US20010013581A1 - Charged-particle-beam exposure device and charged-particle-beam exposure method - Google Patents
Charged-particle-beam exposure device and charged-particle-beam exposure method Download PDFInfo
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- US20010013581A1 US20010013581A1 US09/826,913 US82691301A US2001013581A1 US 20010013581 A1 US20010013581 A1 US 20010013581A1 US 82691301 A US82691301 A US 82691301A US 2001013581 A1 US2001013581 A1 US 2001013581A1
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01J—ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
- H01J37/00—Discharge tubes with provision for introducing objects or material to be exposed to the discharge, e.g. for the purpose of examination or processing thereof
- H01J37/02—Details
- H01J37/04—Arrangements of electrodes and associated parts for generating or controlling the discharge, e.g. electron-optical arrangement, ion-optical arrangement
- H01J37/147—Arrangements for directing or deflecting the discharge along a desired path
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B82—NANOTECHNOLOGY
- B82Y—SPECIFIC USES OR APPLICATIONS OF NANOSTRUCTURES; MEASUREMENT OR ANALYSIS OF NANOSTRUCTURES; MANUFACTURE OR TREATMENT OF NANOSTRUCTURES
- B82Y10/00—Nanotechnology for information processing, storage or transmission, e.g. quantum computing or single electron logic
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B82—NANOTECHNOLOGY
- B82Y—SPECIFIC USES OR APPLICATIONS OF NANOSTRUCTURES; MEASUREMENT OR ANALYSIS OF NANOSTRUCTURES; MANUFACTURE OR TREATMENT OF NANOSTRUCTURES
- B82Y40/00—Manufacture or treatment of nanostructures
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01J—ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
- H01J37/00—Discharge tubes with provision for introducing objects or material to be exposed to the discharge, e.g. for the purpose of examination or processing thereof
- H01J37/02—Details
- H01J37/21—Means for adjusting the focus
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01J—ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
- H01J37/00—Discharge tubes with provision for introducing objects or material to be exposed to the discharge, e.g. for the purpose of examination or processing thereof
- H01J37/30—Electron-beam or ion-beam tubes for localised treatment of objects
- H01J37/304—Controlling tubes by information coming from the objects or from the beam, e.g. correction signals
- H01J37/3045—Object or beam position registration
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01J—ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
- H01J37/00—Discharge tubes with provision for introducing objects or material to be exposed to the discharge, e.g. for the purpose of examination or processing thereof
- H01J37/30—Electron-beam or ion-beam tubes for localised treatment of objects
- H01J37/317—Electron-beam or ion-beam tubes for localised treatment of objects for changing properties of the objects or for applying thin layers thereon, e.g. for ion implantation
- H01J37/3174—Particle-beam lithography, e.g. electron beam lithography
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01J—ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
- H01J2237/00—Discharge tubes exposing object to beam, e.g. for analysis treatment, etching, imaging
- H01J2237/02—Details
- H01J2237/024—Moving components not otherwise provided for
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01J—ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
- H01J2237/00—Discharge tubes exposing object to beam, e.g. for analysis treatment, etching, imaging
- H01J2237/15—Means for deflecting or directing discharge
- H01J2237/1502—Mechanical adjustments
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01J—ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
- H01J2237/00—Discharge tubes exposing object to beam, e.g. for analysis treatment, etching, imaging
- H01J2237/15—Means for deflecting or directing discharge
- H01J2237/1504—Associated circuits
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01J—ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
- H01J2237/00—Discharge tubes exposing object to beam, e.g. for analysis treatment, etching, imaging
- H01J2237/21—Focus adjustment
- H01J2237/216—Automatic focusing methods
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01J—ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
- H01J2237/00—Discharge tubes exposing object to beam, e.g. for analysis treatment, etching, imaging
- H01J2237/30—Electron or ion beam tubes for processing objects
- H01J2237/304—Controlling tubes
- H01J2237/30472—Controlling the beam
Abstract
Description
- 1. Field of the Invention
- The present invention generally relates to charged-particle-beam exposure devices, and particularly relates to a charged-particle-beam exposure device which forms a pattern on a wafer by exposing the wafer to charged particles.
- 2. Description of the Related Art
- As the circuit density of semiconductor integrated circuits increases, a finer processing technique is required. Compared to the light exposure method widely used in the manufacturing of LSI chips, the charged-particle exposure method has much superior characteristics in terms of the resolution and the focus depth. With respect to the resolution, a processing limit of the photolithography method is about 0.3 μm, while processing as fine as 0.1 μm can be achieved in the charged-particle-beam exposure method.
- However, the charged-particle-beam exposure method is inferior compared to the light exposure method in terms of an exposure positioning accuracy, an overlay accuracy, and a field stitching accuracy. Because of this, the charged-particle-beam exposure method is not widely used in the field for manufacturing purposes of LSI chips.
- The charged-particle-beam exposure device has a smaller area to be able to be exposed at one time, compared to a light exposure device such as a stepper. (This area is called a deflection field hereinafter.) Thus, in order to expose one LSI chip, stage movement is required to successively shift the deflection field on the LSI chip. In doing so, if the connecting precision across borders of the deflection fields is low, severance of wires and/or short-circuits are generated which greatly degrades the yield of the chips.
- In order to improve the yield, the connecting precision at the field borders must be enhanced, which requires a higher precision of the deflection of the charged-particle beam. In the charged-particle-beam exposure device, the charged-particle beam is generally deflected by a magnetic field generated by coils. The coils include two systems for x-direction deflection and for y-direction deflection. Separate currents are applied to these two systems to deflect the beam in the x direction and the y direction independently. Unfortunately, the amount of beam deflection is not in proportion to the amount of current applied to the deflection coils, but is represented as a complex function of the current amount.
- In order to deflect the beam with a high precision, the amount of the current applied to the deflector must be corrected. There are two types of corrections. One is a distortion correction for establishing a linear relation between the input and the deflection amount, and the other is a deflection-efficiency correction for correcting coefficients for linear factors. The distortion correction is a time consuming process since it requires data collection at various points within the field. However, the data needs to be collected only one time since a time variation of the distortion is small. On the other hand, correction coefficients can be obtained in a short period of time for the deflection-efficiency correction. However, the deflection-efficiency-correction coefficients must be frequently obtained because the deflection efficiency varies over time due to a change in thermal distribution of the deflector, etc.
- In order to calibrate the deflection field, coordinates of the deflector are generally matched with coordinates of the stage, whose measure and orthogonality are guaranteed through the laser-interferometer system. In order to measure the coordinates of the deflector, an actual position of the charged-particle beam must be obtained by directing the beam to mark positions on a wafer and detecting reflected charged particles.
- FIG. 1A is an illustrative drawing for explaining a method of detecting mark positions through the charged-particle-beam scan. As shown in FIG. 1A, the charged-particle beam is scanned by the deflector over a
mark 306 formed as a groove in a reference chip 305.Reflection detectors adder 302. A signal after the addition is successively obtained in synchronism with the scan of the deflector, providing a reflection signal form to be analyzed. When such a process is conducted by using the position-detection mark 306 as shown in FIF. 1A, a reflection signal form as shown in FIG. 1B is obtained. The reflection signal form obtained in this manner is analyzed by an analyzingdevice 303 to detect a center position of the mark. A result of the analysis is sent from the analyzingdevice 303 to a control-purpose computer 304, which uses the result in processes such as a correction of the beam. In general, a groove (dent) formed in a wafer (silicon) is used as a mark. - The detection of the position mark described above is conducted at various points by shifting the mark on a wafer through stage movement. In this manner, the deflection-efficiency-correction coefficients for correcting the linear factors and a distortion map of the deflector for the distortion correction are obtained.
- In the mark-position-detection method described above, the detected mark positions contain errors. This is because a relative position of the mark with respect to the reflection detectors changes when the mark is detected at various points.
- When the mark is detected at various points, an angle at which charged particles are reflected by the mark toward a reflection detector varies depending on a relative position of the mark with respect to the reflection detector. When reflected charged particles are detected in a configuration as shown in FIG. 2A, signal forms as shown in FIG. 2B are obtained. As shown in figures, a reflection signal having a symmetric form without a distortion can be obtained when the mark is positioned at an equal distance from the two reflection detectors. When the mark is positioned at other locations, however, a reflection signal form having an asymmetry is obtained. This is because the angle of the reflection is different for the different reflection detectors.
- In addition to the problems of errors regarding the mark-position detection, there is a problem concerning the focusing of the charged-particle beam in the charged-particle-beam exposure device.
- FIG. 3 is an illustrative drawing showing a configuration for the focusing of the beam in the related-art charged-particle-beam exposure device. AS shown in FIG. 3, an optical system310, using a type of light not affecting a resist, is provided between a wafer and a charged-particle lens. The optical system 310 includes a
light source 311 and a light detector 312. When the wafer is exposed to the charged-particle beam, thelight source 311 illuminates light on the wafer, and the light detector 312 detects light reflected from the wafer to measure the height of an exposed surface. Based on the height of the exposed surface, a focusing distance of the charged-particle lens is changed. - Such a related-art charged-particle-beam exposure device has such problems as:
- a) when the focusing distance of the reflection path is changed, the deflection path of the charged-particle beam is affected to cause a displacement of the beam position on the wafer surface; and
- b) since structures under the exposed surface have complex patterns in a LSI device, light reflected from these patterns has an adverse effect of causing errors in the detection of the height.
- The problem a) will be described below. In the charged-particle-beam exposure device, deflection coordinates X=(X, Y), having an origin at the axis of the beam optical system, are entered into a correction circuit to obtain corrected deflection coordinates X′=(X′, Y′).
- X′=Gx*X+Rx*Y+Dx(X, Y) (1)
- Y′=Ry*X+Gy*Y+Dy(X, Y) (2)
- Here, G=(Gx, Gy) are correction coefficients concerning the gain, R=(Rx, Ry) are correction coefficients concerning the rotation, and D=(Dx, Dy) are distortions of higher orders other than the gain and the rotation. In the charged-particle-beam exposure device, a current proportional to the corrected deflection coordinates X′=(X′,Y′) is applied to the deflector to direct the beam at a desired position X=(X, Y) on the wafer.
- When the focusing distance of the lens is changed, the beam cannot be directed to the desired position X. Thus, G, R, and the distortion D(X) must be changed in accordance with the change in the focusing distance.
- In order to direct the charged-particle beam at a desired position X on a wafer surface having a given focusing distance (height) f, the correction coefficient G, the correction coefficient R, and the distortion D(X) at various heights f must be measured. In this manner, correction coefficients having the height as a variable, i.e., the correction coefficient G(f), the correction coefficient R(f), and the distortion D(X, f), are obtained. Taking these measurements, however, increases the time for adjusting the beam deflection, and leads to the correction circuit being more complex.
- The problem b) will be described below. Instead of using the optical system of FIG. 3 to take the real-time measurement of the height at the time of exposure, reference marks provided on each chip to be exposed can be used for the measurement of the height. Namely, the height of each chip is measured by using the reference marks arranged at four corners of the chip to carry out the focusing and the correction. Since the reference marks have the same predetermined structure irrespective of the chips, the use of such marks allows an easy measurement of the height. In this method, however, the reference marks at the four corners must be detected for the measurement of the height each time the exposure is made. Thus, the processing time is increased. Also, the same as the method of measuring the height in real time, errors in the measurements lead to deviation of the focusing. Further, in case that the heights of the reference marks are not measured for some reason, the focusing on the chip surface cannot be carried out.
- In addition to the problems of the mark-position-detection errors and the focusing described above, there is another problem concerning the accuracy of exposed patterns in the charged-particle-beam exposure device.
- FIG. 4 is an illustrative drawing for explaining a process of the charged-particle exposure on a wafer. The wafer is divided into areas of a 20-mm square. Here, an IC chip pattern or the like exposed on the wafer generally has a size ranging from a 5-mm square to a 20-mm square. When the IC chips are small, four to nine chips are included together in one area. When the IC chips are large, one chip is included in one area. At the time of exposure, the corrections of the gain, the rotation, the distortion are carried out for each area on the wafer. In general, the exposure data is set for each area unit.
- The charged-particle-beam exposure device generally has a main deflector capable of deflecting the beam within a large region and a sub-deflector capable of deflecting the beam at high speed within a small region. The main deflector first directs the beam at a predetermined desired position, and, then, the sub-deflector draws a pattern around the predetermined desired position. In FIG. 4, one area is divided into cells (hereinafter called cell fields), in each of which the main deflector can deflect the beam. When a center point of one cell field is aligned with the axis of the beam optical system, the main deflector can deflect the beam over this cell field. Each cell field has a size of a 1-to-2 mm square. Thus, one area is comprised of about. 100 cell fields. Further, the cell field is divided into sub-fields having a size of about a 100 μm square. The sub-deflector can deflect the beam within the sub-field.
- The measurements of the deflector-correction data prior to the exposure are conducted within the cell field. Based on the correction data, the correction coefficients of the main-deflector coordinates, the sub-deflector coordinates, and the distortion relative to the stage coordinates are determined. Normally, the correction coefficients of the main deflector are set for each area, and the correction coefficients of the sub-deflector are set for each cell.
- The exposure is conducted for a frame, which is a region comprised of a plurality of cell fields arranged in a line. Since the width of the frame is the same as that of a cell field, the beam can be deflected by the main deflector within the width of the frame. For the exposure along a longitudinal direction of the frame, the wafer is successively shifted in the longitudinal direction of the frame through the stage movement. Namely, for the exposure in a transverse direction of the frame, the main deflector deflects the beam for positioning thereof, and the sub-deflector is used for the exposure. For the exposure in the longitudinal direction of the frame, the wafer is successively moved by the stage. After a completion of a one frame exposure, the stage takes a U turn to move the wafer in an opposite direction.
- In general, the accuracy of the exposed pattern must be within a 10% tolerance of the exposed pattern. For example, when a 0.15-μm pattern is exposed, the accuracy must be higher than 0.015 μm. In order to achieve this accuracy, the beam correction described above must be precisely conducted. Moreover, there is an effect of a thermal drift of the deflectors during the wafer exposure. Thus, the correction coefficients of the main and sub-deflectors obtained prior to the exposure must be updated during the exposure.
- In order to achieve a high precision, therefore, the updating of the correction coefficients must be conducted for each cell or more frequently. The correction coefficients stored in a correction operation circuit must be updated during a break of the exposure such as between the cells or between the sub-fields. Unfortunately, the updating of the correction coefficients is a time consuming process. Thus, frequent updating leads to an increase in exposure time, thereby degrading the performance.
- In order to obviate this problem, all the correction coefficients may be calculated and transferred to the correction operation circuit during a time period from a data collection prior to the exposure to the beginning of the exposure. Assuming that 40 coefficients are required for one cell, for example, these 40 coefficients must be calculated for about 4000 points when a 6-inch wafer is used. This means that 1-to-5 seconds are required for the calculation. The data transfer also needs a similar time period. Furthermore, a large-volume memory for storing the correction coefficients is needed in the correction operation circuit. Also, when the correction coefficients are updated during the exposure, all the correction coefficients need to be rewritten after the collection of the correction data.
- As described above, there are problems of the mark-position-detection errors, the focusing of the beam, and the setting of the correction coefficients in the related-art charged-particle-beam exposure device. A combination of these problems leads to defects of the generated exposure pattern. When counter measures are taken to avoid these defects, the time required for the adjustment and the exposure is increased, and the device becomes undesirably complex.
- Accordingly, there is a need for a device and a method of exposing the charged-particle beam which can create accurate exposure patterns with high productivity.
- Also, there is a need for a device and a method of exposing the charged-particle beam which can achieve high-accuracy beam focusing and high-accuracy beam positioning without requiring a long time for beam-deflection adjustment.
- Also, there is a need for a device and a method of exposing the charged-particle beam which can accurately detect a mark position.
- Also, there is a need for a device and a method of exposing the charged-particle beam which can use correction coefficients provided for small units of areas without sacrificing the exposure processing time.
- It is general object of the present invention to provide a charged-particle-beam exposure device which can satisfy the needs described above.
- It is another and more specific object of the present invention to provide a device and a method of exposing the charged-particle beam which can create accurate exposure patterns with high productivity.
- It is still another object of the present invention to provide a device and a method of exposing the charged-particle beam which can achieve high-accuracy beam focusing and high-accuracy beam positioning without requiring a long time for beam-deflection adjustment.
- In order to achieve the above objects according to the present invention, a method of exposing a wafer to a charged-particle beam by directing to the wafer the charged-particle beam deflected by a deflector includes the steps of arranging a plurality of first marks at different heights, focusing the charged-particle beam on each of the first marks by using a focus coil provided above the deflector, obtaining a focus distance for each of the first marks, obtaining deflection-efficiency-correction coefficients for each of the first marks, and using linear functions of the focus distance for approximating the deflection-efficiency-correction coefficients to obtain the deflection-efficiency-correction coefficients for an arbitrary value of the focus distance.
- In order to achieve the same objects according to the present invention, a device for exposing a wafer to a charged-particle beam by directing to the wafer the charged-particle beam deflected by a deflector includes a focus coil provided above the deflector, a unit for arranging a plurality of first marks at different heights, a unit for focusing the charged-particle beam on each of the first marks by using the focus coil, a unit for obtaining a focus distance for each of the first marks, a unit for obtaining deflection-efficiency-correction coefficients for each of the first marks, and a unit for obtaining the deflection-efficiency-correction coefficients for an arbitrary value of the focus distance by using linear functions of the focus distance for approximating to the deflection-efficiency-correction coefficients.
- According to the method and the device described above, the deflection-efficiency-correction coefficients for any focus distance are obtained by simply measuring the deflection-efficiency-correction coefficients and the focus distances for the marks arranged at different heights. Thus, the method and the device can achieve high-accuracy beam positioning without requiring a long time for beam-deflection adjustment.
- The above method further includes the steps of positioning a second mark at a center of an optical system of the charged-particle beam, obtaining a first position and a first focus distance of the second mark by focusing the charged-particle beam on the second mark through the focus coil, obtaining a second position of the second mark after shifting the second mark to a second focus distance different from the first focus distance, and using a linear function of the focus distance for approximating to a displacement of the charged-particle beam based on the first position, the second position, the first focus position, and the second focus position to obtain the displacement for an arbitrary value of the focus distance, obtaining a reference focus distance for each of the reference marks provided on the wafer by focusing the charged-particle beam on each of the reference marks through the focus coil, using a function of coordinates on the wafer for approximating the reference focus distance through a least square method to obtain an exposure focus distance for an arbitrary point on the wafer, and carrying out positioning and exposure of the wafer by using the exposure focus distance, the deflection-efficiency-correction coefficients for the exposure focus distance, and the displacement for the exposure focus distance.
- The above device further includes a unit for positioning a second mark at a center of an optical system of the charged-particle beam, a unit for obtaining a first position and a first focus distance of the second mark by focusing the charged-particle beam on the second mark through the focus coil, a unit for obtaining a second position of the second mark after shifting the second mark to a second focus distance different from the first focus distance, a unit for obtaining a displacement of the charged-particle beam for an arbitrary value of the focus distance by using a linear function of the focus distance for approximating to the displacement of the charged-particle beam based on the first position, the second position, the first focus position, and the second focus position, a reference-focus-distance obtaining unit for obtaining a reference focus distance for each of reference marks provided on the wafer by focusing the charged-particle beam on each of the reference marks through the focus coil, a unit for obtaining an exposure focus distance for an arbitrary point on the wafer by using a function of coordinates on the wafer for approximating the reference focus distance through a least square method, and a unit for carrying out positioning and exposure of the wafer by using the exposure focus distance, the deflection-efficiency-correction coefficients for the exposure focus distance, and the displacement for the exposure focus distance.
- According to the method and the device described above, the displacement of the charged-particle beam is approximated to by the linear function of the focus distance, and, also, the exposure focus distance on the surface of the wafer is approximated by the function of coordinates on the wafer. Thus, higher orders of the deflection distortion dependent on the height need not be measured, so that the time required for the adjustment of the entire system can be shortened. Also, failure to focus the beam at the time of exposure is avoided so as to greatly reduce the blurring of patterns.
- It is still another object of the present invention to provide a device and a method of exposing the charged-particle beam which can accurately detect a mark position.
- In order to achieve the above object according to the present invention, a method of exposing a wafer to a charged-particle beam by directing to the wafer the charged-particle beam deflected by a deflector, the method comprising the steps of positioning a position-detection mark at predetermined locations, the position-detection mark including heavy metal buried in a substrate which has lower reflectivity than the heavy metal, the heavy metal and the substrate having the same flat surface, and detecting positions of the position-detection mark by using the charged-particle beam.
- In order to achieve the same object according to the present invention, a device for exposing a wafer to a charged-particle beam by directing to the wafer the charged-particle beam deflected by a deflector, the device comprising, a wafer stage carrying the wafer to move the wafer, and a position-detection mark provided on the wafer stage, the position detection mark including heavy metal buried in a substrate which has lower reflectivity than the heavy metal, the heavy metal and the substrate having the same flat surface.
- According to the method and the device described above, the position detection mark is formed from the heavy metal and the substrate, so that a difference in the reflection intensity between the heavy metal and the substrate can be detected at a time of mark detection. Thus, the use of such a position detection mark eliminates errors in the mark-position detection.
- It is a further object of the present invention to provide a device and a method of exposing the charged-particle beam which can use correction coefficients provided for small units of areas without sacrificing the exposure processing time.
