Patent Publication Number: US-8976363-B2

Title: System aspects for a probe system that utilizes structured-light

Description:
CROSS-REFERENCE TO RELATED APPLICATIONS 
     This application is a Continuation of and claims priority from U.S. Ser. No. 12/249,513, now U.S. Pat. No. 8,107,083, filed Oct. 10, 2008 entitled System Aspects for a Probe System that Utilizes Structured-Light which is incorporated herein by reference. 
    
    
     BACKGROUND OF THE INVENTION 
     1. Field of the Invention 
     The subject matter described herein relates generally to borescopes and endoscopes, and more particularly, to a borescope/endoscope which provides 3D surface mapping and dimensional measurement. 
     2. Related Art 
     Borescopes and endoscopes are typically used for inspection inside a remote cavity. Most borescopes/endoscopes, referred to herein as a probe, employ an external light source coupled to fiber optic bundles in the probe to provide illumination of a remote object or surface at the distal end. When the object is illuminated, an internal image is formed by a lens system on an image sensor, and the image is relayed to a connected display, such as a video screen. The image sensor may be located at the proximal end of the probe, as with an optical rigid borescope or fiberscope, or at the distal end as with a video borescope or endoscope. Such systems are often used to inspect inaccessible locations for damage or wear or to verify that parts have been properly manufactured or assembled. Among other things, it is desirable to obtain dimensional measurements to verify that damage or wear does not exceed an operational limit or that a manufactured part or assembly meets its specifications. It may also be desirable to produce a 3D model or surface map for comparison to a reference, 3D viewing, reverse engineering, or detailed surface analysis. 
     Phase-shift technology is well suited to addressing these measurement needs, but its implementation in a borescope or endoscope presents numerous system-level challenges. It is desirable to address these challenges in a manner that yields a reliable and easy-to-use system. 
     BRIEF DESCRIPTION OF THE INVENTION 
     In accordance with an embodiment of the present invention, a probe system comprises an imager and an inspection light source. The probe system is configured to operate in an inspection mode and a measurement mode. During inspection mode, the inspection light source is enabled. During measurement mode, the inspection light source is disabled, and a structured-light pattern is projected. The probe system is further configured to capture at least one measurement mode image. In the at least one measurement mode image, the structured-light pattern is projected onto an object. The probe system is configured to utilize pixel values from the at least one measurement mode image to determine at least one geometric dimension of the object. 
     In another embodiment of the invention, a probe system comprises an imager, and the probe system is configured to operate in an inspection mode and a measurement mode. Diffuse illumination light is projected during inspection mode, and a structured-light pattern is projected during measurement mode. The probe system is further configured to capture at least one measurement mode image. In the at least one measurement mode image, the structured-light pattern is projected onto an object. The probe system is configured to utilize pixel values from the at least one measurement mode image to determine at least one geometric dimension of the object. The probe system is also configured to detect relative movement between a probe and the object between captures of two or more of a plurality of images. 
    
    
     
       BRIEF DESCRIPTION OF THE DRAWINGS 
       The following detailed description is made with reference to the accompanying drawings, in which: 
         FIG. 1  is a schematic diagram of a borescope/endoscope system in accordance with an embodiment of the present invention. 
         FIG. 2  is a graph showing the trajectory of an exemplary projection set projected from one side of the FOV. 
         FIG. 3  is a graph showing the trajectory of the structured-lines of one fringe set in each of a first and second exemplary projection set relative to a field of view. 
         FIG. 4  is a flow chart illustrating an exemplary embodiment of the steps involved in motion detection. 
         FIG. 5  is flow chart illustrating an exemplary alternative embodiment of the steps involved in motion detection. 
         FIG. 6  is a flow chart illustrating an exemplary embodiment of the steps involved during an image capture sequence of the present invention. 
     
    
    
     DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT 
     Illustrated in  FIG. 1 , a borescope/endoscope system or probe system  10  according to an embodiment of the invention is shown. An insertion tube  40  comprises elongated portion  46  and detachable distal tip  42 . Elongated portion  46  comprises a main long, flexible portion, a bending neck, and a camera head. Delineation line  41  shows where the camera head starts on elongated portion  46 . The camera head of elongated portion  46  typically includes at least imager  12 , electronics  13 , and probe optics  15 . Detachable distal tip  42  typically attaches to the camera head of elongated portion  46 , mentioned above. Detachable distal tip  42  contains viewing optics  44  which are used in combination with probe optics  15  to guide and focus light received from the viewed surface or object (not shown) onto imager  12 . 
     The elements shown in tip  42  could alternatively be located on elongated portion  46 . These elements include viewing optics  44 , at least one emitter module  37 , at least one intensity-modulating element  38 , and light passing element  43 . In addition, the at least one light emitter module  37 , comprising a plurality of light emitters, could be fixedly attached to insertion tube  40  while the at least one intensity-modulating element is disposed on detachable tip  42 . In this case, precise and repeatable alignment between detachable tip  42  and elongated portion  46  is required, but it is advantageous because allows different fields of view while eliminating the need for contacts between elongated portion  46  and detachable tip  42 . 
     Shown in  FIG. 1 , imager  12  is located at the distal end of insertion tube  40 . Alternatively, imager  12  may be located at the proximal end of insertion tube  40 . The alternative configuration may be suitable, for example, in a rigid borescope or fiberscope. 
     Imager  12  obtains at least one image of the viewed surface. Imager  12  may comprise, for example, a two-dimensional array of light-sensitive pixels that outputs a video signal in response to the light level sensed at each pixel. Imager  12  may comprise a charge-coupled device (CCD), complementary metal-oxide-semiconductor (CMOS) image sensor, or other devices of similar function. The video signal is buffered by electronics  13  and transferred to imager interface electronics  31  via signal line  14 . Imager interface electronics  31  may include, for example, power supplies, a timing generator for generating imager clock signals, an analog front end for digitizing the imager video output signal, and a digital signal processor (DSP)  51  for processing the digitized imager video data into a more useful format for video processor  50 . 
