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Optical Alignment Using The Point Source Microscope

ABSTRACT

We give an example of a Point Source Microscope (PSM) and describe its uses as an aid in the alignment of optical systems including the referencing of optical to mechanical datums. The PSM is a small package (about 100x150x30 mm), including a point source of light, beam splitter, microscope objective and digital CCD camera to detect the reflected light spot. A software package in conjunction with a computer video display locates the return image in three degrees of freedom relative to an electronic spatial reference point. The PSM also includes a Köhler illumination source so it may be used as a portable microscope for ordinary imaging and the microscope can be zoomed under computer control. For added convenience, the laser diode point source can be made quite bright to facilitate initial alignment under typical laboratory lighting conditions. The PSM is particularly useful in aligning optical systems that do not have circular symmetry or are distributed in space such as off-axis systems. The PSM is also useful for referencing the centers of curvatures of optical surfaces to mechanical datums of the structure in which the optics are mounted. By removing the microscope objective the PSM can be used as an electronic autocollimator because of the infinite conjugate optical design.

1. INTRODUCTION

In the last decade or two the optics community has seen huge strides made in the improvement of optical image quality due to the widespread availability of phase-measuring quantitative-interferometry. Surface topography data from phase measuring interferometers is now commonly used by fine figuring processes such as ion milling1, MRF2 and other computer controlled polishing methods to produce optical surfaces accurate to a few nanometers peak-to-valley. A few decades ago one would have asked “Why do you want surface figure this good?” With the luxury of hindsight we see that some of the applications for highly precise figure include the optics that corrected the error in the Hubble Space Telescope and the ever increasing demands of the semiconductor industry.

With an eye on the past it is clear that if another significant improvement in overall optical quality could be made in optical systems there would be applications waiting for those improvements. However, it is probably unrealistic to assume that the optical figure quality of surfaces can be made much better, or at least better at an affordable cost. On the other hand there is an area where significant improvements can be made; the alignment of the surfaces within an optical system to one another. The same sorts of optical performance improvement that have been made in figure can be achieved by the alignment of optical components to tighter tolerances. What is needed to accomplish this are the tools, and a new way of thinking about achieving better alignment.

There are at least three reasons to think that improvements could be made in alignment. The majority of optical systems are getting smaller which means the absolute tolerances are getting tighter. As the optical tolerances get tighter, the tolerances on mating features of cell and lens get tighter and become prohibitively expensive to manufacture. Finally, using the periphery and seat of an optical element to control centering is operating at the optically insensitive end of the optical lever arm. Optics should be centered based on aligning their centers of curvature directly, again for at least two reasons. The edges and seats of lenses and cells have a poor finish relative to the optical surfaces and it is difficult to impossible to control a tolerance to better than the finish of the part. An optical surface is fabricated well enough to produce a return spot a few microns in diameter at its center of curvature. These spots can be located to a small fraction of their diameter in space and provide the information to align centers of curvature coaxially, or in three dimensional space, to a micron or so.

In this paper we will describe the Point Source Microscope (PSM) 3, an instrument for locating the centers of curvature of optical surfaces to micron accuracy for alignment of optical elements that is analogous to the use of a phase measuring interferometer to provide information used to guide the figuring of optical components. Once the location of the center of curvature of an optical surface is known it is easy to position that center on the optical axis of the system in analogy to what ion milling or MRF can do for surface figure.

First we will describe the PSM and explain of how it works along with the companion PSM Align©4 software. Then we give several examples of how the PSM is used to align various types of optical systems using contrasting alignment techniques. Finally we will discuss how the PSM compares with other commercially available alignment instruments.

2. DESCRIPTION OF THE PSM

2.1 PSM hardware
The PSM is a video metallographic, or reflected illumination, microscope with a Köhler light source to provide uniform illumination over the field of view. In addition, the PSM has a point source of illumination produced by the end of a fiber pigtailed laser diode that is conjugate to the microscope object surface as shown in Fig. 1 below.

Both light sources are controlled though the companion computer by the PSM Align© software and may be used one at a time or simultaneously as well as adjusted in intensity. The diffuse, Köhler illumination is used for metallographic imaging of opaque surfaces while the point source produces a cat’s eye retro-reflection from a surface at the microscope objective focus that produces a bright spot on a dark background on the video screen as seen in Fig. 2 (middle).

Both sources can be used simultaneously as shown in the right-hand image in Fig. 2. Because the point source produces a retro-reflection, its centroid will always appear in the same pixel location on the video screen but its size (and shape, if the surface is rough) will vary depending on how well the microscope is focused on the surface. A crosshair (Fig. 2, middle) can be aligned to the retro-reflected spot so that if the point source is turned off the location in the image plane where it would appear is known. The PSM could be used with an external fiber source to illuminate a particular pixel location on a surface with an alternative wavelength of light if this were useful. The point source is also useful when trying to image a transparent surface with virtually no defects on which to focus. When the surface is in focus there will be a bright return from the point source retro-reflection even though no other surface detail may be visible in the image.

2.2 PSM Align© software
The video image is captured with a 1/3” format Point Grey Flea Firewire camera6 with a 1024×760 pixel, 12 bit CCD array of which 8 bits are currently used. The captured image is processed with the PSM Align© software to derive image statistics and reference locations. Figure 3 shows the user interface for the software that includes the control panel, a National Instruments IMAQ7 cursor toolbox, the main video window and a binary video window to aid in adjusting image thresholds.

When the cursor is positioned over a particular pixel, the IMAQ toolbox gives the x and y pixel location and the 8-bit intensity (gray value). These tools also allow zoom and un-zoom centered on the cursor position. The PSM Align© “Thresholds” tab illustrated is used to set the thresholds in the binary video window and include intensity and adjacent pixel areas as well as geometrical parameters. The control panel also manages the camera shutter and gain, image snap, save and load, image feature size and location relative to a settable reference crosshair location. The illumination source and intensity are also set here. This completes a brief summary of the hardware and software features of the PSM. The balance of the paper illustrates how these features are used in various alignment applications.

3. ALIGNMENT APPLICATIONS

3.1 Alignment of the PSM with a sphere
We have described how the PSM produces a retro-reflected spot when focused on a surface. When the PSM objective focus is at the center of curvature of a concave sphere, light will be reflected from the sphere at normal incidence and produce a focused spot at the PSM objective focus. The same is true for a convex sphere whose radius of curvature is limited by the working distance of the objective. The PSM then relays this spot back to the CCD detector as shown in Fig. 4. The difference between this point image and the retro-reflected spot is that the spot image from the center of curvature is sensitive to the lateral alignment of the PSM to the center of curvature as well as to focus.

As can be seen in the right half of Fig. 4, if the PSM objective focus is not coincident with the center of curvature of the sphere the return image will neither be centered on the out-going focus nor well focused. Consequently, the return spot centroid will be shifted laterally on the CCD array and be out-of-focus. With any practically useful microscope objective (5x to 50x and sufficient numerical aperture) the PSM has 1 μm or less lateral sensitivity when used in conjunction with the PSM Align© software and a focus sensitivity of about 1 μm when used with a 20x or 50x objective.

The PSM can equally well be used with convex spheres, the only requirement is that the radius of the sphere is less than the working distance of the objective, or that an auxiliary lens is used to create a long working distance as will be illustrated in the example of the doublet below. Because the PSM can be used with convex spheres and cylinders many kinds of mechanical tooling hardware become practical and useful optical alignment tooling. Some examples of this tooling are shown in Fig. 5. Surprisingly, these mechanical spheres and cylinders are very accurate figure-wise and are inexpensive compared to most optical hardware. CERBEC™ silicon nitride balls8 are rounder and have better finish than the best chrome steel balls plus are opaque and approximately match the reflectivity of bare glass.

It may not be obvious at first sight, but cylindrical tooling such as plug gauges are as useful with the PSM as balls for alignment purposes; instead of the center of a ball or sphere producing a point image, the axis of a cylindrical object produces a line image. Again, the cylinder establishes three degrees of freedom just as a ball. Rather than three translational degrees of freedom defined by two lateral motions and focus, the cylinder can be located by one lateral position perpendicular to its axis, another translation indicated by best focus of the line and a third by the angle the line makes with respect the coordinate system. The PSM Align© software calculates these two translations and the angle just as it does the three translations for the ball or sphere. The lateral and focus sensitivities are the same as for the ball and the angular sensitivity is about 5 seconds.

Finally, it should be noted that the PSM also works as an electronic autocollimator when the objective is removed and that is why we have shown the gauge block target mirror among the tooling in Fig. 5. A collimated 6.5 mm diameter Gaussian beam exits the PSM with no objective, is reflected by a plane specular surface and is focused on the CCD detector by the internal tube lens. In the autocollimator mode the angular sensitivity is better than 5 seconds.

3.2 Alignment of a simple doublet lens
This example is given to show how the PSM can be used for alignment in cementing a simple doublet. The optical parameters of this example are such that adequate performance does not require precision alignment; however it is a convenient example to illustrate some of the principles of the PSM. The technique also shows the power of using rotary tables for centering systems with rotational symmetry.

Mindful of the background in Sec. 3.1 on using the PSM at the center of curvature, consider cementing an f/5 doublet objective. Assume the flint is sitting on a cup on a precision rotary table, the surface to be cemented facing up as shown in Fig. 6 (left). This element has been centered with the PSM so that the reflected images from both surfaces are stationary as the table is rotated. The rear (flatter) surface is viewed through the upper surface via an auxiliary lens to converge the light enough to get convergence of the reflected light, in other words, to give the PSM a long working distance to get at the apparent center of curvature. A lens design program is used to find the correct conjugates and, in general, there will be spherical aberration in the return image. If the spherical aberration is objectionably large, the aperture of the lens can be stopped down to the limit where diffraction begins to make the spot larger rather than smaller. The upper surface can be viewed directly at its center of curvature.

Mindful of the background in Sec. 3.1 on using the PSM at the center of curvature, consider cementing an f/5 doublet objective. Assume the flint is sitting on a cup on a precision rotary table, the surface to be cemented facing up as shown in Fig. 6 (left). This element has been centered with the PSM so that the reflected images from both surfaces are stationary as the table is rotated. The rear (flatter) surface is viewed through the upper surface via an auxiliary lens to converge the light enough to get convergence of the reflected light, in other words, to give the PSM a long working distance to get at the apparent center of curvature. A lens design program is used to find the correct conjugates and, in general, there will be spherical aberration in the return image. If the spherical aberration is objectionably large, the aperture of the lens can be stopped down to the limit where diffraction begins to make the spot larger rather than smaller. The upper surface can be viewed directly at its center of curvature.

With the flint centered, a drop of cement is placed in the concavity and the mating crown element set in place. Once the cement has been reduced to an appropriate thickness, the crown element may be centered by either of two methods, see Fig. 6 (right). The auxiliary lens may be used to view the center of curvature of the convex surface directly or the PSM can view the reflection off the rear of the flint as seen through the crown. Both methods have similar sensitivity using the parameters of this example but looking directly at the center of curvature is most sensitive. In either case, a 0.01º tilt of the front surface produces a 15 μm or more decenter of the spot that is doubled by rotating the table. If one were to use a contact indicator at the edge of the upper surface, this same tilt would register a 5 μm total indicated runout.

As was explained at the beginning of this section, this example illustrates how to use the PSM for cementing a doublet even though the optical parameters do not warrant this degree of precision and accuracy. There are cases not substantially different from this example for wide field of view projection systems or very fast imaging lenses used in the visible where these sort of centering tolerances are necessary to obtain the desired lens performance. The next example is one where the alignment accuracy is definitely needed.

3.3 Alignment of an Offner relay mirror system
In an example where the need for micron alignment is truly required, consider the Offner9 relay shown below in Fig 8a. Because this is an all reflective system it can be used at a 13.5 nm wavelength in the soft X-ray region and now precision alignment becomes a necessity. The question is how to assemble the two spherical mirrors as well as possible to the mechanical hardware that position the relay optics relative to the rest of the lithography system.