- In order to achieve the above object according to the present invention, a device exposes a wafer to a charged-particle beam deflected by a deflector, in which each of the frames defined on the wafer is successively exposed to the charged-particle beam while the wafer is continuously shifted through stage movement. The device includes an obtaining unit for obtaining data regarding correction of the deflector in order to correct positioning of the charged-particle beam for a precise exposure of the wafer, a data storing unit for storing the data, a coefficient calculating unit for calculating, based on the data stored in the data storing unit, correction coefficients of the correction for a first frame of the frames prior to an exposure, and for calculating, based on the data stored in the data storing unit, the correction coefficients of the correction for a n+1-th (n:integer) frame of the frames during a period when a n-th frame of the frames is being exposed, a coefficient storing unit for storing the correction coefficients, and a correction calculating unit for correcting the charged-particle beam to expose one of the frames based on the correction coefficients calculated while an immediately previous one of the frames is being exposed.
- In order to achieve the same object according to the present invention, a method exposes a wafer to a charged-particle beam in a charged-particle beam exposure device having a main deflector deflecting the charged-particle beam within a first area and a sub-deflector deflecting the charged-particle beam within a second area smaller than the first area, an exposed surface of the wafer being divided into areas, each of the areas being divided into cell fields, each of cell fields corresponding to the first area and being divided into sub-fields, each of the sub-fields corresponding to the second area, the cell fields being arranged in a plurality of lines defining frames on the wafer, each of the frames being successively exposed to the charged-particle beam by moving the wafer through stage movement. The method includes the steps of obtaining data regarding corrections of the main deflector and the sub-deflector prior to an exposure of the wafer in order to correct positioning of the charged-particle beam for a precise exposure of the wafer, calculating correction coefficients of the corrections for a first frame of the frames based on the data prior to the exposure of the wafer, calculating the correction coefficients for a given frame of the frames based on the data while a frame immediately before the given frame is being exposed, and correcting the charged-particle beam to expose one of the frames based on the correction coefficients calculated while a frame immediately before the one of the frames is being exposed.
- According to the method and the device, when densely provided complex correction coefficients are set in the device for enhancement of exposure precision, the calculation and storage of the correction coefficients are carried out in parallel with other processes required for the exposure. Therefore, a large amount of calculation is carried out, and the correction coefficients are set, without increasing the processing time for the exposure. That is, high-speed processing the same as the prior-art device can be achieved. Furthermore, since the correction coefficients for only two frames are stored, a large volume memory is not necessary for the storage of the correction coefficients.
- Other objects and further features of the present invention will be apparent from the following detailed description when read in conjunction with the accompanying drawings.
- FIG. 1A is an illustrative drawing for explaining a method and a device for detecting a mark position through charged-particle-beam scan;
- FIG. 1B is an illustrative drawing showing a signal form for detecting a mark position obtained by the device of FIG. 1A;
- FIGS. 2A and 2B are illustrative drawings for explaining asymmetry observed in the signal form when the mark position is detected;
- FIG. 3 is an illustrative drawing showing a configuration for the focusing of the beam in a related-art charged-particle-beam exposure device;
- FIG. 4 is an illustrative drawing for explaining a process of the charged-particle exposure on a wafer;
- FIG. 5 is an illustrative drawing showing a charged-particle-beam exposure device using a contrast-detection-type mark according to a first principle of the present invention;
- FIGS. 6A and 6B are illustrative drawings showing examples of the contrast-detection-type mark formed in a reference chip;
- FIG. 7 is a flowchart of a process of exposing a wafer in the charged-particle-beam exposure device of FIG. 5 according to a first embodiment of the present invention;
- FIG. 8 is a flowchart of another process of exposing the wafer in the charged-particle-beam exposure device of FIG. 5 according to a second embodiment of the present invention;
- FIG. 9 is an illustrative drawing of a charged-particle-beam exposure device according to a first embodiment of the second principle;
- FIG. 10 is a flowchart of a process of obtaining deflection-efficiency-correction coefficients as well as a displacement by using the device of FIG. 9;
- FIGS. 11A through 11C are illustrative drawing showing chips and marks used in the process of FIG. 10;
- FIG. 12 is a flowchart of an exposure process for a wafer by using the device of FIG. 9;
- FIGS. 13A and 13B are illustrative drawings for explaining a method of detecting a just focus value of the charged-particle beam;
- FIG. 14 is an illustrative drawing of a charged-particle-beam exposure device according to a second embodiment of the second principle;
- FIG. 15 is a block diagram of an exemplary charged-particle-beam exposure device for conducting an exposure process according to a third principle of the present invention;
- FIG. 16 is a block diagram of a correction-coefficient calculating and setting unit according to a first embodiment of the third principle;
- FIG. 17 is a block diagram of a coefficient storing unit according to a second embodiment of the third principle;
- FIG. 18 is a block diagram showing an example in which a dual-port memory is used as frame-coefficient storing units of FIG. 17;
- FIG. 19 is an illustrative drawing showing portions in one area where frame exposures begin and end;
- FIG. 20 is a block diagram of a portion for controlling the updating of cell-correction coefficients and area-correction coefficients according to a third embodiment of the third principle of the present invention;
- FIG. 21 is a block diagram of a variation of the third embodiment of the third principle;
- FIG. 22 is a table showing an example of a correction-coefficient pattern set by a correction-coefficient-pattern storing unit of FIG. 21;
- FIG. 23A is a circuit diagram of an example of a dual-port memory controlled by the configuration of FIG. 17;
- FIG. 23B is a chart showing data to be stored in the dual-port memory of FIG. 23A;
- FIG. 24 is an illustrative drawing showing a first related-art method of obtaining a map of deflection-efficiency-correction coefficients of a sub-deflector;
- FIG. 25 is an illustrative drawing showing a second related-art method of obtaining a map of deflection-efficiency-correction coefficients of the sub-deflector;
- FIG. 26 is an illustrative drawing showing a fourth principle of the present invention;
- FIG. 27 is an illustrative drawing showing a fifth principle of the present invention;
- FIG. 28 is a block diagram of an exemplary charged-particle-beam exposure device carrying out a deflection-efficiency correction according to the fourth and fifth principles of the present invention;
- FIG. 29 is an illustrative drawing showing a mark-position detecting portion of a charged-particle-beam exposure device of FIG. 28;
- FIG. 30 is an illustrative drawing showing a reference chip provided with four position-detection marks according to the fourth principle of the present invention;
- FIG. 31 is a flowchart of a process of correcting a deflection efficiency of a sub-deflector of FIG. 28 according to a first embodiment of the fourth principle;
- FIG. 32 is an illustrative drawing for explaining calculations of correction coefficients;
- FIG. 33 is a flowchart of a process of correcting the deflection efficiency of the sub-deflector of FIG. 28 according to a second embodiment of the fourth principle;
- FIG. 34 is a flowchart of a process of correcting the deflection efficiency of the sub-deflector of FIG. 28 according to a third embodiment of the fourth principle;
- FIG. 35 is a flowchart of a process of correcting the deflection efficiency of the sub-deflector of FIG. 28 according to an embodiment of the fifth principle;
- FIG. 36 is an illustrative drawing showing a configuration of an example of a charged-particle-beam exposure device using a block exposure technique;
- FIG. 37 is an illustrative drawing showing an example of a block mask of FIG. 36;
- FIG. 38 is a block diagram of an exemplary driving unit of a main deflector of FIG. 36;
- FIGS. 39A through 39C are time charts showing signals observed at various points of FIG. 38;
- FIG. 40 is an block diagram of a main part of a charged-particle-beam exposure device according to a first embodiment of a sixth principle of the present invention;
- FIGS. 41A through 41D are time charts showing signals observed at various points of FIG. 40;
- FIG. 42 is a block diagram of a main part of a charged-particle-beam exposure device according to a second embodiment of the sixth principle of the present invention;
- FIG. 43 is a block diagram of an example of a data-timing-adjustment circuit of FIG. 42 shown with memories;
- FIG. 44A is a time chart showing a clock provided from a clock unit of FIG. 36 to a digital-to-analog converter and a clock generating circuit of FIG. 42;
- FIG. 44B is a time chart showing an output signal observed at a node D of FIG. 42 when a pulse generating circuit of FIG. 42 is not provided;
- FUG.44C is a time chart showing a clock provided from the clock generating circuit to a DAC of FIG. 42;
- FIG. 44D is a time chart showing a correction pulse signal output from an IV converter of FUG.42;
- FIGS. 45A and 45B are time charts showing output voltages obtained through a simulation;
- FIG. 46 is a flowchart of a process of obtaining optimal pulse parameters;
- FIG. 47 is a block diagram of a main part of a charged-particle-beam exposure device according to a third embodiment of the sixth principle of the present invention;
- FIG. 48 is a flowchart of a process of obtaining the optimal pulse parameters according to the third embodiment of the sixth principle;
- FIG. 49 is a block diagram of a main part of a charged-particle-beam exposure device according to a fourth embodiment of the sixth principle of the present invention;
- FIG. 50 is a flowchart of a process of obtaining the optimal pulse parameters according to the fourth embodiment of the sixth principle;
- FIGS. 51A and 51B are circuit diagrams showing configurations of the dynamic-mask stigmator DS of FIG. 36;
- FIGS. 52A through 52D are charts showing the ringing of an output signal of an amplifier of FIG. 51A for various turn numbers of the coils LX1 through LX4 of FIG. 51A;
- FIG. 53 is a circuit diagram of the dynamic-mask-focus coil DF of FIG. 36;
- FIG. 54 is a circuit diagram of a main part of a charged-particle-beam exposure device according to a first embodiment of a seventh principle;
- FIG. 55 is a chart showing a variation in a current density of the electron beam passing through a round aperture of FIG. 36 when a position of the electron beam is displaced by a drift in an output of amplifiers;
- FIG. 56 is a chart showing the drift in the output of the amplifier;
- FIG. 57 is an illustrative drawing showing an example of a configuration of stigmator-coil portions of FIG. 54 when six are provided;
- FIG. 58 is a circuit diagram of a main part of a charged-particle-beam exposure device according to a second embodiment of the seventh principle;
- FIG. 59 is a chart showing a variation in the current density of the electron beam passing through the round aperture when a position of the electron beam is displaced by a drift in an output of amplifiers;
- FIGS. 60A and 60B are illustrative drawings showing an example of a configuration of the focus-coil portions of FIG. 58 when five are provided;
- FIG. 61 is an illustrative drawing showing a configuration of a charged-particle-beam exposure device of the related art using a stencil mask;
- FIG. 62 is an illustrative drawing showing a configuration of another charged-particle-beam exposure device of the related art;
- FIG. 63 is a chart for showing a temporal change in a driving voltage of deflectors of FIG. 61 and FIG. 62 and for showing a settling time of the deflectors;
- FIG. 64 is an illustrative drawing of a configuration of a charged-particle-beam exposure device according to a first embodiment of the eighth principle of the present invention;
- FIG. 65 is an illustrative drawing showing a configuration of the deflectors of FIG. 64;
- FIGS. 66A and 66B are illustrative drawings for explaining trajectories of the charged-particle beam deflected by the deflectors;
- FIGS. 67A through 67C are illustrative drawings showing an extent of the charged-particle beam passing through electromagnetic lenses of FIG. 64 with an enlargement of this extent in a direction perpendicular to a beam axis;
- FIG. 68 is a flowchart of a process of determining focusing Al to correct a position of a cross-over image in FIG. 64;
- FIG. 69 is a flowchart of a process of obtaining desirable focusing L and an optimal value of a ratio in FIG. 64;
- FIG. 70 is a chart showing a settling time shortened by a correction process;
- FIG. 71 is an illustrative drawing of a configuration of a charged-particle-beam exposure device according to a second embodiment of the eighth principle of the present invention;
- FIG. 72 is an illustrative drawing of a configuration of a charged-particle-beam exposure device according to a third embodiment of the eighth principle of the present invention;
- FIGS. 73A and 73B are illustrative drawings for explaining trajectories of the charged-particle beam deflected by deflectors of FIG. 72;
- FIG. 74 is an illustrative drawing of a configuration of a charged-particle-beam exposure device according to a fourth embodiment of the eighth principle of the present invention;
- FIG. 75 is an illustrative drawing of a configuration of a charged-particle-beam exposure device according to a fifth embodiment of the eighth principle of the present invention;
- FIG. 76A is a chart for explaining a relation between a difference dV and a settling time of VMl in FIG. 75;
- FIG. 76B is a chart for explaining a relation between a difference dIO and a settling time of I in FIG. 75;
- FIG. 76C is a chart showing a change of a voltage VS1 and a settling time of VS1 in FIG. 75; and
- FIG. 76D is a chart showing an example of a correction value D3 for given pattern-selection data D1 in FIG. 75.
- In the following, principles and embodiments of the present invention will be described with reference to the accompanying drawings.
- A first principle of the present invention will be described below. The first principle is concerned with a device and a method of exposing a charged-particle beam which can accurately detect a mark position for the purposes of beam correction and beam positioning.
- The first principle of the present invention uses a mark of buried heavy metal instead of a dent mark. When the dent mark is used, charged particles reflected by the dent with a strong reflection in a certain direction are detected. Thus, depending on the detector's position relative to the dent mark, the detector may detect a strong reflection or may detect a weak reflection. Accordingly, if the detector's relative position to the mark is different, a magnitude and a profile of the detected reflection signal will be different. As a result, when a dent mark is used, the detected reflection signal is asymmetrically deformed unless the detectors are arranged symmetrically with respect to the mark.
- For a mark defined by a buried heavy metal according to the first principle of the present invention, a mechanism of detecting the mark is principally different from that of the dent mark (hereinafter called an edge-detection-type mark). For the mark of the first principle, a difference in the reflection intensity between the heavy metal and the background (silicon) is detected. Namely, a contrast in the reflection intensity is detected for the mark of the first principle. Hereinafter, the mark utilizing a difference in the reflection intensity is called a contrast-detection-type mark.
- According to the first principle, the use of the contrast-detection-type mark eliminates errors in the mark-position detection.
- FIG. 5 is an illustrative drawing showing a charged-particle-
beam exposure device 10 using the contrast-detection-type mark. The charged-particle-beam exposure device 10 includes a charged-particle-beam generator 11, adeflector 12,reflection detectors adder 15, a signal analyzing unit 16, a XY stage 17, and awafer holder 18. Thewafer holder 18 includes areference chip 19 and awafer 20. Each of thereference chip 19 and thewafer 20 includes a contrast-detection-type mark 21 and positioning marks 22. The charged-particle-beam exposure device 10 also includes a control unit (not shown) to control the charged-particle-beam generator 11, thedeflector 12, the signal analyzing unit 16, the XY stage 17, etc. - FIGS. 6A and 6B are illustrative drawings showing examples of the contrast-detection-
type mark 21 formed in thereference chip 19. As shown in FIGS. 6A and 6B, the contrast-detection-type mark 21 is formed by buryingheavy metal 24 such as Au, Ta, W, etc., in asubstrate 23 such as silicon. A surface of thereference chip 19 can be made smoothly flat within a 0.1-μm accuracy by using the CMP (chemical mechanical polishing) method or the like. The CMP method is a well-known mechanical polishing method using a chemical polishing substance, and a description thereof will be omitted. - As shown in FIG. 5, a charged-particle beam emitted from the charged-particle-
beam generator 11 is deflected by thedeflector 12, and is directed to thereference chip 19 or to thewafer 20. At the time of obtaining the distortion map and the deflection-correction coefficients, the beam is scanned over the contrast-detection-type mark 21 of thereference chip 19. Thereflection detectors adder 15 adds outputs of the detectors. A detected reflection signal after the addition is measured in synchronism with the scan of the deflector, and, then, is analyzed by the signal analyzing unit 16 to detect a center position of the mark. The contrast-detection-type mark 21 is successively positioned at predetermined locations by the XY stage 17. Thus, errors of the mark-position detections by using thedeflector 12 can be known based on the coordinates of the XY stage 17. - The mark-position detection described above is carried out for various positions of the mark by successively shifting the contrast-detection-
type mark 21 through the XY stage 17. In this manner, the distortion map and the deflection-efficiency-correction coefficients of thedeflector 12 are obtained. - Since an exposure stage comes immediately after the growth of a layer to be patterned in the LSI process, most of the positioning marks22 on the
wafer 20 are edge-detection-type mark. In order to position thewafer 20, therefore, the positioning marks 22 of the edge-detection type are successively positioned at a center of the beam optical system to be detected. At the center of the beam optical system, position-detection errors are not generated even if the edge-detection-type mark is used. In this manner, the precise position and rotation of a pattern under a surface of thewafer 20 can be known. - FIG. 7 is a flowchart of a process of exposing the
wafer 20 in the charged-particle-beam exposure device 10 according to a first embodiment of the present invention. - At a step S1, a deflection-distortion map is obtained by using a contrast-detection-type mark on a reference chip to calibrate the charged-particle beam.
- At a step S2, marks on a wafer are scanned, and the beam is focused on the wafer.
- At a step S3, a plurality of positioning marks on the wafer are successively positioned at a center of the field through a XY stage to detect the mark positions. In this manner, the precise position and rotation of patterns under a surface of the wafer are known.
- At a step S4, deflection-efficiency-correction coefficients are obtained by using the contrast-detection-type mark.
- At a step S5, a pattern is exposed on the wafer. This ends the procedure.
- When a long-time exposure is carried out, the deflection-efficiency-correction coefficients may be repeatedly obtained at the step S4 at predetermined time intervals to update these coefficients.
- According to the procedure described above, the distortion map and the deflection-efficiency-correction coefficients are obtained by using the contrast-detection-type marks. Thus, the precise calibration and correction of the beam deflector can be carried out. Also, the positioning marks are detected at the center of the field, i.e., at the center of the beam optical system, so that the precise positions and rotations of the underneath patterns can be known. Therefore, exposed patterns are precisely connected across field borders.
- FIG. 8 is a flowchart of another process of exposing the
wafer 20 in the charged-particle-beam exposure device 10 according to a second embodiment of the present invention. In the second embodiment, the positioning marks of the edge-detection type on the wafer are used to obtain the deflection-efficiency-correction coefficients. Errors in the correction coefficients obtained by using the edge-detection-type marks have a repeatability in the same device if the marks have the same structure. Thus, displacements commensurate with the errors measured in advance can be added to the correction coefficients to obtain the correct correction coefficients. - At a step S11, a deflection-distortion map is obtained by using a contrast-detection-type mark on a reference chip to calibrate the charged-particle beam.
- At a step S12, marks on a wafer are scanned, and the beam is focused on the wafer.
- At a step S13, a plurality of positioning marks on the wafer are successively positioned at a center of the field through a XY stage to detect the mark positions. In this manner, the precise position and rotation of patterns under a surface of the wafer are known.
- At a step S14, deflection-efficiency-correction coefficients are obtained by using the positioning marks on the wafer. Furthermore, displacements of the correction coefficients measured in advance are added to the obtained deflection-efficiency-correction coefficients to obtain correct correction coefficients.
- At a step S15, a pattern is exposed on the wafer. This ends the procedure.
- When a long-time exposure is carried out, the deflection-efficiency-correction coefficients may be repeatedly obtained at the step S14 at predetermined time intervals to update these coefficients.
- According to the procedure described above, an accurate distortion map is obtained by using the contrast-detection-type marks. Also, the deflection-efficiency-correction coefficients are obtained by using the positioning marks on the wafer, and the displacements measured in advance are added to the obtained correction coefficients to obtain correct correction coefficients. Also, the positioning marks are detected at the center of the field, i.e., at the center of the beam optical system, so that the precise positions and rotations of the underneath patterns can be known. Therefore, exposed patterns are precisely connected across field borders.
- According to the first and second embodiments of the first principle of the present invention, exposed patterns are precisely connected across field borders even for underneath patterns having the positioning marks of the edge-detection type, such underneath patterns being used in the patterning of semiconductor integrated circuits.
- In the following, a second principle of the present invention will be described below. The second principle is concerned with a device and a method of exposing a charged-particle beam which can achieve high-accuracy beam focusing and high-accuracy beam positioning without requiring a long time for beam-deflection adjustment.
- The second principle of the present invention uses the deflection-correction coefficients varying in proportion to the focusing distance after focusing the beam by a lens (focus coil) provided above the deflector.
- In order to focus the beam on a wafer surface at different heights without greatly changing the deflected-beam path, a lens (focus coil) provided above the main and sub-deflectors must be used. When the beam is focused in this manner, the deflected-beam path is not affected by the focusing of the beam. However, the deflected beam is not incident on the wafer surface at a normal angle. Therefore, when the height of the wafer surface is varied, a position of the deflected-beam path on the wafer surface is changed even though the deflected beam remains on the same path.
- In this case, a displacement of the position is proportional to a change in the height and the amount of the deflection. Thus, it is sufficient to change the coefficients G and R in proportion to the height f.
- G(f)=g 0 +g 1 *f (3)
- R(f)=r 0 +r 1 *f (4)
- Here, the distortion D(X) is not dependent on the height f.
- When a center axis of the focus coil is displaced relative to the axis of the beam, the beam is deflected by the excitation of the focus coil, so that the deflection field on the wafer surface is displaced in its entirety. When the displacement of the center axis is small, however, an angle of the beam deflection is proportional to the focus value. Thus, the displacement δ can be regarded as being proportional to the focus value.
