Thermal expansion material normally can generate ˜5% of elongation for a temperature rise of 100° C. The length of the material inside the OCT is originally 20 mm, which can therefore generate a thermal elongation of 1 mm. Polymers, including photosensitive polymers and shape memory polymers are able to generate &gt;100% of photo-induced elongations or shrinkages. The material inside the OCT is originally 1 mm, which can therefore generate a thermal elongation of another 1 mm.  
         [0000]     Generally:  
         [0145]     Optical tomographic instrumentation may be specified by spectrally resolved bandwidth, which is equivalent to number of spectrally resolvable cells. Each spectrally resolvable cell has a width δν, such that number of cells resolvable by the instrument is N instrument =Δν/δν, where Δν is the available optical bandwidth of source light. The range of group-time delays the optical tomographic instrument can resolve is given by: Δτ instrument =1/δν. The smallest resolvable group-time delay the optical tomographic instrument can resolve is Δτ coherence =1/Δν. Number of spectrally resolvable cells the optical tomographic instrument may resolve is given by:
 
 N   instrument=Δτ   instrument /Δτ coherence .
 
         [0146]     For 1 OCT A-scan into the object being imaged, the requirement for number of spectrally resolvable cells is −N A-scan =Δz/L c , Lc˜c g /Δv, Δz=imaging depth, L c  (coherence length), and c g  is the group velocity of light in the object.
 
N A-scan =Δτ A-scan Δv
 
 Where Δτ A-scan =Δz/c g  is the round-trip propagation time for light to propagate from the most superficial and deepest position (to be imaged) in the object. 
 
         [0147]     For some optical tomographic imaging instruments (e.g., those that employ narrow linewidth tunable laser sources or high resolution spectrometers),
 
 N   instrument   /N   A-scan =Δτ instrument /Δτ A-scan =Δν/δν&gt;&gt;1
 
         [0148]     The above condition can be stated in three manners: a) the number of spectrally resolvable cells for the instrument (N instrument ) is much greater than that required for one A-scan (N A-scan ); 2) the range of group time delays the instrumentation is capable of resolving (Δτ instrument ) is much greater than the group-time delay for a single A-scan (Δτ A-scan ); 3) available optical bandwidth of source light (Δν) is much greater than spectral width of each resolvable cell of the instrumentation (δν).  
         [0149]     Because the instrument can resolve many more cells than that required for one A-scan, multiplexing techniques are presented here to efficiently utilize the information carrying capacity (bandwidth) afforded by optical tomographic imaging instruments.  
         [0150]     Selection criteria of multiplexing techniques employed may be derived in part by the ratio N instrument /N A-scan =Δτ instrument /Δτ A-scan =Δν/δν. Larger ratios provide a wider selection of possible multiplexing techniques and more candidate domains (polarization, space, angle, temporal) to multiplex into. Moreover, multiplexing spectral information into just one domain (e.g. spatial) is not the only envisioned approach. Generally, additional spectral information may be resolved into multiple domains (e.g., polarization and spatial).  
         [0000]     Specific Implementations:  
         [0151]     A. Polarization: The additional spectral cells may be used to record information in the polarization domain using a system indicated in  FIG. 31 . At least two incident polarization states 90° apart on the Poincare sphere are input into the interferometer. The polarization signature of the light reflected from the sample, such as a vessel wall or nerve fiber layer, is compared to known polarization signatures of materials, such as plaques or a diseased nerve fiber layer. The reflected light and thus the material from which it was reflected is then identified. The fiber delivery system described in PCT patent application number PCT/US2004/012773, incorporated by reference herein, can be used.  
         [0152]     The theory of operation of this approach is described using Mueller matrices or the spectrally-resolved Jones calculus. By inserting a FOSPI in the detection path of the spectral domain optical coherence tomography (SD-OCT) instrumentation, the full set of Stokes parameters of light backscattered at the specific depth in the specimen can be obtained without any other polarization controlling components in reference/sample/detection path of the interferometer and the prior knowledge of the polarization state of the light incident on the sample. In this configuration, two factors determine the spectral modulation. One is optical path length difference between the reference and sample surface, (Δ(ν)), introduced by the common-path SDOCT and the other is phase retardations, φ 1 (ν) and φ 2 (ν) generated by the retarder system in the FOSPI. Therefore, output from the presented single channel polarization sensitive (PS)SD-OCT in the time-delay domain is the convolution of the output from FOSPI and that from SD-OCT.  
         [0000]     The Stokes parameters of light at the output of the interferometer are
 