In the example Offner relay used, the total field is about 90 μm in width, the distance from the object plane to the primary is 250 mm and the object is 40 mm off the axis of symmetry. Given this design, Fig. 7 shows the effect decentering or despacing have on performance. Not unexpectedly, performance at the edge of the field is worse than the center but also the image plane is tilted. Knowing the tilt would allow compensating or correcting for the error. Clearly the biggest loss in performance is despace but this can also be corrected by an axial shift in the image plane.

The PSM is particularly useful if some thought to alignment has been made in the initial system opto-mechanical design by incorporating features such as tooling balls to locate critical datums. Assuming critical datums have been defined mechanically, we start the alignment by placing a ball where the two mirrors have their common centers of curvature.

Next, using an auxiliary lens with a focal length slightly longer than the radius of curvature of the secondary mirror, align the PSM focus conjugate with the center of the ball in three directions so that the return image is centered and in focus in the PSM image. Then insert the secondary mirror and align it to the PSM image using the reflection from the secondary convex surface that is conjugate to its center of curvature as in Fig. 8b.

Move the PSM so it faces the primary mirror and align the PSM focus to the center of the ball as in Fig. 8c. Remove the ball and align the primary to the PSM focus so light reflected from the primary is centered on the PSM image and is in focus. Now the two mirrors are concentric and located precisely to the optical bench datum indicated by the ball.

Once the Offner relay is aligned optically and located precisely to its mechanical structure via the tooling ball, light from an object on one side of the system axis of symmetry will be nearly perfectly imaged on the other side of the axis. The relay will have been optimized for a particular object distance off the axis but this distance is not highly critical to the relay performance. It is important to know exactly where the input is imaged on the other side of the axis. If a tooling ball is placed so that its center is at the center of the object field, the PSM can precisely determine where the image will be located by using the relay in double pass, see Fig. 8d. Light from the point source in the PSM is brought to focus by the PSM objective and sent on through the relay until it reflects off the center of the ball located with its center at the object plane of the relay. The light then retraces itself exactly back to the PSM focus where it is imaged by the CCD and its location shown on the video monitor. When the return spot is centered in the reference cross hair and is at best focus, the PSM focus is in focus at the center of the relay image plane. This check of object and image location also permits a double check that the alignment was done correctly, something that is always useful when the tolerances are tight.

We conclude this example by saying the Offner 1:1 relay is the simplest sort of all reflecting, ring field microlithography optical systems. The all reflective systems that will be used to make future IC chips will contain six or more mirrors with their centers of curvature located along a common optical axis.10 If these systems are to meet their theoretical optical design performance, they will have to be assembled so their centers of curvature truly lie on the optical axis to 1 μm or better tolerances. Variations on the method described here will make this possible and avoid the inevitable tolerance stack up when optics are centered mechanically by their edges and seats.

3.4 Alignment of an off-axis telescope system
In this example we will describe two other modes of using the PSM for optical alignment and alignment of optics to mechanical datums. In practice, though not often thought of this way, all optical alignment deals with positioning optical surfaces in a particular relationship to mechanical datums as in the case of centering a single lens element. The optical axis is the line joining the centers of curvature of the two optical surfaces. Edging a lens is bringing its periphery, a mechanical datum, into concentricity with the optical axis. In this example, the telescope system is similar to the single element with the telescope itself being like one optical surface, the backend of the system like the second surface and the mounting plate for the system like the periphery of the lens. In this case, the periphery was established first and the two halves of the optical system each brought into alignment with the periphery or mounting plate. Figure 9 shows a simplified outline of the telescope system.

The telescope on the left of the mounting plate is an off-axis Ritchey-Chretien with an f/11 output as shown in Figure 9. The telescope and the prism housing are attached to the mounting plate by a three ball and groove kinematic mounting scheme, one coupling of which is shown in Fig. 10. Drilled balls fit into conical countersunk recesses in the telescope frame and prism housing. The two halves are pulled together by a screw through the center of the balls and are located by a pair of pins forming a double sided “V” groove in the mounting plate. In this way the two halves of the telescope are precisely located relative to each other and flexing of the mounting plate (by which the telescope assembly is held in its housing) will not disturb the alignment of the telescope system. Test fixtures for both sides of the telescope system used the same mounting scheme to accurately locate the halves during individual assembly and test.

3.4.1 Alignment of the telescope
By design the optical axis of the telescope was precisely defined relative to the telescope frame. The telescope frame, in turn, was precisely located relative to the optical table on which the telescope was aligned by means of a fixture incorporating the three ball kinematic mounting scheme as shown in Fig. 11. Two ends of the temporary long screws can be seen in the upper kinematic locators clamping the telescope frame to the test fixture.

Prior to aligning the telescope, the telescope alignment test fixture was adjusted in four degrees of freedom relative to the collimator; two degrees of tilt to make it square to the collimated beam and two degrees in translation to center the apertures. Then two balls were placed on the table relative to the test fixture and table so as to provide reference positions accessible to the PSM at the short focus of the hyperbolic primary and at the system focus. The line joining the centers of these balls defined the optical axis of the telescope mechanically

The telescope mirrors were then aligned in two steps against a collimator, first the primary alone and then the combination of primary and secondary. Initially the PSM was positioned so that it was looking into the center of the primary with its focus at the center of the ball at the primary focus. The collimator was then de-focused to produce a focus far behind the primary at the long focus of the hyperbolic primary. The source in the collimator also had to be raised precisely because the optical axis of the collimator and telescope were at known but different heights.

Once the PSM was aligned with the ball defining the location of the primary short focus, the ball was removed so the PSM could view the light from the collimator and focused by the primary. It was necessary to adjust the primary in five degrees of freedom, three to correctly position the focus and two to remove the aberrations caused by the primary optical axis not lying on the collimator axis. First the primary was adjusted so that light from the collimator and reflected by the primary was in focus and centered on the PSM crosshairs and in the computer monitor. This process aligned the first three degrees of freedom but the image showed substantial astigmatism, exactly what would be expected from a misaligned off-axis hyperbola.11 (It should be noted that since this was an off-axis telescope the aberration was largely astigmatism with a little coma and the two aberrations decreased together as the primary was aligned. Had this been a symmetrical telescope the only aberration seen due to misalignment would have been coma.)

The next step was to adjust the primary tilt and decenter to maintain the image centration and focus on the PSM crosshairs and to reduce the astigmatism. The most straight forward method of doing this is tilt and decenter sideways to straighten the astigmatic image so it is perpendicular to the optical table. Then adjust vertically relative to the table to reduce the length of the image until it is round and symmetrical. This procedure worked in a quick, directed fashion. The images observed with the PSM corresponded to the images in reference 11. Further, the PSM had sufficient magnification to view the “star” image to reduce the astigmatism to at least the tenth wave level. The star test is very sensitive to symmetry in the image and by going through focus the least astigmatism is very apparent.

Once the primary was adjusted so that it focused in the correct location and was free of aberrations indicating that its optical axis and the mechanical optical axis were coincident and parallel to the collimator axis, the PSM was mounted looking into the telescope centered on the secondary mirror aperture with its focus centered on the ball defining the system focus. Alignment of the secondary followed the same sequence as the primary but now the collimator was set at infinity focus with its source on axis. Fig. 12 shows this phase of the alignment with the PSM barely visible behind the telescope while the monitor shows the image from the telescope in the crosshair. The kinematic base at which the ball screwdriver is pointing accepts the posts (lying on their sides) that hold the balls that define the locations of the primary and secondary foci.

First the secondary mirror was adjusted in tilt and decenter so that the image was centered on the PSM crosshairs and was focused as well as could be determined given the residual astigmatism. Then the secondary was adjusted using a combination of tilt and decenter to reduce the astigmatism to give a well focused, symmetrical image while keeping the image centered on the PSM display crosshairs. Once this alignment had been performed we knew that the telescope focus was located the correct distance behind the test fixture and that the optical axis of the telescope as defined by the line between the primary focus and the telescope of secondary focus was perpendicular to the test fixture and correctly positioned relative to the three kinematic mounting locations on the test fixture.

The main difference between this telescope alignment technique and those described previously is that by using aberrations as well as locations, the PSM can monitor alignment in five degrees of freedom, something that would be impossible using an alignment telescope. Further, because the PSM operates with a relatively fast cone of light it is much less confusing than an alignment telescope in terms of selecting the reflection from the surface of interest. The alignment of telescope took less than a day and the secondary, which had more refined adjustments on the mount, took less than ½ hour including PSM setup time.

3.4.2 Alignment of the prisms in the prism housing
There were numerous prisms and fold mirrors in the prism housing to direct light from the telescope to various sensors as well as a path to direct light into the telescope and a path to couple a display into the eyepiece. All of these paths had to be boresighted so that as the operator changed from one mode of operation to another an object in the center of the
field for one sensor remained centered for another. Further, it was desired that the prism housing and sensors be interchangeable with the telescopes so the center of the field had to be defined relative to a mechanical datum, namely the mounting plate coupling the telescope to the prism housing. To align these various paths two fixtures were used, a projector that produced a converging cone of light that matched the telescopes f/11 focus and a mounting fixture for the prism housing that exactly simulated the mounting plate. This approach is shown schematically in Fig. 13 where the ball in the foreground represents the projector source; the joined base of the cones represents a positive lens to produce the f/11 cone that ends with the far ball at the conjugate focus.

The three balls in the prism housing mate with the test fixture to hold the prism housing correctly in five degrees of freedom. Three degrees of freedom are controlled by the ball at the projector focus. The other two degrees of freedom control the location of the optical axis of the projector relative to the three balls defining the prism housing location. This is exactly the same condition that applied to the telescope so that when the two halves of the system are mated the telescope will focus at the far ball location and the telescope optical axis will be co-axial with the projector axis.

Figure 14 shows the prisms in the housing and the paths into which the prisms direct the beams. These beams need to be correctly positioned to a few pixels on each detector so the final alignment can be accomplished by a very slight lateral adjustment of the sensors themselves. To accomplish this, the test fixture that held the prism housing was drilled and bushings inserted directly beneath the foci of the various paths and rods of the correct lengths were cut to hold balls at the foci as shown in Fig. 15, a picture of the actual fixture set up for locating one of the paths.

Figure 15 is instructive in that it shows almost all of the elements of the alignment discussed to this point. The f/11 light cone is coming in from the left and going through the prism visible in the prism housing that is attached to the test fixture via the three kinematic locators clearly visible on the back of the fixture. A metering rod is located in one of the bushings and has a ball sitting on its top. The PSM is aligned pointing down the diverted beam path and the PSM objective focus is aligned to the center of the ball. The PSM is supported by a substantial x-y-z stage to facilitate its alignment with the ball center. The PSM tilt adjustments are relaxed because they only control vignetting.

The next step in the alignment of this beam path was to remove the ball and metering rod so light diverted by the prism could be viewed by the PSM. Crude adjustment of the prism was made with the projector source set at maximum intensity. The focus of the projected beam was easily visible on a card in front of the objective and the prism was tapped lightly to tilt the prism and bring the beam focus in front of the objective. Once the beam entered the objective the source intensity was reduced and the beam position monitored on the computer display. The real-time visual feedback of spot location and focus made positioning the prism straightforward and rapid. Another feature of the PSM allows left/right and up/down image flips so the displayed image always had the expected or natural orientation independent of mirror flips of the beam. This ergonomic feature make alignment easier because adjustments appear to work in the direction expected instead of the way they actually move.

Once the prism had been adjusted so the spot of light was positioned within tolerance, UV cement was carefully applied to several places along the edges of the prism and the prism tacked in place with a UV source. Once tacked and still properly aligned, epoxy cement was applied and allowed to cure slowly. The next prism in the chain was added, the proper metering rod located in the next bushed hole and the procedure repeated for the remaining prisms in the paths. The procedure for alignment of the six paths in the prism housing was so efficient that all the paths could be aligned in two hours. In addition to the time savings, the mechanical tolerances on the prisms and their holders did not have to be very tight. Ledges to guide the initial prism placement were all that was required. The balance of the alignment was done by slight taps and shimming to correctly position the prisms.

