JPH0115082B2 - - Google Patents
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- Publication number
- JPH0115082B2 JPH0115082B2 JP7897781A JP7897781A JPH0115082B2 JP H0115082 B2 JPH0115082 B2 JP H0115082B2 JP 7897781 A JP7897781 A JP 7897781A JP 7897781 A JP7897781 A JP 7897781A JP H0115082 B2 JPH0115082 B2 JP H0115082B2
- Authority
- JP
- Japan
- Prior art keywords
- cos
- light
- diffraction gratings
- aligned
- interference
- Prior art date
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Links
- 230000001427 coherent effect Effects 0.000 claims description 15
- 239000004065 semiconductor Substances 0.000 description 10
- 235000012431 wafers Nutrition 0.000 description 10
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 4
- 238000010586 diagram Methods 0.000 description 4
- 238000001514 detection method Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 229910052786 argon Inorganic materials 0.000 description 2
- 238000006073 displacement reaction Methods 0.000 description 2
- 239000011295 pitch Substances 0.000 description 2
- 101100269850 Caenorhabditis elegans mask-1 gene Proteins 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 230000003321 amplification Effects 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000003199 nucleic acid amplification method Methods 0.000 description 1
- 230000010355 oscillation Effects 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 238000004611 spectroscopical analysis Methods 0.000 description 1
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D3/00—Control of position or direction
- G05D3/12—Control of position or direction using feedback
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- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Control Of Position Or Direction (AREA)
Description
【発明の詳細な説明】
本発明は、平行配置された2枚の回折格子を用
いて位置合わせを行なう装置に係わり、特に各回
折格子間のギヤツプ変動の影響を受け難くし、か
つ構成の簡略化をはかつた位置合わせ装置に関す
る。DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a device that performs alignment using two diffraction gratings arranged in parallel, and in particular, an apparatus that is less susceptible to the influence of gap fluctuations between each diffraction grating and has a simplified configuration. This invention relates to an alignment device that has been developed.
従来、この種の位置合わせ装置には、平行配置
した2枚の回折格子の少なくとも一方を可干渉光
の照射方向に振動させて格子間距離を変化させる
か、もしくは可干渉光の波長を変調することによ
り回折光の位相を変調させ、これにより床面振動
等による各回折格子間距離(ギヤツプ)の変動の
影響を除去するようにしたもの(特願昭54−
10080号)がある。そして、この装置は、現在例
えば半導体ウエハとICマスクとの間の位置合わ
せに適用されている。 Conventionally, this type of alignment device involves vibrating at least one of two diffraction gratings arranged in parallel in the irradiation direction of the coherent light to change the distance between the gratings, or modulating the wavelength of the coherent light. This modulates the phase of the diffracted light, thereby eliminating the influence of fluctuations in the gap between each diffraction grating due to floor vibration, etc.
10080). This device is currently being applied, for example, to alignment between a semiconductor wafer and an IC mask.
ところが、近年半導体ウエハの大形化に伴ない
ICマスクの直径が大きくなつてきている。この
ため、前記従来の位置合わせ装置を用いて、例え
ばICマスクを微小振動させることにより回折光
の位相を変調させると、ICマスク全面を一様に
振動させることが困難なため、検出個所により位
置ずれ検出量に偏りが生じて精度の低下を招くお
それがあつた。 However, as semiconductor wafers have become larger in recent years,
The diameter of IC masks is becoming larger. For this reason, if the phase of the diffracted light is modulated by, for example, micro-vibrating the IC mask using the conventional alignment device, it is difficult to vibrate the entire surface of the IC mask uniformly, so the detection location may vary depending on the position. There was a risk that the detected amount of deviation would be biased, leading to a decrease in accuracy.
一方、可干渉光の波長を変調させて回折光の位
相を変調する手法を適用した場合には、上記IC
マスクの大形化に何ら影響を受けないが、可干渉
光を得るためのレーザ発振装置が複雑化および大
形化するため、装置が極めて高価となつて実用に
適さなかつた。 On the other hand, when applying a method that modulates the wavelength of coherent light to modulate the phase of diffracted light, the above IC
Although it is not affected by the increase in the size of the mask, the laser oscillation device for obtaining coherent light becomes complicated and large, making the device extremely expensive and not suitable for practical use.