- δ(f)=δ0+δ1 *f (5)
- According to the second principle of the present invention, higher orders of the deflection distortion dependent on the height need not be measured, so that the time required for the adjustment of the entire system can be shortened. Also, failure to focus the beam at the time of exposure is avoided to greatly reduce the blurring of patterns.
- FIG. 9 is an illustrative drawing of a charged-particle-beam exposure device according to a first embodiment of the second principle.
- A charged-particle-
beam exposure device 30 of FIG. 9 includes the charged-particle-beam generator 11, thedeflector 12, thereflection detectors adder 15, the signal analyzing unit 16, a projection lens 31, and a focus coil 32. The charged-particle-beam exposure device 30 also includes the XY stage 17 (not shown) and a control unit (not shown) in the same manner as in FIG. 5 to control the charged-particle-beam generator 11, thedeflector 12, the signal analyzing unit 16, the XY stage 17, the projection lens 31, the focus coil 32, etc. In FIG. 9 the same elements as those of FIG. 5 are referred by the same numerals, and a description thereof will be omitted. A charged-particle beam emitted from the charged-particle-beam generator 11 exposes a predetermined pattern on a wafer 33. On the wafer 33 are provided reference marks 34. - The focusing of the beam is carried out not by the projection lens31 provided at the bottom but by the focus coil 32. As shown in FIG. 9, the focus coil 32 is provided separately from the beam-deflection field of the
deflector 12. By changing the amount of an excitation current applied to the focus coil 32, it is possible to focus the beam on a wafer surface without changing a deflected-beam path. - FIG. 10 is a flowchart of a process of obtaining the deflection-efficiency-correction coefficients G(f) and R(f) as well as the displacement δ(f).
- At a step S21, a focus value (just focus) fi and the correction coefficients G(fi) and R(fi) are measured by using three reference marks Mi (i=1, 2, 3) provided at the height fi (i=1, 2, 3), respectively. As the reference marks Mi, marks 37 formed on a chip 36 held in a slanted position in a
wafer holder 35 can be used as shown in FIG. 11A. A method of achieving a just focus for obtaining the focus value fi will be described later. - Dent marks may be used as the reference marks here. Also, the contrast-detection-type marks with a buried heavy metal according to the first principle of the present invention may be used as the reference marks. Alternately, contrast-detection-type marks as shown in FIGS. 11B and 11C may be used as the reference marks. In FIGS. 11B and 11C, a contrast-detection-type mark21A is formed by patterning a heavy-metal layer 24A of such metal as Au, Ta, W, or the like on a heavy-metal layer 24A. The heavy-metal layer 24A for forming the contrast-detection-type mark 21A has a thickness of about 0.2 μm.
- At a step S22, G(f)=g0+g1f is fitted by applying the least-square method to G(fi) (i=1, 2, 3) obtained above for the three points, so that the coefficients g0 and g1 are obtained. R(f)=r0+r1*f is fitted by applying the least-square method to R(fi) (i=1, 2, 3) obtained above for the three points, so that the coefficients r0 and r1 are obtained.
- At a step S23, the reference mark M is moved to the center of the deflection field.
- At a step S24, the reference mark M is detected by using the just focus value f, a focus value f+df, and a focus value f-df (df is a change in the focus value). By doing so, δ(f), δ(f+df), and δ(f−df) representing the displacements of the entire deflection field depending on the focus value are measured.
- At a step S25, δ(f)=δ0+δ1*f is fitted by applying the least-square method to δ(f), δ(f+df), and δ(f-df) obtained above, so that the coefficients δ0 and δ1 are obtained. This ends the procedure.
- In this manner, the deflection-correction coefficients G(f) and R(f) as well as the displacement δ(f) are easily and quickly obtained. Use of these values for exposure makes it possible to generate a precise exposure pattern.
- FIG. 12 is a flowchart of an exposure process for the wafer33.
- At a step S31, a plurality (m) of chips to be focused on are selected based on information about a chip arrangement on the wafer 33.
- At a step S32, the beam is directed to a mark on the wafer 33 to measure the focus value f0. Here, this mark is a mark for the beam adjustment located near the center of the beam optical system.
- At a step S33, the beam is successively directed to the reference marks 34 located at coordinates (Xi, Yi) in the m selected chips, so that the focus values f(Xi, Yi) are obtained.
- At a step S34, an interpolation function F(X, Y) is fitted to the focus values f(Xi, Yi) by applying the least-square method, wherein the interpolation function F(X, Y) is provided as:
-
- Through the least-square fitting, the coefficients Akl are obtained. Here, the highest order n of the interpolation function is predetermined based on a flatness and a distortion of the wafer 33.
- At a step S35, the positioning of the beam on the wafer 33 and an exposure thereof is carried out by using the focus distances obtained from the interpolation function and the deflection-efficiency-correction coefficients obtained from the focus distances. Namely, the focus value F(X, Y) is obtained by using a coordinate (X, Y) to be exposed on the wafer 33. Then, the focus value f of the focus coil 32 is set to F(X, Y), and the deflection-efficiency-correction coefficients G(f) and R(f) of the
deflector 12 are set in accordance with the equation (3) and (4), respectively. Further, the displacement obtained by the equation (5) is incorporated in the deflection data of thedeflector 12 to cancel the displacement. - FIGS. 13A and 13B are illustrative drawings for explaining a method of detecting the just focus value of the charged-particle beam.
- The charged-particle beam is scanned over a
dent mark 43 in achip 42 covered with a resist 41, and reflected charged particles are detected. An exemplary detected reflection signal is shown in FIG. 13B. In order to obtain the just focus value, the reflection signal of FIG. 13B is successively measured as the focusing of the beam is varied. Then, a reflection signal having the steepest slope at an edge indicated by an arrow in FIG. 13B is selected from the reflection signals of various focus values. The focus value of this selected reflection signal is the just focus value. The same method can be used for obtaining a just focus value for a contrast-detection-type mark. - FIG. 14 is an illustrative drawing of a charged-particle-beam exposure device according to a second embodiment of the second principle. In FIG. 14, the same elements as those of FIG. 9 are referred by the same numerals, and a description thereof will be omitted. A charged-particle-beam exposure device50 of FIG. 14 includes the XY stage 17 (not shown) and a control unit (not shown) in the same manner as in FIG. 5 to control the charged-particle-
beam generator 11, thedeflector 12, the signal analyzing unit 16, the XY stage 17, the projection lens 31, the focus coil 32, etc. - In FIG. 14, the charged-particle-beam exposure device50 also includes a
light sensor 51 and aheight detector 52. Thelight sensor 51 illuminates light on the wafer 33, and detects light reflected therefrom. Here, light which does not have a photosensitive effect on the wafer 33 is used. An output from thelight sensor 51 is provided to theheight detector 52. Theheight detector 52 measures the height of a surface of the wafer 33 based on the output from thelight sensor 51. In this manner, when the reference marks 34 have such a structure that the height thereof cannot be detected by the beam scan, the height of the mark on the wafer is optically measured by using theheight detector 52. - Here, the height f0 optically measured is different from the focus value (focus distance) f which is used for the charged-particle beam. In order to convert the height f0 to the focus value f, a difference fod between the height and the focus value should be obtained. By using a reference mark to which both the optical measurement method and the beam measurement method can be applied, the difference fod is obtained as fo-f. This process may be carried out only once in advance. In order to perform the focusing and calibration of the beam, the focus value f can be calculated as fo-fod.
- According to the first and second embodiments of the second principle of the present invention, the focus value F(X, Y) at any point (X, Y) on the wafer can be obtained in a short period of time. Based on the obtained focus value, the deflection-efficiency-correction coefficients and the displacement, which are dependent on the focus value, are easily obtained. Even in the case that the focusing of the beam fails for a certain reference mark or that the obtained focus values contain errors to some extent, precise focusing of the beam is still possible because the interpolation function serves to smooth out a distribution of focus values. Also, there is a case in which the reference marks have such a structure that the focusing of the beam is difficult for these marks. In this case, the height of the mark is measured by the optical measurement method, so that the focus value of the focus coil can be determined.
- Furthermore, instead of measuring the focus values at the same time as exposure or measuring the focus values for each chip, a global alignment method used in positioning by an optical stepper may be used for the focusing of the beam. In this case, a variation of the measurements or a deviation of the focus point can be eliminated.
- In the following, a third principle of the present invention will be described. The third principle is concerned with a device and a method of exposing the charged-particle beam which can use correction coefficients provided for small units of areas without sacrificing the exposure processing time.
- In the third principle of the present invention, data for obtaining the correction coefficients is collected and stored in a memory area prior to an exposure process. Then, the correction coefficients used for a first frame are calculated from the data and stored prior to an exposure of the first frame. After that, the correction coefficients used for a N+1-th frame are calculated from the data and stored during an exposure of a N-th frame.
- Memory means for storing the two-frame correction coefficients is a conventional memory having enough storage capacity. This memory means may have a memory area storing all the correction coefficients for two frames such that the correction coefficients for one frame can be written while the correction coefficients for the other frame is read. In this case, writing/reading of the correction coefficients are smoothly conducted. Such memory means includes a buffer memory, a FIFO memory, a dual-port memory of a certain type, and a combination of these.
- In the third principle of the present invention, when densely provided complex correction coefficients are set in the device for enhancement of exposure precision, the calculation and storage of the correction coefficients are carried out in parallel with other processes required for the exposure. Therefore, a large amount of calculation is carried out, and the correction coefficients are set, without increasing the processing time for the exposure. That is, high-speed processing the same as the prior-art device can be achieved. Furthermore, a large volume memory is not necessary for the memory means. Since the correction coefficients for only two frames are stored in the memory means, updating of cell-correction coefficients and the like can be easily and quickly carried out during the exposure.
- Moreover, the data for the deflector correction may be newly collected during an exposure of the wafer, and the correction coefficients are calculated by using the newly collected data and stored in the memory means. Thus, all the correction coefficients stored in the memory area do not have to be updated even when new correction data becomes necessary during the exposure. Thus, a precise exposure pattern is created by using densely distributed correction coefficients without increasing the exposure processing time.
- FIG. 15 is a block diagram of an exemplary charged-particle-beam exposure device for conducting an exposure process according to the third principle of the present invention.
- In FIG. 15, a charged-particle-
beam exposure device 100 includes an exposure-column unit 110 and acontrol unit 150. The exposure-column unit 110 includes a charged-particle-beam generator 114 having acathode 111, agrid 112, and ananode 113. The exposure-column unit 110 further includes afirst slit 115 providing a rectangular shape of the charged particle beam, afirst lens 116 converging the shaped beam, and aslit deflector 117 deflecting a position of the shaped beam on amask 120 based on a deflection signal S1. The exposure-column unit 110 further includes second andthird lenses mask 120 mounted movably in a horizontal direction between the second andthird lenses fourth deflectors 121 through 124 deflecting the beam between the second andthird lenses mask 120. The exposure-column unit 110 further includes a blanking 125 cutting off or passing the beam according to a blanking signal, afourth lens 126 converging the beam, anaperture 127, arefocus coil 128, and afifth lens 129. The exposure-column unit 110 further includes adynamic focus coil 130, adynamic stigmator coil 131, anobjective lens 132 projecting the beam on to a wafer, and amain deflector 133 and a sub-deflector 134 positioning the beam on the wafer according to exposure-position signals S2 and S3. The exposure-column unit 110 further includes astage 135 carrying the wafer to move it in X-Y directions, and first-to-fourth alignment coils. - The
control unit 150 includes amemory media 151 comprising a disk or MT recorder for storing design data of integrated circuits, and aCPU 152 controlling the charged-particle-beam exposure device. Thecontrol unit 150 further includes a data-management unit 153, an exposure-management unit 159, a mask-stage controlling unit 160, a main-deflector-deflection setting unit 161, and astage controlling unit 162, all of which are connected via a data bus (i.e., VME bus). Exposure data includes main-deflector data and sub-deflector data, and is stored in abuffer memory 154 via the data-management unit 153 prior to the exposure process. Thebuffer memory 154 is used as a high-speed buffer for reading the exposure data, thereby negating an influence of low-speed data reading from thememory media 151. - The main-deflector data is set in the main-deflector-
deflection setting unit 161 via the exposure-management unit 159. The exposure-position signal S2 is output after the deflection amount is calculated, and is provided to themain deflector 133 via the DAC/AMP 170. Then, the sub-deflection data for exposing a selected field is read from the data-management unit 153, and is sent to the sub-deflector-deflection setting unit 155. In the sub-deflector-deflection setting unit 155, the sub-deflection data is broken down into shot data by thepattern generating unit 156, and is corrected by the pattern-correction unit 157. These circuits operates in a pipeline according to a clock signal generated by theclock setting unit 158. - After the processing of the pattern-
correction unit 157, a signal S1 for setting a slit size, mask-deflection signals P1 through P4 for determining a deflected position on themask 120 of the beam deflected according to the signal S1 after passing through thefirst slit 115, a signal S3 for determining a position on the wafer of the beam shaped by themask 120, and a signal S4 for correcting distortion and blurring of the beam are obtained. Also, theclock setting unit 158 provides ablanking controlling unit 165 with a B signal for controlling the blanking operation. - An exposure position on the wafer is controlled by the
stage controlling unit 162. In doing so, a coordinate position detected by alaser interferometer 163 is supplied to thestage controlling unit 162. Referencing to the coordinate position, thestage controlling unit 162 moves thestage 135 by driving amotor 164. - In this manner, the
control unit 150 controls the exposure-column unit 110 such that the charged-particle beam emitted from the charged-particle-beam generator 114 is rectangularly shaped by thefirst slit 115, converged by thelenses mask deflectors mask 120. The beam having passed through themask 120 passes through the blanking 125, is converged by thefourth lens 126, is deflected to a center of a sub-field of about 100-μm square by themain deflector 133, and is deflected within this sub-field by the sub-deflector 134. - Elements concerning the detection and analysis of reflection signals necessary for the positioning of the wafer and the calibration of the beam are the same as those shown in FIG. 5, and, thus, are omitted in FIG. 15.
- FIG. 16 is a block diagram of a correction-coefficient calculating and setting unit according to a first embodiment of the third principle. The correction-coefficient calculating and setting unit is used in the charged-particle-
beam exposure device 100 of FIG. 15. - In FIG. 16, a correction-coefficient calculating and
setting unit 200 includes a positioning-information measuring unit 201, a height-variation-information measuring unit 202, a data-memory unit 203, a firstcoefficient calculating unit 204, a second coefficient calculating unit 205, a firstcoefficient storing unit 206, a secondcoefficient storing unit 207, a firstcorrection calculating unit 208, and a secondcorrection calculating unit 209. - The positioning-
information measuring unit 201 obtains data for positioning the wafer to be exposed. This data includes a displacement of a beam deflected to a mark as well as beam-size-reduction information. The height-variation-information measuring unit 202 obtains data regarding a variation in the height of the wafer. The data measured by the positioning-information measuring unit 201 and the height-variation-information measuring unit 202 is stored in the data-memory unit 203. The measurement and storing of the data are finished by the start of an exposure. The positioning-information measuring unit 201 and the height-variation-information measuring unit 202 are implemented by thereflection detectors adder 15, and the signal analyzing unit 16 of FIG. 5, for example. The data-memory unit 203 is implemented by thememory media 151 and thebuffer memory 154 of FIG. 15. - Immediately before the start of an exposure, the beam is adjusted. Then, the wafer is moved through stage movement to a position where a first frame is started to be drawn, i.e., the wafer is moved from a position where the beam is adjusted to a position where the exposure is started. This stage movement is controlled by the
stage controlling unit 162. - The first
coefficient calculating unit 204 and the second coefficient calculating unit 205 receive information on a frame position from theCPU 152 controlling thestage controlling unit 162. Based on this information, the firstcoefficient calculating unit 204 and the second coefficient calculating unit 205 calculate the correction coefficients used for a given cell field at the time of a first-frame exposure, and store these correction coefficients in the firstcoefficient storing unit 206 and the secondcoefficient storing unit 207, respectively. The beam adjustment and the stage movement before the start of an exposure take at least 2 seconds. The calculation of the correction coefficients previously described is easily conducted within this time interval. - The first
coefficient calculating unit 204, the firstcoefficient storing unit 206, and the firstcorrection calculating unit 208 are implemented by the main-deflector-deflection setting unit 161 of FIG. 15. The second coefficient calculating unit 205, the secondcoefficient storing unit 207, and the secondcorrection calculating unit 209 are implemented by a sub-deflector-deflection setting unit 155 of FIG. 15. - After the exposure of the first frame is started, the first
coefficient calculating unit 204 and the second coefficient calculating unit 205 calculate the correction coefficients for the second frame, and store the correction coefficients in the firstcoefficient storing unit 206 and the secondcoefficient storing unit 207, respectively. In the same manner, while an N-th frame is being exposed, the correction coefficients used for an N+1-th frame are calculated. Even if the calculation and storing of the correction coefficients for the N+1-th frame are completed before the end of the exposure of the N-th frame, the correction coefficients used for the next (N+2-th) frame are not calculated. - An address corresponding to each cell field of two frames is necessary in the first
coefficient storing unit 206 and the secondcoefficient storing unit 207. When a wafer of an 8-inch diameter is used with a cell field of a 1-mm square, the number of addresses required for one frame is 200. 400 addresses are used for two frames. Thus, only a small memory volume is required. Here, each correction coefficient needs 32 bits. - The correction coefficients needing to be updated during an exposure include area-correction coefficients (G, R, D, and δ) for correcting a beam within an area totaling 8 coefficients for X and Y coordinates, 8 cell-correction coefficients for transforming coordinates of the main deflector with respect to the stage-movement directions, 8 stage-correction coefficients for aligning the stage-movement directions with wafer coordinates at the time of continuous stage movement, and correction coefficients for determining the beam focus value for each cell. The area-correction coefficients may be updated at the time when the beam shifts across an area border during the stage movement. Other correction coefficients need to be updated for each cell. Hereinafter, correction coefficients needing to be updated for each cell are collectively called cell-correction coefficients.
- The first
correction calculating unit 208 and the second correction-calculatingunit 209 read the correction coefficients from the firstcoefficient storing unit 206 and the secondcoefficient storing unit 207, respectively. These correction coefficients are supplied to the main deflector and the sub-deflector. - FIG. 17 is a block diagram of a coefficient storing unit according to a second embodiment of the third principle. In the second embodiment, the first
coefficient storing unit 206 and the secondcoefficient storing unit 207 of the first embodiments are controlled such that the correction coefficients for one frame can be written while the correction coefficients for another frame are being read. - The first
coefficient storing unit 206 and the secondcoefficient storing unit 207 of FIG. 16 store all the correction coefficients set for the cell fields of two frames. In order to smoothly carry out the reading and writing of the correction data, it is necessary to write the correction coefficients for one frame while the correction coefficients for another frame are being read. - The first
coefficient storing unit 206 or the secondcoefficient storing unit 207 of FIG. 17 includes aninverter 210 and frame-coefficient storing units 211 and 212. A mode selection signal takes a value of 0 or 1, and determines which one of a writing mode and a reading mode is used. The frame-coefficient storing unit 211 receives the mode selection signal, and the frame-coefficient storing unit 212 receives an inverted mode selection signal output from theinverter 210. When the mode selection signal indicates the writing mode, therefore, the correction coefficients are written into the frame-coefficient storing unit 211, and are read out from the frame-coefficient storing unit 212. On the other hand, when the mode selection signal indicates the reading mode, therefore, the correction coefficients are read from the frame-coefficient storing unit 211, and are written in the frame-coefficient storing unit 212. - The mode selection signal reverses each time when an exposure process moves from one frame to a next frame. Hereinafter, the mode selection signal is called a frame-control flag. The frame-control flag may be provided from the
CPU 152 of FIG. 15. In this manner, the writing/reading of data is controlled such that the correction coefficients for one frame can be written while the correction coefficients for another frame are being read. - The frame-coefficient storing units211 and 212 of FIG. 17 may include a buffer memory, a FIFO memory, a dual-port memory of a certain type, or a combination of these. When it includes a buffer memory, control of writing addresses and reading addresses is necessary. When a FIFO memory is used, control of addresses is not necessary as in a buffer memory since the correction coefficients are read in an order in which they are written. However, the control coefficients cannot be used repeatedly in the FIFO memory.
- FIG. 18 is a block diagram showing an example in which a dual-port memory is used as the frame-coefficient storing unit211 and the frame-coefficient storing unit 212 of FIG. 17.
- When a dual-port memory220 is used as shown in FIG. 18, an MSB (most significant bit) of the memory is used as the frame-control flag. The frame-control flag is reversed by an inverter 223 on a data reading side as compared to a data writing side. At a time when a frame is changed (i.e., when the stage movement takes a U-turn), the frame-control flag is reversed. Addresses other than the MSB are used as addresses for storing the correction coefficients by the coefficient calculating unit 221 (204 or 205). In the same manner, the correction calculating unit 222 (208 or 209) uses the addresses other than the MSB as addresses for reading the correction coefficients. Thus, when the correction coefficients are written in either one of the upper or lower half of the memory space, the correction coefficients are read from the other half.
- By using the dual-port memory220 as shown in FIG. 18, the calculation and setting of the correction coefficients are conducted without requiring complex control of an updating timing and a reading timing of the correction coefficients. Also, there is an advantage in that addresses of the correction coefficients for wafer coordinates can be matched between when the data is written and when the data is read.