     Video processor  50  performs various functions not limited to image capture, image enhancement, graphical overly merging, and video format conversion and stores information relating to those functions in video memory  52 . Video processor  50  may comprise field-programmable gate array (FPGA), camera DSP, or other processing elements and provides information to and receives information from central processing unit (CPU)  56 . The provided and received information may relate to commands, status information, video, still images, and/or graphical overlays. Video processor  50  also outputs signals to various monitors such as computer monitor  22 , video monitor  20 , and integral display  21 . Video processor  50  also comprises motion detection module  53  and/or fringe contrast determining function  54 . Alternatively, CPU  56  or microcontroller  30 , described below, or probe electronics  48  comprising camera control electronics (not shown), may include motion detection module  53 . 
     When connected, each of computer monitor  22 , video monitor  20 , and/or integral display  21  typically display images of the object or surface under inspection, menus, cursors, and measurement results. Computer monitor  22  is typically an external computer type monitor. Similarly, video monitor  20  typically includes an external video monitor. Integral display  21  is integrated and built into probe system  10  and typically comprises a liquid crystal display (LCD). 
     CPU  56  preferably uses both program memory  58  and non-volatile memory  60 , which may include removable storage devices. CPU  56  may also use volatile memory such as RAM for program execution and temporary storage. A keypad  64  and joystick  62  convey user input to CPU  56  for such functions as menu selection, cursor movement, slider adjustment, and articulation control. Computer I/O interface  66  provides various computer interfaces to CPU  56  such as USB, Firewire, Ethernet, audio I/O, and wireless transceivers. Additional user devices such as a keyboard or mouse may be connected to computer I/O interface  66  to provide user control. CPU  56  generates graphical overlay data for display, provides recall functions and system control, performs phase-shift analysis and measurement processing, and provides image, video, and audio storage. CPU  56  and the previously discussed video processor  50  may be combined into one element of probe system  10 . In addition, components of probe system  10  including, but not limited to, CPU  56  and video processor  50  may be integrated and built into probe system  10  or, alternatively, be externally located. 
     Referring to the at least one emitter module  37 , light from the at least one emitter module  37  projects at least one structured-light pattern on the surface suitable for phase-shift analysis. The structured-light pattern preferably comprises parallel light and dark lines comprising sinusoidal intensity profiles. Line patterns having square, trapezoidal, triangular, or other profiles may be projected on the surface as well when used with appropriate phase-shift analysis to determine phase of the pattern. The pattern may also comprise other than straight, parallel lines. For example, curved lines, wavy lines, zigzagging lines, or other such patterns may be used with appropriate analysis. 
     The structured-light pattern projected from the at least one emitter module  37  may be created a number of ways. Emitter module  37  may comprise at least one light emitting element formed to include appropriate parallel light and dark lines. Light from the light emitting element may be passed through intensity modulating element  38 . Alternatively, emitter module  37  may comprise a plurality of light emitters. The plurality of light emitters may be strategically positioned to form a structured-light pattern on the surface and/or light from the plurality of light emitters may be passed through intensity modulating element  38 . In an embodiment of the present invention, intensity modulating element  38  comprises a line grating, which creates a structured-light pattern when light from emitter module  37  passes through to the surface or object (not shown). 
     A plurality of fringe sets are projected from the probe onto the viewed surface or object. A fringe set comprises at least one structured-light pattern. The structured-light pattern of one fringe set exhibits a spatial or phase-shift relative to the structured-light patterns of other fringe sets. The structured-light pattern preferably comprises parallel light and dark lines comprising sinusoidal intensity profiles. Line patterns having square, trapezoidal, triangular, or other profiles may be projected on the surface as well when used with appropriate phase-shift analysis to determine phase of the pattern. The pattern may also comprise other than straight, parallel lines. For example, curved lines, wavy lines, zigzagging lines, or other such patterns may be used with appropriate analysis. 
     When emitter module  37  comprises a plurality of light emitters, a fringe set comprises a structured-light pattern projected when one emitter group comprising a group of at least one light emitter is emitting light. In other words, a different subset of the plurality of light emitters emits light to project each of a plurality of structured-light patterns. The plurality of light emitters of emitter module  37  are positioned such that the structured-light pattern projected when one emitter group is emitting light exhibits a spatial or phase-shift relative to the structured-light patterns projected when other emitter groups are emitting light. 
     Light from the plurality of light emitters disposed on detachable tip  42  is passed through at least one intensity modulating element  38  to alter the distribution of light and project at least one structured-light pattern on the viewed surface suitable for phase-shift analysis. In one embodiment, the plurality of light emitters comprising an emitter group are spaced apart along the axis perpendicular to the lines on the line grating by a distance equal to an integer number of periods of the line grating. As a result, when the plurality of light emitters comprising one emitter group are simultaneously emitting light, the structured-light patterns produced by each of the multiple emitters sum together. This forms a brighter line pattern than would be generated by a single emitter element. 
     In another embodiment, the plurality of light emitters in an emitter group are arranged in a line parallel to the lines on the line grating and are electrically connected in series. This approach reduces the current needed to achieve a given light output relative to the current that would be required with a single emitter. This is beneficial as the emitter power is generally supplied through small wires having significant resistance, and reducing the drive current reduces the power dissipated in the wires and supplied by the emitter drive circuit. 
     A plurality of light emitting diodes (LEDs) may comprise the plurality of light emitters of the at least one emitter module  37 . LEDs are practical in probe system  10  at least because LEDs offer consistent, uniform illumination, no speckling, and fast switching between fringe sets. However, any light emitting source(s) offering the qualities mentioned above are sufficient for use in probe system  10 . Other such light sources include, but are not limited to, organic LEDs, plasma elements, fiber coupled lasers, and laser arrays. 