本発明は、上記事情に着目してなされたもの
で、その目的とするところは、被位置合わせ物の
大きさに関係なく常に安定で精度の高い位置合わ
せを行ない得、しかも構成が簡単で安価な位置合
わせ装置を提供することにある。 The present invention has been made in view of the above circumstances, and its purpose is to always perform stable and highly accurate alignment regardless of the size of the object to be aligned, and to have a simple and inexpensive configuration. The object of the present invention is to provide a positioning device that is suitable for use.
本発明では、平行配置した2つの回折格子に対
しそれぞれ波長の異なる複数の可干渉光を垂直照
射し、各回折格子による回折光の+n次方向の干
渉強度および−n次方向の干渉強度の差を上記各
可干渉光毎に各々検出し、これらの各干渉強度の
2乗平均を求めてこの値を各回折格子相互のずれ
量、つまり被位置合わせ物相互のずれ量とするこ
とにより、前記目的を達成する。 In the present invention, two diffraction gratings arranged in parallel are vertically irradiated with a plurality of coherent lights having different wavelengths, and the difference between the interference intensity in the +n-order direction and the -n-order direction of the diffracted light by each diffraction grating is is detected for each of the above-mentioned coherent lights, the root mean square of each of these interference intensities is determined, and this value is used as the mutual displacement amount of each diffraction grating, that is, the mutual displacement amount of the objects to be aligned. Achieve your purpose.
先ず、本発明の原理を説明する。第1図に示す
如く、間隔dで相互に平行配置された回折格子
1,2に可干渉光3を垂直照射した場合、その回
折光は次の3種類となる。すなわち、
(i) 回折格子1で反射された回折光3a,3a
(ii) 回折格子1を透過したのち回折格子2で正反
射され、再び回折格子1で回折された回折光3
b,3b
(iii) 回折格子1を透過したのち回折格子2で反射
回折された回折光3c,3c
である。そしてこれらの各回折光3a,3b,3
cの振幅をそれぞれa,b,cとすると、これら
の各回折光3a,3b,3cによる+n次方向の
干渉光の干渉強度I+nは、
I+n=a2+b2+c2+2ab cos4πd/λ
+2ac cos(4πd/λ+2πn・ΔX/P)
+2bc cos(2πn・ΔX/P) ……(1)
となり、一方−n次方向の干渉光の干渉強度I-n
は、
I-n=a2+b2+c2+2ab cos4πd/λ
+2ac cos(4πd/λ−2πn・ΔX/P)
+2bc cos(2πn・ΔX/P) ……(2)
となることが知られている。ただし、Pは回折格
子1,2の格子ピツチ、ΔXは回折格子1,2相
互間のずれ量である。 First, the principle of the present invention will be explained. As shown in FIG. 1, when coherent light 3 is perpendicularly irradiated onto diffraction gratings 1 and 2 which are arranged parallel to each other with an interval d, the following three types of diffracted light are generated. That is, (i) Diffracted light 3a, 3a reflected by the diffraction grating 1 (ii) Diffracted light 3 transmitted through the diffraction grating 1, specularly reflected by the diffraction grating 2, and diffracted by the diffraction grating 1 again
b, 3b (iii) These are the diffracted lights 3c, 3c which are transmitted through the diffraction grating 1 and then reflected and diffracted by the diffraction grating 2. And each of these diffracted lights 3a, 3b, 3
Letting the amplitudes of c be a, b, and c, respectively, the interference intensity I + n of interference light in the +n-order direction by these diffracted lights 3a, 3b, and 3c is I +n = a 2 + b 2 + c 2 + 2ab cos4πd /λ +2ac cos (4πd/λ+2πn・ΔX/P) +2bc cos (2πn・ΔX/P) ...(1) On the other hand, the interference intensity of the interference light in the -n order direction is I -n
It is known that I -n = a 2 + b 2 + c 2 + 2ab cos4πd/λ + 2ac cos (4πd/λ-2πn・ΔX/P) +2bc cos (2πn・ΔX/P) ...(2) There is. However, P is the grating pitch of the diffraction gratings 1 and 2, and ΔX is the amount of deviation between the diffraction gratings 1 and 2.