- FIG. 19 is an illustrative drawing showing portions in one area where frame exposures begin and end. In FIG. 19, cells are denoted by 1-1, 1-2, m-1, m-2, n-1, and n-2. The cell-correction coefficients for each cell are different for a different cell, and the area-correction coefficients for one area are the same for all the cells in FIG. 19. While an m-th frame is under an exposure, the correction coefficients for an n-th frame are calculated and stored in the coefficient storing unit. However, the area-correction coefficients for the m-th frame and the n-th frame are the same so that there is no need to update the area-correction coefficients in this case.
- FIG. 20 is a block diagram of a portion for controlling the updating of the cell-correction coefficients and the area-correction coefficients according to a third embodiment of the third principle of the present invention.
- According to the third embodiment of the third principle, the updating of the cell-correction coefficients and the area-correction coefficients are controlled by an exposure controlling unit. The exposure controlling unit may be implemented in the exposure-
management unit 159 of FIG. 15. - In FIG. 20, an
exposure controlling unit 230 provides acorrection calculating unit 231 with a timing signal indicating a timing of a cell-to-cell shift and a timing of an area-to-area shift. Thecorrection calculating unit 231 reads the correction coefficients from acoefficient storing unit 232 based on the timing signal. Namely, thecorrection calculating unit 231 reads the cell-correction coefficients from thecoefficient storing unit 232 at a timing of a cell-to-cell shift, and reads the area-correction coefficients as well as the cell-correction coefficients at a timing of an area-to-area shift. - In order to provide the timing signal indicating a timing of a cell-to-cell shift and a timing of an area-to-area shift, the
exposure controlling unit 230 needs to keep a constant observation of exposure positions. This is achieved by using a counter or the like for counting a cell number and an area number. - FIG. 21 is a block diagram of a variation of the third embodiment of the third principle. In this variation, a pattern of stored correction coefficients is kept in a memory. Information on the correction-coefficient pattern is provided to the
correction calculating unit 231 based on the timing signal. - In FIG. 21, an exposure controlling unit230A provides a timing signal to a correction calculating unit 231A and to a correction-coefficient-
pattern storing unit 233. The correction-coefficient-pattern storing unit 233 keeps a pattern of the stored correction coefficients, and provides the correction calculating unit 231A with information indicating an area-to-area shift or a cell-to-cell shift. In this configuration, the updating of the correction coefficients can be controlled based only on an output of the correction-coefficient-pattern storing unit 233. - An example of the correction-coefficient pattern is shown in FIG. 22. In FIG. 22, “00” of first data (00, AREA) indicates that a cell to be exposed next is a first cell, and “AREA” thereof indicates that this cell belongs to a new area. “01” of second data (01, CELL) indicate that a cell to be exposed next is a second cell, and “CELL” thereof indicates that there is no area change. In the example of FIG. 22, fifth data (04, AREA) indicates that a fifth cell belongs to a new area. Namely, the first area includes four cells in FIG. 22. The correction-coefficient pattern of FIG. 22 is merely an example, and variations thereof may be used in the present invention to indicate needs, as well as no need, for updating particular ones of the correction coefficients.
- The correction-coefficient-
pattern storing unit 233 of FIG. 21 may preferably include a buffer memory, a FIFO memory, or a dual-port memory. Among these memories, the FIFO memory is the best. The correction-coefficient pattern is determined based on exposure arrangement information, so that an entire correction coefficient pattern covering up to an end of an exposure can be determined at a time of a beginning of the exposure. Thus, it is preferable to use a FIFO memory in terms of convenience of use since the FIFO memory has such a structure that data can be consecutively read and written. - FIG. 23A is a circuit diagram of an example of a dual-port memory controlled by the configuration of FIG. 17. In FIG. 23A, the frame-control flag is assigned to the MSB of address lines of the dual-port memory, and left-hand-side data of the FIFO output of FIG. 22, i.e., “00, 01, 02, ***”, is input to bits other than the MSB. Here, a DSP (digital signal processor) is used as the correction calculating unit231A.
- A circuit of FIG. 23A includes the correction calculating unit231A, dual-
port memories inverter 253, adecoder 254, a correction-coefficient-updating-pattern register 255, aresister 256, andinverters 257 and 258. The dual-port memories - The least significant bit of an address signal is provided to a chip-selection node CS of the dual-
port memory 251. Also, a reversed signal of the least significant bit by theinverter 253 is input to a chip-selection node CS of the dual-port memory 252. Thus, data provided to the circuit is supplied in turn to one of the dual-port memory 251 and the dual-port memory 252. The reason why the dual-port memory 251 and the dual-port memory 252 are provided is because the two dual-port memory, rather than one, can increase a memory volume to store more correction coefficients. In FIG. 23A,bits 4 through 11 of address inputs on a data writing side are provided with data on the data bus instead of address data on the address bus. This is because this configuration can boost a processing speed. In this configuration, the data on the data bus is decoded by thedecoder 254 to determine an address. - FIG. 23B is a chart showing data to be stored in the dual-
port memory 251, for example. As shown in FIG. 23B, the lowest four bits (bits 0 through 3) of the address correspond to each correction coefficient, and eight bits (bits 4 through 11) next to these four bits represent a cell number. Thus, assuming that a correction coefficient Rac is stored at an address of a hexagonal 3 of the lowest four bits, Rac for a first cell is stored at an address “003”, and Rac for a 256-th cell is stored at an address “FF3”. - Assume that data is output from the FIFO as shown in FIG. 22. An upper address of the dual-
port memory 251 or the dual-port memory 252 is determined by the first data (00, AREA). For example, the dual-port memory 251 may be selected by the correction calculating unit 231A as a chip to be used. In this case, based on information “AREA” of the first data, the correction calculating unit 231A reads all the data stored inaddresses 0 through 9 of the dual-port memory 251 to use the data for correction of the charged-particle beam. After an exposure of a first cell is completed, the second data (01, CELL) is provided from the FIFO to determine the upper address of the dual-port memory 251. Based on information “CELL” of the second data, the correction calculating unit 231A reads data stored inaddresses 0 through 5 to use the data for correction of the beam. - The correction-coefficient-updating-
pattern register 255 is arranged in parallel with the dual-port memories pattern register 255 is used when the correction coefficients are controlled at a level finer than the level of the area-correction coefficients and the cell-correction coefficients such that some of the area correction coefficients are not updated at a certain timing, etc. By using information stored in the correction-coefficient-updating-pattern register 255, the correction calculating unit 231A can avoid reading unnecessary correction coefficients based on information about the correction coefficients needed to be updated. There is a case in which all the correction coefficients do not have to be updated when an exposure is made. In a case where requirements for an exposed-pattern precision are not so high, for example, a desired precision may be achieved without frequently changing the correction coefficient. In this case, information on the correction coefficients with no need to be updated is stored in the correction-coefficient-updating-pattern register 255 in advance. Then, before the start of an exposure, this information is input to input ports of the correction calculating unit (DSP) 231A. Based on this information, the correction calculating unit (DSP) 231A reads only necessary correction coefficients from the dual-port memories - In the third principle, when the complex and densely distributed correction coefficients are set for an enhancement of exposure precision, the calculation and setting of the correction coefficients are carried out in parallel with other processes required for the exposure. Thus, the calculation and setting of a large number of correction coefficients are conducted without increasing the processing time for the exposure. Also, there is no need for a large memory volume, only the correction coefficients for two frames being stored. Therefore, the cell-correction coefficients can be easily updated at high speed during the exposure. As a result, it is possible to create an exposure pattern only by taking almost the same processing time as required in the related art without sacrificing the precision. Thus, the third principle of the present invention greatly contributes to the development of the manufacturing technology for the LSI chips having fine patterns.
- As described above, according to the present invention, the measured deflection-efficiency-correction coefficients are approximated by using the linear functions of the focus distance, the deflection-efficiency-correction coefficients are easily obtained as functions of the focus distance.
- Also, according to the present invention, the measured displacement is approximated to by using the linear function of the focus distance, the displacement is easily obtained as a function of the focus distance.
- Also, according to the present invention, the height of the wafer surface is approximated as a function of the coordinates to provide the focus distances, and the positioning and exposure of the wafer are conducted by using the deflection-correction coefficients and the displacement corrected with respect to the focus distances. Therefore, the data collection for correction of the beam does not require much time and labor, yet a precise exposure pattern being created.
- Also, according to the present invention, the height of the wafer surface is optically measured even when focusing on the reference marks fails. Therefore, a precise exposure pattern is created for wafers having any types of reference marks.
- Furthermore, according to the present invention, the position-detection marks of the contrast-detection type allowing a detection based on differences in the reflection intensities are used. Thus, errors in the detection of mark positions are eliminated.
- Also, according to the present invention, the position-detection marks of the contrast-detection type having a high precision of surface flatness are used. Thus, errors in the detection of mark positions are eliminated.
- Also, according to the present invention, the position-detection marks of the contrast-detection type allowing a detection based on differences in the reflection intensities are used. Thus, the deflection-distortion map and the deflection-efficiency-correction coefficients free from errors are obtained.
- Also, according to the present invention, the position-detection marks of the contrast-detection type allowing a detection based on differences in the reflection intensities are used to expose the wafer after correcting the charged-particle beam. Therefore, a precise exposure pattern is created.
- Also, according to the present invention, the distortion of the charged-particle beam is corrected by using the position-detection marks of the contrast-detection type allowing a detection based on differences in the reflection intensities, and the deflection efficiency of the beam is corrected by canceling the measurement errors in the correction-efficiency-correction coefficients obtained from the positioning marks or the beam adjustment marks provided on the wafer. Therefore, a precise exposure pattern is created on the wafer.
- Also, according to the present invention, the positioning marks may be detected at the center axis of the beam optical system to eliminate errors in the detection of the positioning marks.
- Furthermore, according to the present invention, the correction coefficients for a N+1-th frame are calculated while the correction coefficients for a N-th frame are being exposed, so that the exposure process and the calculation of the correction coefficients are conducted in parallel (simultaneously). Thus, a precise exposure pattern is created by using densely distributed correction coefficients without increasing the exposure processing time.
- Also, according to the present invention, it is sufficient to store only the correction coefficients for two frames. Thus, a precise exposure pattern is created by using densely distributed correction coefficients without increasing the exposure processing time.
- Also, according to the present invention, the writing and reading of the correction coefficients are smoothly conducted in parallel. Thus, a precise exposure pattern is created by using densely distributed correction coefficients without increasing the exposure processing time.
- Also, according to the present invention, the correction coefficients with no need to be updated are not updated during an exposure of a given frame to achieve an efficient correction of the deflector. Thus, a precise exposure pattern is created by using densely distributed correction coefficients without increasing the exposure processing time.
- Also, according to the present invention, the correction coefficients for a given frame are updated while another frame is being exposed. Thus, a precise exposure pattern is created by using densely distributed correction coefficients without increasing the exposure processing time.
- Also, according to the present invention, the data for the deflector correction may be newly collected during an exposure of the wafer, and the correction coefficients are calculated by using the newly collected data. Thus, the correction coefficients stored in the memory do not have to be updated even when new correction data become necessary during the exposure. Thus, a precise exposure pattern is created by using densely distributed correction coefficients without increasing the exposure processing time.
- Moreover, there are other problems concerning the present invention, and these problems will be described below.
- The charged-particle-beam exposure method has superior characteristics in terms of the resolution and the focus depth, compared to the light exposure method widely used in the manufacturing of LSI chips. However, the charged-particle-beam exposure method is inferior in terms of an exposure positioning accuracy and an overlay accuracy. Thus, the charged-particle-beam exposure method is not widely used in the field for manufacturing purposes.
- In general, a charged-particle-beam exposure device controls a charged-particle beam through an electromagnetic field to draw patterns on photosensitive material. Therefore, the positioning of the beam can be corrected for each pattern. On the other hand, a correction operation is complex, and a beam adjustment (calibration) for determining various correction coefficients is lengthy.
- The charged-particle-beam exposure device generally has a main deflector for deflecting the beam within a large area and a sub-deflector for deflecting the beam within a small area at high speed. A combination of these two deflectors makes it possible to draw patterns in a large area at high speed. Typically, the main deflector is a coil, and the sub-deflector is a static-charge deflector.
- The charged-particle beam deflected by the main deflector passes through an electric field generated by the sub-deflector with the electric field deflecting the beam at high speed. In this case, a position of the beam passing through the sub-deflector varies according to the deflection amount (deflection angle) incurred by the main deflector. Since there is a distortion in the electric field generated by the sub-deflector, a variation in the position of the passing beam leads to the deflection amount of the sub-deflector being changed accordingly.
- In the charged-particle-beam exposure device having more than one deflector, therefore, a deflection efficiency of the sub-deflector is changed depending on the path of the charged-particle beam deflected by the main deflector. In order to correct a distribution of the deflection efficiency, typically, the deflection efficiency of the sub-deflector is measured for each deflection amount of the main deflector.
- FIG. 24 is an illustrative drawing showing a first related-art method of obtaining a map of deflection-efficiency-correction coefficients of the sub-deflector. The first related-art method will be described with reference to FIG. 24.
- In an example of FIG. 24, a deflection area of the main deflector is a 2000-μm square, and a deflection area of the sub-deflector is a 100-μm square. The deflection area of the main deflector is divided into 400 (20×20) fields of a 100-μpm square. Within this field, a pattern is drawn by deflecting the beam through the sub-deflector without using the main deflector. The area of the 2000-μpm square is called a main field, and the area of the 100-μm square is called a sub-field.
- In this example, the sub-deflector's deflection efficiency should be measured at 20×20 points of deflection positions of the main deflector, each of the 20×20 points being arranged in a corresponding one of the 100-μm squares. A procedure for measuring the sub-deflector's deflection efficiency at the 20×20 points includes the steps of:
- (1) setting the deflection position of the main deflector at a center of a sub-field (Ix, Iy);
- (2) carrying out the following two steps at the four corners of the sub-field;
- (2)-1 positioning a position-detection mark at a corner of the sub-field through stage movement;
- (2)-2 deflecting the beam through the sub-deflector to the corner provided with the position-detection mark to detect a position of the position detection mark;
- (3) calculating deflection-efficiency-correction coefficients based on differences between the detected positions of the mark and the actual positions (as defined by the stage movement) thereof at the four corners; and
- (4) repeating the steps (1) through (3) for all the sub-fields at Ix=1, 2, ***, 20 and Iy=1, 2, ***, 20.
- This procedure takes time for the measurement since 1600 (20×20×4) stage movements are required. Assuming that a time period required for a stage vibration caused by the stage movement to be settled is 500 ms, the measurement of all the correction coefficients for the sub-fields takes 13 minutes and 20 seconds (800 seconds).
- In response, a method of reducing the number of the stage movements to one fourth without decreasing the number of the measurement points has been proposed. FIG. 25 is an illustrative drawing showing a second related-art method of obtaining a map of deflection-efficiency-correction coefficients of the sub-deflector.
- In an example of FIG. 25, sizes of the main field and the sub-field are the same as in the first related-art method. A procedure for measuring the sub-deflector's deflection efficiency at the 20×20 points includes the steps of:
- (1) positioning a position-detection mark at a center of a sub-field (Ix, Iy) through stage movement, and setting the deflection position of the main deflector at the center of the sub-field (Ix, Iy);
- (2) carrying out the following three steps at the four corners of the sub-field;
- (2)-1 deflecting the beam at a corner of the sub-field through the sub-deflector;
- (2)-2 deflecting the beam back to the center of the sub-field through the main deflector;
- (2)-3 detecting a position of the position-detection mark at the center of the sub-field by using the beam;
- (3) calculating deflection-efficiency-correction coefficients based on differences between the detected positions of the mark and the actual position (as defined by the stage movement) thereof; and
- (4) repeating the steps (1) through (3) for all the sub-fields at Ix=1, 2, ***, 20 and Iy=1, 2, ***, 20.
- This procedure does not require a stage movement at the step (2), so that the number of the stage movements becomes equal to the number of sub-fields, which is 400 (20×20) in this case. Assuming that a time period required for a stage vibration caused by the stage movement to be settled is 500 ms, the measurement of all the correction coefficients for the sub-fields takes 3 minutes and 20 seconds (200 seconds). This time period is one fourth of that of the first related-art method.
- However, the second related-art method has a drawback in that errors involved in the measured coefficients become large when the sub-deflector's deflection efficiency has much dependency on the deflection amount of the main deflector. In order to measure the sub-deflector's deflection efficiency for the sub-field (Ix, Iy), the deflection amount of the main deflector should be set at the center of this sub-field. In the second related-art method, however, the deflection amount of the main deflector is changed at the step (2)-2. Strictly speaking, the second related-art method measures the differences between the detected positions and the actual positions of the mark at the corners of a sub-field displaced by (50 μm, 50 μm) from the actual sub-field. Assuming that the deflection efficiency of the sub-field displaced by (50 μm, 50 μm) is different from that of the actual sub-field by 0.1 %, the differences at the corners contain errors of 0.05 μm. Thus, correct deflection-efficiency-correction coefficients are not obtained.
- The first related-art method does not contain such errors. However, it requires four times as long a measurement time as that of the second related-art method as previously.described.
- Accordingly, there is a need in the field of a beam adjustment of charged-particle-beam exposure devices for a method which can carry out a more precise deflection-efficiency correction than the related-art methods without sacrificing the processing time.
- In the following, fourth and fifth principles of the present invention and embodiments-thereof will be described with reference to the accompanying drawings.
- FIG. 26 is an illustrative drawing showing the fourth principle of the present invention. In the fourth principle, four position-detection marks arranged at relative positions corresponding to the four corners of a sub-field are used as shown in FIG. 26. First, a stage is moved so as to position the position-detection marks at the four corners of a given sub-field. Then, the main deflector deflects the charged-particle beam to a center of the given sub-field. Further, the sub-deflector successively deflects the charged-particle beam to the corners of the given sub-field to detect positions of the position-detection marks.
- In this manner, data for the four corners of the given sub-field is obtained through only one stage movement. In this case, the charged-particle beam deflected by the main deflector is positioned at the center of the given sub-field, thereby generating no error in the deflection-efficiency-correction coefficients. However, if the four position-detection marks contain errors in their relative positions, these errors will be contained in the sub-deflector's deflection-efficiency-correction coefficients for all the sub-fields. Namely, all the sub-fields will have the same errors. In order to eliminate these errors, one of the following methods may be used:
- (1) correcting the correction coefficients at a time of the data measurement by using arrangement errors of the position-detection marks measured in advance and stored in a memory;
- (2) correcting the correction coefficients by using the arrangement errors of the position-detection marks measured through stage movement at-the time of the data measurement; and
- (3) positioning one of the position-detection marks through stage movement at a center of a sub-field located at a center of the main field after the data measurement, deflecting the beam at the center of the sub-field using the main deflector, deflecting the beam successively at the four corners of the sub-field using the sub-deflector, detecting the one of the position-detection marks after directing the beam back to the center of the sub-field using the main deflector, and correcting errors of the sub-deflector based on an assumption that the main deflector contain no error in the deflection thereof.
- In either one of these three methods, the same error compensation can be applied to all the sub-fields.
- According to the fourth principle of the present invention, the charged-particle beam deflected by the main deflector is positioned at the center of the main deflector, so that there is no error in the correction coefficients. Also, the number of stage movements is one fourth that of the first related-art method, and is the same as that of the second related-art method, so that the data measurement time is rather short. In the case in which the number of sub-fields is 20×20 and the time length for the stage vibration to subside is 500 ms, the correction data is measured taking 3 minutes and 20 seconds (20×20×0.5 sec).
- The above description of the fourth principle has been given by taking an example of four position-detection marks. However, it is apparent that the time length required for the data measurement is shorter than that of the first related-art method as long as more than one position-detection mark is used.
- FIG. 27 is an illustrative drawing showing the fifth principle of the present invention. In the fifth principle, one position-detection mark is positioned through stage movement at a point where four surrounding sub-fields share a corner point thereof, as shown in FIG. 27. Then, the main deflector deflects the charged-particle beam to a center of one of the four surrounding sub-fields. Further, the sub-deflector deflects the charged-particle beam to the position-detection mark to detect a position of the position-detection mark and to store a difference between the detected position and the actual position of the mark. The same procedure is carried out for the four surrounding sub-fields.
- In this manner, the correction data is measured for a respective corner of the four surrounding sub-fields, requiring only one stage movement. This data measurement is carried out at all the sub-field corners. Then, the correction coefficients are calculated based on the detected differences for each of the sub-fields.
- According to the fifth principle of the present invention, the charged-particle beam deflected by the main deflector is positioned at the center of the main deflector, so that there is no error in the correction coefficients. Also, the number of stage movements is one fourth that of the first related-art method, and is almost the same as that of the second related-art method, so that the data measurement time is rather short. In the case in which the number of the sub-fields is 20×20 and the time length for the stage vibration to subside is 500 ms, the correction data is measured taking 3 minutes and 20 seconds (20 ×20×0.5 sec).
- In the following, embodiments of the fourth and fifth principles of the present invention will be described with reference to the accompanying drawings.
- FIG. 28 is a block diagram of an exemplary charged-particle-beam exposure device carrying out a deflection-efficiency correction according to the fourth and fifth principles of the present invention.
