EP1588122A1 - Reference de mesure optique ponctuelle - Google Patents

Reference de mesure optique ponctuelle

Info

Publication number
EP1588122A1
EP1588122A1 EP03816399A EP03816399A EP1588122A1 EP 1588122 A1 EP1588122 A1 EP 1588122A1 EP 03816399 A EP03816399 A EP 03816399A EP 03816399 A EP03816399 A EP 03816399A EP 1588122 A1 EP1588122 A1 EP 1588122A1
Authority
EP
European Patent Office
Prior art keywords
signal
board
digital phase
phase
signals
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
EP03816399A
Other languages
German (de)
English (en)
Other versions
EP1588122A4 (fr
Inventor
John P. Flowers
Lee C. Kalem
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Agilent Technologies Inc
Original Assignee
Agilent Technologies Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Agilent Technologies Inc filed Critical Agilent Technologies Inc
Publication of EP1588122A1 publication Critical patent/EP1588122A1/fr
Publication of EP1588122A4 publication Critical patent/EP1588122A4/fr
Withdrawn legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B9/00—Measuring instruments characterised by the use of optical techniques
    • G01B9/02—Interferometers
    • G01B9/02055—Reduction or prevention of errors; Testing; Calibration
    • G01B9/02062—Active error reduction, i.e. varying with time
    • G01B9/02067—Active error reduction, i.e. varying with time by electronic control systems, i.e. using feedback acting on optics or light
    • G01B9/02069—Synchronization of light source or manipulator and detector
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B9/00—Measuring instruments characterised by the use of optical techniques
    • G01B9/02—Interferometers
    • G01B9/02015—Interferometers characterised by the beam path configuration
    • G01B9/02027—Two or more interferometric channels or interferometers
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B9/00—Measuring instruments characterised by the use of optical techniques
    • G01B9/02—Interferometers
    • G01B9/02083—Interferometers characterised by particular signal processing and presentation
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B2290/00—Aspects of interferometers not specifically covered by any group under G01B9/02
    • G01B2290/45—Multiple detectors for detecting interferometer signals