また、これらの各干渉強度I+nI-nの差は、
I-n−I+n=2ac{cos(4πd/λ−2πn・ΔX/P)
−cos(4πd/λ+2πn・ΔX/P)}
=4ac sin(2πn・ΔX/P)sin(4πd/
λ)
……(3)
となる。 Also, the difference between these interference strengths I +n I -n is I -n −I +n = 2ac {cos (4πd/λ−2πn・ΔX/P) −cos (4πd/λ+2πn・ΔX/P) } =4ac sin(2πn・ΔX/P) sin(4πd/
λ) ...(3).
したがつて、例えば波長λ1,λ2なる2つの可干
渉光を照射した場合にも、各可干渉光毎の干渉強
度差I〓1,I〓2は、
I〓1=I〓1 -n−I〓1 +n
=4ac sin(2πn・ΔX/P)sin(4πd/λ1)……
(4)
I〓2=I〓2 -n−I〓2 +n
=4ac sin(2πn・ΔX/P)sin(4πd/λ2)……
(5)
と表わされる。 Therefore, for example, even when two coherent lights with wavelengths λ 1 and λ 2 are irradiated, the interference intensity difference I〓 1 , I〓 2 for each coherent beam is as follows: I〓 1 = I〓 1 - n −I〓 1 +n = 4ac sin (2πn・ΔX/P) sin (4πd/λ 1 )...
(4) I〓 2 =I〓 2 -n −I〓 2 +n =4ac sin(2πn・ΔX/P) sin(4πd/λ 2 )……
(5)
そして、擬似的に可干渉光を変調させた場合と
同等の効果を得るため、上記各干渉強度I〓1,I〓2
を合成して平均する。すなわち、上記I〓1とI〓2と
の2乗平均を求めると、
となる。またこの式は、
sin2θ=1−cos2θ/2
の関係を用いると、
と変形され、さらに
cosθ+cos=2cosθ+/2・cosθ−/2
の関係より
となる。 In order to obtain the same effect as when modulating the coherent light in a pseudo manner, each of the above interference intensities I〓 1 , I〓 2
Combine and average. That is, if we calculate the square mean of the above I〓 1 and I〓 2 , we get becomes. This formula also becomes, using the relationship sin 2 θ=1−cos2θ/2, And further, from the relationship cosθ+cos=2cosθ+/2・cosθ−/2 becomes.
ここで、cos{4πd(1/λ1−1/λ2)}≪1
ならば
cos{4πd(1/λ1+1/λ2)}cos
{4πd(1/λ1−1/λ2)}≪1
となり、上記第(7)式の
は略1となる。一方
cos{4πd(1/λ1−1/λ2)}≪1
なる関係は、
4πd(1/λ1−1/λ2)≒(m+1/2)π(mは
整数)
のとき、すなわち、
d≒1/4(λ1λ2/λ2−λ1)(m+1/2)
のときに成立する。 Here, if cos {4πd (1/λ 1 -1/λ 2 )}≪1, then cos {4πd (1/λ 1 +1/λ 2 )} cos {4πd (1/λ 1 -1/λ 2 ) }≪1, and the above equation (7) is approximately 1. On the other hand, the relationship cos{4πd(1/λ 1 -1/λ 2 )}≪1 is obtained when 4πd(1/λ 1 -1/λ 2 )≒(m+1/2)π (m is an integer), that is, , d≒1/4(λ 1 λ 2 /λ 2 −λ 1 )(m+1/2).
したがつて、前記第(7)式は
d≒1/4(λ1λ2/λ2−λ1)(m+1/2)……
(8)
のとき
I≒4ac sin(2πn・ΔX/P) ……(9)
となる。 Therefore, the above formula (7) is d≒1/4 (λ 1 λ 2 /λ 2 -λ 1 ) (m+1/2)...
When (8), I≒4ac sin(2πn・ΔX/P)...(9).
この関係についてさらに詳しく説明する。すな
わち、前記第(7)式では√ の項が回折格子1,2
間のギヤツプdによる変化成分を表わすものであ
り、ギヤツプdによる影響を排除するということ
は√ 内の
cos{4πd(1/λ1+1/λ2)}
×cos{4πd(1/λ1−1/λ2)}
の値が常に略Oに、つまり
cos{4πd(1/λ1+1/λ2)}
またはcos{4πd(1/λ1−1/λ2)}
の少なくとも一方が常に略Oになればよいという
ことである。 This relationship will be explained in more detail. That is, in Equation (7) above, the term √ is the difference between diffraction gratings 1 and 2.
