Method for determining on-chip sheet resistivity

Abstract

A method measures a resistance in a test structure to determine the sheet resistivity of a test structure. In one embodiment, a family of test structures is provided to determine the effective sheet resistivity of a conductor as a function of its width. The method is applicable to conductors in manufacturing processes in which “slots” or “islands” are created in the conductor to prevent dishing during chemical-mechanical polishing.

Description

BACKGROUND OF THE INVENTION

1. Field of the Invention

The present invention relates to integrated circuit manufacturing. In particular, the present invention relates to determining values of sheet resistivity for use in an integrated circuit design to ensure manufacturability and performance.

2. Discussion of the Related Art

Interconnect process parameters are parameters that represent the physical properties of interconnect layers (i.e., conductors used in connecting circuit elements of an integrated circuit) and the intervening insulator layers. Interconnect process parameters include physical dimensions and coefficients of conducting and insulating properties. Typical interconnect process parameters used in designing integrated circuits include thicknesses, widths, and such material properties as sheet resistances of conducting layers (e.g., polysilicon and metal) and permittivities of intervening insulator layers (e.g., silicon dioxides). From measurements of these interconnect process parameters, the electrical properties of conductive traces of an integrated circuit can be individually modeled as resistances, capacitances, and inductances. The resistances, capacitances and inductances can be obtained numerically for any structure manufactured under a manufacturing process using simulation programs, including programs commonly referred to as “field solvers”.

A field solver is a computer program which calculates a distribution of an electric field, based on solving the Poisson's equation numerically in two or three dimensions. Thus, a field solver can be used to calculate interconnect electrical properties (e.g., resistances and capacitances) based on a physical model of an interconnect structure. One such field solver, named “Raphael™”, is available from Avant! Corporation, Fremont, Calif. Alternatively, the “QuickCap™” program available from Random Logic Corporation, Fairfax, Va., while strictly speaking not a field solver, can also be used.

In the prior art, field solvers did not play a direct role in determining values of interconnect process parameters. Instead, values of interconnect process parameters are derived from measurements using test structures designed to allow the values of the interconnect process parameters to be computed using closed-form formulae. Typically, a field solver is used only to check whether the values of these interconnect process parameters obtained from these close-formed formulae correctly predict the electrical properties of structures.

Because the interconnect structures in an integrated circuit design below the half-micron level typically contribute a substantial portion of the signal propagation delays, variations in these interconnect structures can result in significant variations in the electrical properties of the interconnect, and thus significant variations in circuit performance. Thus, interconnect process parameters must be accurately extracted. Alternatively, the physical dimensions of interconnect structures are obtained primarily by measuring, for example, scanning-electron microscope (SEM) micrographs of one or more cross-sections of a fabricated test structure. However, poor instrument calibrations can limit the accuracy of such measurements.

In the prior art, when interconnect structures account for a much smaller portion of the electrical properties of the integrated circuit, interconnect process parameters are measured by process engineers for process monitoring purposes, rather than for obtaining accurate measurements of the electrical properties under various load conditions. Consequently, AC and DC electrical measurements are performed on relatively simple test structures (e.g., the van der Pauw structure can be used to measure conductor and diffusion sheet resistances. Similarly, a parallel-plate capacitor can be used to measure capacitance per unit area). Typically, however, these measurements are used to determine directly the capacitance associated with a particular structure, not to determine values of the underlying interconnect process parameters. For example, a parallel-plate structure can be used to determine the capacitance per unit area of a conductor plate. As another example, a conductor line can be provided over a conductor plate. The capacitance per unit length of the conductor line can be determined from such a structure. However, such simple test structures are unsuitable for modeling local variation effects of electrically conductive traces.

Examples of a resistance measurement and a sheet resistivity measurement are provided here. FIG. 6 shows schematically a four-point Kelvin technique in the prior art for measuring the resistance value of a device 6000 (e.g., a resistor) in an integrated circuit. In FIG. 6 , device 6000 is connected to four terminals (pads) 6001 - 6004 . According to the four-point Kelvin technique, a current I is forced through device 6000 via terminals 6001 and 6002 , resulting in a voltage difference V1−V2 across device 6000 . The voltage difference is measured across the other two terminals 6003 and 6004 . The resistance R of device 6000 is provided by:

R=(V1−V2)/I.

Sheet resistance p is a convenient measure of resistivity of a conducting layer. In the prior art, to measure resistivity, one form of the four-point Kelvin structure, known as a van der Pauw structure can be used. A van der Pauw structure 800 is shown in FIG. 8 . As shown in FIG. 8 , test structure 800 includes probe pads 801 - 804 , and a cross-shaped structure 805 , which is formed by conductor traces 805 a , 805 b , 805 c and 805 d in the conductor layer for which sheet resistance is to be determined. Conductor traces 805 a - 805 d intersect at a square portion 805 e . The resistance of square portion 805 e is used to determine the sheet resistance of interest. As in the resistance measurement discussed above, a current I is forced across probe pads 804 and 803 in test structure 800 , and a voltage difference ΔV=V2−V1 is measured across probe pads 801 and 802 . In test structure 800 . the sheet resistance ρ is given by the relation:

ρ=π/ln(2)*ΔV/I

However, van der Pauw structures are difficult to use in highly conductive layers, such as aluminum. In highly conductive layers, resistivity ρ is small. Consequently, the sheet resistance of a square of conductor having this resistivity is also low. As a result, a high current I through the test structure is required to create a measurable voltage difference ΔV. Such a large current can cause a heating effect that affects measurement accuracy and, in some instances, can destroy the test structure.

“Micro-loading” is an effect caused by the local density of conductors within the same conductive layer on each other. Micro-loading, which can result in non-uniformity in conductor widths, occurs in an area of low local conductor density where the etchant is locally depleted due to removal of a large amount of material. Micro-loading results in an under-etching of the conductive layer, i.e., the resulting conductor widths are wider than desired. Conversely, in an area of high local conductor density, an excessive amount of active etchant can remain when only a small amount of conductive material is to be removed. The excess amount of active etchant results in an over-etching of the conductive layer, i.e., resulting conductor widths are narrower than desired.

The non-uniformity resulting from micro-loading, or other mechanisms leading to an under-etch or an over-etch of a conductor, can be characterized by an interconnect process parameter “CD loss.” CD loss affects the electrical characteristics (e.g., a resistance or a capacitance) of a conductor. Thus, CD loss is an important design parameter. Test structures such as test structure 800 , or similar structures with a square or nearly-square central region, are often used because of relative insensitivity to CD loss. In test structure 800 , for example, the square central region 805 e maintains a constant aspect ratio of 1:1 despite CD loss, i.e., its width and length are equally reduced by critical dimension loss. Typically, CD losses are in the order of 0.1 micron for a 0.35-micron process.