- In FIG. 28, a charged-particle-
beam exposure device 400 includes an exposure-column unit 410 and acontrol unit 450. The exposure-column unit 110 includes a charged-particle-beam generator 414 having acathode 411, agrid 412, and ananode 413. The exposure-column unit 410 further includes afirst slit 415 providing a rectangular shaping of the charged particle beam, afirst lens 416 converging the shaped beam, and aslit deflector 417 deflecting a position of the shaped beam on amask 420 based on a deflection signal S1. The exposure-column unit 410 further includes second andthird lenses mask 420 mounted movably in a horizontal direction between the second andthird lenses fourth deflectors 421 through 424 deflecting the beam between the second andthird lenses mask 420. The exposure-column unit 410 further includes a blanking 425 cutting off or passing the beam according to a blanking signal, afourth lens 426 converging the beam, anaperture 427, arefocus coil 428, and afifth lens 429. The exposure-column unit 410 further includes adynamic focus coil 430, adynamic stigmator coil 431, anobjective lens 432 projecting the beam onto a wafer, and amain deflector 433 and a sub-deflector 434 positioning the beam on the wafer according to exposure-position signals S2 and S3. The exposure-column unit 410 further includes astage 435 carrying the wafer to move it in X-Y directions, and first-to-fourth alignment coils. - The
control unit 450 includes amemory media 451 comprising a disk or MT recorder for storing design data of integrated circuits, and aCPU 452 controlling the charged-particle-beam exposure device. Thecontrol unit 450 further includes a data-management unit 453, an exposure-management unit 459, a mask-stage controlling unit 460, a main-deflector-deflection setting unit 461, and astage controlling unit 462, all of which are connected via a data bus (i.e., VME bus). Exposure data includes main-deflector data and sub-deflector data, and is stored in abuffer memory 454 via the data-management unit 453 prior to the exposure process. Thebuffer memory 454 is used as a high-speed buffer for reading the exposure data, thereby negating an influence of low-speed data reading from thememory media 451. - The main-deflector data is set in the main-deflector-
deflection setting unit 461 via the exposure-management unit 459. The exposure-position signal S2 is output after the deflection amount is calculated, and is provided to themain deflector 433 via the DAC/AMP 470. Then, the sub-deflection data for exposing a selected field is read from the data-management unit 453, is broken down into shot data by thepattern generating unit 456, and is corrected by the pattern-correction unit 457. These circuits operates in a pipeline according to a clock signal generated by theclock setting unit 458. - After the processing of the pattern-
correction unit 457, a signal S1 for setting a slit size, mask-deflection signals P1 through P4 for determining a deflected position on themask 420 of the beam deflected according to the signal S1 after passing through thefirst slit 415, a signal S3 for determining a position on the wafer of the beam shaped by themask 420, and a signal S4 for correcting distortion and blurring of the beam are obtained. Also, theclock setting unit 458 provides a blanking controlling unit 465 with a B signal for controlling the blanking operation. - An exposure position on the wafer is controlled by the
stage controlling unit 462. In doing so, a coordinate position detected by alaser interferometer 463 is supplied to thestage controlling unit 462. Referencing to the coordinate position, the stage controlling-unit 462 moves thestage 435 by driving amotor 464. - In this manner, the
control unit 450 controls the exposure-column unit 410 such that the charged-particle beam emitted from the charged-particle-beam generator 414 is rectangularly shaped by thefirst slit 415, converged by thelenses mask deflectors mask 420. The beam having passed through themask 420 passes through the blanking 425, is converged by thefourth lens 426, is deflected to a center of a sub-field of an about 100-μm square by themain deflector 433, and is deflected within this sub-field by the sub-deflector 434. - FIG. 29 is an illustrative drawing showing a mark-position detecting portion of the charged-particle-
beam exposure device 400. In FIG. 29, the mark-position detecting portion includes reflection detectors 480 and 481, a signal analyzing device 482, and a control-purpose computer 483. The control-purpose computer 483 includes theCPU 452 of FIG. 28, RAM, and ROM. - As shown in FIG. 29, a position-detection mark485 may be formed from a heavy-metal layer patterned on a silicon 484. The charged-particle-
beam exposure device 400 scans the charged-particle beam over the silicon 484 and the position-detection mark 485 in predetermined directions. The reflection detectors 480 and 481 detect charged particles scattered by the silicon 484 or the position-detection mark 485. The signal analyzing device 482 analyzes a reflection signal obtained by scanning the charged-particle beam, and detects a position of the position-detection mark 485 based on a difference in reflection intensities between the position-detection mark 485 and the silicon 484. - FIG. 30 is an illustrative drawing showing a reference chip490 provided with four position-detection marks according to the fourth principle of the present invention. The reference chip 490 is placed on the
stage 435 of the charged-particle-beam exposure device 400. The reference chip 490 is preferably a heavy-metal layer such as Ta, W, Au, or the like patterned on an Si wafer. - FIG. 31 is a flowchart of a process of correcting the deflection efficiency of the sub-deflector according to a first embodiment of the fourth principle.
- At a step S41, the reference chip 490 is placed on the
stage 435 of the charged-particle-beam exposure device 400. - At a step S42, positions of the four position-detection marks are detected at a center of the main field, and errors of the relative positions of the four position-detection marks are stored in a memory of the control-purpose computer 483.
- At a step S43, position errors (differences between detected positions and actual positions of the four position-detection marks) are measured. First, a center of the four position-detection marks is moved to a center of a given sub-field, and the charged-particle beam is deflected through the main deflector to the center of the sub-field. Then, the charged-particle beam is successively deflected through the sub-deflector to the four corners to detect positions of the position-detection marks. Finally, the position errors are calculated based on the detected positions of the position-detection marks.
- At a step S44, the errors of the relative positions of the four position-detection marks stored in the memory are subtracted from the position errors, so that remaining position errors are calculated.
- At a step S45, the deflection-efficiency-correction coefficients are calculated based on the remaining position errors. This ends the procedure.
- The calculation of the deflection-efficiency-correction coefficients is carried out as follows.
- A correction of the sub-field may be made by using correction coefficients Gx, Gy, Rx, Ry, Hx, and Hy as follows.
- X′=Gx*X+Rx*Y+Hx*X*Y (7)
- Y′=Ry*X+Gy*Y+Hy*X*Y (8)
- Here, X′ and Y′ are voltages applied to the sub-deflector, and X and Y are coordinates to which the charged-particle beam is to be deflected. The correction coefficients Gx, Gy, Rx, Ry, Hx, and Hy are obtained as a map in the main field to carry out the sub-deflector's deflection-efficiency correction.
- In order to obtain the correction coefficients Gx, Gy, Rx, Ry, Hx, and Hy, the following calculations are carried out. FIG. 32 is an illustrative drawing for explaining the calculations of the correction coefficients. Position errors detected at four corners A, B, C, and D of a rectangle having a side length L as shown in FIG. 32 are denoted as (δxa, δya), (δxb, δyb), (δxc, δyc), and (δxd, δyd), respectively. The following calculations are carried out first.
- δGx=(−δxa+δxb+δxc−δxd)/2L (9)
- δGy=(−δya−δyb+δyc+δyd)/2L (10)
- δRx=(−δxa−δxb+δxc−δxd)/2L (11)
- δRy=(−δya+δyb+δyc−δyd)/2L (12)
- δHx=(δxa−δxb+δxc−δxd)/L 2 (13)
- δHy=(δya−δyb+δyc−δyd)/l 2 (14)
- Here, δGx, δGy, δRx, δRy, δHx, and δHy are differences between the correction coefficients used at present and the correction coefficients which should be used. These differences are added to the correction coefficients used at present as shown in the following equations to update the correction coefficients.
- Gx new =Gx old +δGx (15)
- Gy new =Gy old +δGy (16)
- Rx new =Rx old +δRx (17)
- Ry new =Ry old +δRy (18)
- Hx new =Hx old +δHx (19)
- Hy new =Hy old +δHy (20)
- The equations (9) through (14) for obtaining the differences are approximations derived by assuming that L is much greater than δx and δy. Thus, the measurement of the position errors and the updating of the correction coefficients are repeated until the position errors become sufficiently small. Then, the correction coefficients thus obtained are stored as a map.
- In the first embodiment of the fourth principle, the reference chip having a plurality of the position-detection marks is used, so that the correction coefficients for the entire main field are obtained through stage movements equal to the number of the sub-fields. Therefore, the correction coefficients for the entire main field are obtained in a short period of time. Also, the errors of the relative positions of the position-detection marks may be measured in advance to cancel these errors at the time of obtaining the deflection efficiency. Thus, the correction coefficients are obtained in a short period of time at high precision.
- FIG. 33 is a flowchart of a process of correcting the deflection efficiency of the sub-deflector according to a second embodiment of the fourth principle.
- At a step S51, the reference chip 490 is placed on the
stage 435 of the charged-particle-beam exposure device 400. - At a step S52, position errors (differences between detected positions and actual positions of the four position-detection marks) are measured. First, a center of the four position-detection marks is moved to a center of a given sub-field, and the charged-particle beam is deflected through the main deflector to the center of the sub-field. Then, the charged-particle beam is successively deflected through the sub-deflector to the four corners to detect positions of the position-detection marks. Finally, the position errors are calculated based on the detected positions of the position-detection marks.
- At a step S53, errors of the relative positions of the four position-detection marks are measured by successively shifting the reference chip 490 through stage movement while keeping the charged-particle beam at a fixed position.
- At a step S54, the errors of the relative positions of the four position-detection marks are subtracted from the position errors, so that remaining position errors are calculated.
- At a step S55, the deflection-efficiency-correction coefficients are calculated based on the remaining position errors. This ends the procedure.
- In the second embodiment of the fourth principle, the errors of the relative positions of the four position-detection marks are eliminated by using the position-detection mechanism through the stage movement in the charged-particle-beam exposure device. Thus, the correction coefficients are quickly obtained at a high precision without using another position detecting device.
- FIG. 34 is a flowchart of a process of correcting the deflection efficiency of the sub-deflector according to a third embodiment of the fourth principle.
- At a step S61, the reference chip 490 is placed on the
stage 435 of the charged-particle-beam exposure device 400. - At a step S62, position errors (differences between detected positions and actual positions of the four position-detection marks) are measured. First, a center of the four position-detection marks is moved to a center of a given sub-field, and the charged-particle beam is deflected through the main deflector to the center of the sub-field. Then, the charged-particle beam is successively deflected through the sub-deflector to the four corners to detect positions of the position-detection marks. Finally, the position errors are calculated based on the detected positions of the position-detection marks.
- At a step S63, the deflection-efficiency-correction coefficients are calculated from the position errors.
- At a step S64, errors of the relative positions of the position-detection marks contained in the obtained deflection-efficiency-correction coefficients are measured by using one position-detection mark. First, the position-detection mark is moved to a center of the main field, and the charged-particle beamis deflected through the main deflector to the center of the main field. Next, the charged-particle beam is deflected through the sub-deflector to a corner of the sub-field, and, then, is deflected back to the center through the main deflector to detect a position of the position-detection mark. The same procedure is carried out for all the four corners of the sub-field. In this manner, the errors of the relative positions of the four position-detection marks contained in the position errors measured at the step S62 are obtained by using the main deflector as a reference.
- At a step S65, the deflection-efficiency-correction coefficients are modified based on the errors of the relative positions of the four position-detecion marks. This ends the procedure.
- In the third embodiment of the fourth principle, the errors of the relative positions of the position-detection marks are eliminated by using one position-detection mark and the deflection amount of the sub-deflector as a reference. Thus, the precise correction coefficients are quickly obtained through a simple method.
- FIG. 35 is a flowchart of a process of correcting the deflection efficiency of the sub-deflector according to an embodiment of the fifth principle.
- At a step S71, a position-detection mark is moved through stage movement to one of 21×21 measurement points in the main field having 20×20 sub-fields.
- At a step S72, position errors are measured by deflecting the charged-particle beam through the sub-deflector from centers of four surrounding sub-fields to a position of the position-detection mark. First, the charged-particle beam is deflected through the main deflector to a center of one of the four surrounding sub-fields. Then, the charged-particle beam is deflected through the sub-deflector to the position-detection mark to detect the position-detection mark, and a detected position error is recorded. The same procedure is carried out for all the four surrounding sub-fields.
- At a step S73, a check is made whether the measurements are made for all the 21×21 measurement points. If there are one or more remaining measurement points to be measured, the procedure goes back to the step S71 to repeat the above steps for the next measurement point. If there is no remaining measurement point, the procedure proceed to a step S74.
- At the step S74, the deflection-efficiency-correction coefficients are calculated for all the measurement points based on the position errors. This ends the procedure.
- In the embodiment of the fifth principle, the position-detection mark is moved through stage movement only once for each of the measurement points when the correction coefficients are to be obtained for each of the sub-fields. This utilizes the fact that a plurality of sub-fields share the measurement points as corners thereof. Namely, the correction coefficients for the entire main field are obtained through stage movements equal to the number of the measurement points. Thus, the correction coefficients are obtained taking a short period of time.
- As described above, according to the fourth principle of the present invention, use of the reference chip having a plurality of position-detection marks makes it possible to collect the correction data for a plurality of points by requiring only one stage movement. Thus, the correction data is obtained in a short period of time.
- Also, according to the fourth principle of the present invention, the correction coefficients for the entire main field are obtained through stage movements equal to the number of the sub-fields. Thus, the correction coefficients for the entire main field are obtained taking a short period of time.
- Also, according to the fourth principle of the present invention, the errors of the relative positions of the position-detection marks can be eliminated by measuring these errors in advance. Thus, the correction coefficients are obtained at high precision in a short period of time.
- Also, according to the fourth principle of the present invention, the errors of the relative positions of the position-detection marks are measured by using the position detecting mechanism of the charged-particle-beam exposure device. Thus, the correction coefficients are obtained at high precision in a short period of time without requiring another position detection device. Here, the position detecting mechanism of the charged-particle-beam exposure device may be a mechanism of the stage movement, which can be used as a measure for detecting the relative positions of the position-detection marks.
- Also, according to the fourth principle of the present invention, the correction coefficients may be corrected by using the deflection amount of the main deflector as a reference. Thus, the precise correction coefficients are quickly obtained through a simple method.
- Also, according to the fourth principle of the present invention, the errors of the relative positions of the position-detection marks contained in the correction coefficients are eliminated by using one position-detection mark and the deflection amount of the deflector as a reference. Thus, the precise correction coefficients are quickly obtained through a simple method.
- Furthermore, according to the fifth principle of the present invention, the position-detection mark is moved through stage movement only once for each of the measurement points when the correction coefficients are to be obtained for each of the sub-fields. This utilizes the fact that a plurality of sub-fields share the measurement points as corners thereof. Namely, the correction coefficients for the entire main field are obtained through stage movements equal to the number of the measurement points. Thus, the correction coefficients are obtained taking a short period of time.
- Consequently, according to the fourth and fifth principles of the present invention, highly precise beam calibration is carried out in a short period of time. Thus, the fourth and fifth principles of the present invention can greatly contribute to the development of the semiconductor exposure technology.
- Moreover, there are other problems concerning the present invention, and these problems will be described below.
- With recent advancement in the circuit density of integrated circuits, there has been a shift in use of technology for patterning semiconductor wafers from the photolithography technique widely used for a long tine to the charged-particle-beam exposure technique employing such beam as an electron beam.
- The charged-particle-beam exposure technique includes the variable-rectangle technique and the block exposure technique classified according to a pattern shape formed by one beam shot. In the block exposure technique, a charged-particle beam passes through a mask having unit patterns, so that even a complex pattern can be exposed at one shot. These unit patterns are generally the patterns which repeatedly appear on one chip. Thus, the block exposure technique is particularly useful for 256-Mbit DRAM chips, for example, because most areas of the chip has repetitive basic patterns despite micro structure thereof. Also, there is a technique called the BAA (blanking aperture array) technique. The BAA technique uses a BAA having apertures arranged therethrough in a matrix form, apertures being provided with a pair of electrodes. By switching on/off the voltage applied to the electrodes, each of the charged-particle beams passing through the apertures is independently turned on/off to form a pattern.
- FIG. 36 is an illustrative drawing showing a configuration of an example of the charged-particle-beam exposure device using the block exposure technique. The electron-beam exposure device includes an electron-
beam gun 501, an electron-lens system Lla, a rectangular-hole plate 502, an electron-lens system L1b, abeam shaping deflector 503, a first mask deflector MD1, a dynamic-mask-focus coil DF, an electron-lens system L2a, amask stage 505 carrying ablock mask 504, an electron-lens system L2b, a third mask deflector MD3, a blankingdeflector 506, a fourth mask deflector MD4, a convergence-electron-lens system L3, around aperture 507, a projection-electron-lens system L4, amain deflector 508, a sub-deflector 509, a projection-electron-lens system L5, awafer stage 511 carrying awafer 510, and a control system. The control system includes aCPU 521, aclock unit 522 generating various clocks including an exposure clock, abuffer memory 523, acontrol unit 524, a data-correction unit 525, amask memory 526, and a main-deflector setting unit 527. TheCPU 521 controlling operations of the entire device is connected to aclock unit 522, amask memory 526, and a main-deflector setting unit 527 via abus 528. In the figure, the data-correction unit 525 and the main-deflector setting unit 527 are shown as including a digital-to-analog converting function and an amplifying function for convenience. A laser interferometer for measuring a position of thewafer stage 511 and a stage-movement mechanism for shifting thewafer stage 511 are disclosed in U.S. Pat. No. 5,173,582 and U.S. Pat. No. 5,194,741, respectively, for example. Thus, these are not shown in the figure, and a description thereof will be omitted. - An electron beam emitted from the electron-
beam gun 501 passes through the rectangular-hole plate 502, and is deflected by the first mask deflector MD1 and the second mask deflector MD2 to a desired pattern on theblock mask 504. The electron beam having a cross-sectional shape of the desired pattern is brought back to the optical axis through focusing functions of the electron-lens system L2a and the electron-lens system L2b and through deflection functions of the third mask deflector MD3 and the fourth mask deflector MD4. Then, the electron beam having the cross section converged through the convergence-electron-lens system L3 is directed to thewafer 510 by the projection-electron-lens system L4 and the projection-electron-lens system L5. In this manner, the desired pattern is exposed on the wafer. - The
buffer memory 523 stores exposure-pattern data regarding patterns to be exposed on thewafer 510 and block data regarding mask patterns formed through theblock mask 504. The exposure-pattern data includes main-deflector data supplied to themain deflector 508. Themask memory 526 includes relations between mask-pattern positions and deflection data measured prior to an exposure process, and includes correction data used for correcting the deflection data supplied to the dynamic-mask stigmator DS and the dynamic-mask-focus coil DF. - The exposure-pattern data stored in the
buffer memory 523 after being read by theCPU 521 includes pattern-data codes PDC indicating which one of the mask patterns on theblock mask 504 is to be used for an exposure. Thecontrol unit 524 uses the pattern-data codes PDC to read from themask memory 526 the deflection data for deflecting the electron beam to a position of a selected mask pattern, and, then, supplies the deflection data to the first through fourth deflector MD1 through MD4 for selecting the pattern. The deflection data read from themask memory 526 is also provided for the data-correction unit 525. Here, the reading of the deflection data from themask memory 526 is carried out based on an exposure clock generated by theclock unit 522. - The main-
deflector setting unit 527 reads main-deflector data for themain deflector 508 from thebuffer memory 523 based on a clock from theclock unit 522, and supplies the main-deflector data to themain deflector 508. Deflection data for the sub-deflector 509, thebeam shaping deflector 503, and the blankingdeflector 506 is broken down into shot data by thecontrol unit 524 according to data stored in thebuffer memory 523. The shot data is supplied to the sub-deflector 509, thebeam shaping deflector 503, and the blankingdeflector 506 via the data-correction unit 525. Namely, thecontrol unit 524 determines a size of the electron beam and a position on theblock mask 504 of the electron beam according to the data stored in thebuffer memory 523 to supply the size and the position to the data-correction unit 525 when the variable-rectangle exposure is used. The data-correction unit 525 corrects the deflection data of the electron beam for a pattern to be exposed based on the correction data read from themask memory 526. The deflection data of thebeam shaping deflector 503 determines the size of the variable rectangle of the electron beam, and the deflection data of the blankingdeflector 506 is set for each shot of exposure. - FIG. 37 is an illustrative drawing showing an example of the
block mask 504. In the figure, theblock mask 504 includes a substrate 504 a made of metal or semiconductor like silicon and deflection areas 504-1 through 504-12 formed on the substrate 504 a. Each of the deflection areas 504-1 through 504-12 has a plurality of mask patterns formed therein. In the electron-beam exposure device using the block exposure, an area of the mask patterns which can be selected by deflecting the electron beam from a predetermined position on themask stage 505 is limited. Each of the deflection areas 504-1 through 504-12 is a 5-mm square, for example, corresponding to this limit. When the mask patterns within the deflection area 504-8 are to be exposed, for example, themask stage 505 is shifted such that the electron-optical-system axis of the device roughly coincides with a center of the deflection area 504-8. - As shown in an example of FIG. 37, the number of the mask patterns arranged in the deflection area504-8 is 48. Each of the mask patterns is identified based on the pattern-data codes PDC. Namely, the pattern-data codes PDC are an indicator for reading data corresponding to a given mask pattern from the
mask memory 526 by using an exposure clock of maximum 10 MHz, for example, provided from theclock unit 522. As described above, themask memory 526 stores the relations between the mask-pattern positions and the deflection data and the correction data to be supplied to the dynamic-mask stigmator DS and the dynamic-mask-focus coil DF for deflecting the electron beam to a given mask pattern. The deflection data and the correction data for a given deflection area are obtained by adjusting the electron beam prior to an exposure process, and are stored in themask memory 526. - In order to conduct an exposure process at higher speed, a waiting time for a shot, i.e., a time period required for deflecting the electron beam, must be reduced. Although an illustrative description is omitted in FIG. 36, the deflection data is provided for the
main deflector 508, etc., via amplifiers. Thus, a settling time of such amplifiers (a time period required for the amplifiers to become stable) largely determines the waiting time for a shot. Therefore, it is desirable to reduce the waiting time for a shot by reducing the settling time of such amplifiers, so that a redundant time involved in the drawing of patterns is decreased in the electron-beam exposure device to boost the throughput. - FIG. 38 is a block diagram of an exemplary driving unit of the
main deflector 508. In the figure, the deflection data from the main-deflector setting unit 527 is supplied to adriving system 610 via a digital-to-analog converter (DAC) 601, a current-to-voltage converter (IV converter) 602, and aresistor 603. Thedriving system 610 includes aresistor 604, aresistor 605, adifferential amplifier 606, and acapacitor 607. Themain deflector 508 includes acoil 608 which is an inductor impedance. - In the driving unit of FIG. 38, there is a large delay in the feedback because of the
main deflector 508 comprising thecoil 608. FIGS. 39A through 39C are time charts showing signals observed at various points of FIG. 38. When an input signal shown in FIG. 39A is applied to a node A of FIG. 38, for example, an output signal appearing at a node B would have a ringing effect as shown in FIG. 39B if thecapacitor 607 were not provided. - In order to shorten the settling time of the output signal, the
capacitor 607 for preventing the ringing effect is connected in parallel with theresistor 604 to lower the frequency range of thedifferential amplifier 606. Namely, the existence of thecapacitor 607 lowers a frequency characteristic of thedifferential amplifier 606 to reduce a through rate. - The existence of the
capacitor 607, however, makes a change in the input of thedifferential amplifier 606 extremely slow, so that a signal as shown in FIG. 39C is observed as the output signal at the node B. This creates a problem of a long settling time of thedifferential amplifier 606. Because of this, the waiting time for a shot should be set in accordance with this long settling time, thereby hindering an effort to enhance the throughput of the device. - Accordingly, there is a need for a charged-particle exposure device which can shorten the settling time of the amplifier to reduce the waiting time for a shot by suppressing the ringing effect of an amplifier output without lowering the frequency range of the amplifier.