 S   i   =S   i,1   +S   i,2   +S   i,i 
 
 where the first two terms are the Stokes parameters of light from the reference and sample path, respectively, and the last term is the contribution of interference. Consider the birefringent sample with phase retardation δ and fast-axis oriented at angle of α. Then, the Stokes parameters of the light from the sample (S i,2 ) and interference (S i,i ) are calculated in terms of the Stokes parameters of light from the reference, S 0,1 , S 1,1 , S 2,1 , S 3,1 .
 
S 0,2 =r s   2 S 0,1 
 
 S   1,2   r   s   2 (cos 2 2α+cos δ sin 2 2α) S   1,1   +r   s   2 (1−cos δ)sin2α cos2 αS   2,1   −r   s   2 sin δ sin2 αS   3,1 
 
 S   2,2   =r   s   2 (1−cos δ)sin2α cos2 αS   1,1   +r   s   2 (sin 2 2α+cosδ cos 2 2α) S   2,1   +r   s   2 sin δ sin2 αS   3,1 
 
 S   3,2   =r   s   2 sin δ sin2 αS   1,1   −r   s   2 sin δ cos2 αS   2,1   +r   s   2 cosδS 3,1   (1)
 
  
                 S     0   ,   i       =       2   ⁢     r   s     ⁢   cos   ⁢           ⁢   Δcos   ⁢     δ   2     ⁢     S     0   ,   1         +     2   ⁢     r   s     ⁢   sin   ⁢           ⁢   Δ   ⁢           ⁢   sin   ⁢           ⁢     δ   2     ⁢     (       cos   ⁢           ⁢   2   ⁢           ⁢   α   ⁢           ⁢     S     1   ,   1         +     sin   ⁢           ⁢   2   ⁢           ⁢   α   ⁢           ⁢     S     2   ,   1           )           ⁢     
     ⁢       S     1   ,   i       =       2   ⁢     r   s     ⁢   cos   ⁢           ⁢     Δ   ⁡     (       cos   ⁢           ⁢     δ   2     ⁢     S     1   ,   1         -     sin   ⁢           ⁢     δ   2     ⁢   sin   ⁢           ⁢   2   ⁢           ⁢   α   ⁢           ⁢     S     3   ,   1           )         +     2   ⁢     r   s     ⁢   sin   ⁢           ⁢   Δ   ⁢           ⁢   sin   ⁢           ⁢     δ   2     ⁢   cos   ⁢           ⁢   2   ⁢           ⁢   α   ⁢           ⁢     S     0   ,   1             ⁢     
     ⁢       S     2   ,   i       =       2   ⁢     r   s     ⁢   cos   ⁢           ⁢     Δ   ⁡     (       cos   ⁢           ⁢     δ   2     ⁢     S     2   ,   1         +     sin   ⁢           ⁢     δ   2     ⁢   sin   ⁢           ⁢   2   ⁢           ⁢   α   ⁢           ⁢     S     3   ,   1           )         +     2   ⁢     r   s     ⁢   sin   ⁢           ⁢   Δ   ⁢           ⁢   sin   ⁢           ⁢     δ   2     ⁢   cos   ⁢           ⁢   2   ⁢           ⁢   α   ⁢           ⁢     S     0   ,   1             ⁢     
     ⁢       S     3   ,   i       =     2   ⁢     r   s     ⁢   cos   ⁢           ⁢     Δ   ⁡     (       sin   ⁢           ⁢     δ   2     ⁢   sin   ⁢           ⁢   2   ⁢           ⁢   α   ⁢           ⁢     S     1   ,   1         -     sin   ⁢           ⁢     δ   2     ⁢   cos   ⁢           ⁢   2   ⁢           ⁢   α   ⁢           ⁢     S     2   ,   1         +     cos   ⁢           ⁢     δ   2     ⁢     S     3   ,   1           )                   (   2   )             
 