3.4.3 Alignment using the PSM mounted on a CMM
It should be noted that there is an analogous approach to aligning the prisms that has been very successfully used OPG on another off-axis optical system, that is to mount the PSM on the ram of a coordinate measuring machine (CMM) and use the CMM to position the PSM at the end of each path rather than use the fixture as we have just described12, 13. Generally the CMM approach is more effective when there are either only a few prototype systems or a variety of systems to align while the fixture method is more suited to production. The geometry and complexity of the system may influence the decision as to which approach would be best as well as the availability of a CMM.

Using the CMM eliminates two aspects of the fixture. Using the example of the prisms above, a source projector is still required but the location of the source focus and the position of the optical axis can be determined using the PSM and stored in the CMM. To accomplish this, the first step is to mount the PSM on the CMM ram in place of a touch tip probe and set the probe tip radius set to zero in the CMM software. Next the PSM objective is focused at the center of the CMM master ball and the coordinate system zeroed in all three directions simultaneously. Then the PSM is moved to the projector source and the PSM focus made coincident with the source focus. The coordinates of the source are noted. Then the PSM is moved to the image of the source and that location noted. This defines the five degrees of freedom of the source location as shown in Fig. 16, four degrees define the axis and one is the axial location of the focus.

Now the PSM would be rotated 180 degrees about a vertical axis and the PSM focus zeroed again on the master ball. Then the locations of the three balls defining the location of the prism holder can be found, see Fig. 16. The telescope mechanical design defines where these three balls must be relative to the optical axis and focus of the source projector to be aligned. Using COTS alignment stages the prism housing can be brought into alignment with those three positions to locate it correctly relative to the source projector. Once the housing is correctly positioned, the PSM can be rotated to look down the first path to be aligned, zeroed again on the master ball and moved to the first path focus ready to sense the position of the first beam. The CMM software displays the global coordinates of PSM objective focus after each zeroing on the master ball. All that is necessary is to read from the design where the next focus is and move the PSM to that location and lock the CMM axis motions until the prism is aligned. Once the concept of using a CMM as an assembly tool is understood, the implementation is straight forward, and the CMM takes on added value as an assembly tool in addition to its traditional use as an inspection tool through use of the PSM.

Another way of aligning an optical system with powered elements on a CMM is to place the optical bench onto which the elements will be mounted on the CMM bed. Assuming provisions have been made in the opto-mechanical design, after zeroing the PSM on the CMM master ball, pick up three known tooling ball locations on the optical bench. Since these locations will be known by design relative to the optical axis and centers of curvature of the various optical elements, the PSM objective focus can be located precisely as each element is added. By picking up the three tooling balls on the optical bench, the CMM software establishes a coordinate system in the optical bench space and displays x-y-z coordinates in this space. When the first optical element is introduced the PSM can be located at the centers of curvature (or apparent centers of curvature) of the two surfaces. The element is then adjusted by tapping or shimming until it is correctly located within the given tolerances. Again, neither the element nor the holder need to be machined to tight tolerances because the element location can be adjusted far better using its optical axis, which is the line joining its centers of curvature. This alignment method largely eliminates tolerance stack up because the usual glass-metal (or optical-mechanical) interface features are not used to define optical alignment.

4. COMPARISON OF THE PSM WITH OTHER OPTICAL ALIGNMENT TOOLING

Now that various methods of using the PSM for the alignment of complex optical systems has been explained, we compare the features of the PSM with other more familiar optical alignment tooling. First, it should be said that the PSM is a compliment to existing tooling, not a replacement for it. For example, in Figs. 12 and 15 an alignment telescope is clearly visible. At the same time, there are other situations where it is very handy to have more than one PSM available.

4.1 Autocollimators
Although no examples have been given of the PSM used as an autocollimator, it is one if the objective is removed because the microscope is based on infinite conjugate optics. With the 100 mm tube lens and tenth pixel sensitivity, the PSM has angular sensitivity of about 5 seconds in reflection over a 6 mm beam diameter. While this is almost an order of magnitude worse than what can be achieved with a Davidson14 or Nikon15 autocollimator, there are situations where this electronic autocollimating capability is very useful, particularly in cramped locations and for use in conjunction with a CMM to move the PSM without pitch or yaw from interrogating one plane surface to another for parallelism.

An ergonomic feature of the PSM in this mode is the display on a computer monitor as opposed to looking through an eyepiece that might not be conveniently located. A very practical advantage of the PSM used as an autocollimator is that it is easy to align initially under normal lab lighting because of the bright laser source. With the more traditional autocollimators it is often difficult to find the return beam initially even if the lab lights are turned off.

4.2 Alignment telescopes
The PSM is probably most analogous to an alignment telescope in terms of what it does best but direct comparisons are difficult. A typical alignment telescope locates a line of sight to about 1 part in 800 of the full field at the object distance that the telescope is focused. This works out to roughly 5 seconds, the same as the PSM used as an autocollimator. The PSM has a minimum of 760 pixels across the field and is sensitive to 0.1 pixels when centered on a spherical surface and is thus about an order of magnitude more sensitive than the alignment telescope. The alignment telescope can bring objects on that line of sight into focus one after another as the focus is changed from near (about 16”) to infinity. This is very convenient when all the objects are in a line because no part of the test setup needs to be moved during the alignment. On the other hand, the alignment telescope is nearly useless if the objects needing alignment are in a three dimensional space such as the paths in the prism housing example or in aligning the components of a spectrometer.

The PSM is perhaps best thought of as a null or end point detector in three dimensions and it does this to about 1 μm laterally and a few μm axially. The ideal way to use the PSM is either mounted on the ram of a CMM where it can locate spherical and cylindrical features to better than the accuracy of most CMM’s over any reasonable distance, or in conjunction with a fixture like that described for aligning the prisms. In both cases, the PSM can locate centers of curvature and axes of cylinders to as well as or better than the mechanics of the CMM, or fixtures can establish the desired mechanical datums in three dimensional space. In this sense the PSM has a sensitivity of at least an order of magnitude better than an alignment telescope. Coupled with its small size, light weight, ability to be used as an autocollimator and ergonomically convenient to use display, the PSM can turn tedious assembly and alignment operations into rapid, accurate and easily documented procedures.

5. CONCLUSIONS

We have described the Point Source Microscope and illustrated its usefulness in the alignment of various optical systems by accurately linking mechanical datums to optically functional surfaces and these surfaces to each other. In comparison with other optical tooling, the PSM is a flexible compliment to, rather than replacement for, traditional autocollimators and alignment telescopes. A combination of the PSM’s accuracy and its use aligning the optically significant features of an opto-mechanical system make it possible to achieve higher alignment accuracy than attempting alignment via strictly mechanical features. This leads to systems with better optical performance than can presently be achieved at a reasonable cost.

With insight as to how the PSM works it is clear that the PSM, in a very practical sense, makes many alignment operations easier and quicker to perform to a higher level of accuracy, particularly for optical systems that are distributed in three, rather than two, dimensions, or do not have circular symmetry. Although difficult to document specifically, we have seen the time taken to align complex optical systems drop by a factor of ten while achieving better alignment than more traditional methods. Furthermore, by aligning using the optically functional surfaces of a system, both tolerance build up and the expense of precisely made parts can be largely eliminated.

6. ACKNOWLEDGEMENTS

The telescope referred to in Sec. 3.4 was a team effort of Breault Research Organization, Inc (BRO)16 and Optical Perspectives Group, LLC (OPG). The lead optical engineer on the project was Matthew Dubin of BRO who had many insightful and useful comments regarding the use of the PSM. OPG’s primary responsibility was assembly and test of the system that was performed at BRO with the able assistance of Joe Barcelo. The optical design of the telescope and sensor optics was performed by Richard Buchroeder of Optical Design Service under contract to BRO. The mechanical design of the telescope was done by Kris Tvedt of BRO. The details of the kinematic location features were due to Bryan Loucks, an opto-mechanical design consultant working with OPG.

7. REFERENCES

1 See www.rcopticalsystems.com/ionmill.html, for example
www.qedmrf.com/technology/tech.shtml
3 US Patent pending
4 www.optiper.com
www.nikon-instruments.jp/eng/page/products/list11.aspx
6 www.ptgrey.com/products/flea/index.html
sine.ni.com/nips/cds/view/p/lang/en/nid/12892
www.cerbec.com/TechInfo/TechSpec.asp
9 A. Offner, US Patent 3,748,015
10 D. M. Williamson, “Evolution of ring field systems in microlithography”, Proc. SPIE, 3482, 369-76, (1998).
11 R. E. Parks, “Alignment of off-axis conic mirrors”, Optical Fabrication and Testing Workshop Technical Notebook, OSA, Falmouth, MA Sept. 1980, pp. 139-45. Revised reprint available at www.optiper.com/Documents/Alignment%20of%20Off-axis%20Conic%20Mirrors.pdf
www.optiper.com.
12 R. E. Parks and W. P. Kuhn, “Using a CMM for optical system assembly and alignment”, ASPE Proceedings Spring Topical Meeting on Coordinate Measuring Machines, 29, 3-8, (2003)
13 US Patent Application 20020054296
14 www.davidsonoptronics.com/catalog.htm
15 www.nikonusa.com/template.php?cat=3&grp=30&productNr=6B6D
16 www.breault.com/consulting/consulting-overview.php

Alignment Of Optical Systems

1. Introduction

As optical systems become more complex and packaging requirements more severe and multi-dimensional, proper alignment becomes more challenging. Yet with current improvements in the manufacture and measurement of optical surfaces to nm levels, alignment is one of the few remaining opto-mechanical aspects of optical system manufacture and assembly where improvement in optical performance can be made. There are four approaches to aligning optical systems. These will be described and the advocated method illustrated by examples.

The preferred alignment method overcomes most of the difficulties of traditional methods but requires a new way of thinking about alignment. The method also requires alignment considerations must be studied immediately after the optical design is complete so that the necessary opto-mechanical datums can be incorporated into the mechanical design of the optical system cell, chassis or lens bench.

2. Methods of alignment

While one could argue with these definitions of alignment methods, they illustrate the point to be made. First is “snap together” or drop the elements into a cell which is the method traditionally used from the beginnings of centered optical systems. A cell and lenses are manufactured to tolerances governed by cost and performance considerations and then the lenses are set in the cell against their seats and held down by retainers. One then lives with the assembled performance of the system that is well modeled by Monte Carlo analysis. Since there will be a spectrum of performance outcomes in keeping with the model, optimum system performance will be achieved in only a few of these systems. However, this is the only economical method of assembling large volumes of optical systems.

Another method used on limited quantity, high performance, high cost systems is to assemble lenses into their seats while measuring each lens at its periphery for centration and vertex for spacing, and then testing the performance against a go/no go standard. If the performance falls below the acceptance criteria, the system is taken apart and reassembled as carefully as possible according to the design and tested again. This is a very tedious and costly procedure that exposes the optical components to many sources of damage through dis- and re-assembly.

A third method is a more systematic approach similar to the second but where the performance of the system is measured quantitatively in the pupil plane, possibly at a number of field points. If the system does not perform to an acceptable level optical design software is used to figure out what spacings and misalignments are causing the less than optimum performance, these adjustments are made and the system is tested again. Sometimes a second round of adjustments is necessary as changes in alignment affect performance non-linearly. While this method is more systematic it is still tedious and requires substantial careful testing and analysis of the test results.

The fourth method that this paper advocates for high end, modest production systems is to locate the centers of curvature of each powered optical element at the exact design nominal location, or “true position” in mechanical engineering terms, and each plane mirror tilted and spaced so the beam focuses at the design nominal position after the fold. For centered systems this is most easily done by centering a datum seat in the cell on a rotary table and then checking that the light from the centers (or apparent centers) of curvature of the elements as they are assembled, one by one, do not nutate as the table is rotated as shown in Fig. 1.