- FIG. 40 is an block diagram of a main part of a charged-particle-beam exposure device according to a first embodiment of a sixth principle of the present invention. In FIG. 40, the same elements as those of FIG. 38 are referred to by the same numerals. In this embodiment, the sixth principle of the present invention is applied to an electron-beam exposure device, and a first embodiment of a charged-particle-beam exposure method is used in the device.
- FIG. 40 shows a driving unit of the
main deflector 508. In the figure, the deflection data from the main-deflector setting unit 527 is supplied to thedriving system 610 via the digital-to-analog converter 601, the current-to-voltage converter 602, and theresistor 603. Thedriving system 610 includes theresistor 604, theresistor 605, and thedifferential amplifier 606. Themain deflector 508 includes thecoil 608 which is an inductor impedance. A node N connects theresistor 603, theresistor 604, aresistor 705, and a reverse input node of thedifferential amplifier 606 together. The other input node of thedifferential amplifier 606 is connected to a ground. A node D connects theresistor 604 and theresistor 605, and thecoil 608 is interposed between the node D and the output node of thedifferential amplifier 606. - A
pulse generating circuit 701 generates a pulse signal having a reversed phase to a first wave of the ringing appearing in the output of thedifferential amplifier 606 in order to cancel the first wave of the ringing. The generation of the pulse signal is based on the deflection data provided from the main-deflector setting unit 527. The pulse signal is supplied to thedifferential amplifier 606 via theresistor 705. A pulse length of the pulse signal is shorter than a time period from a start of the first wave of the ringing to a start of the second wave of the ringing. Thepulse generating circuit 701 includes a pulse-parameter outputting circuit 702, aDAC 703, and anIV converter 704. The pulse-parameter outputting circuit 702 generates pulse parameters to suppress the ringing appearing at the node D based on the deflection data from the main-deflector setting unit 527. The pulse parameter include a pulse-delay time, a pulse length, a magnitude, etc., of the pulse signal generated by thepulse generating circuit 701. The pulse parameters are applied to a node C via theDAC 703 and theIV converter 704. It is desirable to be able to set at least one of the pulse parameters, and, also, it is desirable to be able to set each of the pulse parameters independently from each other. - FIGS. 41A through 41D are time charts showing signals observed at various points of FIG. 40. FIG. 41A shows an input signal applied to the node A of FIG. 40. FIG. 41B shows an output signal which would appear at the node D if the
pulse generating circuit 701 were not provided. FIG. 41C shows a pulse signal generated by thepulse generating circuit 701 and applied to the node C. FIG. 41D shows an output signal appearing at the node D when thepulse generating circuit 701 is provided. In the first embodiment, the pulse signal appearing at the node C is added to a signal applied to the reverse input node of thedifferential amplifier 606 to cancel the delayed response fed back to thedifferential amplifier 606, so that the ringing shown in FIG. 41B is suppressed. Therefore, thedifferential amplifier 606 for an inductor impedance has a shorter settling time without sacrificing the frequency characteristic of thedifferential amplifier 606. - FIG. 42 is a block diagram of a main part of a charged-particle-beam exposure device according to a second embodiment of the sixth principle of the present invention. In FIG. 42, the same elements as those of FIG. 40 are referred to by the same numerals. In this embodiment, the sixth principle of the present invention is applied to an electron-beam exposure device, and a second embodiment of a charged-particle-beam exposure method is used in the device.
- In FIG. 42, the deflection data is generated by a pattern generating (PG)
unit 527A, and is supplied to the digital-to-analog converter 601 and apulse generating circuit 711. Thepulse generating circuit 711 includes a data-timing-adjustment circuit 712, amemory 713, amemory 714, aclock generating circuit 715, theDAC 703, and theIV converter 704. A clock supplied to the digital-to-analog converter 601 and theclock generating circuit 715 is provided from theclock unit 522 of FIG. 36, for example. TheDAC 703 is provided with a clock from theclock generating circuit 715. An output signal at the node D is supplied to acontrol unit 716 via a analog-to-digital converter (ADC) 717 constituting a feedback-adjustment system. Thecontrol unit 716 corresponds to thecontrol unit 524 of FIG. 36, for example. - A change in the data from the
pattern generating unit 527A from n-th data to n+1-th data appears as a change in the output of thedifferential amplifier 606. The feedback of the voltage change at the node D to thecontrol unit 716 via the analog-to-digital converter 717 makes it possible for the analog-to-digital converter 717 to monitor the output change of thedifferential amplifier 606. Thecontrol unit 716 takes a derivation of the data fed back via the analog-to-digital converter 717, and obtains pulse parameters which make the derivation become zero in the shortest period of time. That is, the pulse parameters for suppressing the first wave of the ringing appearing at the node D are obtained. In practice, thecontrol unit 716 calculates derivations of the data provided from the analog-to-digital converter 717 while changing the pulse parameters, and obtains optimal values of the pulse parameters with which the derivation becomes zero the fastest. When obtaining the optimal values of the pulse parameters, thecontrol unit 716 supplies pulse parameters regarding the pulse delay and the pulse length to theclock generating circuit 715, and supplies a pulse parameter concerning the pulse magnitude to theDAC 703. - The optimal pulse parameters obtained by the
control unit 716 are stored in thememories pattern generating unit 527A. Here, the optimal pulse parameters regarding the pulse delay and the pulse length are stored in thememory 713, and the optimal pulse parameter regarding the pulse magnitude is stored in thememory 714. The storing of the optimal pulse parameters in thememories - δpara =P(X n+1 =X n)×Q(X n) (21)
- In the equation (21), P is a function of a jump amount of the data, and Q is a linear interpolation function.
- Namely, the pulse parameters are proportional to a change in the input data, i.e., a difference in the data or the jump amount of the data, and receives an effect of the jump-start point Xn as a correction by a multiplication form. Q(Xn) is a linear interpolation function having values equal to monitored values at points monitored by the
control unit 716. Based on the approximation function δpara, the optimal pulse parameters are obtained for every possible input-data change, i.e., every possible jump amount. Then, the optimal pulse parameters are finely adjusted by repeating the same procedure as that of having obtained the optimal pulse parameters the first time. Therefore, the optimal pulse parameters for every possible input-data change are obtained in a relatively short period of time. - An operation at a time of exposure will be described below. The deflection data provided from the
pattern generating unit 527A for the n+1-th pattern data is supplied as a data change from the n-th data to the n+1-th data to thedifferential amplifier 606 via the digital-to-analog converter 601, the current-to-voltage converter 602, and theresistor 603. The data-timing-adjustment circuit 712 adjusts the data timing of the n-th data and the n+1-th data to provide them simultaneously for thememories memory 713 to be supplied to theclock generating circuit 715. Also, the pulse parameter regarding the pulse magnitude is read from thememory 714 to be supplied to theDAC 703. - FIG. 43 is a block diagram of an example of the data-timing-
adjustment circuit 712 shown with thememory 713 and thememory 714. In the figure, thememory 713 and thememory 714 are shown as one memory for convenience of explanation. The data-timing-adjustment circuit 712 includes a register 712A, so that the n-th data temporarily stored in the register 712A is supplied to the memory at the same time as the n+1-th data is supplied. - The
clock generating circuit 715 generates a clock in response to a clock synchronizing with the n+1-th data from theclock unit 522 based on the pulse parameters regarding the pulse delay and the pulse length read from thememory 713. The generated clock is sent to theDAC 703. The pulse parameter regarding the pulse magnitude read from thememory 714 is supplied to theDAC 703 as weighting data. An output of theDAC 703 is provided for the node N via theIV converter 704 and theresistor 705 to be added to an output of the digital-to-analog converter 601 provided via the current-to-voltage converter 602 and theresistor 603. A signal after the addition is supplied to the reverse input node of thedifferential amplifier 606. - FIG. 44A is a time chart showing a clock provided from the
clock unit 522 to the digital-to-analog converter 601 and theclock generating circuit 715. FIG. 44B is a time chart showing an output signal observed at the node D when thepulse generating circuit 711 is not provided. FIG. 44C is a time chart showing a clock provided from theclock generating circuit 715 to theDAC 703. FIG. 44D is a time chart showing a correction pulse signal output from theIV converter 704. - FIGS. 45A and 45B are time charts showing output voltages obtained through a simulation. FIG. 45A shows an output voltage obtained at the node D when the
pulse generating circuit 711 for applying the correction pulse signal to the node N is not provided. FIG. 45B shows an output voltage obtained at the node D when thepulse generating circuit 711 is provided to apply the correction pulse signal to the node N. As shown in FIGS. 45A and 45B, the ringing of the output voltage is suppressed according to the second embodiment of the sixth principle of the present invention. - FIG. 46 is a flowchart of a process of obtaining the optimal pulse parameters. The process of obtaining the optimal pulse parameters will be described with reference to FIG. 46 and FIG. 42.
- At a step S81, the deflection data generated by the
pattern generating unit 527A is supplied to thedifferential amplifier 606 via the digital-to-analog converter 601, the current-to-voltage converter 602, and theresistor 603. - At a step S82, the pulse delay and the pulse magnitude are set in the
pulse generating circuit 711 by thecontrol unit 716. - At a step S83, the
pulse generating circuit 711 generates a correction pulse signal based on the pulse parameters set at the step S82. - At a step S84, the
control unit 716 monitors an output signal appearing at the node D via the analog-to-digital converter 717. - At a step S85, the
control unit 716 measures the settling time of the monitored output signal. - At a step S86, the
control unit 716 checks whether the correction pulse signal is generated by thepulse generating circuit 711 for all the pulse magnitudes and the pulse delays. If the answer is yes, the procedure goes to a step S87. Otherwise, the procedure goes back to the step S82. - At the step S87, the
control unit 716 obtains the pulse magnitude and the pulse delay of the shortest settling time. - At a step S88, the
control unit 716 checks whether sufficient data for obtaining the approximation function δpara is collected. If it is not, the procedure goes back to the step S81. Otherwise, the procedure goes to a step S89. - At the step S89, the
control unit 716 obtains the approximation function δpara by using the collected data. - At a step S90, the
control unit 716 obtains pulse parameters regarding the pulse magnitude, the pulse delay, and the pulse length for all the deflection data (deflection pattern). - At a step S91, the
control unit 716 stores the obtained pulse parameters in thememories - FIG. 47 is a block diagram of a main part of a charged-particle-beam exposure device according to a third embodiment of the sixth principle of the present invention. In FIG. 47, the same elements as those of FIG. 42 are referred to by the same numerals, and a description thereof will be omitted. In this embodiment, the sixth principle of the present invention is applied to an electron-beam exposure device, and a third embodiment of a charged-particle-beam exposure method is used in the device.
- In FIG. 47, the feedback adjustment system includes a error-band setting circuit722 for setting an error-band width based on an instruction given by the
control unit 716, and, also, includes a window comparator 721. The window comparator 721 compares the output signal obtained from the node D with the error-band width obtained from the error-band setting circuit 722 to generate a signal indicating whether the output signal falls in the error-band width. This signal is supplied to thecontrol unit 716. Thecontrol unit 716 changes the pulse parameters to obtain the shortest time period from a start of a change in the output signal (voltage) at the node D to a time when the output signal falls within the error-band width. At the same time, thecontrol unit 716 continues the feedback operation through the window comparator 721 to obtain the optimal pulse parameters. Other operations are the same as those of the second embodiment of the sixth principle described with reference to FIG. 42. - FIG. 48 is a flowchart of a process of obtaining the optimal pulse parameters according to the third embodiment of the sixth principle. This process of obtaining the optimal pulse parameters will be described with reference to FIG. 48 and FIG. 47.
- At a step S101, the
control unit 716 sends an instruction to the error-band setting circuit 722 to set an error-band width. - At a step S102, the deflection data generated by the
pattern generating unit 527A is supplied to thedifferential amplifier 606 via the digital-to-analog converter 601, the current-to-voltage converter 602, and theresistor 603. - At a step S103, the pulse delay and the pulse magnitude are set in the
pulse generating circuit 711 by thecontrol unit 716. - At a step S104, the
pulse generating circuit 711 generates a correction pulse signal based on the pulse parameters set at the step S103. - At a step S105, the
control unit 716 monitors a signal obtained from the window comparator 721. - At a step S106, the
control unit 716 measures the settling time of the monitored signal, i.e., measures a time period passing before the output signal at the node D falls within the error-band width. - At a step S107, the
control unit 716 checks whether the correction pulse signal is generated by thepulse generating circuit 711 for all the pulse magnitudes and the pulse delays. If the answer is yes, the procedure goes to a step S108. Otherwise, the procedure goes back to the step S103. - At the step S108, the
control unit 716 obtains the pulse magnitude and the pulse delay of the shortest settling time. - At a step S109, the
control unit 716 checks whether sufficient data for obtaining the approximation function δpara is collected. If it is not, the procedure goes back to the step S102. Otherwise, the procedure goes to a step S110. - At the step S110, the
control unit 716 obtains the approximation function δpara by using the collected data. - At a step S111, the
control unit 716 obtains pulse parameters regarding the pulse magnitude, the pulse delay, and the pulse length for all the deflection data (deflection pattern). - At a step S112, the
control unit 716 stores the obtained pulse parameters in thememories - FIG. 49 is a block diagram of a main part of a charged-particle-beam exposure device according to a fourth embodiment of the sixth principle of the present invention. In FIG. 49, the same elements as those of FIG. 42 are referred to by the same numerals, and a description thereof will be omitted. In this embodiment, the sixth principle of the present invention is applied to an electron-beam exposure device, and a fourth embodiment of a charged-particle-beam exposure method is used in the device.
- In FIG. 49, the feedback adjustment system includes a
reflection detector 731 detecting electrons of the electron beam scattered by thewafer 510, anamplifier 732 amplifies a detected signal of thereflection detector 731, and anADC 733 converting an output of theamplifier 732 to digital data to be supplied to thecontrol unit 716. Thecontrol unit 716 monitors movement of the electron beam based on the digital data provided from theADC 733. In the same manner as in the second embodiment of the sixth principle, thecontrol unit 716 takes a derivation of the digital data sent from theADC 733 while changing a position of the electron beam, so as to obtain the optimal pulse parameters with which the derivation becomes zero in the shortest period of time. When obtaining the optimal pulse parameters, thecontrol unit 716 supplies the pulse parameters regarding the pulse delay and the pulse length to theclock generating circuit 715, and supplies the pulse parameter regarding the pulse magnitude to theDAC 703. Other operations are the same as those of the second embodiment of the sixth principle described with reference to FIG. 42. - FIG. 50 is a flowchart of a process of obtaining the optimal pulse parameters according to the fourth embodiment of the sixth principle. This process of obtaining the optimal pulse parameters will be described with reference to FIG. 50 and FIG. 49.
- At a step S121, the deflection data generated by the
pattern generating unit 527A is supplied to thedifferential amplifier 606 via the digital-to-analog converter 601, the current-to-voltage converter 602, and theresistor 603. - At a step S122, the pulse delay and the pulse magnitude are set in the
pulse generating circuit 711 by thecontrol unit 716. - At a step S123, the
pulse generating circuit 711 generates a correction pulse signal based on the pulse parameters set at the step S122. - At a step S124, the
control unit 716 uses thereflection detector 731 to detect the scattered electrons while changing a position of the electron beam. - At a step S125, the
control unit 716 monitors a detected signal of thereflection detector 731 via theamplifier 732 and theADC 733. - At a step S126, the
control unit 716 measures the settling time of the monitored detected signal. - At a step S127, the
control unit 716 checks whether the correction pulse signal is generated by thepulse generating circuit 711 for all the pulse magnitudes and the pulse delays. If the answer is yes, the procedure goes to a step S128. Otherwise, the procedure goes back to the step S122. - At the step S128, the
control unit 716 obtains the pulse magnitude and the pulse delay of the shortest settling time. - At a step S129, the
control unit 716 checks whether sufficient data for obtaining the approximation function δpara is collected. If it is not, the procedure goes back to the step S121. Otherwise, the procedure goes to a step S130. - At the step S130, the
control unit 716 obtains the approximation function δpara by using the collected data. - At a step S131, the
control unit 716 obtains pulse parameters regarding the pulse magnitude, the pulse delay, and the pulse length for all the deflection data (deflection pattern). - At a step S132, the
control unit 716 stores the obtained pulse parameters in thememories - The above description of the sixth principle has been provided through an example in which the deflector is an electromagnetic deflector such as a main deflector. However, the sixth principle of the present invention can be applied to any types of deflectors as well as an electromagnetic deflector and a main deflector.
- FIGS. 51A and 51B are circuit diagrams showing configurations of the dynamic-mask stigmator DS of FIG. 36. FIG. 51A shows a configuration of an X-axis portion of the dynamic-mask stigmator DS, and FIG. 51B shows a configuration of a Y-axis portion of the dynamic-mask stigmator DS.
- In FIG. 51A, the X-axis portion of the dynamic-mask stigmator DS has a stigmator coil portion including coils LX1 through LX4, each comprising 40 turns, for example. The data having 12 bits, for example, is supplied via a
DAC 741 and anamplifier 742 to the coils LX1 through LX4 connected in a series. In FIG. 51B, the Y-axis portion of the dynamic-mask stigmator DS has a stigmator coil portion including coils LY1 through LY4, each comprising 40 turns, for example. The data having 12 bits, for example, is supplied via aDAC 751 and anamplifier 752 to the coils LY1 through LY4 connected in a series. Settling times of theamplifiers amplifiers - The load amount of the coils is basically determined by configurations of the beam-deflection system and the lens system, so that the load amount cannot be freely reduced to shorten the settling time of the
amplifiers amplifier 742 for various turn numbers of the coils LX1 through LX4. FIG. 52A shows the output signal of theamplifier 742 when the turn number is 0, i.e., the coils are short-circuited. FIGS. 52B through 52D show cases in which the turn number is 20, 30, and 40, respectively. As shown in the figures, the ringing of the output signal of theamplifier 742 increases as the turn number increases to raise the load amount. - FIG. 53 is a circuit diagram of the dynamic-mask-focus coil DF of FIG. 36.
- In FIG. 53, a focus coil portion of the dynamic-mask-focus coil DF include a coil LF having 40 turns, for example. The data having 12 bits, for example, is supplied via a
DAC 761 and anamplifier 762 to the coil LF. A settling time of theamplifier 762 supplying the data to the dynamic-mask-focus coil DF is mainly determined by the load of the dynamic-mask-focus coil DF. Namely, the settling time of theamplifier 762 is dependent on various parameters of the coil LF such as the diameter, the number of turns (laps) determining the self-inductance, and a mutual inductance determining a mutual dependency between the coils. - The load amount of the coils is basically determined by configurations of the beam-deflection system and the lens system, so that the load amount cannot be freely reduced to shorten the settling time of the
amplifier 762. - However, it is possible to add the correction pulse signal of the above embodiments of the sixth principle to the input of the amplifiers so that the ringing of the output signals of the
amplifiers - Also, in order to shorten the settling time of the amplifiers, the effective load of the coils can be suppressed as shown in the following embodiments.