CD loss can be determined using a conductor trace of a drawn width W, and same-layer parallel conductor traces of the same width W, spaced a distance of S length units apart. Such a test structure 1100 is shown in FIG. 11 . In FIG. 11 , test structure 1100 is a four-point Kelvin structure which includes portion 11101 of a length L and a width W. Portion 11101 is surrounded by a large number of pairs of neighboring conductor traces which are labeled 11102 a , 11102 b . . . , placed at spacing S apart. To illustrate, for a 0.35 μm technology, Kelvin structure 1100 , together with neighboring wires 11102 a , 11102 b , . . . span a distance of about 40 μm on each side (i.e., 30 to 40 neighboring traces on each side). The line-width correction ΔW associated with the CD loss for W and S is provided by the equation:

ΔW=W−(L*ρ/R)

where ρ is the sheet resistivity of the conductor layer.

In the prior art, circuit behaviors (e.g., speed) are not as critically affected by the detailed interconnect structure. Therefore, a test structure for monitoring CD loss typically consists of conductor lines of a single width, provided either at minimal or very large spacings. Thus, the prior art only illuminates how to determine critical dimensions in isolated situations, but provides no general means for characterizing CD loss systematically for the full range of interesting situations.

Another mechanism that brings about non-uniformity is the “proximity effect.” For example, planarization techniques using chemical-mechanical polishing techniques can yield thicknesses that vary systematically according to the local conductor density in the conductor layer underlying the interlayer dielectric (ILD) layer. This systematic variation (the “proximity effect”) causes a greater interlayer dielectric thickness in a region of higher underlying conductor density than a region of lower conductor density. In addition to the proximity effect, interconnect structures outside a region can also affect uniformity in ILD thicknesses within a region. A non-uniform ILD thickness can affect electrical properties profoundly.

In the prior art, an ILD thickness can be obtained by measuring the capacitance C of a parallel-plate test structure, such as test structure 650 shown in FIG. 2 . Test structure 650 is used to determine the ILD thickness above a conductor plate 602 of conductor layer L 2 . To measure capacitance C, conductor plate 603 of layer L 3 , and any structures above conductor layer L 3 , are connect to one probe pad 604 to form a first electrode, and conductor plate 602 of conductor layer L 2 , and any other conductor structures below conductor layer L 2 , are connected to another probe pad 605 to form a second electrode. The ILD thickness h L2-L3 between conductor layers L 2 and L 3 is the calculated using the equation:

C=ε 0 *A/(h L2-L3 /k L2-L3 )

where C is the measured capacitance, the k L2-L3 is the associated interlayer dielectric permittivity, ε 0 is the permittivity of free space, and A is the surface area of test structure 650 (as viewed from the top).

SUMMARY OF THE INVENTION

The present invention provides a method for measuring sheet resistivity of interconnect lines under a given semiconductor manufacturing process, using a family of test structures. Under this method, a test structure which incorporates a resistive portion is fabricated. In that test structure, the resistive portion has an effective length which is substantially greater than the effective width. At the same time, the effective width of the resistive portion is substantially greater than a predetermined minimum conductor width for use in that manufacturing process. Under this configuration, the test structure is relatively insensitive to CD loss, while at the same time allowing accurate electrical measurement of the conductor layer's sheet resistivity without causing excessive heating, as is prone in the prior art.

In one embodiment, a method of the present invention is applied to measure the effective sheet resistivity of an interconnect line that is formed with dielectric slots or islands.

The present invention is better understood upon consideration of the detailed description below and the accompanying drawings.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 illustrates the interconnect process parameters measured in a representative fabrication process which includes as conductors two levels of metallization and a one level of polysilicon.

FIG. 2 shows a test structure 650 for determining interlayer dielectric thickness above a conducting layer containing a solid plate.

FIG. 3 illustrates the use of a field solver in calculating the interconnect process parameters.

FIG. 4 shows one type of a test structure 400 , illustrating a relation between a test structure and a field solver.

FIG. 5 shows in top and cross-sectional views the structure of probe pad 500 , which is used for electrical access to one or more conductor layers of a test structure.

FIG. 6 shows a four-point Kelvin structure 600 of the prior art for measuring resistance of a device 6000 .

FIG. 7 shows a parallel-plate-capacitor test structure 705 including a ruler 704 in conductor layer 7003 .

FIG. 8 shows a van der Pauw test structure 800 of the prior art for determining a sheet resistivity for a conductor layer.

FIG. 9 a shows a conductor pattern 900 , including parallel conductors 901 - a , 901 - b , 901 - c and 901 - d used as a ruler in a SEM photomicrograph.

FIG. 9 b illustrates a SEM photograph 902 of conductor pattern 900 positioned in a horizontal direction.

FIG. 9 c illustrates a SEM photograph 903 of conductor pattern 900 positioned in a vertical direction.

FIG. 10 shows a four-point Kelvin test structure 1000 for determining a sheet resistivity for a conductor layer; four-point Kelvin test structure is relatively insensitive to critical-dimension loss.

FIG. 11 shows a test structure 1100 for determining a critical-dimension loss.

FIG. 12 a shows a test structure 1200 for determining the effect of micro-loading on critical-dimension loss.

FIG. 12 b shows a test structure 1250 for determining the effect of micro-loading on critical-dimension loss, using a fixed number of neighboring conductor traces of various widths.

FIG. 13 a illustrates a method applied to measure capacitance C of a parallel-plate test structure 1300 , in which an ILD thickness above an absent conductor plate 21102 in conductor layer L 2 is measured.

FIG. 13 b illustrates a method applied to measure capacitance C of a parallel-plate test structure 1310 , in which an ILD thickness above a grating 21102 of conductors in conductor layer L 2 is measured.

FIG. 14 illustrates a method applied to a test structure 1500 , which provides a measured capacitance C relating the intralayer dielectric constant k L2 between conductor traces 3102 , for a given width W and spacing S in interconnect layer L 2 .

FIG. 15 shows, in processes where a metal layer includes a capping or barrier layer 1502 in conjunction with an conducting core 1501 , conductor traces with I-shaped cross-sections are formed.

FIG. 16 a shows, on a semiconductor wafer 90001 , a conductor pattern placed within an area 90003 and a row of test structures 90001 a to 90001 z placed along an axis of wafer 90001 positioned to measure a global effect of the conductor pattern on local dielectric thickness in the test structures within and outside area 90003 .

FIG. 16 b plots the local dielectric thicknesses in test structures 90001 a to 90001 z of FIG. 16 a along one axis of wafer 90001 .

FIG. 16 c shows, on semiconductor wafer 90001 of FIG. 16 a , a conductor pattern comprising two conductor plates 90201 and 90202 within area 90003 , representing a conductor array in which the conductor spacing is zero.

FIG. 17 a shows plan and cross-sectional views of a wide interconnect line 1701 provided with “slots” 1702 a , 1702 b and 1702 c for preventing “dishing” during chemical and mechanical polishing.