     The at least one emitter module  37  on detachable tip  42  may further comprise electronics for control/sequencing of emitters, sensing temperature, and storage/retrieval of calibration data. The at least one emitter module  37  may include a heat sink made of a ceramic or metal, for example, to reduce the temperature rise of the plurality of light emitters. 
     System  10  further comprises contacts  36  that electrically couple elongated portion  46  to detachable tip  42  through the camera head. Contacts  36  may be spring loaded and also provide electrical power from drive conductor  35  to emitter module  37 . In an embodiment of the invention, drive conductor  35  carries power from emitter drive  32  to the plurality of light emitters disposed on the distal end of insertion tube  40 . Drive conductor  35  comprises one or more wires and may be incorporated with signal line  14  in a common outer jacket (not shown). Drive conductor  35  may also share conductors with signal line  14  and/or utilize the insertion tube  40  structure for carrying current. Emitter drive  32  includes, for example, an adjustable current source with a variable on time to compensate for light emitters with differing power capabilities and efficiencies. 
     Discussed above, video processor  50  or CPU  56  comprises a brightness or fringe contrast determining function  54  to determine whether one emitter or multiple emitters should be enabled for each emitter group. In an embodiment of the present invention, brightness determining function  54  communicates with emitter drive  32  to selectively transmit current through specific wires connected to emitter module  37  to light an appropriate number of emitters per emitter group. Further control over brightness can be achieved by varying the drive level applied to the emitters or the duration of time the emitters are driven. 
     When brightness determining function  54  is located separately from emitter drive  32  one drive wire of drive conductor  35  connects emitter drive  32  to emitter module  37 , and one or more control wires (not shown) controlled by brightness determining function  54  are also connected to emitter module  37 . A circuit (not shown) included on emitter module  37  can selectively connect one or multiple emitters to the drive wire in response to signals on the control wire. Alternatively, when emitter drive  32  comprises brightness determining function  54 , drive conductor  35  comprises one or more drive wires (not shown) per emitter. In this case, brightness determining function  54  selectively transmits current through specific drive wires of drive conductor  35  to light an appropriate number of emitters per emitter group. 
     In an embodiment of the invention, at least one calibrating-light pattern is projected onto the viewed surface or object. Projecting light from at least one of the plurality of light emitters may be used to create the at least one calibrating-light pattern on the surface or object. The calibrating-light pattern may comprise at least one structured-light pattern, and passing light from at least one of the plurality of light emitter through intensity modulating element  38  may create at least one calibrating-light pattern on the object. The calibrating-light pattern may include, but is not limited to, angled lines, a single line, a plurality of lines, a dot, a plurality of dots, and a plurality of parallel light and dark lines. It can be appreciated that fringe sets&#39;and calibrating-light patterns may be projected from the same emitter module  37 . This may be accomplished, for example, by spacing apart fringe set emitters and calibrating pattern emitters and passing light from them through separate areas of intensity modulating element  38 . 
     In another embodiment of the present invention, a first projection set and a second projection set is projected onto a surface. A projection set comprises at least one fringe set comprising a structured-light pattern. When a projection set comprises a plurality of fringe sets, the structured-light pattern of one fringe set of the first projection set exhibits a phase-shift relative to the structured-light patterns of the other fringe sets of the first projection set. Similarly, the structured-light pattern of one fringe set of the second projection set exhibits a phase-shift relative to the structured-light patterns of other fringe sets of the second projection set. Typically, the first projection set is projected from one side of viewing optics  44  and the second projection set is projected from the other side of viewing optics  44 . Depending on the configuration of detachable tip  42 , a first projection set may alternatively be projected from the top of viewing optics  44  and a second projection set may be projected from the bottom of viewing optics  44 , or vise versa. Even if insertion tube  40  is rotated, the first and second projection sets are projected from opposite positions or angles relative to the FOV. Therefore, the first projection set may be projected from any position or angle around viewing optics  44  that is opposite that of the second projection set. 
     Fringe sets  0 ;  1 , and  2  of  FIG. 2  comprise an exemplary projection set. In the case of  FIG. 2 , a plurality of fringe sets comprise the projection set. When a projection set comprises a plurality of fringe sets, the plurality of fringe sets comprising the projection set are typically projected from approximately the same origin relative to the FOV. 
     To further illustrate this,  FIG. 3  shows a graph of two fringe sets. Each fringe set is a projection from opposite sides of the FOV. The fringe set in  FIG. 3  represented by the solid lines projected from one side of the FOV comprises a first projection set, while the fringe set in  FIG. 3  represented by the dashed lines projected from the other side of the FOV comprises a second projection set. Regarding the exemplary case of  FIG. 3 , only one fringe set per each projection set is shown; however a plurality of fringe sets may comprise each projection set. In an embodiment of the invention, a projection set comprises a plurality of fringe sets, each fringe set comprising a structured-light pattern, wherein the light pattern of one fringe set exhibits a phase-shift relative to the light patterns of the other fringe sets. When a first projection set and a second projection set are projected, a first image set and a second image set are captured. The first image set comprises fringe set images of the first projection set, and the second image set comprises fringe set images of the second image set, where one fringe set is projected onto the surface or object per image. 
     The probe operates in measurement mode when the at least one structured-light pattern is projected onto the surface. In an embodiment of the invention, emitter module  37  is enabled to project at least one structured-light pattern on the surface during measurement mode. During measurement mode, CPU  56  or video processor  50  captures a plurality of measurement mode images wherein the at least one structured-light pattern is projected onto the object. The measurement mode images may comprise fringe sets where no more than one fringe set is projected onto the object per measurement mode image. Measurement mode images of that sort are also referred to herein as fringe set images. Phase-shift analysis may then be performed directly on the plurality of fringe set images. 