Definitions

  • This invention relates to laser interferometer positioning systems.
  • Typical applications for a laser interferometer positioning system include integrated circuit (IC) manufacturing equipment (wafer steppers, step and scan tools, and E-beam lithography systems), precision machine tools, and custom stages.
  • IC integrated circuit
  • the positioning system measures the position and controls the motion of the platform with great precision and accuracy.
  • a laser interferometer positioning system includes a first board having a first phase meter and a second phase meter.
  • the first phase meter outputs a digital reference phase signal based on an analog electrical reference signal and a clock signal.
  • the digital reference phase signal is the only digital reference signal for a laser head in the system.
  • the second phase meter outputs a digital phase measurement signal based on an electrical measurement signal and the clock signal.
  • the first board is inserted into a backplane.
  • the backplane includes a bus that carries the digital phase reference signal and the digital phase measurement signal to a second board.
  • the second board subtracts the digital phase reference signal from digital phase measurement signals it receives from multiple first boards.
  • Fig. 1 illustrates a laser interferometer positioning system.
  • FIG. 2 and 3 illustrate a computer system in the system of Fig. 1.
  • Fig.4 is a block diagram of a computer system in a laser interferometer positioning system in one embodiment of the invention.
  • Fig. 4A illustrates a laser interferometer positioning system in one embodiment of the invention.
  • Fig. 5 is a block diagram of a phase measurement board in the system of Fig. 4 in one embodiment of the invention.
  • Fig. 6 is a block diagram of a combiner board in the system of Fig. 4 in one embodiment of the invention.
  • Fig. 7 is a block diagram of a phase measurement and combiner board in a computer system of a laser interferometer positing system in one embodiment of the invention.
  • Fig. 1 illustrates a typical laser interferometer positioning system 10 used with IC manufacturing.
  • a power supply 12 provides power to a laser head 14 that generates a light beam 16.
  • An optical element 18 splits light beam 16 into beams 20 and 22.
  • a reference optical receiver 24 converts beam 20 to an analog electrical reference signal and transmits it to a computer system 26 (e.g., a Versa Modular European bus mainframe).
  • An optical element 28 splits beam 22 into beams 30 and 32.
  • beam 30 is reflected off a mobile stage 34 along a first axis (e.g., the X-axis) and then received by an optical receiver 36.
  • beam 32 is reflected offstage 34 along a second axis (e.g., the Y-axis) and then received by an optical receiver 38.
  • Optical receivers 36 and 38 convert beams 30 and 32 to analog electrical measurement signals, respectively, and transmit them to computer system 26. Of course, additional axes of measurement can be taken.
  • Computer system 26 may be coupled to air sensor 40 and temperature sensor 42 to compensate the dependency of the laser wavelength on its environment. Computer system 26 uses the phase differences between the reference signal from receiver 24 and the measurement signals from receivers 36 and 38 to determine the position of stage 34 along the measurement axes. Computer system 26 then uses an actuator 44 to move stage 34.
  • Fig. 2 illustrates a front panel of a typical computer system 26A used in system 10. Computer system 26A includes multiple measurement axis boards 60 to 70. Each board receives the analog electrical reference signal and one or more measurement signals to determine the position of stage 34 along a measurement axis. The analog electrical reference signal is received directly from receiver 24 by one of the measurement axis boards. A front panel ribbon cable 71 then routes the analog electrical reference signal from that board to the other boards in parallel.
  • Fig. 3 illustrates a front panel of another typical computer system 26B used in system 10.
  • Computer system 26B includes multiple measurement axis boards 80 to 90.
  • One of the boards e.g., board 85
  • receives the analog optical reference signal e.g., beam 20
  • Board 85 then routes the analog electrical reference signal to adjacent boards 84 and 86 using cables 102 and 104.
  • each board propagates the analog electrical reference signal to its adjacent board in a daisy chain fashion.
  • Both computer systems 26A and 26B suffer several disadvantages.
  • the circuitry required to convert the reference signal from its analog form to its digital form is duplicated for every measurement axis board.
  • the reference signal may not be replicated accurately as it is passed from board to board due to changes in loading from the addition of more boards, buffering between the boards, and electrostatic discharge (ESD) on the cables.
  • ESD electrostatic discharge
  • the cabling takes up precious space on the front panels of the boards.
  • the reference signal may age differently on the way to the boards due to varying signal paths.
  • the cabling makes it difficult to change the routing of the reference signal.
  • the system requires predetermined wiring if multiple reference signals are required. Thus, what is needed is a laser interferometer positioning system that addresses these disadvantages.
  • Fig. 4 is a block diagram of a computer system 120 in a laser interferometer positioning system 121 (Fig.4A) in one embodiment of the invention.
  • System 120 includes phase measurement boards 124-1, 124-2 . . . and 124-i plugged into a backplane 125 in an electronic rack.
  • each phase measurement board (“PMB") accepts multiple fiber optic input signals 126-1, 126-2 . . . and 126-j.
  • Each fiber optic input signal can be an analog optical reference signal from laser head 14 or an analog optical measurement signal reflected from stage 34 along a measurement axis.
  • input signal 126-j is a reference optical signal from laser head 14 (e.g., beam 20 in Fig.
  • input signal 126-1 is a measurement optical signal reflected from stage 34 (e.g., beam 30 in Fig. 4A) along the first measurement axis
  • input signal 126-2 is a measurement optical signal reflected from stage 34 (e.g., beam 32 in Fig. 4A) along a second measurement axis.
  • receivers 24, 36, and 38 are replaced by optical lenses 24A, 36A, and 38A (Fig. 4A) coupled to optical fibers that transport beams 20, 30, and 32 to system 120.
  • the PMB measures the phase of each input signal, whether reference or measurement, relative to an internal clock signal that is synchronized between all the PMBs in system 120.