 with a reflection coefficient of the sample r s  and an optical path length difference between the sample and reference path Δ. Here, the terms including trigonometric functions of Δ represent the interference between the light from reference and sample paths. 
 
         [0153]     The measured intensity from SDOCT passing through the FOSPI for a birefringent sample, then, is  
                 I     out   ,   i       ⁡     (   v   )       =         r   s     ⁢   cos   ⁢           ⁢   Δ   ⁢           ⁢   cos   ⁢           ⁢     δ   2     ⁢     S     0   ,   1         +       r   s     ⁢   sin   ⁢           ⁢   Δ   ⁢           ⁢   sin   ⁢           ⁢     δ   2     ⁢     (       cos   ⁢           ⁢   2   ⁢           ⁢   α   ⁢           ⁢     S     1   ,   1         +     sin   ⁢           ⁢   2   ⁢           ⁢   α   ⁢           ⁢     S     2   ,   1           )       +       1   2     ⁢       r   s     ⁡     [         (       cos   ⁢           ⁢     δ   2     ⁢     S     1   ,   1         -     sin   ⁢           ⁢     δ   2     ⁢   sin   ⁢           ⁢   2   ⁢           ⁢   α   ⁢           ⁢     S     3   ,   1           )     ⁢     cos   ⁡     (     Δ   -     φ   2       )         +     sin   ⁢           ⁢     δ   2     ⁢   cos   ⁢           ⁢   2   ⁢           ⁢   α   ⁢           ⁢     S     0   ,   1       ⁢     sin   ⁡     (     Δ   -     φ   2       )           ]         +       1   2     ⁢       r   s     ⁡     [         (       cos   ⁢           ⁢     δ   2     ⁢     S     1   ,   1         -     sin   ⁢           ⁢     δ   2     ⁢   sin   ⁢           ⁢   2   ⁢           ⁢   α   ⁢           ⁢     S     3   ,   1           )     ⁢     cos   ⁡     (     Δ   +     φ   2       )         +     sin   ⁢           ⁢     δ   2     ⁢   cos   ⁢           ⁢   2   ⁢           ⁢   α   ⁢           ⁢     S     0   ,   1       ⁢     sin   ⁡     (     Δ   +     φ   2       )           ]         +       1   4     ⁢       r   s     ⁡     [         (       cos   ⁢           ⁢     δ   2     ⁢     S     2   ,   1         +     sin   ⁢           ⁢     δ   2     ⁢   cos   ⁢           ⁢   2   ⁢           ⁢   α   ⁢           ⁢     S     3   ,   1           )     ⁢     cos   ⁡     (     Δ   -     φ   2     +     φ   1       )         +       {       sin   ⁢           ⁢     δ   2     ⁢   sin   ⁢           ⁢   2   ⁢           ⁢     α   ⁡     (       S     0   ,   1       +     S     1   ,   1         )         -     sin   ⁢           ⁢     δ   2     ⁢   cos   ⁢           ⁢   2   ⁢           ⁢   α   ⁢           ⁢     S     2   ,   1         +     cos   ⁢           ⁢     δ   2     ⁢     S     3   ,   1           }     ⁢     sin   ⁡     (     Δ   -     φ   2     +     φ   1       )           ]         +       1   4     ⁢       r   s     ⁡     [         (       cos   ⁢           ⁢     δ   2     ⁢     S     2   ,   1         +     sin   ⁢           ⁢     δ   2     ⁢   cos   ⁢           ⁢   2   ⁢           ⁢   α   ⁢           ⁢     S     3   ,   1           )     ⁢     cos   ⁡     (     Δ   +     φ   2     -     φ   1       )         +       {       sin   ⁢           ⁢     δ   2     ⁢   sin   ⁢           ⁢   2   ⁢           ⁢     α   ⁡     (       S     0   ,   1       +     S     1   ,   1         )         +     sin   ⁢           ⁢     δ   2     ⁢   cos   ⁢           ⁢   2   ⁢           ⁢   α   ⁢           ⁢     S     2   ,   1         -     cos   ⁢           ⁢     δ   2     ⁢     S     3   ,   1           }     ⁢   sin   ⁢     (     Δ   -     φ   2     -     φ   1       )         ]         -       1   4     ⁢       r   s     ⁡     [         (       cos   ⁢           ⁢     δ   2     ⁢     S     2   ,   1         +     sin   ⁢           ⁢     δ   2     ⁢   cos   ⁢           ⁢   2   ⁢           ⁢   α   ⁢           ⁢     S     3   ,   1           )     ⁢     cos   ⁡     (     Δ   +     φ   2     +     φ   1       )         +       {       sin   ⁢           ⁢     δ   2     ⁢   sin   ⁢           ⁢   2   ⁢           ⁢     α   ⁡     (       S     0   ,   1       +     S     1   ,   1         )         -     sin   ⁢           ⁢     δ   2     ⁢   cos   ⁢           ⁢   2   ⁢           ⁢   α   ⁢           ⁢     S     2   ,   1         +     cos   ⁢           ⁢     δ   2     ⁢     S     3   ,   1           }     ⁢     sin   ⁡     (     Δ   +     φ   2     +     φ   1       )           ]                   (   3   )             
 