FIG. 17 b shows plan and cross-sectional views of a wide interconnect line 1751 provided dielectric islands 1752 a - 1752 n for preventing “dishing” during chemical mechanical polishing.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

FIG. 1 illustrates the interconnect process parameters measured using a representative fabrication process that includes as conductors two levels of metallization and one level of polysilicon. Of course, the present invention is not limited by the number of layers of conductors or the nature of the conductor or dielectric materials.

As shown in FIG. 1 , the cross-sectional view of an idealized interconnect structure 100 includes metal traces 101 a and 101 b in metal layer 102 (M 2 ), metal traces 103 a and 103 b in metal layer 104 (M 1 ), and polysilicon traces 105 a and 105 b in polysilicon layer 106 (P 1 ). Each metal trace in metal layer 102 (e.g., either one of metal traces 101 a and 101 b ) has a thickness t M2 . Likewise, each metal trace in M 1 layer 104 (e.g., either one of metal traces 103 a and 103 b), and each polysilicon trace in P 1 layer 106 (e.g. either one of polysilicon traces 105 a and 105 b ) have thicknesses t M1 and t p1 respectively.

Between polysilicon layer 106 and metal layer 104 and between metal layer 104 and metal layer 102 are interlayer dielectric (ILD) layers 107 and 108 , designated I P1-M1 and I M1-M2 , respectively. I P1-M1 and I M1-M2 have thicknesses h p1-M1 and h M1-M2 respectively. In addition, the spaces between conductors of metal layer 102 (e.g. conductors 101 a and 101 b ) are filled by intralayer dielectric 110 , designated I M2 . Similarly, the spaces between conductors of metal layer 104 (e.g., conductors 103 a and 103 b ) and between conductors of polysilicon layer 106 (e.g., conductors 105 a and 105 b ) are filled by intralayer dielectric layers 111 and 112 , designated I M1 and I P1 , respectively. Intralayer dielectric 110 , 111 and 112 have thicknesses t M2 , t M1 and t p1 respectively

Because of processing imperfections, the final dimensions of metal traces in M 1 layer 104 and M 2 layer 102 and polysilicon traces in P 1 layer 106 may differ from their design or “drawn” widths. The differences between actual and design widths are characterized by line-width correction factors ΔW M1 , ΔW M2 and ΔW p1 respectively. Since the actual or fabricated widths are usually narrower than the drawn widths, the line-width correction factors shown in the drawing usually have positive values. Process engineers often refer to this loss of line-width as the “critical dimension loss,” or the “CD loss.”

Each conductor layer is characterized by a sheet resistance. For example, conductor layers 102 , 104 and 106 of FIG. 1 are each characterized by sheet resistances ρ M2 , ρ M1 and ρ p1 , respectively. Similarly, each dielectric layer is characterized by a permittivity. Thus, intralayer dielectric 110 , 111 and 112 are characterized by their respective permittivities k M2 , k M1 and k p1 and interlayer dielectric layers 108 , 107 and 109 are characterized by their respective permittivities k M1-M2 , k p1-M1 and k Fox . (In FIG. 1 , the lowest interconnect conductor layer, i.e., polysilicon layer 106 , is shown fabricated on a field oxide layer 109 , which has a permittivity k Fox and a thickness h FOX .)

The line-width correction factors, the thicknesses, the sheet resistances, and the permittivities of FIG. 1 are some of the interconnect process parameters measured by the methods described herein. FIG. 1 shows conductor traces and intralayer dielectrics as having rectangular cross-sections, and interlayer dielectrics as having uniform thicknesses. In cross-section, the interconnect structures resemble a brick wall composed of many kinds of rectangular “bricks.” Generally, this “brick wall” model approximates actual typical interconnect structures sufficiently well to allow relatively accurate prediction of electrical characteristics. Accordingly, in the discussions of interconnect structures, this detailed description generally assumes this idealized brick wall model. Nevertheless, structures in some processes can possess significantly non-rectangular cross-sections.

The methods are described using an interconnect model. The interconnect model matches the fabricated interconnect structures sufficiently closely to allow field solvers or other tools to accurately predict the electrical properties of these fabricated interconnect structures. To achieve such an interconnect model, it is not necessary to mimic every detail of the physical interconnect. For example, if an intralayer dielectric layer consists of two sub-layers of different materials, the intralayer dielectric layer need only be modeled as a single layer for most purposes. To provide the requisite accuracy for predicting capacitance, however, the permittivity is provided as a function of conductor spacing.

The idealized interconnect model of FIG. 1 provides a single value to characterize each line-width correction and interlayer dielectric thickness. In actually fabricated structures, however, both of these interconnect process parameter values may vary systematically. For example, local configurations of the interconnect structures may result in systematic non-uniformity across the wafer. The methods described below fully characterize the systematic variation of these interconnect process parameters. In particular, one method provides a line-width correction factor to apply to a conductor trace as a function of the widths and spacings of same-layer neighboring traces, and the density of neighboring conductor traces within a relevant distance. Another method fully characterize ILD thicknesses, taking into consideration proximity effects and other processing artifacts.

Using a Field Solver to Determine Interconnect Parameters

The methods herein make extensive use of field solvers. FIG. 3 illustrates the role of a field solver 301 . Given a description of a physical structure of interconnect (e.g., its dimensions 302 and the related materials properties 303 ), a field solver can compute the structure's electrical properties relying only on basic physical laws. For example, a field solver can compute the capacitance 304 between conductors in an interconnect structure given physical dimensions and dielectric constants. In the methods herein field solvers play a direct role in determining the values of interconnect process parameters. In particular, one method uses a field solver to extract the values of an interconnect process parameter. Typically, a suitable test structure is fabricated, which is designed to have a measurable electrical property (e.g., capacitance) which depends upon the value of the interconnect process parameter of interest. Typically also, a closed-form solution providing the value of the interconnect process parameter of interest does not exist. Starting from an estimated value for the interconnect process parameter of interest, and keeping the values of any other interconnect process parameters constant, the field solver reiterates until a converged value of the interconnect process parameter of interest is obtained.

For example, given an actually measured capacitance, resistance, or inductance of a test structure, the interconnect process parameter can be obtained by successive approximation. In particular, successively refined approximations of the interconnect process parameter of interest are fed into a field solver until the field solver predicts, within predetermined tolerance limits, the measured capacitance. The current approximation of the interconnect process parameter when the predicted value converges to the measured value is the desired value for the interconnect process parameter. Convergence can be achieved using well-known numerical methods, such as the binary search or Newton-Raphson iteration.