- FIG. 54 is a circuit diagram of a main part of a charged-particle-beam exposure device according to a first embodiment of a seventh principle. In FIG. 54, the same elements as those of FIGS. 51A and 51B are referred by the same numerals, and a description thereof will be omitted. In this embodiment, the seventh principle is applied to an electron-beam exposure device, and a first embodiment of a charged-particle-beam exposure method is used in the device.
- FIG. 54 shows a stigmator-coil portion DSxl through DSxN for the X axis of the dynamic-mask stigmator DS. A drawing for a stigmator-coil portion DSy1 through DSyN for the Y axis of the dynamic-mask stigmator DS is the same as FIG. 52, and is thus omitted. The stigmator-coil portion DSx1 for the X axis of the dynamic-mask stigmator DS includes coils LX1-1 through LX4-1, each comprising 40 turns, for example. Data having 12 bits, for example, is supplied via a DAC 741-1 and a amplifier 742-1 to the coils LX1-1 through LX4-1 arranged in a series. In the same manner, data having 12 bits is supplied via a DAC 741-2 and a amplifier 742-2 to coils LX1-2 through LX4-2 arranged in a series. The coils LX1-2 through LX4-2 constitute the stigmator-coil portion DSx2. Also, data having 12 bits is supplied via a DAC 741-N and a amplifier 742-N to coils LX1-N through LX4-N arranged in a series. The coils LX1-N through LX4-N constitute the stigmator-coil portion DSx2.
- In FIG. 54, even when the same amplifiers are used for the amplifiers742-1 through 742-N of different stages, an output of each amplifier will have some drift depending on temperature. Namely, because of thermal-condition changes and the like caused by changes in the ambient temperature and heat generation of the amplifiers, outputs of the amplifiers have some drift. Therefore, when a plurality of stages of the stigmator-coil portions are arranged along the axis of the electron beam, the electron beam passing through the
round aperture 507 will have a variation in the current density and will be blurred. - FIG. 55 is a chart showing a variation in the current density of the electron beam passing through the
round aperture 507 when a position of the electron beam is displaced by the drift in the output of the amplifiers. As shown in FIG. 55, in order to keep the variation of the current density within a 1-% range, the electron beam must be positioned with an extreme precision. In this embodiment, thus, two stigmator-coil portions adjacent to each other (e.g, DSx1 and DSx2) are driven by electric currents of opposite directions, as shown by arrows in FIG. 54. - FIG. 56 is a chart showing a drift in an output of an amplifier. As shown in the figure, the drift increases over time in a negative direction when a current of a positive direction is applied. When a current of a negative direction is applied, the drift increases over time in a negative direction as well. Therefore, when every two stigmator-coil portions adjacent to each other are driven by electric currents of opposite directions, the drifts in the outputs of the amplifiers are canceled with each other.
- FIG. 57 is an illustrative drawing showing an example of a configuration of the stigmator-coil portions when six of them are provided. Each of the stigmator-coil portions DSx1 through DSx6 has a diameter of 15 mm and a length of 4 mm along the electron-beam axis, and is arranged at a 0.8-mm interval. A total length from the stigmator-coil portion DSx1 to the stigmator-coil portion DSx6 along the electron-beam axis is 28 mm.
- A-configuration of the stigmator-coil portions DSy1 through DSyN for the Y axis of the dynamic-mask stigmator DS is the same as that of FIG. 57, except that they are arranged with a phase displacement of 45° relative to the stigmator-coil portions DSx1 through DSxN around the electron-beam axis.
- In the first embodiment of the seventh principle, four coils are provided. However, the number of coils can be 2 or more than 4, as long as the coils are arranged such that magnetic fields generated by the coils are canceled at a center position between the coils.
- FIG. 58 is a circuit diagram of a main part of a charged-particle-beam exposure device according to a second embodiment of the seventh principle. In FIG. 58, the same elements as those of FIG. 53 are referred by the same numerals, and a description thereof will be omitted. In this embodiment, the seventh principle is applied to an electron-beam exposure device, and a second embodiment of a charged-particle-beam exposure method is used in the device.
- FIG. 58 shows a focus-coil portion of the dynamic-mask-focus coil DF. The focus-coil portion of the dynamic-mask-focus coil DF includes coils LF1 through LFN, each comprising 40 turns, for example. Data having 12 bits, for example, is supplied via a DAC 761-1 and an amplifier 762-1 to the coil LF1. In the same manner, data having 12 bits is supplied via a DAC 761-2 and an amplifier 762-2 to the coil LF2. The coil LF2 constitutes the focus-coil portion. Also, data having 12 bits is supplied via a DAC 761-N and an amplifier 762-N to the coil LFN. The coil LFN constitutes the focus-coil portion.
- In FIG. 58, even when the same amplifiers are used for the amplifiers762-1 through 762-N of different stages, an output of each amplifier will have some drift depending on temperature. Namely, because of thermal-condition changes and the like caused by changes in the ambient temperature and heat generation of the amplifiers, outputs of the amplifiers have some drift. Therefore, when a plurality of stages of the focus-coil portions are arranged along the axis of the electron beam, the electron beam passing through the
round aperture 507 will have a variation in the current density and will be blurred. - FIG. 59 is a chart showing a variation in the current density of the electron beam passing through the
round aperture 507 when a position of the electron beam is displaced by the drift in the output of the amplifiers. As shown in FIG. 59, in order to keep the variation of the current density within a 1-% range, the electron beam must be positioned with an extreme precision. In this embodiment, thus, two focus-coil portions adjacent with each other (e.g, LF1 and LF2) are driven by electric currents of opposite directions, as shown by arrows in FIG. 59. - FIGS. 60A and 60B are illustrative drawings showing an example of a configuration of the focus-coil portions when five of them are provided. FIG. 60A shows the focus-coil portion of the dynamic-mask-focus coil DF of the electron-beam exposure device, and FIG. 60B shows an enlarged view of the configuration of the focus-coil portions of the dynamic-mask-focus coil DF. FIG. 60B also shows a magnetic field B distributed along the electron-beam axis of the electron-lens system L2a. Each of focus coils LF1 through LF5 has a 5-mm diameter Φ, and is arranged at a 5-mm interval P. A total length TL from the focus coil LF1 to the focus coil LF5 along the electron-beam axis of the electron-beam exposure device is 20 mm. In this configuration, the intervals must be larger than or equal to the diameter Φ.
- In the first and second embodiments of the seventh principle of the present invention, the correction pulse signal may be added to the input of each amplifier as in the first through fourth embodiments of the sixth principle. In this case, an adverse effect of the drift in the output of the amplifier is reduced, and, at the same time, an adverse effect of the ringing of the output of the amplifier is alleviated.
- Applications of the sixth and seventh principles of the present invention are not limited only to electron-beam exposure devices. The sixth and seventh principles of the present invention can be applied to any charged-particle-beam exposure devices.
- According to the sixth principle of the present invention, the pulse signal is added to the input of the amplifier to cancel the delayed response fed back to the amplifier, thereby suppressing the ringing. Therefore, an amplifier having a short settling time used for inductor impedance is provided without sacrificing the frequency characteristics of the amplifier.
- According to the sixth principle of the present invention, the optimal pulse parameters for the correction pulse signal are stored in memories, and the pulse signal is generated based on the optimal pulse parameters. Therefore the ringing is suppressed by using a simple circuit structure.
- According to the seventh principle of the present invention, the use of a plurality of stages of coils enables a reduction in the effective load of the coils, and enables a cancellation of the drift in the output of the amplifier. Therefore, the settling time of the amplifier is shortened.
- Accordingly, the charged-particle-beam exposure device according to the sixth and seventh principles of the present invention can shorten the settling time of the amplifier to reduce the waiting time for a shot by suppressing the ringing effect of an amplifier output without lowering the frequency range of the amplifier.
- Moreover, there are other problems of concern to the present invention, and these problems will be described below.
- FIG. 61 is an illustrative drawing showing a configuration of a charged-particle-beam exposure device of the related art using a stencil mask.
- A charged-particle beam (e.g., electron beam) emitted from a charged-
particle gun 810 passes through a selected hole pattern formed through astencil mask 812 so that a cross section of the beam is shaped in a selected pattern. The beam having the shaped cross section is converged and positioned on a wafer (not shown). FIG. 61 shows a beam axis AX and abeam trajectory 813A. The charged-particle-beam exposure device of FIG. 61 also includeselectromagnetic lenses aperture plates - The charged-particle beam passing through
electromagnetic lens 821B along the beam axis AX is deflected by adeflector 845, and, then, bent by adeflector 846 to become parallel to the beam axis AX. In this manner, the charged-particle beam runs in a vertical direction when it passes through the selected hole pattern of thestencil mask 812. The charged-particle beam having passed through thestencil mask 812 is deflected by adeflector 847 and bent by adeflector 848 to be placed along the beam axis AX. - In the charged-particle-beam exposure device of this configuration, the charged-particle beam is incident to the
stencil mask 812 from a normal direction, so that the cross section of the beam is shaped with high precision. Also, a hole pattern of thestencil mask 812 can be selected from a wide-range area. - However, when a deflection amount of any of the
deflectors 845 through 848 is changed, there is a huge positional displacement of the charged-particle beam on theaperture plate 831 and on the wafer. This crates a problem when a hole pattern of thestencil mask 812 is selected. When the deflection amount of thedeflector 846 is slightly increased, for example, the charged-particle beam has abeam trajectory 813B as shown in FIG. 61. A high precision such as within a range of 0.01 μm, for example, is required for the positioning of the charged-particle beam on the wafer. When a hole pattern is selected, thedeflectors 845 through 848 receive driving voltages having a step change. In this case, a long settling time is required. - In order to precisely direct the charged-particle beam at a target position on the wafer, the charged-particle beam is blanked during the settling time by a blanking deflector (not shown) and the
aperture plate 831. A beam exposure on the wafer should wait until the settling time lapses, thereby creating a dead time to reduce throughput of the exposure process. - FIG. 62 is an illustrative drawing showing a configuration of a charged-particle-beam exposure device disclosed in Japanese Patent Laid-Open Application No.62-206828.
- In the device of FIG. 62, cross-over images CO1 and CO2 of a gun cross over CO of the charged-
particle gun 810 are positioned between theelectromagnetic lens 821B and anelectromagnetic lens 822 and positioned between theelectromagnetic lens 822 and theelectromagnetic lens 823. Adeflector 840 is arranged such that a center point thereof is positioned at a position of the cross-over image CO1. Also, adeflector 849 is arranged such that a center point thereof is positioned at a position of the cross-over image CO2. Apath 813C shows an extent of the charged-particle beam, enlarged in a direction perpendicular to the beam axis AX, passing through theelectromagnetic lenses deflectors - The charged-particle beam deflected by the
deflector 840 to pass through a selected hole pattern of thestencil mask 812 is focused at a position of the cross-over image CO2 through a convergence effect of theelectromagnetic lens 822. The charged-particle beam is then deflected by thedeflector 849 to run along the beam axis AX. - In the charged-particle-beam exposure device of FIG. 62, deflectors functionally equivalent to the
deflectors stencil mask 812 can be selected becomes narrower than that of FIG. 61. - In FIG. 62, the cross-over image CO2 is positioned several millimeters from the top of the
electromagnetic lens 823. Because of such a short distance, the center point of thedeflector 849 cannot be positioned at the position of the cross-over image CO2. Then, the charged-particle beam deflected by thedeflector 849 deviates from the beam axis AX to deteriorate positional accuracy of the charged-particle beam on the wafer. Also, deflection efficiencies of thedeflectors aperture plate 831 and the wafer become larger than those of FIG. 61, thereby lengthening the setting time. - FIG. 63 is a chart of a temporal change in a driving voltage of a deflector for showing a settling time of the deflector. In FIG. 63, a time position ta indicates a settling time required for the device of FIG. 61, and a time position tb indicates a settling time required for the device of FIG. 62.
- Accordingly, there is a need for a charged-particle-beam exposure device and a charged-particle-beam exposure method which can improve the positional accuracy of the charged-particle beam on a wafer, and which can shorten the settling time required when there is a step change in a driving voltage of a deflector.
- In the following, embodiments of an eighth principle of the present invention will be described with reference to the accompanying drawings.
- FIG. 64 is an illustrative drawing of a configuration of a charged-particle-beam exposure device according to a first embodiment of the eighth principle of the present invention. A charged-particle beam (e.g., electron beam) emitted from the charged-
particle gun 810 exposes a resist layer on awafer 811. Thestencil mask 812 has a plurality of hole patterns frequently used in exposure processes. The charged-particle beam passes through a selected hole pattern so that a cross section of the charged-particle beam is shaped into a desired pattern. This pattern is converged and projected to thewafer 811. - A
beam trajectory 813 shows an extent of the charged-particle beam passing throughelectromagnetic lenses 821 through 825, and is shown enlarged in a direction perpendicular to the beam axis AX. Theelectromagnetic lens 821 includes theelectromagnetic lens 821A and theelectromagnetic lens 821B, and theaperture plate 830 is placed between theelectromagnetic lenses electromagnetic lens 821A passes through a square hole of theaperture plate 830 such that the charged-particle beam has a cross-sectional size covering only one hole pattern of thestencil mask 812. Theelectromagnetic lens 822 includes theelectromagnetic lens 822A and theelectromagnetic lens 822B, and thestencil mask 812 is placed between theelectromagnetic lenses electromagnetic lens 822A passes through a selected hole pattern of thestencil mask 812. Theelectromagnetic lenses aperture plate 831 having a round aperture is placed between theelectromagnetic lens 823 and theelectromagnetic lens 824. Theelectromagnetic lens 825 is an objective lens, and converges the charged-particle beam on thewafer 811. - A
main deflector 832 and a sub-deflector 833 deflect the charged-particle beam to a target position on thewafer 811. - The cross-over image CO1 of the gun cross over CO is positioned between the
electromagnetic lens 821B and theelectromagnetic lens 822A. The cross-over image CO2 of the gun cross over CO is positioned between theelectromagnetic lens 822B and theelectromagnetic lens 823. Also, a cross-over image CO3 of the gun cross over CO is located between theelectromagnetic lens 823 and theelectromagnetic lens 824. - In order to deflect the charged-particle beam from the beam axis AX to a selected hole pattern of the
stencil mask 812, thedeflector 840 is placed between theelectromagnetic lens 821B and theelectromagnetic lens 822A. Here, a center point of thedeflector 840 is positioned at a position of the cross-over image CO1. In order to deflect the charged-particle beam having passed through theelectromagnetic lens 822B back to the beam axis AX,def lectors electromagnetic lens 822B and theelectromagnetic lens 823. Thedeflector 842 is situated nearer to theelectromagnetic lens 823. However, since the cross-over image CO2 is positioned only several millimeter from the top of theelectromagnetic lens 823, a center point of thedeflector 842 cannot be located at a position of the cross-over image CO2. Because of this reason, thedeflector 841 is situated nearer to theelectromagnetic lens 822B. - The
aperture plate 831 is situated such that a center of the round aperture coincides with a position of the cross-over image CO3. - Because of a variation in a thermal expansion due to ambient-temperature changes and a variation in the atmospheric pressure, the electromagnetic lenses are subjected to varying stresses. Also, as electrodes of the charged-
particle gun 810 are worn over a long time, the positions of the cross-over images CO1 and CO2 vary slightly. Because of these factors and deviations from design specifications, the charged-particle beam having passed through theelectromagnetic lens 823 is displaced from the beam axis AX. In order to correct this displacement, acorrection deflector 843 is provided between thedeflector 840 andelectromagnetic lens 822A, and acorrection deflector 844 is provided between thedeflector 841 and thedeflector 842. - An output of an
amplifier 850 is connected to thedeflector 840, and an output of anamplifier 851 is connected to thedeflector 841 and thedeflector 842. Also, outputs ofamplifiers correction deflectors deflectors 840 through 844 are static-charge-type deflectors, each having opposing electrodes. The opposing electrodes receive voltages having the same magnitude and a reversed phase. Since each of thedeflectors 840 through 844 generates only a small deflection angle, a trajectory of the charged-particle beam keeps a linear relation with the voltage applied to a deflector. Voltage ratios between thedeflectors 840 through 844 are kept constant irrespective of a position of a selected pattern of thestencil mask 812. - FIG. 65 is an illustrative drawing showing a configuration of the
deflectors - Each of the
deflectors deflector 840 and thecorrection deflector 843 also have the same configuration.) Because of these eight electrodes, theamplifier 851 of FIG. 64 includesamplifiers 1011 through 1018. Outputs of theamplifiers 1011 through 1018 are connected toelectrodes 911 through 918 of thedeflector 841, respectively, and are also connected toelectrodes 921 through 928 of thedeflector 842, respectively. - The
deflector 841 and thedeflector 842 are supported by asupporter 860 and asupporter 861, respectively. Center axes of thedeflectors deflector 840 and thecorrection deflector 843 of FIG. 64 also have the same configuration.) Rotation errors of thedeflectors amplifiers 1011 through 1018. However, since the same output of the same amplifier is applied to a respective electrode of thedeflector 841 and thedeflector 842, the electrical correction is effective only for one of thedeflector 841 and thedeflector 842. In response,teeth 862 are formed on part of the side surface of thesupporter 860, and aworm 863 is fitted to theteeth 862. Theworm 863 has awheel 864 attached thereto, and rotation of thewheel 864 allows a mechanical correction of thedeflector 841. - FIGS. 66A and 66B are illustrative drawings for explaining trajectories of the charged-particle beam deflected by the deflectors.
- In FIG. 66A, the
deflectors 841 through 843 receive a zero voltage. When the charged-particle beam is deflected by thedeflector 840, a linearly approximatedtrajectory 813D of the charged-particle beam is obtained as shown in FIG. 66A. Namely, since the center point of thedeflector 840 is positioned at the position of the cross-over image CO1, the charged-particle beam deflected by thedeflector 840 becomes parallel to the beam axis AX after passing through theelectromagnetic lens 822A. Also, after passing through theelectromagnetic lens 822B, the charged-particle beam reaches the position of the cross-over image CO2, and, then, reaches the position of the cross-over image CO3. - In FIG. 66B, voltages applied to the
deflectors aperture plate 831 and that the charged-particle beam is deflected by thedeflector 841 and thedeflector 842. In this case, a linearly approximated trajectory 813E as shown in FIG. 66B is obtained. Here, a deflection by thedeflector 841 is set to such an amount that a dotted line running through points P3 and P4 and extended upstream runs through the position of the cross-over image CO2. If setting is made to satisfy this condition when the same voltage is applied to thedeflector 841 and thedeflector 842, this condition will be satisfied for any voltages as long as these voltages are within a range allowing the linear approximation. The charged-particle beam having passed through theelectromagnetic lens 822B is paralleled to the beam axis AX. After passing through theelectromagnetic lens 822A, the charged-particle beam runs through the position of the cross-over image CO1. - Assume that when a voltage VMl is applied to the
deflector 840 in FIG. 66A and a voltage VM2 is applied to thedeflectors - When the voltage VM1 is applied to the
deflector 840 and the voltage VM2 is applied to thedeflectors deflector 840 will have a linearly approximated trajectory running through points P1, CO1, P2, and P3 of FIG. 66A and through points P4, P5, and P6 of FIG. 66B. - The
deflectors deflector 841 and thedeflector 842. - In FIG. 64, when there is no positional error of the cross-over images CO1 and CO2, changes in the voltages VM1 and VM2 will not bring about a change in the position of the charged-particle beam on the
aperture plate 831 and the wafer 811 (the deflection efficiency is zero). On the other hand, changes in voltages VS1 and VS2 (shown in FIG. 64) result in the position of the charged-particle beam being changed on theaperture plate 831 and thewafer 811. As for thedeflectors 840 through 844, they have following characteristics. - (1) Even when the cross-over images CO1 and CO2 have positional errors, the deflection efficiency on the
aperture plate 831 and thewafer 811 is larger for thecorrection deflectors deflectors 840 through 842. Also, thecorrection deflectors correction deflectors deflectors 840 through 842. - (2) The length of the
correction deflector 843 along the beam axis AX is much shorter than that of thedeflector 840, and the cross-over image CO1 is distanced from thecorrection deflector 843. Thus, thedeflector 840 has much larger deflection efficiency on thestencil mask 812 than does thecorrection deflector 843. The fact that an effect of thecorrection deflector 843 on a beam position on thestencil mask 812 is small is quite favorable. - Positional errors of the cross-over images CO1 and CO2 can be corrected by using the
electromagnetic lens 821B, thecorrection deflector 843, and thecorrection deflector 844. This will be described below. - FIGS. 67A through 67C are illustrative drawings showing an extent of the charged-particle beam passing through the
electromagnetic lenses 821 through 823 with an enlargement of this extent in a direction perpendicular to the beam axis AX. Beam extents 13F through 13H are shown in FIGS. 67A through 67C, respectively, when voltages applied to thedeflectors 840 through 844 are zero. - A current I passing through the aperture of the
aperture plate 831 is measured by aFaraday cup 855 placed under the aperture. - FIGS. 67A and 67C show cases when the position of the cross-over image CO1 is displaced from the center point of the
deflector 840. In these cases, when thedeflector 840 deflects the charged-particle beam while no voltage is applied to thedeflectors 841 through 844, the current I changes according to the deflection amount. Then, a current applied to the electromagnetic lens 821 (electromagnetic lens 821B of FIG. 64 to be exact) is changed to shift the focusing thereof, so that the position of the cross-over image CO1 is changed along the beam axis AX. When the position of the cross-over image CO1 coincides with the center point of thedeflector 840 as shown in FIG. 67B, a change in the deflection amount of thedeflector 840 will not affect the current I. - In order to correct the position of the cross-over image CO1, voltages applied to the
deflectors 841 through 844 are set to zero, and the focusing of theelectromagnetic lens 821 is changed step by step. For each step of the focusing, a change in the current I in response to a change in the deflection amount of thedeflector 840 is measured. Then, the focusing A1 of theelectromagnetic lens 821 when the change in the current I is the smallest is obtained. - In order to correct the position of the cross-over image CO2, voltages applied to the
deflectors electromagnetic lens 821 is changed step by step. For each step of the focusing, a change in the current I in response to changes in the deflection amounts of thedeflectors electromagnetic lens 821 when the change in the current I is the smallest is obtained. - When the focusing of the
electromagnetic lens 821 is A1, the cross-over image CO1 does not have a positional error, but the cross-over image CO2 does. On the other hand, when the focusing of theelectromagnetic lens 821 is A2, the cross-over image CO1 has a positional error, but the cross-over image CO2 does not. That is, desirable focusing of theelectromagnetic lens 821 is not A1 nor A2. Assuming that the desirable focusing is L, the focusing of theelectromagnetic lens 821 is set to L. - Then, voltages applied to the
deflectors deflector 840 is applied to thecorrection deflector 843. Then, the factor K1 is changed step by step. For each step of the factor K1, a change in the current I in response to a change in the deflection amount of thedeflector 840 is measured. The factor K1 for the smallest change in the current I is then determined. Then, voltages applied to thedeflectors deflectors correction deflector 844. Then, the factor K2 is changed step by step. For each step of the factor K2, a change in the current I in response to changes in the deflection amounts of thedeflectors stencil mask 812. - An analysis of a relation between the desirable focusing L of the
electromagnetic lens 821 and the ratio M:N will be provided below. If M/(M+N) is larger than N/(M+N), the focusing L is expected to be nearer to A1 than to A2. On the other hand, if M/(M+N) is smaller than N/(M+N), the focusing L is expected to be nearer to A2 than to A1. - Voltages applied to the
deflectors 841 through 844 are set to zero, and the focusing of theelectromagnetic lens 821 is changed step by step. For each step of the focusing, a change in the current I in response to a change in the deflection amount of thedeflector 840 is measured. Then, the focusing Al of theelectromagnetic lens 821 when the change in the current I is the smallest is obtained. - Voltages applied to the
deflectors electromagnetic lens 821 is changed step by step. For each step of the focusing, a change in the current I in response to changes in the deflection amounts of thedeflectors electromagnetic lens 821 when the change in the current I is the smallest is obtained. - Then, the desirable focusing L is determined as:
- L=(M*A1+N*A2)/(M+N) (2)
- The ratio M:N has an initial value 1:1, for example, and the focusing L is obtained for this initial value by using the equation (22). Then, the ratio M:N is obtained as described above by using the focusing L. Such a process is carried out one or more times to move the ratio M:N closer to an optimal ratio.