     The probe operates in inspection mode when inspection light source  23  is enabled. Light is projected from inspection light source  23  onto a surface or object. During inspection mode, the at least one structured-light pattern may be absent. Generally, at least one image, referred to herein as an inspection mode image, is captured when light is projected from inspection light source  23  onto the viewed surface or object. Inspection light source  23  outputs relatively uniform light or diffuse illumination light from the distal end of insertion tube  40 . The elements that produce and deliver light during inspection mode may collectively be referred to as an inspection light delivery system. In one embodiment, the inspection light delivery system comprises inspection light source  23 , source fiber bundle  24 , shutter mechanism  34 , probe fiber bundle  25 , and light passing element  43 . In other embodiments, the inspection light delivery system may comprise very different elements such as, in the case of distally-located white LEDs, an LED drive circuit that can be disabled or provides an adjustable output current, wires for delivering power to the LEDs, the LEDs themselves, and a protective element to protect the LEDs. In another embodiment, the inspection light delivery system comprises a proximal LED coupled to a fiber bundle, which delivers light to the distal end of insertion tube  40 , and an LED drive circuit. 
     Referring again to measurement mode, the intensity of light output from the inspection mode light delivery system originating from light source  23  is automatically decreased or disabled during measurement mode to avoid reducing the contrast of the at least one projected structured-light pattern. For example, CPU  56  may be configured to give an original command to turn off light source  23  electronically prior to projecting the at least one structured-light pattern through an enable/disable input to light source  23 . Inspection light source  23  may then be automatically enabled, for example, electronically after a plurality of measurement mode images are captured or upon exiting measurement mode. 
     Similarly, CPU  56  may also be configured to give an original command to turn on or off light from the inspection delivery system through the use of shutter mechanism  34 . Shutter mechanism  34  is configured to allow light output from the inspection light delivery system during inspection mode or regular inspection and block or otherwise inhibit light output originating from inspection light source  23  during measurement mode. Shutter mechanism  34  includes, for example, a solenoid or motor driven mechanical shutter or an electric light source disabler. When shutter mechanism  34  allows light from inspection light source  23  to pass, shutter mechanism  34  is in an open position. When shutter mechanism  34  blocks light from inspection light source  23 , shutter mechanism  34  is in a closed position. During inspection mode, shutter mechanism  34  is configured to be in an open position. In contrast, during fringe set projection, shutter mechanism  34  is configured to be in a closed position. The location of shutter mechanism  34  can vary based on its implementation. In an embodiment of the invention, when shutter mechanism  34  allows light to pass, probe fiber bundle  25  delivers light to the surface or inspection site via light passing element  43 . 
     Inspection light source  23  is typically a white light source, but may comprise any appropriate light source for a probe such as a mercury or metal halide arc lamp, halogen lamp, laser/phosphor system, or LED based light source which could be either proximally or distally located. When a fiber based light source is used, source fiber bundle  24  may be included in system  10 . Source fiber bundle  24  comprises a non-coherent or semi-coherent fiber optic bundle and transmits light to shutter mechanism  34 . Alternatively, source fiber bundle  24  may be omitted, and shutter mechanism  34  may be located directly between inspection light source  23  and probe fiber bundle  25 . Probe fiber bundle  25  comprises a non-coherent fiber optic bundle. Light passing element  43  comprises a glass cane, formed fibers, and/or distribution control features such as lenses or a diffuser. 
     In some cases, projected light patterns in captured measurement mode images can be distracting and can make it more difficult for operators to see details on the viewed object. It is thus desirable to allow the operator to view a normal inspection mode image while placing measurement cursors rather than a measurement mode image that includes one or more structured-light patterns. Preferably, at least one counterpart inspection mode image and at least one counterpart measurement mode images are captured. The at least one counterpart measurement mode image comprises at least one of the plurality of measurement mode images, and the at least one counterpart inspection mode image comprises at least one inspection mode image captured in close time proximity to the at least one counterpart measurement mode image. Inspection mode images and measurement mode images captured in close proximity are referred to herein as counterpart images. Ideally, counterpart images comprise images of an object in the same position relative to the FOV. 
     Capturing counterpart images in close time proximity is advantageous at least because the relative movement between the probe&#39;s distal tip and the viewed object between the captures the counterpart images is minimized. Geometrical features, such as defects and edges, will appear in the same position in the counterpart images so that the locations of cursors positioned on an inspection-mode image correspond to the same points on the viewed object in the measurement-mode images. In an embodiment of the invention, motion detection module  53  analyzes inspection mode and measurement mode counterpart images. 
     Motion detection module  53  may be configured to analyze the images once all of the images have been captured. Alternatively, motion detection module  53  may be configured to analyze the images sequentially after the capture of each image. Motion detection module  53  is configured to automatically detect probe and/or surface movement between measurement mode images, also referred to herein as fringe set images or the images captured comprising structured-light patterns. Motion detection module  53  may be configured to compare only inspection mode images or only measurement mode images. Furthermore, motion detection module  53  may optionally be configured to compare at least one measurement mode image with its counterpart inspection mode image(s). In an embodiment of the invention, counterpart inspection mode image(s) may be captured at the beginning and/or the end of its counterpart measurement mode capture sequence. 
     Motion detection module  53  could be further configured to compare one or more captured images from each of two or more successive measurement mode capture sequences such that images having the same illumination and/or structured light patterns present may be compared rather than attempting to compensate for differences in pattern position or illumination. The term “measurement mode capture sequence” used herein is defined as the capture of a plurality of structured-light images, each captured image comprising one projected fringe set. During a measurement mode capture sequence a plurality of measurement mode images are captured. 