Alternatively, instead of using an iterative technique such as described above, a table can be provided which summarizes the electrical properties predicted by the field solver as a function of the interconnect parameter, provided over an appropriate range of values. An approximation to the interconnect process parameter can be interpolated or extrapolated from the table using the measured electrical properties from the test structure. The interpolated or extrapolated value may give a sufficiently accurate answer itself, or it may serve as a good initial estimate for the successive-approximation technique used in conjunction with a field solver, as described above. Using the table method reduces both the number of field solver runs necessary to find an acceptably accurate answer and the overall time to measure a set of test structures. Since the table can be compiled from the field solver runs prior to actual physical measurement, the turnaround time from receiving the measured data to completing the parameter calculations can be considerably shorter than the successive approximation method described above.

Typically the interconnect process parameters can be determined one at a time. However, the same technique clearly can be generalized to permit determining two or more interconnect process parameters at once, based on a corresponding number of suitable electrical measurements, using well-known numerical methods.

Test Structures for Determining Interconnect Process Parameters

Since the test structures are typically fabricated on a production wafer along side valuable integrated circuits, the test strictures are designed to be minimally intrusive and to occupy no more than the necessary amount of silicon area. Thus, the test structures are minimized subject to two primary constraints: (a) the test structure should be large enough so that appropriate physical characteristics (e.g., interlayer thickness, critical-dimension loss, proximity effect) dominate the capacitances and resistances to be measured; and (b) the measured capacitance) and resistance value should be large enough to be measured by routinely available equipment. For example, to measure parallel-plate capacitance in a 0.35 μm feature size process, a fabricated test structure occupying an area of a 300 μm on a side ensures that edge effects do not dominate the capacitance to be measured and provides an easily measurable capacitance of a few pico-farads. In some instances, active circuitry could be used to relax condition (b).

FIG. 4 shows a generalized design of one type of test structure 400 . In FIG. 4 , a test structure 400 , shown in top and cross-sectional views, includes a upper conductor layer 401 , a lower conductor layer 404 , and numerous conductor traces (“fingers”) 403 a- 403 n in a conductor layer 403 . Conductor traces 403 a - 403 n are electrically shorted to each other by an orthogonally running conductor trace (not shown), forming a comb structure. Conductor traces 403 a - 403 n run in conductor layer 403 , which is located between conductor layers 401 and 404 . Probe pads 402 a , 402 b and 402 c , which are connected to layers 401 , 403 and 404 respectively, allow access to these conductor layers for electrical measurements. Conductor traces 403 a - 403 n are fabricated in a large number to satisfy conditions (a) and (b) just discussed.

FIG. 5 shows, in top and cross-sectional views, the structure of a probe pad 500 for electrical access to a conductor layer of a test structure. Probe pad 500 , for example, can be used to perform the functions of probe pads 402 a - 402 c of FIG. 4 . As shown in FIG. 5 , probe pad 500 includes conductor plates 501 - 504 , for a corresponding number of conducting layers. Each of conductor plates 501 - 504 connects with a neighboring conductor plate through a large number of vias located around the periphery of the conductor plate. Probe pad 500 then connects to portions of the test structures through interconnect wiring to the appropriate layers.

Where the connection between a probe pad and a test structure affects measurement, a dummy structure consisting only of the probe pad and its interconnect conductors are provided. The capacitance of the dummy structure can then be subtracted from the measured value to give the capacitance of the test structure.

Where a field solver is used to predict the electrical properties of a test structure, it is some time necessary to extrapolate the electrical property of interest from one or a few small, representative, and repetitive elements of the test structure. For example, the electrical properties of the test structure 400 can be extrapolated from representative unit 405 of the test structure. As shown in FIG. 4 , representative unit 405 includes a section of upper conductor 401 , a section of lower conductor 404 and three conductor traces in layer 403 , indicated by reference numerals 403 j - 403 l . The field solution for representative unit 405 is mirrored at the indicated boundaries of 407 and 408 of element 405 , so as to mimic repetitions of representative unit 405 . The potentials in the upper and lower conductors 401 and 404 , and conductor traces 403 j - 403 l of conductor layer 403 are assigned the same potentials under which capacitance on test structure 400 is measured. The overall capacitance of test structure 400 then equals the predicted capacitance for the representative unit 405 multiplied by the number of such units required to occupy the area of test structure 400 .

A test structure for measuring capacitance generally includes a top conductor plate and a bottom conductor plate. If the top conductor plate is the lowest conductor layer of the given process, the substrate underneath the top plate is considered the bottom conductor plate.

Creating a SEM “ruler”

In a method for calibrating SEM photographs, a test structure provides a grating of parallel conductors with known lateral pitch in one or more layers, which can then be used as a built-in reference for dimensional measurements along different directions of the SEM photograph.

FIG. 9 a shows an example of a test structure 900 , which is used as a reference or “ruler” for dimensional measurements along a lateral dimension in a SEM photograph. Test structure 900 contains a number of conductor fingers 901 - a to 901 - d separated from each other by a known pitch. A cross-section of the fabricated test structure 900 in a SEM photograph 902 is illustrated in FIG. 9 b . Since test structure 900 has a known pitch, the pitch P between the images of any pair of adjacent fingers in fingers 901 - a , 901 - b , 901 - c and 901 - d in SEM photograph 902 is proportional to the actual pitch between any pair of adjacent conductors within conductors 901 - a to 901 - d . Thus, the image of test structure 900 in photomicrograph 902 serves as a ruler for other features in the lateral, or “horizontal,” direction (the “x” direction in FIG. 9 b ).

By rotating test structure 900 90 degrees and then obtaining a SEM photograph 903 , as illustrated in FIG. 9 c , test structure 900 can then serve as a “vertical” ruler in for SEM photographs taken under the same magnification. SEM photograph 903 can then be used to calibrate the vertical direction: since the pitch P′ in SEM picture 903 is proportional to the actual fabricated pitch of conductors 901 - a to 901 d , pitch P′ of SEM picture 903 thus provides a reference for accurate dimensional measurements in the vertical “y” direction , as shown in FIG. 9 c . This technique is particularly useful when a camera in the SEM equipment does not have a 1:1 aspect ratio.

Parallel conductors, such as those similar to conductors 901 a to 901 d of test structure 900 , can be found in many test structures. For such test structures, no additional structures need to be included to provide the ruler. However, for a test structure without such a parallel conductor pattern, the parallel conductor pattern can be provided additionally in a “free” layer (i.e., a layer which is not expected to contribute significantly to the relevant electrical properties of the test structure). By placing the ruler in a free layer, electrical measurements are not compromised. For example, as shown in FIG. 7 , a ruler 704 is provided in conductor layer 7003 above conductor layers 7001 and 7002 forming a parallel-plate capacitor structure 705 .