This example shows the cementing of a double where the flint element is placed in a centering cup and the cup centered until the reflection of a point source of light conjugate to the convex surface center of curvature (C of C) does not nutate. An auxiliary positive lens is needed to reach the apparent C of C but its focal length is not critical. The flint is then slid in the cup about the convex surface until the reflection of a point source of light at the C of C of the concave side remains still. The flint is then considered centered meaning that the line joining the centers of curvature of the two surfaces (the optical axis) is coincident with the axis of the rotary table. Then the lens is lightly clamped.

A drop of cement is placed in the concave well of the flint and the crown element is set in place. The concave surface of the flint now acts as an aligned centering cup so all that is needed is to make the reflection from the upper crown convex surface remain stationary. Again an auxiliary positive lens is required to access the C of C of the crown. The right hand side of Fig. 1 also shows how the apparent C of C of the flint has moved toward the lens due to the refraction of the crown.

In this example we have referred to placing a point source of light at the C of C of a surface and then watching the behavior of the reflected image. The best way of doing this is with an autostigmatic microscope (ASM), a reflecting microscope with a beamsplitter behind objective and a point source of light produced by a single mode fiber located at the long conjugate of the objective. The return image can be viewed through an eyepiece or via a CCD camera. Fig. 2 shows a schematic illustration of the optical paths in a commercially available autostigmatic microscope.1

3. Aligning two and three dimensional systems

Centered systems are a trivial case of locating C of C’s according to an optical design. Of far greater interest are two and three dimensional systems where the chief ray moves over a plane or in three dimensions. Since three dimensional systems are difficult to diagram successfully on paper, a two dimensional example will be given that amply illustrates the three dimensional nature of the problem. An imaging spectrometer from US Patent 6,288,781 by D. R. Lobb with powered prismatic elements is shown to scale in Fig. 3. Light enters a slit on the face of a plane prism at the upper left of Fig. 3. It passes through a prism with power on both the entrance and exit faces and proceeds on to an arrangement of three spherical mirrors similar to an Offner relay. The light exits through another prism with power on both surfaces to the detector plane.

Fig. 4 shows the spectrometer in perspective and traces the chief ray from the entrance slit through the system to the middle of the detector plane. The line joining the entrance slit and detector plane is the axis of the spectrometer in an alignment, or opto-mechanical, sense just as the optical axis of a single refractive element is the line joining the C’s of C of the two surfaces. This axis defines five degrees of freedom of the spectrometer, three translations and two angles. We define the sixth degree of freedom in that we want the centers of all the elements to be the same height above a mounting plane.

It is obvious that the edging tolerances and mount fabrication for the dispersing elements is going to be difficult as they will have to be located precisely and unambiguously in all six degrees of freedom relative to the spectrometer axis as defined by the slits. Of course the three mirrors also have to be properly aligned but this is a relatively simple matter compared to the prisms.

In order to accomplish this alignment we suggest that the next diagram to draw is the one in Fig. 5 where the C’s of C and axes of all the elements are located relative to the entrance slit and center of the detector, all in the plane of the paper. The centers of curvature of the three Offner relay mirrors are clustered together between the entrance and exits slits. Because the two centers of curvature of the dispersive elements each define three degrees of freedom, all six are defined for each element so they may be located precisely and unambiguously without reference to their edges. To illustrate where the dispersive elements lie relative to their axes we show the full elements in Fig. 6. This also illustrates why these elements would be difficult to fabricate without understanding their geometry. Once the geometry is understood the generating and polishing of the surfaces is not much more difficult than the surfaces of any lens.

4. Alignment of the system

In order to align the system a fixture is made either by drilling holes in the optical bench to which the elements of the spectrometer are mounted or in a fixture to which the optical bench is located by pins. In the holes a precision rod is placed with a conical hole in the upper end to serve as a mount for a bearing ball about 10 mm in diameter. A collar on the rod is used to locate the center of the ball to the height of the plane of centers of curvature. The rod and ball can be moved from hole to hole as one element is aligned after the other.

For the three convex surfaces, an auxiliary positive lens is needed to make the C’s of C accessible as already illustrated in Fig. 1. Holes and rods are also needed to support these auxiliary lenses but their locations need not be very precise as long as the lenses are centered on a normal to the convex surface that is roughly in the center of the surface.

The short conjugate of the objective of an autostigmatic microscope is focused and centered on the center of the ball defining the C of C and pointing toward the element of interest. The ball is removed and the element adjusted until its center of curvature is focused and centered on the autostigmatic microscope display. Fig. 7 illustrates first aligning the autostigmatic microscope to the ball that defines the mechanical location of the C of C, removing the ball and aligning the mirror to the microscope. The microscope acts as the transfer device between the mechanical datum at the C of C and the optical surface. In the case of the refractive elements, having two microscopes makes this procedure much easier because both centers of curvature can be viewed simultaneously, one through the auxiliary lens. The order of alignment is governed only by avoiding the obstruction of the line of sight to the next surface.

When the alignment is complete a point source placed at the entrance slit will be well imaged at the detector. There can be no source of error unless the radii of the elements are substantially out of spec or the wrong glass was used. Since a good autostigmatic microscope can locate centers of curvature to < 1 μm, the translational errors of element locations can be held to about the same level and angular errors to a few seconds of arc (although the scale of the angular error will scale with the system size). The alignment is completely deterministic and does not depend on the type of optical system or even any knowledge of how the system will form an image because light is never put through the system the way it will be used during the alignment.

Alignment of folded systems with plane mirrors

Fold mirrors are plane mirrors used to change the direction of a beam of light and are useful in systems that must be made compact. If a light beam is focused it is defined by three degrees of freedom, the x,y,z coordinates of the focus. Since a plane is also defined by three points we have just enough degrees of freedom with two angles and one translation to change the beam direction and keep the distance from the last powered element to the focus constant. This does not count the two translational degrees of freedom needed to keep the beam centered on the plane mirror but these are not critical adjustments.

While we have been talking about folded systems the example we will use to illustrate the alignment of the plane mirrors was chosen to illustrate not only this section but the next concerning using aberration reduction as an alignment tool. Assume we want to put a deformable plane mirror in a telescope system for atmospheric error correction. This amounts to taking the beam of light coming toward the telescope focal plane and diverting it into a black box that corrects the wavefront and then spits the light back out so it focuses in the same place on the focal plane as it would have without the correction system. Whether the black box is in the system or not should be invisible to the detector. How do we align the fold mirrors to get the light in and out of the black box? A generic adaptive optical system (AOS) is shown in Fig. 8.

The AOS consists of a fold mirror to bend the beam headed toward the telescope focus to the entrance focus of the AOS, an off-axis parabola to collimate the beam, a deformable mirror to correct the wavefront, a second off-axis parabola to re-focus the beam and a final plane mirror to direct the output of the AOS to the telescope focus. If the whole optical bench were moved out of the way the focal plane would be none the wiser except the AOS decreases the f/number of the final beam somewhat. Just as in the imaging spectrometer we have identified an axis of the system with the sixth degree of freedom being the arbitrary angle about the axis.

For alignment purposes, the two plane mirrors must be precisely located so that the AOS does not appear to be in the telescope at all. To do this we first place a concave spherical mirror beyond the first fold mirror (mirror at top of Fig. 9) aligned so its center of curvature coincides with the telescope focus using an autostigmatic microscope (ASM) or similar device. Then we move the ASM so that it is focused at the center of the ball locating the exit focus of the AOS and is pointing toward the right. A second concave sphere is aligned to the microscope in tilt and focus.

Then the microscope is moved back to the telescope focus as now defined by the concave sphere at the top and the plane mirror that folds the beam downward is inserted and adjusted in tilt and translation normal to its surface until the reflection from the concave sphere to the right is aligned on itself in the microscope. Now the microscope is focused on the ball at the entrance focus and is set to point toward the left. The entrance plane mirror is inserted and adjusted in three degrees of freedom until the return image from the concave mirror at the top is re-imaged on itself in tilt and focus. Now the plane mirrors are aligned to the telescope focus and the entrance and exit foci of the AOS. It now remains to align the powered optics of the AOS to the entrance and exit foci.

One aspect of this is to note that the alignment steps must be ordered so that no previously aligned optic interferes with the light path to another optic that needs aligning. This is why we had to use two concave spheres as tooling to align the two plane mirrors. Another aspect to note is that if the distances from the mirror to the foci are not equal it will not be possible to adjust the fold mirror so the chief ray follows the angle given in the design but will be incorrect by some angle dependent on the error in distances. This could come about in the design in Fig. 8 if the lens bench were incorrectly located too close or far from the focal plane. Then the exit fold mirror could still be adjusted so the output focus fell on the telescope focus but the chief ray of the AOS output would not be parallel to the chief ray from the telescope. In most cases a small error will not matter but it is something to be aware of.

Alignment using aberrations

Alignment using aberrations is very useful for locating optical elements with axes, particularly aspheric mirrors either symmetric or off-axis. While we will return to the AOS example momentarily, we give an example of where alignment using aberrations is sometimes seen in optical fabrication shops. The optician will want to test an objective lens with an interferometer for the transmitted wavefront quality. The test is so obvious that many fail to realize how sensitive the test can be to aberrations in the field and are surprised to see astigmatism and/or coma.

As an example, take a 25 mm diameter, f/4 cemented doublet. It can be tested interferometrically in either of two ways, collimated light in or focused light in against a flat, as shown in Fig. 10. Although it is not obvious without very careful examination the doublet is tilted 1º about an axis perpendicular to the page relative to the collimated beam from the interferometer (upper) or the return plane mirror (lower). Yet this misalignment that is not obvious without taking great care in the set up of the test yields substantial transmitted wavefront error that is not intrinsic to the doublet but rather due to its incorrect test. Contour maps of the wavefront aberrations are shown in Fig. 11.

This example is a simple demonstration of the importance of proper alignment to achieve full optical system design performance. Small alignment errors can have disastrous consequences on system performance yet be imperceptible without careful monitoring. This leads to the more interesting example of using aberrations for alignment. We will examine two cases, the alignment of a symmetric parabola to a flat (or collimated source) and the same example with an off-axis parabola to show there is fundamentally no difference in the approach.

Assume we have a symmetric parabola with a central hole for the light to pass through. In this case a common test is to locate the test device focus at the mechanical center of the hole, let the out going light reflect off a flat placed at approximately half the focal distance from the parabola so the light fills the parabola and reflects back to the flat nearly collimated as shown in Fig. 12. The light then retraces itself back to the source when everything is aligned. The optical axis of the test setup is the line joining object and image and this we have located as soon as the image lies on top of the object, something easily seen with an ASM or when there are no tilt fringes in an interferometer.

The optical axis of the test set up must be aligned to the optical axis of the parabola for there to be no aberrations. The first step is to move the plane mirror longitudinally to focus the image and tilt the plane mirror until the object and image are coincident. If there is no coma then the parabola is perfectly aligned to the flat. In general this will not be the case. To finish the alignment the ASM focus (or the parabola) must be decentered in a direction to reduce the coma while the flat is tilted to keep object and image coincident. Moving the microscope in the direction of the point of the coma pattern will decrease the coma. Continue the decentering until the image is symmetrical. The location of the focus defines three degrees of freedom while the two tilts of the flat make up the balance of the five degrees of freedom needed for proper alignment. In this example with a 50 mm diameter, f/2 parabola just 23 μm of decenter (equivalent to 23 seconds in the field) will produce 0.1 waves of coma. This may be acceptable for viewing stars but is totally unacceptable for doing lithography.

Going back now to the AOS where we talked about the positioning of the fold mirrors, there are also two off-axis parabolas that need aligning, see Fig. 8. The location of the focus of each has already been used in the fold mirror alignment. The vertices and C of C’s of these mirrors is also indicated in the Figure. If there is no indication of where the optical axis is on the off-axis mirrors the best approach is to put an ASM at the design location of the C of C of one of the mirrors and adjust the mirror to return the light into the ASM objective. As the mirror is moved longitudinally the combination of astigmatism and coma will produce an image that looks somewhat like a fish as shown in Fig. 13. The tail of the fish points toward the vertex of the off-axis segment.