     Probe system  10  is configured to detect relative movement between the probe and the surface or object between the captures of two or more of a plurality of images. In an embodiment of the invention, motion detection module  53  is configured to analyze the images captured and compute a motion metric indicative of relative movement between the probe&#39;s distal tip and the surface or object between the captures of two or more of a plurality of images. These images may comprise the first and the last of a plurality of images. The first of the plurality of images is either an inspection mode image or a measurement mode image. Similarly, the last of the plurality of images is either an inspection mode image or a measurement mode image. If the motion metric indicates a high probability of movement, the capture of the plurality of images is repeated until either the motion metric indicates a low probability of movement or a pre-determined timeout occurs. For example, if the motion metric indicates a high probability of movement between counterpart measurement mode and inspection mode images, the capture of the measurement mode and inspection mode image(s) is repeated until the motion metric indicates a low probability of movement or a pre-determined timeout occurs. However, re-capture of the entire plurality of images may not always be necessary. 
     The value of the motion metric can depend upon the implementation of motion detection. The metric could be pixels of movement, in which case, the metric may be limited to a one pixel movement, for example, for indicating a low probability of movement. In that case any metric representing a movement greater than one pixel would indicate a high probability of movement. The metric limit for a low probability of movement could also be experimentally determined. Among others, one method for experimentally determining metric limits includes using a root mean square (RMS) difference between brightness values. 
       FIG. 4  is a flow chart illustrating an exemplary embodiment of the steps involved in motion detection. Borescope/endoscope or probe system  10  shown in  FIG. 1  is configured to perform the steps indicated in method  400 . Method  400  may be implemented when probe system  10  is in inspection mode, and the CPU  56  receives a command requesting measurement. An operator may request measurement by pressing a button (not shown) on the probe system  10  or selecting a menu item from, for example, integral display  21 . 
     Once the measurement command is received, at step  402 , CPU  56  or video processor  50  captures a first inspection mode image. CPU  56  then sends a command to microcontroller  30  to enter measurement mode. Microcontroller  30  controls emitter drive  32  to perform a measurement mode capture sequence. At step  404 , CPU  56  or video processor  50  captures measurement mode images. At least one measurement mode image is captured per structured-light pattern or fringe set. An operator may pre-program the specifics of the measurement mode capture sequence before the implementation of method  400  by selecting a menu item from integral display  21 . For example, the operator may desire the capture of a plurality of measurement mode images per structured-light pattern or fringe set. In addition, those images of the same structured-light pattern or fringe set may be captured at the same brightness level or at different brightness levels depending on the analysis and/or mapping desired. 
     After the measurement mode images are captured, emitter drive  32  is disabled by microcontroller  30 , and microcontroller  30  configures DSP  51  for inspection mode. At step  406 , CPU  56  or video processor  50  captures a second inspection mode image. Motion detection module  53  then analyzes the first and second inspection mode images to determine a motion metric at step  408 . If the motion metric indicates an unacceptable degree of motion, and the pre-set time limit is not reached, steps  402 - 412  are repeated until the motion metric indicates an acceptable degree of motion or the pre-set time limit is reached. Alternatively, if the motion metric indicates an unacceptable degree of motion at step  410 , and the pre-set time limit is reached at step  412 , the process ends at step  99 . If the motion metric indicates an acceptable degree of motion, the process ends at step  99 . 
     In another embodiment of the invention, motion detection module  53  is configured to analyze the images captured based on techniques such as high-frequency detail position comparison. Points in the images that include fast transitions in brightness can be identified in the first image in the sequence, and those points can be checked in one or more subsequent images to determine whether the fast transitions still occur at the same points; This approach can accommodate differences in illumination as would exist between measurement mode and inspection mode images. Images captured under the same lighting conditions, such as inspection-mode images captured before and after the counterpart measurement-mode images, can be simply subtracted from one another to determine whether the image has substantially changed. 
       FIG. 5  is a flow chart illustrating an exemplary alternative embodiment of the steps involved in motion detection. Borescope/endoscope or probe system  10  shown in  FIG. 1  is configured to perform the steps indicated in method  500 . Method  500  may be implemented when probe system  10  is in inspection mode, and the CPU  56  receives a command requesting measurement. An operator may request measurement by pressing a button (not shown) on the probe  10  or selecting a menu item from, for example, integral display  21 . 
     Once the measurement command is received, at step  502 , CPU  56  or video processor  50  captures an inspection mode image. At step  504 , the CPU  56  or video processor  50  identifies sharp brightness transition points in the inspection mode image captured at step  502 . CPU  56  then sends a command to microcontroller  30  to enter measurement mode. In an embodiment of the invention, microcontroller  30  controls emitter drive  32  to illuminate one emitter group to project a first fringe set. At step  506 , CPU  56  or video processor  50  captures the first fringe set images. At least one measurement mode image is captured for the first fringe set. At step  508 , the CPU  56  or video processor  50  identifies sharp brightness transition points in at least one of the first fringe set images captured at step  506 . 
     Motion detection module  53  then compares the identified sharp brightness transition points of the inspection mode image with those of the fringe set image(s) at step  510 . At step  512  motion detection module  53  determines a motion metric based on that comparison. If the motion metric indicates an unacceptable degree of motion at step  514 , and the time limit is reached at step  516 , the process ends at step  99 . 
     If the motion metric indicates an unacceptable degree of motion, and the pre-set time limit is not reached, steps  502 - 516  are repeated until the motion metric indicates an acceptable degree of motion or the pre-set time limit is reached. Preferably, the sequence is repeated from step  502  to update the inspection mode image because it is unlikely that the measurement mode images will again line up with the original inspection image. Alternatively, the sequence may be repeated from step  506  to compare the captured fringe set images or two or more measurement mode images comprising the same structured-light pattern to each other until they all match up and then capture another inspection mode image at the end. 
     However, if the motion metric indicates an acceptable degree of motion, steps  506 - 514  are repeated for the second fringe set, then the third fringe set, etc. The process ends after sequencing through steps  506 - 514  for the last fringe set fringe set once all of the fringe set images are captured for that last fringe set and the motion metric indicates an acceptable degree of motion for the fringe set image(s) in the last fringe set. 