As mentioned above, many integrated circuits include conductor patterns that can serve as the SEM reference discussed above. These conductors need only have known pitches, and not constant pitches. Thus, the method described above is applicable to SEM measurements in general, and is not limited to test structures. Because a typical manufacturing process results in centerlines of conductors very predictably placed, such a ruler can provide a highly accurate reference. A regular grating provides the easiest reference to use, because its edge-to-edge spacing directly reflects its centerline spacing. Clearly, however, other conductor patterns with know center-to-center spacings can also serve as rulers. Further, this method is self-correcting. For example, if the plane of a cross-section is not perpendicular to the conductors, all features are distorted alike, so that the ruler remains a reference to the features in the cross-section.

Determining Sheet Resistivity

To avoid the destructive effects of a large current in a highly conductive layer and yet providing a structure relatively insensitive to CD loss, a four-point Kelvin structure without a square central portion can be used to determine the resistance of a conductor layer. FIG. 10 shows a Kelvin structure 1000 . In Kelvin structure 1000 , rectangular portion 11201 for which a resistance is measured. Rectangular portion 11201 has a length L which is much greater than its width W. A current I is forced across the length of rectangular portion 11201 via probe pads 11202 and 11203 to create a voltage difference ΔV=V1−V2 along the length of rectangular portion 11201 , which is measured across probe pads 11204 and 11205 . The sheet resistance ρ is thus determined by:

ρ=ΔV/I*W/L

By choosing a width W which is much larger than the minimal width W min for conductors in the layer in question (e.g., W=20*W min ), Kelvin structure 1000 is relatively insensitive to CD loss. Further, by having a length L much greater than its width W, thereby raising its resistance R along length L, test structure 1000 maintains a relatively measurable voltage difference across probe pads 11204 and 11205 , while avoiding excessive heating effects because of the relatively smaller current. Rectangular portion 11201 is provided only for illustrative purpose. In fact, the shape of the portion across which resistance is measured is not essential for achieving the results above. To provide the requisite measurable resistance, an effective length in the direction of current flow which is significantly greater than its effective width suffices. For example, region 11201 could be replaced with a serpentine resistive trace which has a total length greatly exceeding its width, provided that the resistive trace's width significantly exceeds the minimum width W min for the conductor layer. A field solver can be used to calculate the effective length-to-width ratio, and hence the relationship between R and ρ, using well-known techniques.

In some manufacturing processes (e.g., a “damascene” process), interconnect lines are created by phtolithographically forming trenches into a dielectric layer, depositing a conductive material to fill the trenches, and planarizing the surface using a chemical mechanical polishing (CMP) process. In these processes, because of the selectivity of the CMP process, a type of surface non-uniformity (called “dishing”) can occur. To prevent dishing, in a wide interconnect line (e.g., conductive traces for use as data buses, power or ground lines), certain portions of the dielectric layer within the interconnect line are masked so that the corresponding portions of the dielectric layer are not removed when the trenches are formed. In the resulting interconnect line, these portions of dielectric appear as “slots” or “islands” with the interconnect lines. For example, FIG. 17 a shows plan and cross-sectional views of wide interconnect line 1701 provided with “slots” 1702 a and 1702 b . Similarly, FIG. 17 b shows plan and cross-sectional views of wide interconnect line 1751 provided dielectric islands 1752 a - 1752 n , giving a “Swiss Cheese” appearance.

The presence of “slots” and “islands” of dielectric material reduces the effective sheet resistivity of the interconnect line. In general, the positions and the sizes of “slots” and “islands” in a given interconnect line depends on the width W of the interconnect line, so that the effective sheet resistivity becomes a function of the width W. To provide the effective sheet resistivity as a function of the width W, the above method for obtaining sheet resistance can be applied to a family of test structures for sheet resistance measurement, each constructed to correspond to a different width W.

Determining Critical-dimension Loss

As mentioned above, the amount of CD loss depends partly on micro-loading. Micro-loading results from the proximity of an interconnect wire relative to conductors in its surroundings (e.g., spacings between this wire and neighboring lines). Thus, it is desirable to establish the relationship between CD loss of an interconnect wire and the local widths and spacings of neighboring wires. A method can be provided to determine the dependency of the fabricated width of an interconnect trace with respect to the density of neighboring conductors. This method determines both the magnitude of the CD loss and the neighborhood size over which CD loss should be evaluated.

A family of test structures can be derived from the basic structure 1100 shown in FIG. 11 . The number of neighboring traces on either sides of an interconnect trace are varied from 0 to 20 to explore the range of the micro-loading effect. For example, FIG. 12 a shows one member 1200 of a family of test structures. Test structure 1200 is used to examine the micro-loading effect of only two pairs of neighboring traces. Thus, only two neighboring pair of conductor traces (labeled 11102 a and 11102 b , respectively) are provided in test structure 1200 . Other members of the family of test structures provide for four neighboring pair of traces (where only the pairs of neighboring traces corresponding to 11102 a |- 11102 d of FIG. 11 are provided), 6 neighboring trace pairs and so forth. Naturally, no microloading effect is assumed present when no neighboring traces are provided. For each member of the family of test structures, the resistance R of the structure is measured as described above. Then the line-width correction ΔW associated with the CD loss for each configuration is calculated using the equation:

ΔW=W−(L*ρ/R)

where sheet resistance p can be determined using one of the previously described techniques.

In addition, in the family of test structures, the conductor width W and the conductor spacings S are varied for each selected number of neighboring conductor trace pairs. The family of test structures for measuring CD loss is summarized in the following table:

	TABLE 1
	S min	2S min	4S min	“∞”
W min	2, 4, 6, “∞”	2, 4, 6, “∞”	2, 4, 6, “∞”	0
2W min	2, 4, 6, “∞”	2, 4, 6, “∞”	2 ,4 ,6, “∞”	0
4W min	2, 4, 6, “∞”	2, 4, 6, “∞”	2, 4, 6, “∞”	0

In Table 1, W min is the minimum trace width for a given manufacturing process, and S min is the minimum allowed spacing in the same process. Thus, the value (2, 4, 6, “∞”) in entry “W min , S min ” denotes a family of test structures containing a central minimum-width trace, with 1, 2, 3 and 4 neighboring conductor trace pairs in its neighborhood, each conductor trace having minimal width W min , and each neighboring conductor trace being separated a minimal spacing S min , from each of its neighboring conductor trace. (In this instance, the case of infinite number of neighboring traces is approximated by 4 pairs of neighboring conductor traces, and the case of no neighboring traces is approximated by infinite spacing between conductors).

In principle, interconnect widths can vary from W min up to the full width of a die. However, as discussed previously, CD loss affects minimally electrical properties of very wide lines (i.e., where the width greatly exceeds the thickness of the trace). Similarly, interconnect spacing can vary from S min up to the full width of a die. In practice, placing no neighbor within a large multiple of S min , e.g., 40 μm for a 0.35 μm process, will characterize the full range of interesting spacing variations. Therefore, it suffices to apply the method to a few representative widths and spacings of interest, including minimal width W min , and minimum spacing S min . For example, Table 1 suggests a possible family of test structures sufficient to characterize a 0.35 μm process.