It represents the change component due to the gap d between the two, and eliminating the influence of the gap d means cos {4πd (1/λ 1 + 1/λ 2 )} × cos {4πd (1/λ 1 − 1/λ 2 )} is always approximately O, that is, at least one of cos{4πd(1/λ 1 +1/λ 2 )} or cos{4πd(1/λ 1 −1/λ 2 )} is always approximately O. This means that it should be approximately O.
ここで、いま仮にλ1,λ2をアルゴンレーザの代
表的な周期であるλ1=0.4880μm、
λ2=0.5145μmに設定したとすると、上記第(7)
式中のcos{4πd(1/λ1−1/λ2)}は第5図aに
示す如
く表わされ、またcos{4πd(1/λ2+1/λ1)}は
第5図
bに示す如く表わされる。この第5図bは第5図
aのイに示す期間を拡大して示したものである。
この図から明らかなように、cos{4πd(1/λ1−
1/λ2)}の特性の周期(約5μm)はcos{4πd(1/
λ1+
1/λ2)}の特性の周期(約0.12μm)に比べて著し
く長くなる。 Now, if we assume that λ 1 and λ 2 are set to λ 1 = 0.4880 μm and λ 2 = 0.5145 μm, which are typical periods of an argon laser, then the above (7)
Cos {4πd (1/λ 1 -1/λ 2 )} in the formula is expressed as shown in Figure 5 a, and cos {4πd (1/λ 2 +1/λ 1 )} is expressed as shown in Figure 5 b. It is expressed as shown below. FIG. 5b is an enlarged view of the period shown in FIG. 5a.
As is clear from this figure, the characteristic period (about 5 μm) of cos {4πd (1/λ 1 - 1/λ 2 )} is equal to cos {4πd (1/λ 2 )}.
λ 1 + 1/λ 2 )} is significantly longer than the characteristic period (approximately 0.12 μm).
一方、外部振動等に起因する半導体ウエハと
ICマスクとの間のギヤツプの変動は、現在の技
術によれば最大±0.1μm程度に抑えることが可能
である。すなわち、ギヤツプ変動については、こ
の±0.1μmの範囲の変動さえ無視できるようにす
ればよい。 On the other hand, semiconductor wafers caused by external vibrations, etc.
According to current technology, variation in the gap between the IC mask and the IC mask can be suppressed to a maximum of about ±0.1 μm. That is, regarding gap fluctuations, it is sufficient to make it possible to ignore even fluctuations within this range of ±0.1 μm.
したがつて、この条件を上記第5図の特性に適
用してみると、ギヤツプdの最大変動範囲(±
0.1μm)における干渉強度Iの変化量は、cos
{4πd(1/λ1+1/λ2)}については非常に大きい
が、
cos{4πd(1/λ1−1/λ2)}は微小であり無視で
きる程
度となる。このため、上記した第(7)式の
cos{4πd(1/λ1+1/λ2)}
×cos{4πd(1/λ1−1/λ2)}
が常に略Oとなるようにするには、
cos{4πd(1/λ1−1/λ2)}≪1
となるようにギヤツプdの初期値を設定すればよ
いことになる。この値は上記第5図の例では例え
ばd=8.29μmに相当する。このように設定すれ
ば、たとえギヤツプdが±0.1μmの範囲内で変動
しても、cos{4πd(1/λ1−1/λ2)}の変化量は
微小で
あり、≒Oを保つため、上記
cos{4πd(1/λ1+1/λ2)}
×cos{4πd(1/λ1−1/λ2)}
も略Oを保つことになる。この結果、ギヤツプd
の変動による干渉強度Iへの影響は略排除するこ
とが可能となる。しかして、前記第(9)式は成立す
る。 Therefore, when this condition is applied to the characteristics shown in Fig. 5 above, the maximum variation range of the gap d (±
The amount of change in interference intensity I at 0.1μm) is cos
Although {4πd(1/λ 1 +1/λ 2 )} is very large, cos{4πd(1/λ 1 −1/λ 2 )} is so small that it can be ignored. For this reason, cos {4πd (1/λ 1 + 1/λ 2 )} ×cos {4πd (1/λ 1 -1/λ 2 )} in the above equation (7) should always be approximately O. In this case, the initial value of the gap d may be set so that cos{4πd(1/λ 1 −1/λ 2 )}≪1. This value corresponds to, for example, d=8.29 μm in the example of FIG. 5 above. With this setting, even if the gap d fluctuates within the range of ±0.1 μm, the amount of change in cos {4πd (1/λ 1 - 1/λ 2 )} is small and ≒O is maintained. Therefore, the above cos{4πd (1/λ 1 +1/λ 2 )} ×cos {4πd (1/λ 1 −1/λ 2 )} also maintains approximately O. As a result, the gap d
It becomes possible to substantially eliminate the influence of fluctuations in the interference intensity I. Therefore, the above equation (9) holds true.