     Referring back to  FIG. 1 , the previously discussed imager interface electronics  31 , emitter drive  32 , and shutter mechanism  34  are included in the probe electronics  48 . Probe electronics  48  may be physically separated from a main control unit or CPU  56  to provide more local control over probe-related operations. Probe electronics  48  further comprise calibration memory  33 . Calibration memory  33  stores information relating to the optical system of detachable tip  42  and/or elongated portion  46  such as magnification data, optical distortion data, and pattern projection geometry data. 
     Calibration memory  33  stores information relating to the intensity relationship between the light projected from light source  23  and the light projected from emitter module  37 . The intensity relationship between of the light projected by light source  23  and emitter module  37  can be pre-determined before any image capture. Typically, the brightness or intensity from light source  23  is greater than the brightness or intensity from emitter module  37 . Therefore, the imager  12  exposure time and/or the analog gain applied to video signal output by imager  12  during inspection mode image capture should be different from those during measurement mode image capture. 
     Microcontroller  30 , which controls shutter  34 , communicates with CPU  56  and controls emitter drive  32  circuitry, and also communicates with imager interface electronics  31  to determine and set gain and exposure settings, and stores and reads calibration data from the calibration memory  33 . 
     Probe system  10  further comprises one or more of a gain function, an exposure function, a gamma correction function and an edge enhancement function applied to image data originating from imager  12 . Probe system  10  is configured to automatically adjust the parameters of at least one of said functions when switched between inspection mode image capture and measurement mode. 
     In an embodiment of the invention, the relative intensities of the light output by the inspection light delivery system and the structured-light patterns is determined during a calibration step and stored in calibration memory  33 . DSP  51  included in imager interface electronics  31  may be configured to automatically adjust imager  12  exposure and front end analog gain to achieve optimal image brightness for inspection mode image capture. 
     Microcontroller  30  is configured to compute parameters of the exposure function and gain function settings from DSP  51  to use during measurement mode using exposure function and gain function values that are active during inspection mode. Microcontroller  30  is further configured to compute parameters of the exposure and gain functions according to a pre-determined intensity relationship between the light of the structured-light patterns and the light from inspection light source  23  and set DSP  51  to apply the adjusted exposure and gain settings to optimize image brightness for measurement mode image capture. For example, the parameters of the exposure and gain functions are adjusted such that the brightness in the plurality of fringe set images is similar to the brightness in the inspection mode image(s). This approach eliminates the time that would be required for DSP  51  to reach an appropriate image brightness after the switch if DSP  51  were left in automatic exposure and gain adjustment mode, which is desirable to minimize the likelihood of motion between image captures. After the measurement-mode images are captured, DSP  51  may be again configured for automatic gain and exposure adjustment to optimize image brightness for inspection-mode image capture. 
       FIG. 6  is a flow chart illustrating an exemplary embodiment of the steps involved during an image capture sequence of the present invention. The term “image capture sequence” used herein is defined as the capture of counterpart inspection mode and measurement mode images. The term “image capture sequence” is not to be confused with the term “measurement mode capture sequence” defined above. 
     Borescope/endoscope or probe system  10  shown in  FIG. 1  is configured to perform the steps indicated in method  600 . Method  600  may be implemented when probe system  10  is in inspection mode, and the CPU  56  receives a command requesting measurement. An operator may request measurement by pressing a button (not shown) on the probe  10  or selecting a menu item from, for example, integral display  21 . 
     Once the measurement command is received, at step  602 , CPU  56  or video processor  50  captures the inspection mode image(s). At step  604 , CPU  56  sends a command to microcontroller  30  to enter measurement mode. At step  606 , microcontroller  30  reads the analog gain and exposure from DSP  51 , and at step  608 , the microcontroller  30  adjusts the gain and exposure for measurement mode. Discussed above, the measurement mode DSP  51  settings may be adjusted according to a pre-determined intensity relationship between the inspection light delivery system and the structured light patterns. Further at step  608 , microcontroller  30  sets DSP  51  to fixed gain and exposure based on the adjusted values. At step  610 , the inspection light is disabled by microcontroller  30  or CPU  56  as discussed previously. 
     At step  612 , microcontroller  30  controls emitter drive  32  to perform a measurement mode capture sequence. In an embodiment of the invention, performing a measurement mode capture sequence comprises sequencing through emitter groups, different subsets of light emitters, on frame boundaries while possibly adjusting on time or drive level to compensate for different emitter brightness levels. Furthermore, a drive level supplied to one subset light emitters may be adjusted to compensate for a temperature difference between that subset of light emitters and another subset of light emitters. Different emitter brightness levels may be due to differing emitter efficiencies or to heating of the emitters as the sequence progresses. For example, if the emitters are LEDs, the efficiency generally decreases as temperature increases. When the first LED is turned on, emitter module  37  is cooler than when the last LED is turned on. Thus, the last LED requires more drive current to achieve the same output as the first LED. The difference in drive levels may be predetermined through a calibration step. LED forward voltage drop also typically increases as temperature increases. Thus, microcontroller  30  in conjunction with emitter drive  32  may measure the LED forward drop to determine LED temperature to more accurately compensate for the efficiency change. 
     At step  614 , CPU  56  or video processor  50  captures measurement mode images. At least one measurement mode image is captured per fringe set. In addition, a plurality of measurement mode images may be captured per fringe set such that measurement mode images of each fringe set are captured at the same brightness level; also, a plurality of measurement mode images may be captured per fringe set such that the plurality of fringe set images of at least one fringe set are captured at different brightness levels. 