  • PMBs 124-1, 124-2 . . . and 124-i then report the measured phases in digital form over buses 128-1, 128-2 . . . and 128-i, respectively, to a combiner board 130.
  • Buses 128-1 to 128-i also carry the internal clock signal from combiner board 130 to PMBs 124-1 to 124-i, respectively.
  • Combiner board 130 subtracts a phase reference signal from each of the phase measurement signals of PMBs 124-1 to 124-i. From the phase differences, combiner board 130 determines the position of stage 34. Combiner board 130 then reports the position of stage 34 over a bus 132 (e.g., a P2 bus) to a controller 134. Controller 134 can issue commands over a bus 136 (e.g., a Versa Modular European bus) to combiner board 130. Buses 134 and 136 can be implemented on a standard VME (Versa Modular European) backplane 138. Combiner board 130 then passes these commands over a bus 140 on backplane 125 to PMBs 124-1 to 124-i.
  • VME Very Modular European
  • phase reference signal is calculated once by a PMB and then centrally processed by combiner board 130 in its digital form.
  • System 120 eliminates the need to duplicate the reference phase circuitry on each board and the associated front panel cabling. With the front panel cables eliminated, the associated ESD problem of the cabling is also eliminated. Furthermore, the phase reference signal is not affected by the load of additional boards. The position calculations are also now more accurate because the same reference phase signal is compared with phase measurement signals from multiple axes.
  • Fig. 5 illustrates one embodiment of PMB 124-i.
  • PMB 124-i includes measurement channels 160-1, 160-2 . . . and 160-j receiving input signals 126-1, 126-2 . . . and 126-j, respectively.
  • Measurement channels 160-1 to 160-j generate phase signals 161-1, 161-2 . . . and 161-j.
  • signal 161-1 and 161-2 are phase measurement signals
  • signal 160-j is a phase reference signal.
  • each measurement channel includes an optical receiver 162 and a phase meter 164.
  • Optical receiver 162 converts analog optical input signal 126-j to an analog electrical input signal.
  • Phase meter 164 measures the phase of signal 126-j relative to a clock signal Timebase.
  • Clock signal Timebase is provided to PMB 124-i (and the other PMBs) by backplane 125 (Fig. 4).
  • phase meter 164 In response to a clock signal Framesync, phase meter 164 periodically transmits measured phase signal 161-j over backplane 125 to combiner board 130.
  • Fig. 6 illustrates one embodiment of combiner board 130.
  • Combiner board 130 includes a multiplexer 180 that routes the measured phase signals from the measurement channels in the PMBs to any of subtraction blocks 182-1, 182-2 . . . and 182-k.
  • multiplexer 180 routes all the measured phase signals on bus 128-i from PMB 124-i (Figs. 4 and 5) to subtraction block 182-k.
  • Multiplexer 180 can route any one of the measured phase signals as a phase reference signal to be subtracted from the other measured phase signals.
  • multiplexer 180 routes the measured phase signal from optical lens 24A (Fig. 4A) as the phase reference signal while the measured phase signals from optical lenses 36A and 38A (Fig. 4A) as the phase measurement signals.
  • the measured phase signal from optical lens 36A or 38A may be used as the phase reference signal.
  • Multiplexer 180 may be programmed on the fly to route the measured phase signals.
  • each subtraction block includes subtraction circuits 184-1, 184-2 . . . and 184-m.
  • Each subtraction circuit subtracts a reference phase signal from a measurement phase signal.
  • subtraction circuit 184-2 subtracts reference phase signal 161-j from measurement phase signal 161-2.
  • Each subtraction circuit then provides the phase difference to a position processor 186. Using the phase differences, position processor 186 determines the position of stage 34 along the measurement axes.
  • Combiner board 130 also includes a clock 188 that generates clock signals Timebase and Framesync.
  • the lines on backplane 125 (Fig. 4) that carry clock signals Timebase and Framesync to each PMB are of the same length so that clock signals Timebase and Framesync arrive at each PMB at the same time. This ensures that the phases are measured relative to the same clock signal.
  • combiner board 130 is implemented with a field programmable gate array (FPGA) that is configured with the above-described blocks and circuits.
  • the FPGA can be programmed to route any of the measured phase signals as a phase reference signal or a phase measurement signal to any of the subtraction blocks.
  • the FPGA can also be programmed with any method to determine the position of stage 34 from the phase differences.
  • Fig. 7 illustrates one embodiment of a phase measurement and combiner board 210 that includes the features of the PMB and the combiner board.
  • Board 210 includes measurement channels 160-1 to 160-j that receives analog optical input signals 126-1 to 126- j, respectively.
  • Measurement channels 160-1 to 160-j measure the phases of the inputs signals relative to clock signal Timebase from clock 188.
  • Measurement channels 160-1 to 160-j output the phases to multiplexer 180 in response to clock signal Framesync from clock 188.
  • Multiplexer 180 routes one of the phase signals as a reference phase signal to subtraction circuits 184-1 to 184-m, and the remainder of the phase signals as input signals to subtraction circuits 184-1 to 184-m.
  • the reference phase signal and measurement phase signals can be hardwired to predetermined subtraction circuits.
  • Subtraction circuits 184-1 to 184-m calculate the phase differences and output them to position processor 186. Using the phase differences, position processor 186 determines the position of stage 34 along the measurement axes.
  • a single optical reference input signal is necessary for embodiments that use one laser head. All the other input signals can be optical measurement signals. In embodiments that use multiple laser heads, one optical reference input signal is required for each laser head.
  • the optical reference input signals can be received by any of the PMBs as long as multiplexer 180 routes them to the appropriate subtraction circuits.
  • a measurement channel may not include the optical receiver.
  • a phase meters may receive an analog electrical reference or measurement signal from optical receiver 24, 32, or 36 (Fig. 1) that are located off the phase measurement board or the phase measurement and combiner board. Numerous embodiments are encompassed by the following claims.