この関係から明らかなように、各回折格子1,
2間距離(ギヤツプ)を上記第(8)式に相当する値
に設定すれば、その状態で各回折格子1,2間距
離が微小変動したとしても、上記第(9)式はほとん
ど変化せず、回折格子1,2相互間のずれ量ΔX
のみの関数となる。 As is clear from this relationship, each diffraction grating 1,
If the distance between the two diffraction gratings (gap) is set to a value corresponding to equation (8) above, even if the distance between each diffraction grating 1 and 2 changes slightly in that state, equation (9) above will hardly change. First, the amount of deviation ΔX between the diffraction gratings 1 and 2
It becomes a function of only.
したがつて、以上の関係に着目して、位置合わ
せ装置を構成すれば、回折格子1,2間距離dの
変動にほとんど影響を受けない位置合わせを行な
うことができる。 Therefore, if the alignment device is configured with attention to the above relationship, alignment can be performed that is almost unaffected by fluctuations in the distance d between the diffraction gratings 1 and 2.
以下、図面を参照して本発明の一実施例を説明
する。第2図は同実施例における位置合わせ装置
の概略構成図である。同図において、基台11上
を移動自在に設けられた移動テーブル12上に
は、被位置合わせ物としての半導体ウエハ13が
載置してある。この半導体ウエハ13の周縁部に
は、例えば90゜おきに第1の回折格子14が設け
てある。上記移動テーブル12は、パルスモータ
を有するテーブル駆動装置15により精密移動す
るようになつている。一方半導体ウエハ13の上
方位置には、支持台16により支持されて被位置
合わせ物としてのICマスク17が平行配置され
ている。このICマスク17の周縁部には、前記
第1の回折格子14と対向して第2の回折格子1
8が設けてある。これら第1および第2の回折格
子14,18は、格子ピツチがともに同一長に設
定してある。またこれら第1および第2の回折格
子14,18間距離(ギヤツプ)は、前記第(8)式
を満たすべく支持台16の上下動により設定され
ている。 Hereinafter, one embodiment of the present invention will be described with reference to the drawings. FIG. 2 is a schematic diagram of the alignment device in the same embodiment. In the figure, a semiconductor wafer 13 as an object to be aligned is placed on a movable table 12 that is movable on a base 11. On the peripheral edge of the semiconductor wafer 13, first diffraction gratings 14 are provided, for example, every 90 degrees. The moving table 12 is precisely moved by a table driving device 15 having a pulse motor. On the other hand, above the semiconductor wafer 13, an IC mask 17 is supported by a support stand 16 and is arranged in parallel as an object to be aligned. A second diffraction grating 1 is provided at the periphery of the IC mask 17, facing the first diffraction grating 14.
8 is provided. The grating pitches of the first and second diffraction gratings 14 and 18 are both set to have the same length. Further, the distance (gap) between the first and second diffraction gratings 14 and 18 is set by vertical movement of the support base 16 so as to satisfy the above-mentioned formula (8).