     Motion detection module  53  analyzes the images for motion at step  616 . If motion is detected at step  618 , and the pre-set time limit is reached at step  620 , the process ends at step  99 . If motion is detected, and the pre-set time limit is not reached, steps  612 - 620  are repeated until motion is not detected or the pre-set time limit is reached. Alternatively, if motion is not detected at step  618 , CPU  56  sends a command to microcontroller  30  to enter inspection mode. At step  624 , emitter drive  32  is disabled by microcontroller  30 . At step  626 , microcontroller  30  configures DSP  51  for inspection mode by setting DSP  51  for automatic gain and exposure adjustment. At step  628 , CPU  56  or microcontroller  30  enables inspection light output. After step  628 , CPU  56  or video processor  50  may again capture inspection mode image(s), as in step  402 . This marks the end of the image capture sequence. Method  600  may be repeated automatically to sequence through the steps a pre-determined number of times. Alternatively, an operator may manually command the repetition of method  600  by requesting measurement each time a new image capture sequence is desired. 
     Referring back to step  618  of  FIG. 6 , probe system  10  does not have to directly enter inspection mode if there is no motion detected at step  618 . In another embodiment of the invention, if there is no motion detected at step  618 , the user is given an option to either enter inspection mode at step  622  or to enter a measurement screen (not shown). The measurement screen displays a counterpart inspection mode image, preferably captured from step  602 , while analysis or measurement is performed on the at least one counterpart measurement mode image, preferably captured from step  614 . The measurement screen enables the placement of measurement cursors on the counterpart inspection mode image while the actual analysis or measurement is performed on data representing the at least one counterpart measurement mode image. Optionally, when entering the measurement screen, the emitter drive is disabled so that structured-patterns are not projected. The user can choose to enter inspection mode at any point desired while viewing the measurement screen to pick up at step  622 . If the emitter drive was previously disabled from entering the measurement screen, step  624  is skipped. The sequence resumes at step  626 , where microcontroller  30  configures DSP  51  for inspection mode by setting DSP  51  for automatic gain and exposure adjustment. 
     Probe system  10  is configured to change the parameters of imager  12  analog gain and exposure functions through DSP  51  when switched between inspection mode and measurement mode. Probe system  10  is also configured to automatically adjust other processing parameters of DSP  51 , including, but not limited to, gamma correction and edge enhancement, when switched between inspection mode and measurement mode. 
     Regarding gamma correction, typically, imager  12  responds to light in a linear manner. A non-linear re-mapping of the intensity or luminance values is often performed by the DSP  51  to improve the perceived brightness uniformity for image display. Non-linear remapping of the intensity values of images captured during inspection mode may be desirable. However, it is preferable to perform phase-shift analysis on images representative of a linear response to light. Therefore, the linear response to light must be carried over from imager  12  to video processor  50  during measurement mode because phase-shift analysis is generally performed on the structured-light images captured during measurement mode. The probe system  10  is configured to decrease an effective level of gamma correction applied to pixels of at least one measurement mode image relative to the level of gamma correction applied during inspection mode. For example, a linear gamma DSP setting is enabled or switched on during measurement mode. During inspection mode, however, the linear gamma DSP setting is typically disabled, or set to be non-linear, to improve the perceived inspection-mode image quality. 
     Regarding edge enhancement, enabling edge enhancement artificially modifies the brightness linearity of an image. This is generally not desirable for images on which phase-shift analysis is performed as images representative of a linear response to light are preferred. Therefore, the edge enhancement function is disabled or switched off for measurement mode image capture, and may be enabled or switched on for inspection mode viewing and inspection mode image capture. Probe system  10  is configured to reduce an effective level of edge enhancement applied to pixels of at least one measurement mode image relative to the level of edge enhancement applied during inspection mode. 
     Further relating to image capture, it is preferable to perform phase-shift analysis on images with little to no random noise to improve measurement accuracy. To reduce random noise, probe system  10  may be configured to capture a plurality of measurement mode images with the same structured-light pattern or same fringe set present and average or sum two or more of those measurement mode images. The result is a plurality of composite images where only one fringe set is present in each composite image. These plurality of measurement mode images with the same structured-light pattern or same fringe set present may be captured with the same or similar brightness levels. When the composite image of a projected fringe set a result of summing rather than averaging, the dynamic range is increased and noise is reduced. Whether the composite images are a result of summing or averaging, phase-shift analysis and other processes can be performed on the composite images. 
     Furthermore, measurement mode images comprising the same structured-light pattern or same projected fringe set may be captured with different brightness or intensity levels. This is accomplished by either manually or automatically changing the emitter output intensity or duration, imager  12  exposure, analog gain, or some combination thereof. 
     Discussed above, fringe contrast determining function  54  is configured to determine whether one emitter or multiple emitters should be enabled for each emitter group. In order to change the light source intensity, for example, fringe contrast determining function  54  may further be configured to sequence between enabling one emitter and multiple emitters per emitter group to project light. Also discussed above, microcontroller  30  communicates with imager interface electronics  31  to determine and set gain and exposure settings. Similarly, microcontroller  30  may configure emitter drive  32  to alter the amount of power delivered to emitter module  37  and thus vary the intensities of the projected fringe sets. 
     A plurality of measurement mode images captured with different brightness or intensity levels comprising the same projected fringe set may be combined to effectively increase the dynamic range of the system. For example, an image may be captured of a shiny metal surface comprising a structured-light pattern. Reflective properties of the shiny metal surface may prevent adequate intensity levels in dark areas. Therefore, multiple images for each fringe set may be captured with different intensity levels so that, in at least some images, the dark areas are properly illuminated. Then, the captured images for each fringe set may be combined resulting in a single image for each fringe set with sufficient intensity levels across a larger portion of the image than could be achieved with a single image per fringe set. 
     CPU  56  or video processor  50  may be configured to analyze an inspection-mode image prior to capturing the measurement-mode images to determine brightness uniformity. The analysis may be performed by generating and evaluating a histogram of pixel luminance values. A histogram having most of the pixels in a middle brightness range would indicate that a single set of measurement-mode images would likely be adequate. A histogram having mostly very bright pixels and very dark pixels may indicate a highly reflective surface that would benefit from the merging of multiple measurement-mode image sequences captured at different brightness levels. 