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Optics & Photonics (AREA)
  • Signal Processing (AREA)
  • Length Measuring Devices By Optical Means (AREA)
  • Instruments For Measurement Of Length By Optical Means (AREA)

Abstract

L'invention concerne un système de positionnement par interféromètre à laser, qui comprend une première carte présentant un premier mesureur de phase et un second mesureur de phase. Le premier mesureur de phase produit un signal de phase numérique de référence sur la base d'un signal de phase électrique analogique de référence et d'un signal d'horloge. Le signal de phase numérique de référence est le seul signal numérique de référence destiné à une tête laser dans le système. Le second mesureur de phase produit un signal de mesure de phase numérique sur la base d'un signal de mesure électrique et du signal d'horloge. La première carte est insérée dans un panneau arrière comprenant un bus qui achemine le signal de phase numérique de référence et le signal de mesure de phase numérique vers une seconde carte. La seconde carte soustrait le signal de phase numérique de référence des signaux de mesure de phase numérique qu'elle reçoit d'une première série de plusieurs cartes.
EP03816399A 2003-01-28 2003-08-21 Reference de mesure optique ponctuelle Withdrawn EP1588122A4 (fr)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US35326703A 2003-01-28 2003-01-28
US353267 2003-01-28
PCT/US2003/027451 WO2004083775A1 (fr) 2003-01-28 2003-08-21 Reference de mesure optique ponctuelle

Publications (2)

Publication Number Publication Date
EP1588122A1 true EP1588122A1 (fr) 2005-10-26
EP1588122A4 EP1588122A4 (fr) 2006-04-12

Family

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Family Applications (1)

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EP03816399A Withdrawn EP1588122A4 (fr) 2003-01-28 2003-08-21 Reference de mesure optique ponctuelle

Country Status (3)

Country Link
EP (1) EP1588122A4 (fr)
JP (1) JP2006513436A (fr)
WO (1) WO2004083775A1 (fr)

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5019786A (en) * 1989-11-17 1991-05-28 The United States Of America As Represented By The United States Department Of Energy Phase measurement system using a dithered clock
US6049297A (en) * 1998-11-19 2000-04-11 Visidyne, Corp. Digital phase measuring system and method
US6480126B1 (en) * 2001-10-26 2002-11-12 Agilent Technologies, Inc. Phase digitizer

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4799001A (en) * 1987-07-23 1989-01-17 Nicolet Corporation Start of scan circuit for FTIR spectrometer
US5767972A (en) * 1996-06-04 1998-06-16 Zygo Corporation Method and apparatus for providing data age compensation in an interferometer

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5019786A (en) * 1989-11-17 1991-05-28 The United States Of America As Represented By The United States Department Of Energy Phase measurement system using a dithered clock
US6049297A (en) * 1998-11-19 2000-04-11 Visidyne, Corp. Digital phase measuring system and method
US6480126B1 (en) * 2001-10-26 2002-11-12 Agilent Technologies, Inc. Phase digitizer

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See also references of WO2004083775A1 *

Also Published As

Publication number Publication date
WO2004083775A1 (fr) 2004-09-30
JP2006513436A (ja) 2006-04-20
EP1588122A4 (fr) 2006-04-12

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