そして本実施例の位置合わせ装置は、第1およ
び第2の回折格子14,18に対して、例えばア
ルゴンガスレーザ装置20から波長の異なる2つ
のレーザ光(λ1=0.488μmとλ2=0.5145μm)2
1,22をそれぞれ垂直に照射する。そして、上
記各回折格子14,18による+n次方向および
−n次方向の回折光23,24を、分光用回折格
子25,26で各レーザ光21,22に対応する
もの毎に分離して受光器27a,27bおよび2
8a,28bにて検出している。しかるのち、こ
れらの受光器27a,27bおよび28a,28
bの各検出信号をそれぞれ前置増幅器29a,2
9bおよび30a,30bで増幅したのち、同じ
波長のものどうしを差動増幅器31,32で相互
に減算している。そして、これらの各差動増幅器
31,32で得られた干渉強度差に相当する信号
を演算回路33に導入し、ここで上記各干渉強度
差の2乗平均を算出してこの算出値を前記半導体
ウエハ13とICマスク17との間のずれ量とし
て表示装置34に表示させる。また同時に、上記
演算回路33の算出値は、前記テーブル移動装置
15にも導びいている。テーブル移動装置15
は、上記算出値を零にすべく移動テーブル12を
移動させるものである。 The alignment device of this embodiment applies two laser beams of different wavelengths (λ 1 =0.488 μm and λ 2 =0.5145 μm) from, for example, the argon gas laser device 20 to the first and second diffraction gratings 14 and 18. )2
1 and 22 are irradiated vertically. Then, the diffracted lights 23 and 24 in the +n-order direction and the -n-order direction by the respective diffraction gratings 14 and 18 are separated and received by the spectroscopic diffraction gratings 25 and 26 into parts corresponding to the respective laser beams 21 and 22. vessels 27a, 27b and 2
It is detected at 8a and 28b. After that, these light receivers 27a, 27b and 28a, 28
The detection signals of b are respectively transmitted to preamplifiers 29a and 2
After amplification by 9b and 30a, 30b, differential amplifiers 31, 32 subtract signals having the same wavelength from each other. Then, a signal corresponding to the interference intensity difference obtained by each of these differential amplifiers 31 and 32 is introduced into the arithmetic circuit 33, where the root mean square of each of the interference intensity differences is calculated, and this calculated value is used as the above-mentioned. The amount of deviation between the semiconductor wafer 13 and the IC mask 17 is displayed on the display device 34. At the same time, the calculated value of the arithmetic circuit 33 is also led to the table moving device 15. Table moving device 15
is to move the moving table 12 in order to make the above calculated value zero.
このような構成であるから、各回折格子14,
18にレーザ光21,22を照射すると、回折格
子14,18のずれ量に相当する強度の干渉光2
3,24が+n次方向および−n次方向にそれぞ
れ配置した受光器27a,28aおよび27b,
28bで検出され、受光信号に変換される。そし
て、これらの各受光信号は各別に増幅されたのち
演算増幅器31,32に導入され、ここで波長の
同じものどうしの差が求められる。これにより、
受光器27a,27bおよび28a,28bに混
入した外乱光成分が相殺され、除去される。そう
して、外乱光成分が除去された上記各差信号は、
演算回路33でその2乗平均がとられる。この結
果、前記第(9)式から明らかなように回折格子1
4,18間距離dの影響が排除される。したがつ
て、位置合わせ中に床面振動等により回折格子1
4,18間距離dが変動しても、その影響が位置
ずれ量の検出結果に現われることはなくなる。以
上の効果をグラフに示すと第3図のようになる。
すなわち、横軸に回折格子間距離(ギヤツプ)d
をとり、かつ縦軸に演算回路33の出力信号、つ
まり各差信号の2乗平均値Iをとつて、ギヤツプ
dの適当な長さ付近、例えばd=8.29μm付近に
おける2乗平均値Iの値を表わすと、略一定とな
る。これは、既に述べたように演算回路33の出
力信号が回折格子14,18間の距離dの変動に
よりほとんど変化しないことを示している。ちな
みに、ただ1つのレーザ光を用いた場合には、第
4図に示す如く検出値(I-n−I+n)は、ギヤツプ
dの変動により大きく変化し、使用に耐えない。 With such a configuration, each diffraction grating 14,
When the laser beams 21 and 22 are irradiated onto the diffraction gratings 14 and 18, interference light 2 with an intensity corresponding to the amount of deviation between the diffraction gratings 14 and 18 is generated.