Of course, the number of neighboring conductor trace pairs, the conductor widths and the spacings needed to characterize CD loss of a particular process must be determined empirically. Thus, while Table 1 provides a specific example, the method that characterizes CD loss is not limited by widths, spacings, and the number of neighboring traces shown therein. Further, while Table 1 shows integral multiples of conductor widths and spacings, fractional multiples of minimal widths or spacings can also be used, where appropriate, to characterize the limits of the process.

Variations in the family of test structures are also possible. For example, instead of varying the number of neighboring conductor trace pairs, the method can be applied to a family of test structures with a fixed number of neighboring conductor trace pairs (e.g., two neighboring traces), but varying the conductor widths, so as to determine the extent of the microloading effect. This example is illustrated by FIG. 12 b , which shows a test structure 1250 , in which the central trace 11001 of width W and length L is separated by a spacing S from a single pair of neighboring conductor traces 11002 . In this family of test structures, the widths W N of neighboring conductor traces 11002 are varied. Similarly, the method can also be used in conjunction with a family of test structures in which all the neighboring conductor traces are located on one side of the conductor trace which resistance is measured.

Further, even though the measured resistance of a conductor trace is used to calculate CD loss in the above description, the more costly and time-consuming measurements using SEM photographs can also be applied to characterize CD loss.

Determining Interlayer Dielectric Thickness

Similar to CD loss, a method can be provided to characterize “proximity effects,” i.e., the dependency of dielectric thickness with respect to local width and spacing variations of neighboring interconnect wires below the dielectric layer. In addition to the proximity effect, a method can also be provided to characterize the dependency of dielectric thickness within a region on interconnect outside of the region (“global effect”).

One method requires a first determination of the values of certain interconnect process parameters. Metal thicknesses and ILD thicknesses can be determined by well-known techniques, e.g., SEM measurements of cross-sections of interconnect wires. Similarly, interlayer permittivities can by determined by (i) measuring the capacitance C of a parallel-plate capacitor test structure, (ii) measuring the ILD thickness h between the parallel plates using a SEM technique, and (iii) calculating the permittivity k from the relationship:

k=(C*h)/(ε*A)

where ε is the permittivity of the dielectric material and A is the area of the test structure.

A method can be provided to determine a full range of ILD thickness variations, using a family of test structures. Although the method described herein measures ILD thicknesses using an electrical method, the ILD thicknesses can also be determined using SEM measurements.

FIG. 13 a illustrates a method applied to measure capacitance C of a parallel-plate test structure 1300 , in which ILD thickness h L2-L3 between conductor layers L 2 and L 3 , above an absent conductor plate 21302 (i.e., no conductor locally present in conductor layer L 2 ) is measured. Test structure 1300 is one member of a family of test structures for measuring ILD thicknesses. In FIG. 13 a , conductor plate 21303 in conductor layer L 3 , and any conductor structure above conductor layer L 3 (e.g., a SEM ruler, not shown), are connected to one probe pad to form a first electrode, and plate 21301 in conductor layer L 1 , and any other conductor plates below conductor layer L 1 , are connected to another probe pad to form a second electrode. The ILD thickness h L2-L3 is calculated from the equation:

C=ε 0 *A/(h L2-L3 /k L2-L3 +t L2 /k L2 +h L1-L2 /k L1-L2 )

where C is the measured capacitance, t L2 is the metal thickness of conductor layer L 2 , h L1-L2 is the ILD thickness between conductor layers L 1 and L 2 , the k's are the associated inter- and intralayer dielectric constants determined as described above, ε 0 is permittivity constant of free space, and A is the area of the test structure. The various interconnect process parameters can be determined as described above or approximated by well-known techniques.

Another member of the family of the test structures for measuring ILD thicknesses is test structure 1310 shown in FIG. 13 b . Test structure 1310 determines an ILD thickness above conductor layer L 2 using a grating 21102 of conductor traces in conductor layer L 2 . In test structure 1310 , grating 21102 is provided as a set of parallel conductors with a selected width W and a selected spacing S. In the test structure 1310 , the parallel conductors (“fingers”) of grating 21102 of layer L 2 are shorted by conductor trace 21106 , forming a “comb” structure 21104 . Conductor plate 21103 , and any conductor structure above conductor layer L 3 , are connected to one probe pad to form a first electrode, and grating 21102 and conductor plate 21101 , and any conductor structures below conductor layer L 1 , are connected to another probe pad to form a second electrode.

To determine the ILD thickness h L2-L3 for test structure 1310 , a field solver can be used to calculate capacitance C unit of unit 21105 , which represents a representative element of test structure 1310 —two parallel conductors in layer L 2 , between conductor plates 21103 of layer L 3 and 21101 of layer L 1 . Since the total capacitance C of test structure 1310 can be approximated by multiplying C unit by the number of fingers and the length of the fingers in comb structure 21104 , the measured capacitance C can be used to obtain capacitance C unit using the successive approximation technique provided above. The various dimensions (including the line-width correction factors) and permittivities for the representative unit 21105 can be determined as described above. The values of interconnect process parameters ΔW ELL , h L2-L3 , t L2 , k L2 , and k L2-L3 for the representative unit 21105 are determined in the manner described above. The ILD thickness h L2-L3 is that ILD thickness between layers L 2 and L 3 at which the field solver predicts for capacitance C unit a capacitance value which is consistent with the measured capacitance C, holding the values of other interconnect process parameters constant.

In test structure 1310 , if the fingers of comb structure 21104 are closely spaced, most of the electric field lines lie within the space between grating 21102 and conductor plate 21103 of layer L 3 . Consequently, the measured capacitance, and hence, the calculated ILD thickness, depend only weakly on k L2 (the intralayer dielectric constant between conductors in conductor layer L 2 ). Thus, in closely spaced grating, an estimate of intralayer dielectric constant k L2 to within 15% is sufficient to provide an estimate for ILD thickness h L2-L3 to within a few percentage points.

The method measures ILD thicknesses as a function of conductor width W and conductor spacing S, using a family of test structures which includes test structures 1300 and 1310 shown in FIGS. 13 a and 13 b respectively. In particular, in addition to test structure 1300 , the remaining members of the family of test structures are derived by varying conductor layer L 2 's conductor width W and conductor spacing S of test structure 1310 . An ILD thickness which corresponds to each conductor width W and each conductor spacing S is measured. Table 2 summarizes a family of test structures that can be used:

	TABLE 2
	0	S min	2S min	4S min	“∞”
	0					x
	W min		x	x	x
	2W min		x	x	x
	4W min		x	x	x
	“∞”	x

In Table 2, an x in a table entry represents a test structure for the selected conductor width and conductor spacing. Width W min is the minimum allowed conductor trace width for the process, and S min is the minimum allowed spacing for the same process. In principle, the conductor width can vary from 0 up to the full width of a die. However, the case of infinite conductor width (corresponding also to the case of zero conductor spacing) is provided by a blanket layer of conductor L 2 over a sufficiently large area. Similarly, interconnect spacing can vary from 0 up to the full width of a die. However, in the case of infinite conductor spacing (corresponding also to the case of zero conductor width) is the same as an absence of a local conductor structure in layer L 2 over a sufficiently large area.