 for the interference signal. Fourier transform of equation (3) gives seven components in the positive optical path length difference domain which are centered at Δ, Δ±φ 2 , Δ±(φ 2 −φ 1 ), Δ±(φ 2 +φ 1 ), respectively. Inverse Fourier transforms of each component are as follows.  
             Δ   ⁢     :     ⁢     1   2     ⁢     r   s     ⁢     ⅇ   ⅈΔ     ⁢     {       cos   ⁢           ⁢     δ   2     ⁢     S     0   ,   1         -     i   ⁢           ⁢   sin   ⁢           ⁢     δ   2     ⁢     (       cos   ⁢           ⁢   2   ⁢           ⁢   α   ⁢           ⁢     S     1   ,   1         +     sin   ⁢           ⁢   2   ⁢           ⁢   α   ⁢           ⁢     S     2   ,   1           )         }             (   4   )               Δ   +       φ   2     ⁢     :     ⁢     1   4     ⁢     r   s     ⁢     ⅇ     ⅈφ   ⁢           ⁢   2       ⁢     ⅇ   ⅈΔ     ⁢     {       (       cos   ⁢           ⁢     δ   2     ⁢     S     1   ,   1         -     sin   ⁢           ⁢     δ   2     ⁢   sin   ⁢           ⁢   2   ⁢           ⁢   α   ⁢           ⁢     S     3   ,   1           )     -     i   ⁢           ⁢   sin   ⁢           ⁢     δ   2     ⁢   cos   ⁢           ⁢   2   ⁢           ⁢   α   ⁢           ⁢     S     0   ,   1           }               (   5   )               Δ   +     φ   2     -       φ   1     ⁢     :     ⁢     1   8     ⁢     r   s     ⁢     ⅇ     ⅈ   ⁡     (       φ   2     -     φ   1       )         ⁢       ⅇ   ⅈΔ     ⁡     [       (       cos   ⁢           ⁢     δ   2     ⁢     S     2   ,   1         +     sin   ⁢           ⁢     δ   2     ⁢   cos   ⁢           ⁢   2   ⁢           ⁢   α   ⁢           ⁢     S     3   ,   1           )     -     i   ⁢     {       sin   ⁢           ⁢     δ   2     ⁢   sin   ⁢           ⁢   2   ⁢           ⁢     α   ⁡     (       S     0   ,   1       -     S     1   ,   1         )         +     sin   ⁢           ⁢     δ   2     ⁢   cos   ⁢           ⁢   2   ⁢           ⁢   α   ⁢           ⁢     S     2   ,   1         -     cos   ⁢           ⁢     δ   2     ⁢     S     3   ,   1           }         ]                 (   6   )               Δ   +     φ   2     +       φ   1     ⁢     :       -       1   8     ⁢     r   s     ⁢     ⅇ     ⅈ   ⁡     (       φ   2     +     φ   1       )         ⁢       ⅇ   ⅈΔ     ⁡     [       (       cos   ⁢           ⁢     δ   2     ⁢     S     2   ,   1         +     sin   ⁢           ⁢     δ   2     ⁢   cos   ⁢           ⁢   2   ⁢           ⁢   α   ⁢           ⁢     S     3   ,   1           )     -     i   ⁢     {       sin   ⁢           ⁢     δ   2     ⁢   sin   ⁢           ⁢   2   ⁢           ⁢     α   ⁡     (       S     0   ,   1       +     S     1   ,   1         )         -     sin   ⁢           ⁢     δ   2     ⁢   cos   ⁢           ⁢   2   ⁢           ⁢   α   ⁢           ⁢     S     2   ,   1         +     cos   ⁢           ⁢     δ   2     ⁢     S     3   ,   1           }         ]                 (   7   )             
 