Once the off-axis mirror is located approximately correctly based on the location of its C of C an ASM is located at the design location of its focus and a plane mirror is used to reflect the nearly collimated light back into the off-axis mirror and ASM objective. The plane mirror should be used exclusively to get the light back into the ASM objective and centered on the display. Typical images might look like the through focus images in Fig. 14.

Adjustments should be made simultaneously to the off-axis parabola and the plane mirror to hold the image centered in the ASM and to orient the largely astigmatic image with the coordinate system, that is, make the astigmatism either horizontal or vertical. Once this is done tilt and decenter of the off-axis parabola and tilt of the mirror are only needed in one direction to shrink the image to a symmetrical, well focused image.2 As the image approaches symmetry it may be necessary to touch up the alignment in the other direction as the astigmatism may rotate as the image symmetry and focus improve due to better alignment.

For the final example5 we take the single pass alignment of a convex secondary in an off-axis Ritchey-Chretien telescope as shown in Fig. 15. In this case we had already aligned the primary mirror and had collimated light entering the telescope parallel with the primary optical axis. The design indicated precisely where the system should focus relative to the primary vertex. The line between the primary focus and the system focus defined the optical axis of the telescope. The secondary axis had to be aligned to this axis in five degrees of freedom to eliminate any aberrations.

With collimated light entering from the right in Fig. 15 the primary and secondary mirrors brought the light to focus in the vicinity of the autostigmatic microscope objective focus. The microscope objective focus had been located via mechanical tooling (see Fig. 7) and does not move once located mechanically. The secondary is then adjusted in focus and either tilt or decenter until the focused light enters the objective and the badly aberrated spot is roughly centered on the viewing screen. When reasonably well focused light is centered in the microscope objective the secondary has been adjusted in three of the five necessary degrees of freedom.

It is then necessary to use a combination of tilt and decenter plus focus to hold the focused spot centered in the objective and to reduce the aberrations, now a combination of focus, astigmatism and coma. The procedure is exactly as described previously above. If the secondary mirror has five adjustment screws and a minimum of backlash it is possible to do the alignment in a matter of minutes.

Determining aberrations from images

It has been suggested that the alignment described in the above sections of the papers can be performed with an ASM or an interferometer. Except for one embodiment of a commercial interferometer (Fisba), interferometers are too large to conveniently adjust accurately and stably in five degrees of freedom, three degrees of translation with high resolution and two degrees of tilt to be sure apertures are approximately uniformly filled with light. Not only is an ASM easier to move conveniently and accurately adjust to the locations necessary for alignment, but the adjustments needed on the optics being aligned are easier to interpret from the image shapes than from interference fringes. Granted that low order aberration quantities can be read off the interferometer monitor and these used to guide adjustments, the hand/eye human interface using the image shapes tend to be more efficient. The only downside to using the image is that it doesn’t give quantitative results as to the aberrations although an ASM is sensitive to wavefront errors of less that λ/8. In this last section we will describe a simple means of extracting pseudo low order aberration content from the images viewed with an ASM.

Two dimensional images have five symmetries; there is a part of the image that does not vary with azimuth and this part corresponds to all the rotationally symmetric parts of an image such as focus, third order spherical and all the higher order spherical aberrations. There remain four symmetries that describe how the image changes when it is flipped left-to-right, top-to-bottom and both left-right and top-bottom3,4. These are even-even and correspond to 3rd order and higher astigmatisms at 0º, odd-odd that are related to astigmatism at 45º, odd-even that are related to 3rd order and higher comas at 0º and even-odd relating to comas at 90 º.

As an example take the image in Fig.16 where the pixels are 4.5 μm square and the image was magnified by a factor of 5 by the ASM. Because the region of interest around the image comprises relatively few pixels it is a quick calculation to find the even-even part of the image and then extract the rotationally symmetric part from that.

Once the rotationally symmetric part of the image is removed the image is further processed simply by flipping and adding or subtracting the flipped images to make four linear combinations of the original to form the four symmetry groups. Fig. 17 shows the four symmetries derived from the image in Fig. 16 after the rotationally symmetric part was removed. As is clear the four images bear a close resemblance to the two orientations of astigmatism and the two orientations of coma. While there are probably a number of ways to derive quantitative information on how big the proportions are of each symmetry type, we simply used the root sum square of the values at each pixel as the criterion.

Now as the alignment of an optical system becomes relatively good the pseudo aberrations derived from the symmetry of the image can be used to help determine the final adjustments of the alignment. Notice that this approach does not carry a sign for the pseudo aberration; all that can be done is to minimize each of the four aberrations. Also, some of the symmetry in the image will depend on how uniformly the pupil of the system is illuminated. Care should be exercised to make sure the ASM axis is well centered on the pupil of the system being aligned. The simplicity of the calculations makes it possible to update the results at TV frame rates.

5. Conclusions

The method of alignment by locating centers of curvature is a strictly deterministic approach to alignment that is particularly helpful for complex, folded and off-axis optical systems. Further, the method does not impose tight (read costly) tolerances on edging or mounts. The same principles can be applied to the alignment of plane, fold mirrors. Finally, using aberrations is an easy way of aligning aspheric optics. It is not presently widely used because the instrument to determine the aberrations is usually an interferometer and they are generally too large to bring to the optics in question. The ideal device to view images is an autostigmatic microscope and, until recently, there have been no commercial sources for these. Because the commercial ASM’s include software as an integral part of the instrument it is not difficult to derive quantitative values for the pseudo aberrations most useful for alignment.

If planning for this deterministic alignment method is incorporated in the opto-mechanical design of optical systems immediately following the lens design itself there need be no further acknowledgements such as the one that appeared in a recent paper about the design, fabrication and assembly of the ARIES imaging spectrometer used on the 6.5 m Multiple Mirror Telescope6, namely, “Thanks, Koby Smith, for banging your head against the wall to align the thing.” If alignment is approached in a logical and systematic manner as part of the opto-mechanical design from the outset of a project there is no need for anyone to bang their head against a wall.

6. References

1R. E. Parks and W. P. Kuhn, “Optical alignment using the Point Source Microscope”, Proc. SPIE, 58770B, (2005).

2R. E. Parks, “Alignment of off-axis conic mirrors”, Optical Fabrication and Testing Workshop Technical Notebook, OSA, Flamouth, MA Sept. 1980, pp 139-45. A revised reprint is available at http://www.optiper.com/alignment%20of%20off-axis%20conic%20mirrors.pdf.

3C. Ai, L. Shao and R. E. Parks, “Absolute testing of flats(II); using odd and even functions”, Optical Fabrication and Testing Workshop Technical Notebook, OSA, Boston, MA 1992.

4C. Ai and J. C. Wyant, “Absolute testing of flats using even and odd functions,” Appl. Opt. 32, 4698- (1993)

5Work performed in collaboration with Breault Research Organization, Tucson, AZ.

6R. J. Sarlot and D. W. McCarthy, “A Cryogenic, 1-5 Micron Atmospheric Dispersion Corrector for Astronomical Adaptive Optics,” in Current Developments in Lens Design and Optical Engineering II, R. E. Fischer, R. B. Johnson, W. J. Smith, eds., Proc. SPIE 72, 4441 (2001).

Using The Point Source Microscope (PSM) To Find Conjugates Of Parabolic And Elliptical Off-axis Mirrors

ABSTRACT

Although the PSM is primarily an alignment instrument, it can also be used to determine the conjugates of parabolic and elliptical off-axis mirrors. By positioning the PSM at the sagittal and tangential foci of the mirrors, the conjugate distances of the mirror can be found using a laser range finder, for example. Knowing the sagittal and tangential radii of curvature (Rs and Rt), the vertex radius (Rv) is easily calculated. This information is used to verify that the mirror has been correctly manufactured and to aid in positioning the mirror in an optical system. Examples are shown of these steps.

1. INTRODUCTION

The alignment of off-axis aspheres is a subject that few people want to address because it is so different than aligning symmetric optics. An off-axis asphere has an optical axis, as opposed to a sphere that has no optical axis, just a center of curvature. Furthermore, the optical axis of the off-axis asphere usually does not pass through the surface of the mirror and certainly is not parallel to the normal to the surface at the center of the off-axis segment. On the other hand, off-axis aspheres are extraordinarily useful for many optical designs, and familiarity with them is essential for many optical systems.

This paper is an attempt to take some of the mystery out of off-axis parabolas and ellipses in terms of their geometry, and how to use their geometry to aid in their alignment. We will start by discussing some of the geometry that makes off-axis mirrors unique, and then describe how to find and measure the conjugates that are analogues to the center of curvature for a sphere. As opposed to a sphere with a center of curvature, an off axis asphere has two conjugates that define its axis, the two astigmatic foci at the centers of curvature of the tangential and sagittal radii of curvature. With the knowledge of how to find these conjugates, and a method of measuring the radii of curvature, it is possible to see that the mirror was manufactured correctly, and to see how the mirror should be aligned into the optical system for which it is intended.

2. GEOMETRY OF AN OFF-AXIS PARABOLA

Fig. 1 is a scale drawing of an off-axis parabola looking at a meridional section and along the optical axis (black vertical line). The off-axis section is the circle at the right edge of the pie section looking along the optical axis. It is aligned with the three vertical lines that defined the inner and out meridional extents of the off-axis section. The parent parabola is green and the blue circle has a radius equal to the vertex radius of the parabola while the purple circle segment, whose tangential radius is labeled Rt, is the best fit circle to the center of the off-axis segment. The light blue rays stopping at the optical axis define the sagittal radius of curvature, Rs.

The three radii are related by Rt = Rs^3/Rv^2 which makes it easy to find an unknown radius if the other two are known1. If a point source of light is placed on the axis of the parabola, a line image will form at the axis (light blue line perpendicular to the Rs ray). In general, the image will not be a line until the aperture of the off-axis section is masked, or stopped, down to a diameter where the coma in the off-axis asphere does not affect the astigmatism. How big a hole in the mask can be determined empirically, or an estimate of the coma may be made referring to Ref. 2.When the point source of light and the return line image are superimposed, the point source is on the normal to the surface at the center of the hole in the mask. The distance from the surface to the point source/line image is the sagittal radius, Rt. The astigmatic line image will lie in the meridional plane and is helpful in determining the azimuth of the vertex of the offaxis segment as well as determining the sagittal radius.

If the point source of light is moved back along the normal until the astigmatic line image is in focus it will be seen to be perpendicular to the meridional plane. The distance from the point source/line image here is the tangential radius, Rt. Since Rs = sqrt(Rv^2 + h^2) where h is the off-axis distance it is easy to find h.

3. GEOMETRY OF AN OFF-AXIS ELLIPSE

The geometry of an off-axis ellipse is a little more complex but the same basic geometry applies. Fig. 2 is a scale drawing of one of the parts we actually measured using the PSM and FARO arm. The green rays show the extent of the off-axis section relative to the foci to give a feel for the scale. The rays that bisect the rays going to the foci are those seen from the center of curvature of the off-axis segment. The right side of Fig. 2 shows the caustic region to give a better idea of the locations of the sagittal and tangential centers of curvature relative to the center of curvature of the vertex sphere.

As with the parabola, the sagittal foci lie on the axis of symmetry, or optical axis, while the tangential foci lie of the far side of the axis. From the way an ellipse focuses light from one focus to the other, we know the normal to the surface is the perpendicular bisector of the rays between the foci as shown. Just as with the parabola, we can find Rs and Rt, and using these values we can find Rv = (Rs^3/Rt)^1/2. For the ellipse we still need to find the conic constant, k, and the distance off-axis, h. To do this we make a mask as in the case of the parabola and measure Rs and Rt at 2 or 3 locations, h and ±delta h, where delta h is known. Two measurements will give an exact solution, while 3 or more will give a least squares solution using the relation that Rv^2 –k*h^2-Rs^2 = 01. The simplest method is to use 2 measurements at either edge of the off-axis ellipse and find the solution using the quadratic equation. One thing to remember is that delta h measured off the optic will be larger than it actually is, the distance from the axis of symmetry. Entering delta h as 1.4x less than the width of the optic is probably a good guess for a start.