- FIG. 68 is a flowchart of the above-described process of determining the focusing A1 to correct the position of the cross-over image CO. The process of determining the focusing A2 is almost the same as the process of determining the focusing A1 except for the selection of the deflectors, and a flowchart thereof will be omitted.
- At a step S201, voltages applied to irrelevant deflectors are set to zero.
- At a step S202, the focusing of the
electromagnetic lens 821 is changed step by step, and a change in the current I in response to a change in the deflection amount of a relevant deflector is measured for each step of the focusing. - At a step S203, the focusing Al of the
electromagnetic lens 821 for the smallest change in the current I is obtained. This ends the procedure. - FIG. 69 is a flowchart of the above-described process of obtaining the desirable focusing L and the optimal value of the ratio M:N.
- At a step S211, the focusing Al and the focusing A2 are obtained.
- At a step S212, the ratio M:N is set to an initial value.
- At a step S213, the focusing L is obtained by using the equation (22).
- At a step S214, the ratio M:N is obtained as described above by using the focusing L.
- At a step S215, a check is made whether the ratio M:N is close enough to an optimal ratio. If it is not, the procedure goes back to the step S213 to repeat the steps S213 through S215. If the ratio M:N is close enough to an optimal ratio, the procedure ends.
- Alternately, the ratio M:N may be obtained as follows.
- When the
Faraday cup 855 is removed, a position P of the charged-particle beam on thewafer 811 varies depending on the voltages VS1 and VS2. First, the ratio M:N is set to 1:1, for example, and the focusing L is obtained by using the equation (22). Then, an equation representing a relation between the voltages VS1 and VS2, the current I, and the position P is obtained experimentally. Then, the ratio M:N when the current I is maximum and the position P is on the beam axis AX is obtained. Such a process is carried out one or more times to make the ratio M:N closer to an optimal ratio. - The determination of the factors K1 and K2 and the focusing L as described above is carried out when the charged-particle-beam exposure device is calibrated.
- In the first embodiment of the eighth principle of the present invention, not only the
correction deflectors electromagnetic lens 821B are corrected in relation with the current I, so that the correction of the device is precise. - A relation between this correction and the settling time when the voltages VM1 and VM2 show a step change will be explained below.
- In selecting a hole pattern of the
stencil mask 812, the voltages VM1 and VM2 are changed by a given step voltage. A precision required for positioning the charged-particle beam on thewafer 811 is within a range of 0.01 μm. As previously described, the charged-particle beam should be blanked out until this level of precision is guaranteed. Since the charged-particle beam is continuously emitted, the blanking of the beam is carried out by using theaperture plate 831 and a deflector placed above theaperture plate 831. Even if the step change is the same between the voltages VM1 and VM2, the larger the changes in the position of the charged-particle beam (i.e., deflection efficiency) on thewafer 811 with respect to changes in the voltages VM1 and VM2, the longer the settling time (blanking time) is. - Without the correction described above, the deflection efficiency is large so that the settling time is long. FIG. 70 is a chart showing a shortening of the settling time because of the correction. Without the correction, the settling time of the voltage VM1, for example, is lengthy as shown by t2 in FIG. 70. When the correction is conducted, the deflection efficiency is decreased, so that the settling time becomes shorter as shown by t1 in FIG. 70. The settling time tl in this case may be 500 ns, for example. In this manner, throughput of the exposure process is enhanced. Since the correction is accurate as described above, the reduction in the settling time is significant.
- FIG. 71 is an illustrative drawing of a configuration of a charged-particle-beam exposure device according to a second embodiment of the eighth principle of the present invention.
- In the device of FUG.71, the
correction deflector 843 is placed between theelectromagnetic lens 821B and thedeflector 840. Except for this change, the device of FIG. 71 is the same as that of FIG. 64. - In the second embodiment of the eighth principle, the characteristics (1) and (2) described in the first embodiment of the eighth principle are upheld. Thus, what has been described for the first embodiment of the eighth principle can also be applied to the configuration of the second embodiment. To avoid repetition, a description of the second embodiment the same as that of the first embodiment will be omitted.
- FIG. 72 is an illustrative drawing of a configuration of a charged-particle-beam exposure device according to a third embodiment of the eighth principle of the present invention.
- In the device of FIG. 72, deflectors similar to the
deflectors deflectors deflectors electromagnetic lens 821B and theelectromagnetic lens 822A in a mirror-image configuration to thedeflectors amplifier 1151 is applied to thedeflectors amplifier 1154 is applied to thecorrection deflector 1144. The cross-over image CO1 is positioned between theelectromagnetic lens 821B and a contour point of thedeflector 1142. Other elements have the same configuration as those of FIG. 64. - FIGS. 73A and 73B are illustrative drawings for explaining trajectories of the charged-particle beam deflected by the deflectors. FUGS.73A and 73B correspond to FIGS. 66A and 66B, respectively.
- In FIG. 73A, the
deflectors deflectors - In FIG. 73B, voltages applied to the
deflectors aperture plate 831 and that the charged-particle beam is deflected by thedeflector 841 and thedeflector 842. In this case, a linearly approximatedtrajectory 813J as shown in FIG. 73B is obtained. - Assume that when a voltage VM1 is applied to the
deflectors deflectors - When the voltage VM1 is applied to the
deflectors deflectors deflector 1142 will have a linearly approximated trajectory running through points P1, P5A, P4A, P2 and P3 of FIG. 73A and through points P4, P5, and P6 of FIG. 73B. - Other than what has been described above, the same thing as the first embodiment can be applied to the third embodiment of the eighth principle of the present invention.
- FIG. 74 is an illustrative drawing of a configuration of a charged-particle-beam exposure device according to a fourth embodiment of the eighth principle of the present invention.
- The configuration of FIG. 74 differs from that of FIG. 64 only in that the
amplifier 850 of FIG. 64 is removed. Since the voltage applied to thedeflector 840 is in proportion to the voltage applied to thedeflectors deflector 840 in FIG. 74 is designed such that this proportion factor is equal to 1. Then, the voltage VM2 output from theamplifier 851 is applied to thedeflector 840. One of thedeflectors - In the fourth embodiment of the eighth principle of the present invention, the voltage VM2 output from the
amplifier 851 is applied to thedeflectors amplifier 851 has a step change, transient characteristics of the electric fields generated by thedeflector deflector 840 and thedeflectors - FIG. 75 is an illustrative drawing of a configuration of a charged-particle-beam exposure device according to a fifth embodiment of the eighth principle of the present invention.
- As described in the first embodiment of the eighth principle, a trajectory of the charged-particle beam can be expressed by a linear approximation with respect to the voltages applied to the
deflectors 840 through 843. This is because the deflection amount is small. Second orders of the applied voltages can be a cause of an aberration, but does not have any effect on the trajectory of the charged-particle beam along the beam axis. However, third orders of the applied voltages affects the trajectory of the charged-particle beam along the beam axis. Thus, when the applied voltages have step changes, a position of the charged-particle beam at theaperture plate 831 fluctuates. In this case, the amount of current passing through theaperture plate 831 is generally proportional to the third power of the applied voltage. Although a fluctuation in a position of the charged-particle beam on thewafer 811 can be ignored, the fluctuation of the current amount cannot. Therefore, there is a need to take into account the third orders of the applied voltages with respect to the settling time. - Assume that a precision required for positioning the charged-particle beam on the
wafer 811 is 0.01 μm, that a maximum amount of deflection (distance from the beam axis AX) of the charged-particle beam on thestencil mask 812 is 5 mm, and that a reduction rate of a hole pattern of thestencil mask 812 when projected on thewafer 811 is {fraction (1/100)}. In this case, a 5-mm step change at thestencil mask 812 corresponds to a 50-μm step change on thewafer 811. Thus, in order to keep a step change on thewafer 811 within a range of 0.01 μm, a difference dV between the voltage VM1 and a stable voltage VO should satisfy the following inequality: - dV/VO≦0.01/50=1/5000 (23)
- FIG. 76A is a chart for explaining a relation between the difference dV and the settling time. In the figure, the settling time is tl, at which dV/V should be equal to or smaller than {fraction (1/5000)}. In practice, tl is about 500 nsec.
- If a temporal change of VM1 is approximated to by
- VM1(t)=VO{1−exp(−t/a)}, (24)
- and dV/VO becomes equal to {fraction (1/5000)} within 500 nsec, a constant a is 60.3 nsec.
- A current I(t) passing through the aperture of the
aperture plate 831 is proportional to {VM1(t)}3. Thus, I(t) is approximated to by - I(t)=IO{1=exp(−t/a)}3, (24)
- Assume that, in order to have an accurate exposure amount, the charged-particle beam should be blanked out until the current amount of the charged-particle beam on the
wafer 811 reaches approximately 99% of the stable current amount. In consideration of the reduction rate of {fraction (1/100)}, a difference dIO between the current I(t) and a stable current IO should satisfy the following inequality: - DIO/IO≦({fraction (1/100)})({fraction (1/100)})=1/10000 (25)
- FIG. 76B is a chart for explaining a relation between the difference dIO and the settling time. In the figure, the settling time is t3, at which dIO/IO should be equal to or smaller than {fraction (1/10000)}. In practice, t3 is about 620 nsec. In this case, the settling time is determined not by the equation (23) but by the equation (25).
- The settling time t3 of FIG. 76B is compared with a settling time t2 of FIG. 76A, for which no correction described in the first embodiment of the eighth principle is carried out. Because of no correction, the fluctuation in the position of the charged-particle beam at the
aperture plate 831 is large so that the settling time t2 is longer than the settling time t3. - The deflection efficiencies on the
aperture plate 831 and thewafer 811 are greater for thecorrection deflector 843 than for thedeflector 840. Since thecorrection deflector 843 is used for correction of small errors, the voltage VS1 of theamplifier 853 is much smaller than the voltage VM1 of theamplifier 850. Thus, the voltage VS1 output from theamplifier 853 has a settling time much shorter than that of the voltage VM1. FIG. 76C is a chart showing a change of the voltage VS1 and a settling time t6 thereof. Because t6 is much shorter than t1, the correction of the fluctuation of the charged-particle-beam position on theaperture plate 831 can be carried out by using thecorrection deflector 843. - In the device of FIG. 75, the
correction deflector 843 is used for correcting the fluctuation in the position of the charged-particle beam at theaperture plate 831 when the voltages applied to thedeflectors 840 through 844 have step changes to cause the fluctuation through the third order of the applied voltages. The configuration of FIG. 75 includeselements 870 through 884 in addition to the configuration of FIG. 64. - Data D1 for selecting a hole pattern of the
stencil mask 812 is stored in adata generating unit 870. This pattern-selection data Dl sequentially read from thedata generating unit 870 is converted to analog data by a D/A converter 871, and, then, amplified by theamplifier 850 to become the voltage VM1 applied to thedeflector 840. The voltage VS1 generated through a D/A conversion by a D/A converter 872 and the amplification by theamplifier 853 is supplied to thecorrection deflector 843. The D/A converter 872 receives an output of anadder 873 adding correction values D2 and D3 together. The correction value D2 is equal to K1*D1, where K1 is the proportion factor previously described. - When creating a correction value for the
correction deflector 843, the correction value D3 is first set to zero. The pattern-selection data D1 is changed by a step, and a value proportional to the current I passing through the aperture of theaperture plate 831 is detected by a scattered-particle detector 874. A detected signal is amplified by anamplifier 875 and converted to a digital value SE by a D/A converter 876. The digital value SE is provided for acontrol circuit 877. Since thedeflectors 841 through 843 receive voltages proportional to that ofdeflector 840, the voltages input to thedeflectors 841 through 843 have step changes as does the voltage applied to thedeflector 840. - At a time when the step change of the pattern-selection data D1 starts, a load signal supplied from the
data generating unit 870 to a load-control-input node L of acounter 878 is activated. The pattern-selection data D1 is supplied to a data-input node D of thecounter 878. Immediately after these operations, thedata generating unit 870 turns a start signal ST to a high level to open an ANDgate 879. Then, a clock CLK from aclock generator 880 is supplied to a clock-input node of thecounter 878 via the ANDgate 879. A count supplied from a data-output node Q of thecounter 878 serves as an address of amemory 881, and thecontrol circuit 877 writes the scattered-particle amount (digital value) SE in this address of thememory 881. The writing of the data is carried out from data D1 corresponding to each hole pattern of thestencil mask 812. - A
memory 882 stores the correction value D3 which maximizes the scattered-particle amount SE for each data D1 corresponding to a respective hole pattern of thestencil mask 812. The correction value D3 is obtained as follows. - The correction value D3 is changed for given pattern-selection data D1 and given scattered-particle amount SE without correction. Then, the scattered-particle amount SE is measured for each correction value D3 to obtain a function of D3 for representing the scattered-particle amount SE. Then, the correction value D3 for the maximum scattered-particle amount SE is determined. The same procedure is conducted for a plurality of scattered-particle amounts SE without correction. Then, the correction value D3 for every scattered-particle amount SE without correction is obtained. The same procedure is carried out for each data D1 corresponding to a respective hole pattern of the
stencil mask 812. - The correction values D3 (D1, SE) (function of the data D1 and the scattered-particle amount SE) thus obtained are supplied to the
control circuit 877. Thecontrol circuit 877 provides thememory 882 with an address (D1, SE) via aselector 883 to write a correction value D3 at an indicated address. - At a time of exposure, an output of the
memory 881 instead of an output of D/A converter 876 is used. This is because the output of the D/A converter 876 obtained from the output of scattered-particle detector 874 varies depending on a surface structure of thewafer 811. Namely, it is preferable to use the scattered-particle amounts SE detected for a flat surface of thewafer 811 and stored in thememory 881. - At a time of exposure, the
memory 881 and thememory 882 are set to a read state, and theselector 883 is set to select an address from thememory 881. When the data D1 is changed by a step to select a hole pattern of thestencil mask 812, the load-control-input node L of thecounter 878 is activated so that thecounter 878 reads the pattern-selection data D1. Immediately after these operations, the start signal ST is turned to the high level, so that the clock CLK from theclock generator 880 is counted by thecounter 878. A count obtained by thecounter 878 is used for indicating an address of thememory 881 to read the scattered-particle amount SE from thememory 881. This scattered-particle amount SE is provided for thememory 882 as an address, so that the correction value D3 is read from thememory 882 to be supplied to theadder 873. - FIG. 76D is a chart showing an example of the correction value D3 for given pattern-selection data D1. Use of the correction value D3 as shown in FIG. 76D results in the current I passing through the aperture being changed as shown by a dotted line in FIG. 76B. Thus, the settling time is shortened from t3 to t5, which is shorter than t1 of FIG. 76A. Then, the settling time required for selecting a hole pattern of the
stencil mask 812 becomes t1, thereby enhancing throughput of the exposure. - It is possible for the
counter 878 to directly provide an address of thememory 882. Since thememory 881 storing the scattered-particle amounts SE is used in the fifth embodiment of the eighth principle, a relation between the scattered-particle amounts SE and the correction values D3 can be inspected at any time. Thus, it is easier to modify the correction values D3 to more appropriate values. - Further, the present invention is not limited to these embodiments, but variations and modifications may be made without departing from the scope of the present invention.
Claims (118)
Priority Applications (1)
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US09/826,913 US6420700B2 (en) | 1995-06-08 | 2001-04-06 | Charged-particle-beam exposure device and charged-particle-beam exposure method |
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JP14203795A JP3453004B2 (en) | 1995-06-08 | 1995-06-08 | Charged particle beam exposure method and apparatus |
JP7-142037 | 1995-06-08 | ||
JP18423395A JP3388066B2 (en) | 1995-07-20 | 1995-07-20 | Electron beam exposure apparatus and method of adjusting deflection efficiency in the apparatus |
JP7-184233 | 1995-07-20 | ||
JP7-184231 | 1995-07-20 | ||
JP18423195A JP3866782B2 (en) | 1995-07-20 | 1995-07-20 | Electron beam exposure apparatus and exposure method |
JP25639695A JP3461066B2 (en) | 1995-10-03 | 1995-10-03 | Charged particle beam exposure method and apparatus |
JP7-256396 | 1995-10-03 | ||
US08/634,410 US5757015A (en) | 1995-06-08 | 1996-04-18 | Charged-particle-beam exposure device and charged-particle-beam exposure method |
US08/917,464 US5969365A (en) | 1995-06-08 | 1997-08-26 | Charged-particle-beam exposure device and charged-particle-beam exposure method |
US09/353,586 US6242751B1 (en) | 1995-06-08 | 1999-07-15 | Charged-particle-beam exposure device and charged-particle-beam exposure method |
US09/826,913 US6420700B2 (en) | 1995-06-08 | 2001-04-06 | Charged-particle-beam exposure device and charged-particle-beam exposure method |
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US09/353,586 Division US6242751B1 (en) | 1995-06-08 | 1999-07-15 | Charged-particle-beam exposure device and charged-particle-beam exposure method |
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US08/917,464 Expired - Lifetime US5969365A (en) | 1995-06-08 | 1997-08-26 | Charged-particle-beam exposure device and charged-particle-beam exposure method |
US09/353,586 Expired - Lifetime US6242751B1 (en) | 1995-06-08 | 1999-07-15 | Charged-particle-beam exposure device and charged-particle-beam exposure method |
US09/826,913 Expired - Lifetime US6420700B2 (en) | 1995-06-08 | 2001-04-06 | Charged-particle-beam exposure device and charged-particle-beam exposure method |
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US08/917,464 Expired - Lifetime US5969365A (en) | 1995-06-08 | 1997-08-26 | Charged-particle-beam exposure device and charged-particle-beam exposure method |
US09/353,586 Expired - Lifetime US6242751B1 (en) | 1995-06-08 | 1999-07-15 | Charged-particle-beam exposure device and charged-particle-beam exposure method |
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US20030022496A1 (en) * | 2001-07-04 | 2003-01-30 | Isao Ashida | Stencil mask and method of producing the same, semiconductor device produced using the stencil mask and method of producing the semiconductor device |
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Also Published As
Publication number | Publication date |
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US5969365A (en) | 1999-10-19 |
US5757015A (en) | 1998-05-26 |
US6242751B1 (en) | 2001-06-05 |
US6420700B2 (en) | 2002-07-16 |
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