3 and 24 are arranged in the +n-th direction and the -n-th direction, respectively;
The light is detected at 28b and converted into a light reception signal. Each of these received light signals is amplified separately and then introduced into operational amplifiers 31 and 32, where the difference between signals having the same wavelength is determined. This results in
The disturbance light components that have entered the light receivers 27a, 27b and 28a, 28b are canceled out and removed. Then, each of the above difference signals from which the disturbance light component has been removed is
The arithmetic circuit 33 calculates the square mean. As a result, as is clear from equation (9) above, the diffraction grating 1
The influence of the distance d between 4 and 18 is eliminated. Therefore, during alignment, the diffraction grating 1 may be damaged due to floor vibration, etc.
Even if the distance d between 4 and 18 changes, its influence will not appear in the detection result of the amount of positional deviation. The above effects are shown in a graph as shown in Fig. 3.
In other words, the distance between diffraction gratings (gap) d is plotted on the horizontal axis.
, and the output signal of the arithmetic circuit 33, that is, the root mean square value I of each difference signal, is plotted on the vertical axis. When expressed as a value, it is approximately constant. This indicates that the output signal of the arithmetic circuit 33 hardly changes due to the variation in the distance d between the diffraction gratings 14 and 18, as described above. Incidentally, when only one laser beam is used, the detected value (I -n -I +n ) changes greatly due to variations in the gap d, as shown in FIG. 4, and is not usable.
このように、本実施例の位置合わせ装置によれ
ば、波長の異なる2つのレーザ光を用い、それに
より得た各干渉強度の2乗平均値を求めるだけ
で、床面振動等に悪影響を受けることなく精度良
く、かつ簡単に位置ずれ量を求めることができ
る。この結果、半導体ウエハ13とICマスク1
7との位置合わせを正確かつ迅速に行なうことが
可能となる。また、従来のようにレーザ光自体を
変調させる必要がないので、レーザ装置の構成が
複雑化したり大形化することがなく、この結果構
成が簡単で安価な装置を提供することができる。
さらに本実施例では、回折格子を振動させる必要
もないので、たとえ半導体ウエハ13およびIC
マスク17が大きくても、安定でしかも精度の高
い位置合わせを行なうことができる。 As described above, according to the alignment device of this embodiment, by using two laser beams with different wavelengths and simply finding the root mean square value of each interference intensity obtained thereby, it is possible to eliminate the adverse effects caused by vibrations of the floor surface, etc. The amount of positional deviation can be calculated easily and accurately without any problems. As a result, semiconductor wafer 13 and IC mask 1
7 can be accurately and quickly aligned. Further, since there is no need to modulate the laser beam itself as in the conventional case, the structure of the laser device does not become complicated or large, and as a result, a device with a simple structure and low cost can be provided.
Furthermore, in this embodiment, there is no need to vibrate the diffraction grating, so even if the semiconductor wafer 13 and the IC
Even if the mask 17 is large, stable and highly accurate positioning can be performed.
なお、本発明は上記実施例に限定されるもので
はない。例えば、レーザ光の波長は、λ1=
0.488μmとλ2=0.5145μmとを用いる以外に、他の
波長を用いてもよい。またレーザ光の数は、2つ
以外に3つ以上でもよい。この場合には各干渉強
度差をI=√〓1 2+〓2 2+〓3 2+……のように2
乗
平均すればよい。その他、可干渉光の種類や演算
回路の構成等についても、本発明の要旨を逸脱し
ない範囲で種々変形して実施できる。 Note that the present invention is not limited to the above embodiments. For example, the wavelength of laser light is λ 1 =
In addition to using 0.488 μm and λ 2 =0.5145 μm, other wavelengths may be used. Further, the number of laser beams may be three or more instead of two. In this case, each interference intensity difference is calculated by 2 as I=√〓 1 2 +〓 2 2 +〓 3 2 +...
Just take the average value. In addition, the type of coherent light, the configuration of the arithmetic circuit, etc. can be modified in various ways without departing from the gist of the present invention.