 Comparing with equation (2), real part of equation (4) gives S 0,i /4 and real part of equation of (5) after shifting the phase by −φ 2  gives S 1,i /8. Likewise, S 2,i /8 and S 3,i /8 can be obtained by taking the real part of subtraction of (7) from (6) and the imaginary part of addition of (6) and (7) after the appropriate phase shift, −(φ 2 −φ 1 ) and −(φ 2 +φ 1 ) for (6) and (7), respectively. Moreover, simple arithmetic gives phase retardation due to the birefringence of the sample, δ, without knowledge of incident polarization state. The real part of (4), imaginary part of (5), the imaginary part of subtraction of (7) from (6) are  
               1   2     ⁢     r   s     ⁢   cos   ⁢           ⁢     δ   2     ⁢     S     0   ,   1               (   8   )                 -     1   4       ⁢     r   s     ⁢   sin   ⁢           ⁢     δ   2     ⁢   cos   ⁢           ⁢   2   ⁢           ⁢   α   ⁢           ⁢     S     0   ,   1               (   9   )                 -     1   4       ⁢     r   s     ⁢   sin   ⁢           ⁢     δ   2     ⁢   sin   ⁢           ⁢   2   ⁢           ⁢   α   ⁢           ⁢     S     0   ,   1               (   10   )             
 
 after the phase shift by −Δ, −(Δ+φ 2 ), −(Δ+φ 2 −φ 1 ) and −(Δ+φ 2 +φ 1 ), respectively. With a trigonometric identity, the following can be obtained  
               tan   ⁢           ⁢     δ   2       =         2   ⁢           (   9   )     2     +       (   10   )     2             (   8   )       .             (   11   )             
 
         [0154]     Phase retardation due to birefringence [ FIG. 36 ] and fast-axis angle [ FIG. 37 ] of the birefringent sample were estimated from interference between the back surface of the glass window and the back surface of the birefringent sample by using Eqs. above. For this measurement, the birefringent sample was rotated in 5° increments from 0° to 90°. An estimated single-pass phase retardation of 34.06°±2.68° is consistent with a value deduced from the manufacturer&#39;s specification (31.4°). The estimated fast-axis angle is shown in  FIG. 4 ( b ) and is plotted with respect to orientation of the birefringent sample.  
         [0155]     The results show practical demonstration of polarization multiplexing.  
         [0156]     B. Space or Lateral Position: The additional spectral cells may be used to record information in the space or lateral position domain using a system indicated below. 
    1. Existing Multifiber Approach: (described above)     2. Spatially Scanned Light:    
 