Clearly with a concave ellipse this approach will get you close because the foci have to lie on the same line, the optical axis, as the sagittal foci. Also, for any given h, the line joining Rs and Rt lies on the normal to the surface. This will help locate the foci approximately. With this information it is then more precise to try to find the foci directly using the information derived from Rs and Rt. Using a point source such as the end of a single mode fiber at one focus and a microscope at the other focus it should be possible to locate the 2 foci to the precision necessary to meet system tolerances.

4. MEASURING THE SAGITTAL AND TANGENTIAL RADII

Using an autostigmatic microscope such as the PSM3, point the microscope at the mirror and locate the return image. Once the microscope is adjusted so the reflected point source is centered on the objective, focus the microscope to find either the sagittal or tangential focus. In general the reflected image will be too blurred to find a clean line image. Mask the mirror with an aperture small enough to produce a line return image. Adjust focus to get clean looking images such as that in Fig. 3.

When the microscope is well focused, bring a distance measuring device such as a laser distance measurer, or laser range finder4, up in front of the microscope and position it axially to get a focused Cat’s eye reflection off the rear of the distance measurer. Then take a distance reading to the mirror through the hole in the mask. Since most distance measurers calculate the distance from the rear surface of the instrument, the measurer reading is the sagittal or tangential radius, depending on which image is in focus. Fig. 4 shows how the measurement is made schematically.

Once these measurements have been made, the results may be compared with the prescriptions for the off-axis segments to see if the manufactured mirrors are to specification using the equations in the first part of the paper. It turned out in our case that one mirror was in spec and the other was not. Luckily it turned out that the specification was tighter than it needed to be and the mirror did not limit the performance of the system.

Once these measurements have been made, the results may be compared with the prescriptions for the off-axis segments to see if the manufactured mirrors are to specification using the equations in the first part of the paper. It turned out in our case that one mirror was in spec and the other was not. Luckily it turned out that the specification was tighter than it needed to be and the mirror did not limit the performance of the system.

5. USE OF THE SAGITTAL AND TANGENTIAL FOCI FOR ALIGNMENT

There are at least two ways the focus information can be used for the alignment of off-axis mirrors. First, the measurements can be used directly by adding alignment features to the optical bench that the mirrors will be installed in. Since the two foci produce line images in reflection, we can use polished cylindrical artifacts to simulate the line foci. An inexpensive source of suitable artifacts are “plug gauges”5, cylinders about 50 mm long in diameters ranging from <1 mm to 25 mm or more. These are used the same way polished balls are as physical realizations of points to focus a PSM on, but in this case the cylinders are realizations of lines. Kinematic mounts should be made so 2 plug gauges are positioned where the sagittal and tangential foci are supposed to be located in the finished mirror system.

To align an off-axis segment, a PSM is focused on the line image formed at the axis of the plug gauge, the gauge is removed and the mirror adjusted so its focus appears in the same location as the line formed by the plug gauge. Fig. 5 shows a typical image on reflection from a plug gauge. The mirror can be located in 3 degrees of freedom, axially, one degree of translation, and one degree of rotation about the normal to the mirror surface. Once one focus is adjusted, the PSM is moved to the second plug gauge, and focused on it. The gauge is removed and the mirror adjusted by rotating around the first focus until second focus is correctly positioned laterally. This process may take some iteration because it may be difficult to make the mirror rotate around the first focus although with sufficient forethought the mirror mount could be designed with this adjustment built in.

A second method of alignment, an indirect one, is what we did. We located plug gauges at the two foci and then measured the locations of the gauges relative to fiducials on the mirrors. Fig. 6 shows how a plug gauge was adjusted to be at the same location as the line image formed by the mirror sagittal focus, in this case. This meant that when the mirrors were installed in their optical bench using the fiducials around the edges of the mirrors, we were effectively positioning the foci to their correct positions in space.

6. RESULTS OF MEASUREMENTS ON AN OFF-AXIS MIRRORS

The mirrors we measured were about 250 mm square and CNC machined out of 6061-T6 aluminum and then smoothed and polished by hand to a specular surface. One of the mirrors is seen behind the mask in the left hand part of Fig. 6. The ultimate use did not require the polish as they are to go in a terahertz wavelength (857 μm) radio telescope. On the other hand, we wanted to be sure the mirrors were sufficiently good to meet the telescope spec, and had been correctly machined and not deformed by the polishing.

Following the procedure described above we got the results shown in Tables 1 and 2. The standard deviation in terms of setting at the best focus of the line focus was about ±4 mm for the parabola and ±10 mm for the ellipse. The distance measuring laser gauge gave consistent readings within ±1 mm. Thus both mirrors had larger errors in their radii than could be attributed to measurement error. On the other hand, the radius errors amount to sag errors over the full aperture of 30 and 50 μm in the case of the ellipse, and 160 and 190 μm in the case of the parabola, compared with λ = 857 μm.

After reviewing these errors in manufacture in the optical design code it was felt that with a minor spacing adjustment the mirrors would work just fine as they were. This finding coupled with the knowledge of where the fiducials were relative to the radii of curvature meant that the system would perform as expected and could be successfully aligned.

7. CONCLUSION

We have shown how to determine the vertex radius of curvature and off-axis distance of off-axis parabolas by measuring the sagittal and tangential radii of curvature with an autostigmatic microscope such as the PSM. We have gone on to show how the conic constant may be determined as well by making multiple measurements of the radii of curvature for more general conics. This information is useful as part of incoming inspection to see if the optics ordered are the optics delivered. Further, we have shown how the locations of the radii of curvature can be used as a tool in aligning the offaxis mirrors into their optical systems using two different approaches to alignment.

REFERENCES

  1. Smith, W., Modern Optical Engineering, 2nd Ed., McGraw-Hill, New York, 445-6 (1990)
  2. Parks, R. E., Evans, C. J. and Shao, L., “Test of a slow off-axis parabola at its center of curvature”, Appl. Optics, 34, 7174-8 (1995).
  3. See www.optiper.com
  4. For example, see http://www.cpotools.com/bosch-dlr130k-digital-distance-measurerkit/ bshndlr130k,default,pd.html?start=1&cgid=bosch-locators-and-measurers 
  5. See, for example, http://www.mcmaster.com/#plug-gauges/=dbxtba

Method Of Alignment Using A Laser Tracker System

1. Introduction: 

Laser trackers are an accurate and efficient tool for finding the locations of features in a threedimensional space but they rely on Spherically Mounted Retroreflectors (SMR) to return the laser beam to the tracker. If the feature cannot be contacted or it is not convenient to use an SMR another method must be used to follow the beam. We describe methods using a dual imaging and autostigmatic microscope for locating the features and two methods for tracking the microscope location depending on the type of tracker used. This converts a contact probe, large area CMM into a non-contact CMM by coupling a laser tracker with a dual purpose autostigmatic microscope. We begin with a brief description of the microscope followed by the alignment of the microscope to tracking and scanning laser metrology stations.

2. Point Source Microscope: 

The imaging, autostigmatic microscope in question is called a Point Source Microscope (PSM)1 and has both a single mode fiber as a point source of light for the autostigmatic function and a LED behind a diffuser to provide Kohler illumination for imaging. The sources may be used independently or simultaneously. In the autostigmatic mode the PSM has lateral sensitivity of <1μm and similar axial sensitivity with an auxiliary lens for finding the centers of curvature of tooling balls or optics like mirrors and lenses. In the imaging mode the lateral sensitivity depends on the objective used but is in the neighborhood of a couple microns and the Cat’s eye reflection from a surface gives axial sensitivity to a similar resolution. It remains to show how to couple this non-contact ability to locate centers of curvature, the optically important feature of a lens or mirror for alignment purposes, to a high level of sensitivity to laser tracker systems that can determine locations in 3-dimensional space to similar sorts of accuracies.

3. Follower type laser tracking systems: 

A follower type laser tracker is similar to a surveyor’s theodolite but is more sophisticated in that it is active. It sends out a laser beam along the telescope axis and the telescope will follow the beam if it is retroreflected back using a corner cube (generally a SMR that has the feature that the apex of the cube corner is accurately located at the center of the ball or spherical mount). The tracker will also measure distance using an interferometer mode if the SMR is moved from the tracker calibration SMR nest to a nest mounted on the measurand without breaking the laser beam. Fig. 1 shows how the follower tracker scheme works in general.

3.1 Alignment of the PSM to an SMR: 

SMR’s are made in several convenient sizes, ½”, 7/8” and 1½” diameters, along with corresponding SMR “nests”, usually steel cones with a magnet at the apex to hold the SMR seated in the cone. A nest and corresponding SMR are mounted at a convenient location and the tracker is locked onto the SMR and its location in 3-D is noted. The SMR is removed from the nest and a grade 25 or better steel ball of the same diameter is placed in the nest so that its center is in the same location as the SMR. Then the PSM is adjusted so the focus of the objective is located at the ball center, something that can be done to <1μm in all three dimensions.

3.2 Alignment of the tracker to the PSM: 

Attached to the PSM is a plate with a plane mirror in a mount that can be adjusted in tip, tilt and piston and a nest and an SMR. The plane mirror, shown schematically in Fig. 1, is nominally located half way between the objective focus and the SMR on the plate and perpendicular to a line between the focus and SMR. This arrangement is shown in Fig. 2. The mirror reflects the tracker laser beam back toward the SMR on the plate. The plane mirror is adjusted until the reflection from the SMR on the plate has the same apparent location as the SMR originally located at the PSM focus. The mirror is then adjusted such that the tracker sees the virtual image of the SMR at the objective focus. Now the assembly of PSM, plane mirror and SMR can be moved at a unit and the tracker will follow the PSM focus in all three dimensions as long as the PSM is not rotated so far that the tracker laser beam walks off the plane mirror.

4. Scanning type tracker system: 

A scanning type tracker system uses several high speed rotating prism stations to sweep line images around a workspace. The prism scanners are accuracy synchronized with a clock. In the work space are detectors that resister when a beam sweeps by. Comparing the prism clocks and detector signals the detector locations can be accurately determined by time delay triangulation.

4.1 Alignment of the detectors to the PSM: 

With the scanning system, three detectors are fastened to the side of the PSM facing two scanning prism stations. The PSM is focused on the center of a conveniently located steel ball. In this position the detectors are scanned by two scanning stations a known distance apart. Since three detectors on the PSM are scanned the plane of the detectors is determined relative to the scanning stations. The PSM with detectors attached is then moved to a different orientation while still being focused at the center of the ball and another set of data is taken to determine the plane of the detectors. This operation is repeated for a third orientation of the PSM while the PSM is centered on the ball. The three planes defined by the detectors will appear to rotate about the center of the ball, that is, a normal to each of the planes through the center of the ball are all equidistant as shown in Fig. 3.

This means the center of the ball, or focus of the objective, can be determined from the three measurements and once the distance from the center to the planes of the detectors is determined and recorded, any other position of the PSM can be related back to the center of the ball. This calibration is completely analogous to the initial use of a master ball and a touch probe on a Coordinate Measuring Machine (CMM) to establish the zero of the CMM coordinate system.

4.1.1 Using the calibrated PSM: 

Once the center has been determined by this calibration, when the PSM is moved to any other location and the positions of the three detectors determined the location of the focus can be related to the center of the ball in all three coordinate directions. Any software that might be used with a CMM can also be used to analyze the data the scanner tracker gathers. This makes it possible to use the PSM precisely as a non-contacting probe with an apparent zero probe tip radius for any sort of coordinate measurements over large distances.