     In an embodiment of the invention, multiple measurement mode images that comprise the same projected structured-light pattern or fringe set and are captured with different intensity levels are combined by evaluating each pixel intensity in the multiple images and selecting the set of pixels that best meets a set of criteria, such as maximum modulation, brightness values, or pixel unsaturation. Pixel values from more than one measurement mode image comprising the same structured-light pattern or same fringe set may be utilized to determine at least one geometric dimension of the surface or object. 
     The discussion above generally relates to image capture by probe system  10 . The discussion below generally relates to the use and storage of those captured images. 
     In an embodiment of the invention, image(s) comprising structured-light patterns captured during measurement mode are hidden from the operator, and are used only for the actual analysis and measurement. For example, CPU  56  or video processor  50  creates an image file comprising data representing a counterpart inspection mode image and creates a hidden record within the image file comprising data representing its at least one counterpart measurement mode image. The counterpart inspection mode image can be displayed while the operator positions overlay cursors for determining geometric measurements of a viewed object while analysis is performed on the counterpart measurement mode image to determine the geometric measurement results. Therefore, the operator may command analysis or measurement while viewing an inspection mode image even though the analysis or measurement is performed on its counterpart measurement mode image or images. This can also be done prior to image storage, for example, as previously discussed in relation to  FIG. 6 , where the inspection mode image is displayed and the measurement images are processed. 
     The operator skill requirement is reduced by allowing the user to place cursors on a normal, inspection mode, image without having to worry about stereo matching, perpendicularity, shadow position, etc. The operator may use joystick  62  to place cursors on an inspection mode image displayed on integral display  21 . Interchangeably with joystick  62 , keypad  64  and/or computer I/O interface  66  may also be used to place cursors, and interchangeably with integral display  21 , computer monitor  22  and/or video monitor  20  may also be used to display the inspection mode image. 
     Typically, when a measurement is performed on an image, and the image is saved, graphical overlay data is added to the image such as cursor positions, measurement results, accuracy indicators, etc. This graphical overlay must be removable to enable easy re-measurement at a later time where the non-graphical data related to the image is required. A method for storing image-specific data from a probe, specifically calibration data, is known from U.S. Pat. No. 7,262,797. It is further desirable to store measurement data, for example, relating to phase-shift analysis. Measurement data includes, but is not limited to the luminance portion of a structured-light image (luminance data), measurement cursor positions, merged image data, measurement types, results, accuracy indications, etc., calibration data, phase data, and phase-shift analysis data. Phase data may include data representing the phases of the structured-line patterns, for example wrapped phase, unwrapped phase, relative phase, and/or absolute phase. The co-pending application entitled Phase-Shift Analysis System and Method filed on Mar. 5, 2008 as U.S. Ser. No. 12/042800, which is incorporated herein by reference, discusses the implementation of phase data in phase-shift analysis. Phase-shift analysis data includes, but is not limited to, surface or object distance data (z values for each pixel, where z is the object distance from the probe), and point cloud data (x, y, z values for each pixel). As one skilled in the art should understand, the method disclosed in U.S. Pat. No. 7,262,797 should include the additional step of “writing measurement data to file.” 
     Specifically, the system may include a geometric measurement mode in which a counterpart inspection mode image is displayed, an operator positions measurement cursors on the inspection mode image to identify measurement points, and CPU  56  computes and displays measurement results based on 3D data derived through phase-shift analysis performed on the counterpart measurement images utilizing calibration data. When the operator requests an image save, CPU  56  creates an image file. It merges overlay data with the inspection image data and saves the result in the image file such that when the file is opened by a standard image viewer, the inspection mode image and overlay are displayed. CPU  56  also creates hidden records in the image file. In these hidden records, it stores the inspection image data that was overwritten by the overlay data, referred to as overlay-replacement data, and measurement data. Thus, a custom software application can fully recover the original inspection mode image and has all the information needed to replicate the existing measurements and/or perform additional measurements or analysis. 
     Measurement data in bitmap and JPEG images captured using probe system  10  or an accompanying personal computer application is saved by CPU  56  or video processor  50 . This allows images to have “destructive” overlays that are visible in the image using standard image viewing software, but which are removable by a custom application to present a clean image to the viewer or operator. The clean image can either be a measurement mode image or its counterpart inspection mode image. Storing luminance and measurement data in the image also allows the measurements to be repeated on the image using either the probe software or by a custom program, such as a PC-based software package. 
     Once images are captured and, optionally, stored by probe system  10 , the image data can be used in many ways. For example, pixel values from the measurement mode images can be used to determine at least one geometric dimension of the object or surface. In addition, image data can be used for performing 3D geometric measurements or 3D visualization. The image data can also be exported or converted to a data format usable with 3D modeling software for detailed analysis or reverse engineering. 
     The construction and arrangement of systems and methods relating to image capture, as described herein and shown in the appended figures, is illustrative only and is not limited to a probe. Although only a few embodiments of the invention have been described in detail in this disclosure, those skilled in the art who review this disclosure will readily appreciate that many modifications are possible (e.g. variations in sizes, dimensions, structures, shapes and proportions of the various elements, values of parameters, mounting arrangements, use of materials, orientations, etc.) without materially departing from the novel teachings and advantages of the subject matter recited in the appended claims. Accordingly, all such modifications are intended to be included within the scope of the present invention as defined in the appended claims. The order or sequence of any process or method steps may be varied or re-sequenced according to alternative embodiments. In the claims, any means-plus-function clause is intended to cover the structures described herein as performing the recited function and not only structural equivalents but also equivalent structures. Other substitutions, modifications, changes and omissions may be made in the design, operating conditions and arrangement of the preferred and other exemplary embodiments without departing from the spirit of the embodiments of the invention as expressed in the appended claims. Therefore, the technical scope of the present invention encompasses not only those embodiments described above, but also those that fall within the scope of the appended claims.