         [0159]     The schematic of the experimental setup of a fiber-based spatially multiplexed swept source OCT (SM-SS-OCT) system is depicted in  FIG. 32  using the system described in PCT patent application number PCT/US2004/012773, incorporated by reference herein, where the top is preferably rotated at least 100 times for each position.  
         [0160]     A tunable laser and spectrum analyzer (TLSA 1000, Precision Photonics, Inc.) that operates in the 1520-1620 nm wavelength range (λ 0 =1570 nm) with FWHM spectral line width specified at 150 KHz is used as the illuminating source and is equipped with an optical isolator to protect the laser from spurious reflections. The laser output is coupled into one arm of a 2×2 fiber-based coupler (interferometer). The 50%-50% coupler splits this beam into two nearly equal parts, used in the reference and sample arms, respectively. The reference arm has a fixed path length, and simply consists of a fixed mirror that reflects the entire light incident upon it back into the fiber-based coupler. The light exiting the sample arm of the interferometer is collimated, and scanned across the sample by a scanning galvanometer and a focusing lens. The scanning galvanometer and focusing lens is used to rapidly scan the lateral positions of the tissue. The TLSA 1000 completes one complete wavelength sweep in approximately one second. Within this time, the galvanometer is programmed to sweep all lateral positions of the tissue several hundred times. Light returning from the sample interferes with the light from the fixed reference in the fiber-based interferometer, and the resultant spectral interference signal (due to path length variations between sample and reference reflections) is detected by a photodetector placed in the detection arm of the system. The electrical output is digitized, and a non-uniform Fourier Transform (NUFT) of each A-line spectral data gives the depth profile of the sample reflectance.  FIGS. 34 and 35  are images of a 100 micron thick slide recorded with the spatially multiplexed OCT system. The images are of the same object (microscope cover glass) only for one image ( FIG. 34 ) the intensity of the light returning from the sample is displayed on a linear greyscale while in the other image ( FIG. 35 ) is displayed according to logarithm of the intensity.  
         [0161]     C. Angle: The additional spectral cells may be used to record information in the angle domain using a system indicated in  FIG. 33 .  
         [0162]      FIG. 33  depicts a Multi Fiber Angle-domain OCT system. The output of the frequency-swept source A is split into n fibers through the splitter B. The light passes through the circulators C, is collimated, focused through a lens, contacts the tissue, and then is reflected into any of the multiplicity of fibers. A reference reflector for each path is introduced into each fiber segment. For example, the reference reflector can be positioned at the terminal end of each fiber segment. For each i&#39;th input fiber segment, interference is formed between light backscattered from the tissue and into the j&#39;th fiber and the reference reflection from the j&#39;th fiber. For N fibers, N 2  interference fringes are formed each corresponding to an incident (α i ) and backscattered angle (β j ). Light intensity in the spectral domain is then converted to a voltage through a photoreceiver, which outputs to an ADC board, which is read into a computer. This system allows phase-sensitive angle resolved imaging of discrete light paths in and out-of the specimen. Using a space-spatial frequency transformation (e.g., two-dimensional Fourier transformation) lateral structures can be imaged with sub-wavelength resolution.  
         [0163]     D. Space-Angle combinations (e.g. x dimension−space, y dimension−angle): The space and angle dimensions may be combined to form systems that use the additional spectral cells image both space and angles. For example, additional spectral cells may be used to record position information in one dimension (e.g. x) and angle information in the orthogonal dimension (y).  
         [0164]     Although the invention has been described in detail in the foregoing embodiments for the purpose of illustration, it is to be understood that such detail is solely for that purpose and that variations can be made therein by those skilled in the art without departing from the spirit and scope of the invention except as it may be described by the following claims.

Technology Category: 1