5.0 Conclusion: 

We have shown how an autostigmatic microscope, and in particular, the Point Source Microscope (PSM) as a non-contact probe, can be used with laser tracker systems, either the follower type or the scanning type. In the first case an auxiliary mirror and tracker ball are used to make the tracker think it is looking at the focus of the PSM. In the second case, the PSM is calibrated in a way analogous to using the master ball on a CMM and then the PSM can be used as a zero radius probe tip for non-contact coordinate measurements over large distances. In both cases the PSM can be used either to find a center of curvature to 1 micron sensitivity in three dimensions or used in the imaging mode to locate a feature on a surface to 2 o3 microns in all three dimensions. The fact that the PSM images and can be set in all three coordinates to micron precision makes it a valuable part of an extension to contacting laser tracker systems.

6.0 References

1. Optical Perspectives Group, LLC, Tucson, AZ 85750, www.optiper.com.
2. J. Burge, et. al., Use of a commercial laser tracker for optical alignment, Proc. SPIE, 6676, 6676OE, (2007).

Swing Arm Optical Coordinate-Measuring Machine: High Precision Ground Aspheric Surfaces Using A Laser Triangulation Probe

ABSTRACT

The swing arm optical coordinate-measuring machine (SOC), a profilometer with a distance measuring interferometric sensor for in situ measurement of the topography of aspheric surfaces, has shown a precision rivaling the full aperture interferometric test. To further increase optical manufacturing efficiency, we enhance the SOC with an optical laser triangulation sensor for measuring test surfaces in their ground state before polishing. The calibrated sensor has good linearity and is insensitive to the angular variations of the surfaces under testing. Sensor working parameters such as sensor tip location, projection beam angle, and measurement direction are calibrated and incorporated in the SOC data reduction software to relate the sensor readout with the test surface sag. Experimental results show that the SOC with the triangulation sensor can measure aspheric ground surfaces with an accuracy of 100 nm rms or better.

© 2012 Society of Photo-Optical Instrumentation Engineers (SPIE). 
[DOI: 10.1117/1.OE.51.7.073603]

Subject terms: swing arm profilometer; profilometry; aspherics; optical testing; laser triangulation sensor; ground surface metrology.

Paper 120473 received Mar. 30, 2012; revised manuscript received May 16, 2012; accepted for publication May 30, 2012; published online Jul. 6, 2012.

1 Introduction

In the field of optical metrology for aspheric optics fabrication, most of the interferometric tests (visible spectrum range) that provide high-accuracy measurement are used after the test surface is polished. But at the polishing stage, the surface shape, or figure, correction is slow. It is desirable to measure the surface accurately during grinding to minimize figure errors and speed up fabrication.

Different techniques have been developed for testing ground surfaces. One traditional method is to use an infrared interferometer. However, as with visible interferometers, null optics are needed for measuring the aspheric shape. The design and alignment of the null optics are complex and time consuming. The limited infrared material choices and the nonvisible light make the use of the infrared interferometer even more difficult.

A laser tracker or laser tracker plus system1 such as the one used for the Giant Magellan Telescope primary mirror segment is another way to measure a mirror during grinding. The basic idea uses a commercial laser tracker system with the spherically mounted retroreflector (SMR) touching the mirror surface. Since it is a point by point test, it takes time to collect a large number of samples.

There is a new prototype called SLOTS2 based on reflection deflectometry using a long-wave infrared source scanning technique to measure the surface slope variation of ground surfaces. It is a simple, fast, low-cost, and non-null system that can measure surface slopes to microradian precision. The method is promising but needs further development.

The swing arm optical CMM (SOC),3–5 developed at the University of Arizona, is a profilometer with a distance measuring interferometric sensor. It is used for in situ measurement of highly aspheric mirrors, and it has shown a performance rivaling full aperture interferometric tests. The interferometric sensor has high precision and a high data rate, but it only works for polished surfaces. A contact sensor, with a linear variable differential transformer (LVDT), has been used with the SOC to measure ground surfaces, but the measurement is time consuming, because the probe is picked up after each point to avoid scratching the surface.

Different types of sensors have been studied for ground surface metrology. There are some sensors based on the confocal principle6 with linearity at the submicron level. There are sensors based on laser triangulation that have a resolution of 10 nm and are insensitive to surface angular variation. The triangular sensors work on both polished and ground surfaces and were chosen and calibrated7 for use in our application. The laser triangulation technique has been used for many applications, such as inspection of free-form surfaces8,9 and blind guidance.10 The measurement uncertainty due to speckle noise, the test lateral resolution, and the aspect of the test sensitivity to the surface texture distribution have been investigated.11–13 For high-precision optical surface measurement applications like astronomical telescope mirror metrology, the only work reported are some simulations showing the potential measuring accuracy using different types of triangulation sensors.14,15

This paper shows the results of calibrating a triangulation sensor and using it to measure large ground mirrors. The paper is organized as follows: In Sec. 2, we review the basic principle of the SOC and laser triangulation sensors. In Sec. 3, we describe the calibration of a triangulation sensor and show some metrology results compared to an interferometric null test of a highly aspheric mirror. Finally, conclusions are drawn in Sec. 4.

2 Principles

2.1 Principle of the SOC

The basic geometry of the swing-arm profilometer is shown in Fig. 1. A sensor is mounted at the end of an arm that swings across the optic under test such that the axis of rotation of the arm goes through the center of curvature of the optic. The arc defined by the sensor tip trajectory, for a constant sensor reading, lies on a spherical surface defined by this center of curvature. For measuring aspheric surfaces, the sensor that is aligned parallel to the normal to the optical surface at its vertex reads only the surface departure from spherical. The SOC uses this simple geometry with an optical, noncontact, interferometric sensor that measures continuously across the optic. The optic or test part is rotated in azimuth after each profile is measured. Figure 2 shows an example of the profiling pattern we generally use during a test. Since the arcs cross each other while the sensor scans the mirror edge to edge, we know the surface heights must be the same at these scan crossings. The crossing height information is used to stitch the profiles into a surface using a maximum likelihood reconstruction method.3,16,17 Figure 3 shows the results of using the SOC and a full aperture interferometric null test to measure a 1.4-m diameter aspheric surface that has an aspheric departure of 300 μm. The SOC test shows excellent agreement with the interferometric test. The direct subtraction of the maps from the two methods, after alignment terms have been removed, shows a difference of only 9 nm rms, much of which appears to come from the interferometric test.

2.2 Principle of the Laser Triangulation Sensor

Laser triangulation is widely used in various applications to measure distances to objects. A common triangulation principle is to project a light spot on to the object and extract the distance information from the reflected or scattered light.14

High measuring rates, high spatial resolution, large measuring range, and zero applied force are significant advantages of the laser triangulation sensor over other types of distance measuring sensors.

There are two types of triangulation sensors normally used. The first one is an orthogonal sensor, in which the output plane is perpendicular to its optical axis. The second one has a tilted sensor, in which the output plane is tilted according to the Scheimpflug principle. Tilting of the output plane eliminates defocus and makes the sensor insensitive to the angular variations of the test surface due to the imaging effects.14 The sensor investigated and used on the SOC is the second type.

The geometry of the sensor measuring method is shown in Fig. 4. The incident beam with angle θ hits the surface at the sensor’s tip position O, where the sensor reads zero, and then reflects or scatters back and passes through an imaging lens inside the sensor. Finally, the beam falls on the detector of the sensor. The measuring axis is the bisector of the incident and reflected beam. By knowing the spot tip position and incident beam angle, we can trace the ray to O’ when the surface moves up to S2. The ray will reflect or scatter at the surface and be collected by the imaging lens if the distance d is within the sensor’s dynamic range. The sensor’s detector plane is tilted and is conjugate with the OO’ plane according to the Scheimpflug principle. The difference of the spot positions is a function of the displacement d, the projection beam angle, the magnification of the optical system, and the focal length of the imaging lens as described by Mikhlyaev.14 The commercial triangulation sensor is usually calibrated so that the output signal is linear with the test surface displacement.

3 Calibration

The sensor’s linearity, angular sensitivity, and scaling effect were measured experimentally. The zero position (tip position) of the sensor projected beam, the direction of the projected beam, and the measurement axis were calibrated and used as the input for the SOC data reduction. Finally, the system performance with the triangulation sensor was verified by measuring test surfaces with known shapes. The flow Fig. 1 Basic geometry of the swing-arm profilometer. chart in Fig. 5 shows the outline of the calibration steps.

3.1 Linearity

A distance measuring interferometer (DMI)18 was used to check the linearity of the triangulation sensor. The DMI has accuracy at nanometer level. The setup is shown in Fig. 6.

The DMI and the triangulation sensor were aligned to be able to measure simultaneously the motion from a double-sided flat mirror, which was mounted on a flexure. The flexure was driven with a voice coil and function generator to oscillate sinusoidally with a peak-valley motion of 2 mm at a frequency of a few Hz. One side of the double-sided flat mirror was specular as the target for the DMI, while the other side of the flat was ground for evaluating the triangulation sensor.

We budgeted a signal difference of 10 nm or less from the test system alignment and the motion effect. (The sensor has a 10 nm resolution.) The motion of the flexure with the flat mirror was designed and checked with an alignment telescope to show an angular variation of a few arc-seconds. The DMI and the triangulation sensor are aligned to each other to minimize the cosine errors and Abbe errors.

Figure 7 shows an example of the signals obtained from the DMI and the triangulation sensor.

The readout difference from the direct subtraction of the DMI and triangulation sensor data was ∼60 nm rms as shown in Fig. 8. The difference was dominated by the random noise from the environment and the ground mirror surface roughness, because the incident beam from the triangulation sensor moves across the mirror as it is oscillated. Later we show that when the sensor is mounted on SOC and tests a polished surface, a precision of 20 nm rms is achieved when an average of eight single measurements is used.

3.2 Calibration of the Geometry of the Sensor

3.2.1 Sensor tip location and the direction of the projected beam

When measuring a test surface, as seen in Fig. 9, the coordinates of the point of measurement are a function of the sensor position, the direction of the projected light beam relative to the surface, and the test surface shape. Following the SOC coordinate calibration concept described by Su et al.,4,5 we calibrated the relationship between the sensor nominal tip position when the sensor reads zero and the direction of the projected light beam relative to reference features on the sensor case, namely, three laser tracker spherically mounted retroreflectors (SMRs). When the sensor is installed on the SOC, the coordinate relationship is used to determine the sensor tip location and angle of the projected beam relative to the surface under testing. This is done by measuring the three SMRs’ locations with a laser tracker. Then at each scan position, the coordinates of the point of measurement on the test surface can be calculated with a simple ray tracing algorithm in the SOC data reduction code.

To perform the calibration, we used a point source microscope (PSM)19 and a laser tracker.20 As shown in Fig. 10, a piece of 25-μm thick translucent shim stock was located between the sensor and the PSM. The shim stock was positioned normal to the sensor’s measuring axis. The sensor was mounted on an x, y, z stage that brought the sensor up to the shim stock until the sensor read zero. Then a PSM was brought up to focus on the backside of the shim stock, so the PSM was focused on the effective sensor measuring spot as seen through the shim stock. When the sensor and the PSM were in these positions, the locations of the three SMRs on the sensor were measured with the laser tracker. Then the sensor was moved out of the way, and the center of a solid steel ball was positioned at the focus of the PSM objective. Then the solid ball was removed from the SMR nest and replaced with an SMR.

The SMR was measured with the laser tracker as shown in Fig. 11. Now the laser tracker has information about the measuring spot location at the zero height reading of the sensor relative to the SMR nests on the sensor. By moving the shim stock to different sensor height locations of the projected beam and repeating the above procedures, several locations along the projected beam were measured, and the direction of the projection beam was determined. The thickness of the shim stock was backed out during the data processing. The accuracy of the calibration in terms of the SOC coordinates was determined to a few microns.