Thus, while Table 2 provides a specific example of a family of test structures, a method for measuring ILD thicknesses is not limited by conductor widths and conductor spacings. Further, while Table 2 shows integral multiples of conductor widths and spacings, fractional multiples of minimal widths or spacings can also be used, where appropriate, to characterize the limits of the process. Also, a method is not limited to grating structures with constant widths and spacings—including irregular test structures (e.g., alternating two different line widths). In particular, for use in conjunction with CMP or similar planarization techniques, local proximity effects depend only upon the average area covered by conductor traces over fairly large areas of conductor layer L 2 , so that a family of test structures with a suitable range of covered areas can be used.

While the above method provides characterization of a full range of dielectric thicknesses as a function of proximity effects, another method can be used to characterize the magnitude and extent to which a given interconnect pattern in one region affects dielectric thicknesses outside the region. Under this method, test structures are placed both proximate to and away from a relatively large area or region of the substrate on which the interconnect structure is fabricated. This method is illustrated by FIGS. 16 a - 16 c.

FIG. 16 a shows a row of identical test structures 90002 a - 90002 z placed on a semiconductor wafer 90001 . Each of test structures 90002 a - 90002 z can be provided by any of the previously discussed test structures for measuring dielectric thicknesses, e.g., test structure 1300 of FIG. 13 a , test structure 1310 of FIG. 13 b , or test structure 650 of FIG. 2 .

On wafer 90001 is defined as 2 S by 2 H rectangular area 90003 , where 2 S and 2 H are respectively the lengths of the shorter and longer sides of area 90003 . Within area 90003 is provided a regular array of conductor traces of predetermined width and spacing, except within the vicinity of test structures 90002 a to 90002 z (e.g., for a 0.35 μm feature size process, within 20 μm of any of test structures 90002 a to 90002 z ). The conductor traces within area 90003 are provided in the same conductor layer as the conductor layer (e.g., conductor layer L 2 ) on which the ILD thicknesses measured by test structures 90002 a to 90002 z depend. As shown in FIG. 16 a , test structures 90002 i to 90002 p are within area 90003 , and test structures 90002 a to 90002 (i−1) and test structures 90002 (p+1) to 90002 z are outside of area 90003 . Presumably, the dielectric thicknesses in test structures within area 90003 and outside of area 90003 are affected by the presence of the conductor traces within area 90003 . FIG. 16 c illustrates one instance in which the regular array of conductor traces having zero spacings, i.e., area 90003 is provided by two solid conductor places 90201 and 90202 in conductor layer L 2 .

Under one method, the ILD thicknesses in test structures 90001 a to 90001 z are measured electrically, via SEM or by any other method to obtain for each test structure the average ILD thickness within its local region. The magnitude and extent of the global effect imposed by the conductor traces within area 90003 on these local ILD thicknesses can be observed by the difference in average ILD thicknesses between test structures within area 90003 (i.e., test structures 90001 i to 90001 p ) and test structures outside of area 90003 (i.e., test structures 90002 a to 90002 (i−1) and test structures 90002 (p+1) to 90002 z ).

FIG. 16 b is a plot of local ILD thicknesses in a row of test structures across one half of wafer 90001 . As shown in FIG. 16 b , a baseline ILD thickness (t inside ) is seen within area 90003 , up to a distance x min from the center of wafer 90001 , and a base line ILD thickness (t outside ) is seen a distance outside of area 90003 , beyond a distance x max from the center of wafer 90001 . Locations x min and x max are respectively locations where the local ILD thickness deviates from t inside and t outside by a predetermined percentage. Thus, the magnitude of the global effect on local ILD thickness can be defined, for example, as the difference between t inside and t outside . The extent within which the global effect on local ILD thickness operates can be defined as the separation between x max and x min . Of course, the profile shown in FIG. 16 b is just one example provided by one manufacturing process. An entirely different profile may be found under another manufacturing process. For example, the difference between ILD thicknesses t inside and t outside inside and outside of area 90003 can be so small that the magnitude and extent of the global effect on local ILD thickness are both effectively non-existent.

Many variations can exist in the method for measuring the global effect on ILD thickness. Such variations include, for example: (a) test structures need not be placed within area 90003 , so that the regular array of conductor traces can be continuous along the length area 90003 ; (b) multiple rows of test structures can be provided, and (c) multiple conductor layers can be examined on the same wafer simultaneously.

Determining Intralayer Permittivity

As the feature sizes of integrated circuits decrease, the capacitive coupling between conductor traces in the same conductor layer can exceed the coupling between conductor traces of different conductor layers. This intralayer capacitive coupling is especially strong between minimal-width wires of the same conductor layer at minimal spacing. Consequently, new materials, new processing techniques, and multi-layer dielectrics are being developed to reduce this intralayer capacitive coupling. Thus, it is desirable to accurately determine line-width correction factors and intralayer permittivities.

The interconnect model described above in conjunction with FIG. 1 provides for homogeneous intralayer and interlayer dielectric materials. However, in state-of-the-art semiconductor processes, multiple layers of dielectric material may be used for some of these intralayer or interlayer dielectric layers. Some dielectric materials are thin conformal layers, others form pockets. Consequently, the intralayer permittivity between parallel conductors within a conductor layer can vary with conductor spacing in that conductor layer, since the average composition of the dielectric material between conductors due to presence of these pockets and conformal layers can differ because of different spacings.

Under one method, the intralayer permittivity k L2 between parallel conductors of conductor layer L 2 spaced a given spacing apart is calculated. Under that method, which is provided in conjunction with test structure 1500 of FIG. 14 , a measured capacitance C of test structure 1500 provides an intralayer dielectric constant k L2 between conductor traces 3102 of a given width W and spacing S in conductor layer L 2 .

In test structure 1500 , conductor traces 3102 are made up of two interleaved comb structures 3102 h and 31021 in conductor layer L 2 . To measure capacitance C, conductor plate 3103 of conductor layer L 3 , any structure above conductor layer L 3 , and comb structure 3102 h are connected to one probe pad to form a first electrode, and comb structure 31021 , conductor plate 3101 of conductor layer L 1 , and any conductor structure below conductor layer L 1 are connected to another probe pad to form a second electrode.