以上詳述したように、互いに波長の異なる複数
の可干渉光を回折格子に垂直照射し、回折格子に
よる回折光の+n次方向の干渉強度および−n次
方向の干渉強度の差を上記各可干渉光毎に各々検
出し、これらの各干渉強度の2乗平均を求めてこ
の値を被位置合わせ物の位置ずれ量とした本発明
によれば、被位置合わせ物の大きさに関係なく常
に安定精度の高い位置合わせを行ない得、しかも
構成が簡単で安価な位置合わせ装置を提供するこ
とができる。 As detailed above, a plurality of coherent beams having different wavelengths are vertically irradiated onto a diffraction grating, and the difference between the interference intensity in the +n-order direction and the interference intensity in the -n-order direction of the diffracted light by the diffraction grating is determined by According to the present invention, each interference light is detected individually, the square mean of these interference intensities is calculated, and this value is used as the amount of positional deviation of the object to be aligned. It is possible to provide a positioning device which can perform positioning with high stability and accuracy, and which is simple in configuration and inexpensive.
第1図は本発明の原理説明に用いるための模式
図、第2図は本発明の一実施例における位置合わ
せ装置の概略構成図、第3図および第4図は同装
置の作用説明に用いるための特性図、第5図は本
発明の原理説明に用いる特性図である。
1,2,14,18…回折格子、3…可干渉
光、3a,3b,3c…回折光、12…移動テー
ブル、13…半導体ウエハ、15…テーブル移動
装置、17…ICマスク、20…レーザ装置、2
1,22…レーザ光、23,24…回折光、2
5,26…分光用回折格子、27a,27b,2
8a,28b…受光器、29a,29b,30
a,30b…前置増幅器、31,32…演算増幅
器、33…演算回路、34…表示装置。
FIG. 1 is a schematic diagram used to explain the principle of the present invention, FIG. 2 is a schematic diagram of the alignment device in an embodiment of the present invention, and FIGS. 3 and 4 are used to explain the operation of the device. FIG. 5 is a characteristic diagram used to explain the principle of the present invention. 1, 2, 14, 18... Diffraction grating, 3... Coherent light, 3a, 3b, 3c... Diffracted light, 12... Moving table, 13... Semiconductor wafer, 15... Table moving device, 17... IC mask, 20... Laser device, 2
1, 22... Laser light, 23, 24... Diffracted light, 2
5, 26... Diffraction grating for spectroscopy, 27a, 27b, 2
8a, 28b...light receiver, 29a, 29b, 30
a, 30b... preamplifier, 31, 32... operational amplifier, 33... operational circuit, 34... display device.
Claims (1)
を相互に平行配置された被位置合わせ物にそれぞ
れ設けて、各被位置合わせ物相互間の位置合わせ
を行なう位置合わせ装置において、所定の間隔で
配置した前記第1および第2の回折格子にそれぞ
れ波長の異なる複数の可干渉光を垂直に照射する
光源と、前記各回折格子による回折光の+n次方
向の干渉強度および−n次方向の干渉強度の差を
前記各可干渉光毎に検出する手段と、この手段に
より得られた各干渉強度差の2乗平均を求めてこ
の値から前記被位置合わせ物相互間のずれ量を得
る手段とを具備したことを特徴とする位置合わせ
装置。1. In an alignment device in which first and second diffraction gratings of the same grating pitch are provided on objects to be aligned that are arranged parallel to each other, and the objects to be aligned are aligned with each other, a light source that perpendicularly irradiates a plurality of coherent light beams having different wavelengths onto the first and second diffraction gratings arranged therein, and an interference intensity in the +n-order direction and an interference in the -n-order direction of the diffracted light by each of the diffraction gratings. means for detecting the difference in intensity for each of the coherent beams; and means for obtaining the square mean of the interference intensity differences obtained by the means and obtaining the amount of deviation between the objects to be aligned from this value. A positioning device characterized by comprising:
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP7897781A JPS57193818A (en) | 1981-05-25 | 1981-05-25 | Positioning device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP7897781A JPS57193818A (en) | 1981-05-25 | 1981-05-25 | Positioning device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS57193818A JPS57193818A (en) | 1982-11-29 |
| JPH0115082B2 true JPH0115082B2 (en) | 1989-03-15 |
Family
ID=13676948
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP7897781A Granted JPS57193818A (en) | 1981-05-25 | 1981-05-25 | Positioning device |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS57193818A (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| NL194811C (en) * | 1986-01-16 | 2003-03-04 | Mitsubishi Electric Corp | Servo circuit. |
-
1981
- 1981-05-25 JP JP7897781A patent/JPS57193818A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS57193818A (en) | 1982-11-29 |
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