3.2.2 Sensor measurement axis

The readout of the sensor is the displacement d along the axis of the sensor as shown in Fig. 9. Thus it is important to calibrate the sensor measurement direction relative to the sensor axis and align the sensor axis to the SOC test system. This calibration was initially done using the setup in Fig. 6. After the DMI and the triangulation sensor were aligned to minimize the readout difference between the two sensors, we used a laser tracker to measure the three SMRs’ locations on the sensor. Then the double-sided flat mirror and the sensor were removed, and a reference flat mirror was put far from the DMI but normal to the DMI beam as shown in Fig. 12. We used a tracker ball touching the mirror surface to find the mirror surface normal. The sensor’s measuring axis was parallel to the DMI axis and the mirror surface normal. The projected angle θ shown in Fig. 6 can be calculated from these results and the direction of the projected beam.

3.3 Scaling Effect

A scaling factor is introduced if the sensor is tilted relative to the test surface. As seen from Eq. (1), the scaling factor can be derived from the triangulation sensor test geometry. The scaling sensitivity was tested by tilting the sensor relative to the double-sided flat as shown from Fig. 13.

In Fig. 13, θ is the beam projection angle, and φ is in the plane of rotation angle of the sensor. (The sensor readout is insensitive to the out-plane rotations for small angles.) This scaling effect needs to be taken into account during the SOC alignment to the test part. It has a sensitivity of ∼0.015∕ deg for the particular sensor we used. As the test surface aspheric departure gets larger, the scaling effect from the sensor angular alignment becomes more significant. For instance a test surface with a 2 mm peak-valley aspheric departure and with 0.01 deg alignment errors will have scaling induced errors up to 0.3 μm in P-V. This scaling sensitivity puts a long-term stability requirement on the SOC. The test triangulation sensor system is sensitive to the angular drift between the sensor and the test surface.

As seen from Eq. (1), the projection angle can also be checked by varying some known angles between the sensor and the double-sided mirror and then reading out the scaling factor from the difference between the sensor and the DMI readings.

3.4 Angular Dynamic Range

A large angular working range from the sensor is desired, as we would like the sensor to continue to work when the test surface normal is not parallel to the measurement axis of the sensor. This is the situation for the SOC when the surface has a large departure from a sphere or a flat. As seen from Fig. 9, we need to know the angular range over which the sensor reads out the surface sag d, independent of the slope of the surface. The triangulation sensor we are using has the property that the detector plane is conjugate with the testing location, which is along the line of the projected beam as shown in Fig. 4. Due to this imaging relationship, the sensor is insensitive to the local slope variations of the test surface.

A possible experiment layout for testing the sensor angular range based on the existing setup is shown in Fig. 14. However, the angular range of the DMI is only a few minutes of arc and cannot support the large angular range we would like to investigate.

Another approach might be using a wedged double-sided mirror. However, multiple samples would be needed for sampling the angular range we are interested in, and the sampling is not continuous.

Instead, we decided to test the angular range by measuring a ground optical surface with a known shape as described below. The results show that the sensor maintains good linearity over the angular range tested of about +?3 deg.

3.5 System Calibration

3.5.1 Calibration under a CMM with a ground spherical surface

The initial system test was done using a CMM as the scanning device before the sensor was verified for service on the SOC as shown in Fig. 15. The x and y linear stages of the CMM were used to scan and record the coordinates of the mirror under testing. (The coordinates were further corrected with ray tracing.) The CMM z axis was locked, and the surface sag was read out by the sensor. A spherical convex ground surface was measured for calibration. The radius of curvature and diameter of the sample mirror was chosen so that the 2 mm sensor working range and a 3 deg angular range could be checked by scanning the full aperture of the mirror.

The data were collected continuously along the x axis for different y values using the CMM. Figure 16 shows an example of the data obtained from the scans. Each line in the figure corresponds to a particular x scan with a fixed y value. This shows the sag value seen by the sensor relative to the angle between the sensor axis and the normal to the sphere being tested. The performance of the sensor for different working angles is checked by this sampling strategy.

The setup offered a simple way of collecting a large number of data points rather quickly. In addition, it was easy to calculate the theoretical sag of the sphere at each point to compare with the measured values. After removing the ideal spherical shape, the difference map in Fig. 17 shows an rms difference of 0.62 μm. The errors are dominated by the scanning errors from the CMM rails, the deflection of the sensor due to moments induced by the readout cable, and the ground surface roughness. No systematic errors due to sensor angular dynamic range issues were noticed.

3.5.2 Measuring an aspheric surface

To check the system performance, we attached the calibrated sensor to the SOC to guide the grinding of a 1-m diameter 80 μm P-V aspheric surface. Figure 18 shows the comparison of the measurements from the SOC and from a null interferometric test when the mirror was in its polishing stage. The results show the SOC and interferometer data agree with each other to 100 nm rms or better. This shows that the triangulation sensor is reliable for measuring both ground and polished surfaces.

4 Conclusion

The SOC is an important metrology technique for highly aspheric surface testing because of its versatility and high accuracy. It is configurable for measuring concave, convex, and plano surfaces. It can make in situ measurements, and its high-precision performance can rival full aperture interferometric tests. We have shown how the measurement range of the SOC can be extended to ground surfaces by using a calibrated laser triangulation sensor, and we have shown how to carry out that calibration. The experimental data show that the SOC equipped with a triangulation sensor can measure a test surface to a precision of better than 100 nm rms. This significantly improves the optical fabrication efficiency by extending precision metrology into the grinding cycle of the fabrication.

References

1. T. L. Zobrist et al., “Measurements of large optical surfaces with a laser tracker,” Proc. SPIE 7018, 70183U (2008).

2. T. Su et al., “Scanning long-wave optical test system: a new ground optical surface slope test system,” Proc. SPIE 8126, 81260E (2011).

3. P. Su et al., “Swing arm optical CMM for aspherics,” Proc. SPIE 7426, 74260J (2009).

4. P. Su et al., “Swing arm optical coordinate-measuring machine: modal estimation of systematic errors from dual probe shear measurements,” Opt. Eng. 51(4), 043604 (2012).

5. P. Su et al., “Swing arm Optical CMM: self calibration with dual probe shear test,” accepted to Proc. SPIE 8126, 81260W (2011).

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7. Keyence America, “High-speed, high-accuracy CCD laser displacement sensor,” Keyence America (2012) http://www.keyence.com/ products/measure/laser/lkg/lkg.php,
http://www.micro-epsilon.com/ displacement-position-sensors/laser-sensor/index.html.

8. N. Van Gestel et al., “A performance evaluation test for laser line scanners on CMMs,” Optic. Laser. Eng. 47, 336–342 (2009).

9. B. Muralikrishnan et al., “Dimensional metrology of bipolar fuel cell plates using laser spot triangulation probes,” Meas. Sci. Technol. 22, 075102 (2011).

10. J.-H. Wu et al., “The application of laser triangulation method on the blind guidance,” Proc. SPIE 8133, 81330V (2011).

11. R. G. Dorsch, G. Häusler, and J. M. Herrmann, “Laser triangulation: fundamental uncertainty in distance measurement,” Appl. Optic. 33, 1306–1314 (1994).

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Calculation Of The Vertex Radius Of An Off Axis Parabolic Surface Using The Sag Measured With A Three Ball Spherometer

Abstract

We describe a method of calculating the vertex radius of an off-axis parabolic segment using a three ball spherometer to measure the sag. The vertex radius is found by solving a set of six simultaneous, non-linear equations for the three coordinates of one of the ball centers and the corresponding three coordinates of the point of tangency of the ball with the surface.

1. Introduction

Three ball spherometers are the 1” micrometers of an optical shop and have been used for over 100 years to measure the radii of spherical surfaces.1,2 The radius of curvature of a spherical surface can be calculated from a simple, three term formula that includes the measured sagitta, or sag, the distance from the central micrometer or indicator and the center of the balls and the radius of the balls.3,4 Until recently, in spite of the simplicity of the formula that includes a square in one term, spherometers were sold with tables that converted sag readings into radii because optical shop personnel often did not have the skills or time to solve the formula. With the advent of pocket calculators it is now easy to solve the sag equation.

The sag equation is rather simple because the spherometer balls touch the surface at normals to the surface, and for a sphere these go through the center of curvature of the sphere and through the centers of the balls on the spherometer. In the case of an aspheric surface this is not so; the ball centers still lie on the normals to the aspheric surface but the normals do not go through the center of curvature of the asphere. The solution to this problem requires the solution of six non-linear, simultaneous equations, again something not easily undertaken even by rather mathematically adept optical engineers. However, with the advent of equation solvers such as the “Solver” function in Microsoft Excel, solution of these simultaneous equations is straight forward and fast. This is the problem we will illustrate.

2. Measured surface sag (T)

The measured sag, T, is the difference between the spherometer indicator reading when the spherometer is sitting on a plane surface, Fig. 1 (left), and when the spherometer is resting on the aspheric surface to be measured (right). We have shown the case for a convex surface but identical conditions hold for a concave surface with the exception that the sign of the indicator movement is opposite.

3. Geometry of the three ball spherometer

Referring to Figure 2, the spherometer has three balls on the points of an equilateral triangle. D is the diameter of the circle through the centers of the balls, S is the length of the side of the triangle and the distance between ball centers, P is the height of equilateral triangle, Ω the distance from the center of the triangle to the balls and r is the radius of the balls. B10 is the center of the ball located on the meridional plane of the parabolic segment and the vertex of the parabola lies above this ball. B20 and B30 are ball centers located symmetrically with respect to the meridional plane. Relationships of the sides of the spherometer are given below.

4. Geometry of the spherometer resting on the parabolic surface

We use a Cartesian coordinate system where z is the axis of symmetry of the paraboloid and y lies in the meridian plane. The origin is coincident with the vertex of the parent parabolic surface. When the spherometer is first set on the parabolic segment we place ball B10 on the meridional plane with the tip of the indicator approximately centered on the segment. At first we know only that XB10 = 0, YB10 is approximately P less than the center of the segment and ZB10 is r higher along the normal to the surface than where the ball touches the surface, ZF10 = YB10^2/(2Rv) where Rv is the vertex radius of the parabola.

Referring to Fig. 3 we see the spherometer in two states, the final one (subscript 1) sitting on the surface and an initial one (subscript 0) where the calculation is begun. We start by assuming the plane of the three spherometer balls is perpendicular to the normal to the surface at F10. This allows us to calculate a starting position for B20, and by shifting the plane of the ball centers downward by r, the starting position for F20.

Then we assume the spherometer is iteratively rotated down to the surface about the center of B10. The point of contact, F10, will not change nor will the dimensions of the spherometer. However, as the spherometer is rotated so the other two balls rest on the surface the calculated dimensions of the spherometer will change. Since the spherometer dimensions cannot change we have a method of solution by simultaneously solving the six equations below for the centers and points of tangency of the floating balls.

5. Calculation of points of tangency to the parabolic surface of the equilateral triangle base

The six unknown variables are

and they are found by solving six equations simultaneously. The six equations are

The relationship of the ball center to the point of tangency along the normal to the surface

where α, β and γ are the angles of the normals to the surface at F21. Finally the distances between the balls

Once the six unknowns are found it is straight forward to find the coordinates of the center of the spherometer and project the indicator down to the surface of the parabolic segment normal to the plane of the ball centers. In general, the tip of the indicator will not hit the center of the segment exactly and a new value will have to be used for YB10 and the calculation repeated until the tip is close enough to the desired location. Notice too that we have calculated the sag assuming the vertex radius is correct. If the measured sag is different from the desired, the Rv in eq. 5 must be changed until the results match the measured sag.

6. Summary

We have shown how the sag of an off-axis parabolic segment as measured with a three ball spherometer may be used to determine the vertex radius of the segment. While this is not as easy as for a spherical surface, the calculation is well within the capabilities of an optical engineer with access to iterative equation solving software.

7. References

1. Grubb, H., Nature, 34, 85 (1886)

2. Ritchey, G. W., Smithsonian Contributions to Knowledge, 34 (1904)

3. Horne, D. F., “Optical Production Technology”, p. 324, Crane, Russak & Co., Inc., New York 1972

4. Malacala, D. “Optical Shop Testing”, p. 818, 3rd ed., Wiley-Interscience, 2007.