To determine the intralayer dielectric constant k L2 between comb structures 3102 h and 31021 , a field solver can be used to calculate a capacitance C unit of a representative unit 3105 using the measured capacitance C and the successive approximation technique described above. Capacitance C unit is the capacitance between a conductor in comb structure 3102 h and an adjacent conductor in comb structure 31021 . Thus, the measured capacitance C can be approximated by multiplying capacitance C unit by the number of parallel conductor pairs between comb structures 3102 h and 31021 and the length of each conductor. The interconnect process parameters ΔW L2 , h L1-L2 , t L2 , h L2-L3 , k L1-L2 , and k L2-L3 for the representative unit 3105 can be determined as described above or approximated by well-known techniques. Permittivity k L2 is that permittivity value at which the field solver provides a capacitance C unit which agrees with the measured capacitance C, holding the values of other interconnect process parameters constant.

The full range of variations of permittivity k L2 as a function of conductor spacing in layer L 2 is provided by measuring the capacitance of a family of test structures based on test structure 1500 . In these test structures, the widths W and spacings S between the parallel conductor traces of comb structures 3102 h and 31021 are varied. In one method, the full range of variations of the permittivity k L2 is characterized by measuring a sufficiently large number of widths W and spacings S of L 2 conductors. The family of test structures measures a full range of values for an intralayer dielectric constant, for various conductor widths W and conductor spacings S. These results are summarized in Table 3 below:

	TABLE 3
	S min	2S min	4S min
	W min	x	x	x
	2W min	x	x	x
	4W min	x	x	x

In Table 3, an “x” indicate a selected conductor width W and a conductor spacing S for which a test structure derived from test structure 1500 is provided. Width W min is the minimum conductor trace width allowed under the process, and S min , the minimum spacing allowed under the process. In principle, interconnect widths can vary from W min up to the full width of a die. Similarly, interconnect spacing can vary from S min up to the full width of a die. Table 3 provides a possible range for a 0.35 μm feature size process.

Of course, the method for measuring intralayer dielectric is not limited to these width and spacing combinations summarized in Table 3 . In fact, the method can include any number of conductor widths or spacings. In addition, although Table 3 includes only parallel conductors of equal widths and spacings, asymmetrically placed conductors can also be provided. Although integral multiples of minimum widths and spacings are provided in the test structures summarized in Table 3 , fractional multiples of minimal widths or spacings can also be provided to characterize the limits of the process.

Characterizing Conductors with “I”-shaped—Rectangular Cross-sections

In the preceding description, interconnect structures are described using a brick model, under which conductors and intralayer dielectric portions have rectangular cross-sections and interlayer dielectric portions have locally constant thicknesses. However, certain state-of-the-art processes depart significantly from the brick model. In particular, as shown in FIG. 15 , in processes where a metal layer includes a capping or barrier layer 1502 in conjunction with a conducting core 1501 , core 1501 (typically formed by an aluminum layer) tends to etch faster than the barrier layer (typically formed by a tungsten layer), thereby resulting in conductor traces with I-shaped cross-sections.

One method extends the methods described above for measuring CD loss, interlayer dielectric thicknesses and intralayer dielectric thicknesses to conductors with such I-shaped cross sections. That method first determines the widths w 1 , of the conductor core and w 2 of the barrier layer, for example, using SEM photographs of cross-sections of such conductors. In general, a variety of properties between width w 1 , and width w 2 is possible: e.g., the measured width w 2 of the barrier layer is its drawn width, or the ratio of the measured width w 2 of the barrier layer to the measured width w 1 , of the conductor core is found to be constant.

In general, the I-shape model depends upon the thickness t 2 of the barrier layer and its sheet resistance. The cross-section of a conductor trace used in a field solver is replaced by the cross-section predicted under the I-shape model, based on the properties empirically determined above. Given such an augmented interconnect model and the associated interconnect process parameter values, a field solver can predict the electrical characteristics of the resulting metal cross-section. For example, in a state-of-the-art 0.35 μm manufacturing process using tungsten barrier layers far thinner than the aluminum cores of conductors, the CD loss can first be obtained from an electrical (resistance) measurement in the manner described above. Thereafter, the line-width correction factor thus obtained is applied to the width w 1 of the aluminum core. Since the aluminum core is much more conductive and much thicker than the barrier metal, the width w 1 of the aluminum core then can be used to derive width w 2 of the barrier metal layer, without accounting in the measured electrical characteristic the resistivity of the barrier layer.

Similarly, in determining ILD thicknesses from capacitance measurements on test structures having the comb structures described above, the I-shape model can replace the brick model in field-solver runs used to determine or to check ILD thickness, since the values of the other interconnect process parameters are known. Also, in determining intralayer permittivity from capacitance measurements as described above, this I-shape model can again replace the brick model in field-solver runs used to determine or to check permittivity.

Note that the method for I-shape conductors does not require that conductor traces have exactly I-shaped cross-sections, so long as the cross-section can be determined by such methods as the use of SEM photographs. For example, the metal core need not be centered under the capping layers. Alternatively, two capping layers may have different dimensions. The method also applies to other cross-sectional shapes, e.g., a conductor having a trapezoidal cross-section.

The above detailed description is provided to illustrate specific embodiments of the present invention and is not intended to be limiting. Numerous variations and modifications within the scope of the present invention are possible. The present invention is defined by the following claims.

Claims

1. A method for determining a sheet resistance of an interconnect layer in a process for manufacturing an integrated circuit, said method comprising the steps of:fabricating using said manufacturing process a test structure incorporating a resistive portion from which a resistance is measured, said resistive portion having an effective length and an effective width, said effective length being substantially greater than said effective width and said effective width being selected to be substantially greater than an expected critical dimension loss for said process; measuring said resistance; and deriving from said resistance said sheet resistance.

2. A method as in claim 1, wherein said resistive portion comprises a conductor line having embedded therein dielectric structures for preventing dishing during chemical-mechanical polishing.

3. A method as in claim 2, wherein said dielectric structures comprise rectangular slots.

4. A method as in claim 2, wherein said dielectric structures comprise islands.

5. A method as in claim 2, wherein said test structure is a member of a family of test structures, each test structure in said family of test structures differs from another test structure in said family of test structures by the width of said conductor line.

6. A method for determining a sheet resistance of an interconnect layer in a process for manufacturing an integrated circuit, said method comprising the steps of:fabricating using said manufacturing process a test structure incorporating a resistive portion from which a resistance is measured, said resistive portion having an effective length and an effective width, said effective length being substantially greater than said effective width and said effective width being selected to be substantially greater than a predetermined minimum conductor width of said process; measuring said resistance; and deriving from said resistance said sheet resistance.

7. A method as in claim 6, wherein said resistive portion comprises a conductor line having embedded therein dielectric structures for preventing dishing during chemical-mechanical polishing.

8. A method as in claim 7, wherein said dielectric structures comprise rectangular slots.

9. A method as in claim 7, wherein said dielectric structures comprise islands.

10. A method as in claim 7, wherein said test structure is a member of a family of test structures, each test structure in said family of test structures differs from another test structure in said family of test structures by the width of said conductor line.