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Method for testing analog and mixed-signal circuits using functionally related excitations and functionally related measurements Number:7,129,734 from the United States Patent and Trademark Office (PTO) owispatent

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Title: Method for testing analog and mixed-signal circuits using functionally related excitations and functionally related measurements

Abstract: A method for testing a circuit includes determining at least one performance characteristic of the circuit based on a functional relationship between excitation signals or on a functional relationship between measurement devices. The method is implemented either as a part of a built-in self test circuit of an integrated circuit or for production testing.

Patent Number: 7,129,734 Issued on 10/31/2006 to Geiger,   et al.


Inventors: Geiger; Randall (Boone, IA), Parthasarathy; Kumar (Dallas, TX), Chen; Degang (Ames, IA), Jin; Le (Ames, IA), Kuyel; Turker (Austin, TX)
Assignee: Iowa State University Research Foundation, Inc. (Ames, IA)
Texas Instruments, Inc. (Dallas, TX)
Appl. No.: 10/850,854
Filed: May 21, 2004


Current U.S. Class: 324/765
Current International Class: G01R 31/26 (20060101)


References Cited [Referenced By]

U.S. Patent Documents
5298858 March 1994 Harrison
5606515 February 1997 Mockapetris et al.
6005407 December 1999 Arabi et al.
2005/0057271 March 2005 Olleta et al.

Other References

Jin et al., "A Blind Identification Algorithm for Digital Calibration of Pipelined ADC", IEEE Midwest Symposium on Circuits and Systems, Tulsa, Aug. 2002. cited by other .
Jin et al., "A Blind Identification Approach to Digital Calibration of Analog to Digital Converts for Built-In-Self-Test", IEEE International Symposium on Circuits and Systems, May 2002. cited by other .
Parthasarathy et al., "A Modified Histogram Approach for Accurate Self-Characterization of Analog-to-Digital Converters", Proc. 2002 IEEE International Symposium on Circuits and Systems, Arizona, May 2002. cited by other .
Parthasarathy et al., "Accurate Self Characterization and Correction of A/D Converter Performance", 2001 IEEE Midwest Symposium on Circuits and Systems, Aug. 2001. cited by other .
Parthasarathy K. L., et al., "A histogram based AM-BIST algorithm for adc characterization using imprecise stimulus", the 2002 45th Midwest Symposium on Circuits and Systems, Conference Proceedings, Tulsa OK, Aug. 4-7, 2002, Midwest Symposium on Circuits and Systems, New York, NY, vol. 1 of 3, Aug. 4, 2002, pp. 274-277, XP010635378. cited by other .
Kuyel T., et al., "Optimal analog tri techniques for improving the linearity of pipeline ADCs", Proceedings International Test Conference 2000 (nt. Test Conference, Washington, DC, Oct. 3, 2000, pp. 367-375, XP002300186. cited by other.

Primary Examiner: Hollington; Jermele
Attorney, Agent or Firm: McKee, Voorhees & Sease, P.L.C.

Government Interests



GRANT REFERENCE

Work for this invention was funded in part by a grant from the National Science Foundation Grant No. 0120345. The Government may have certain rights in this invention.
Parent Case Text



PRIORITY STATEMENT

This application claims priority to U.S. Provisional Application No. 60/473,182, filed on May 23, 2003, herein incorporated by reference in its entirety.
Claims



What is claimed is:

1. A method for testing a circuit comprising: applying a first excitation signal to the circuit; applying a second excitation signal to the circuit, the second excitation signal having a first functional relationship with the first excitation signal; measuring outputs from the circuit wit first and second excitations with a first measurement device; measuring output from the circuit with first and second excitations with a second measurement device, the first measurement device having a second functional relationship with the second measurement device; determining at least one performance characteristic of the circuit at least partially based on the first functional relationship and the second functional relationship and the measurement results from the first measurement device and the second measurement device.

2. The method of claim 1 where more than two functionally related excitation signals are used.

3. The method of claim 1 where more than two functionally related measurement devices are used.

4. The method of claim 1 wherein the circuit comprises at least a portion of an ADC device.

5. The method of claim 1 wherein the circuit comprises at least a portion of a DAC device.

6. The method of claim 1 wherein the first functional relationship is defined by a nonlinear signal function having a slope.

7. The method of claim 6 wherein the step of determining includes determining an estimate of the slope of the nonlinear signal function.

8. The method of claim 7 wherein the step of determining further includes correcting the estimate of the slope.

9. The method of claim 1 wherein the step of determining includes correcting for at least one source of error.

10. A method for testing a mixed signal circuit comprising: applying a first analog excitation signal to the circuit; applying a second analog excitation signal to the circuit, the second excitation analog signal having a functional relationship with the first analog excitation signal; monitoring digital output signals from the circuit associated with applying the first analog excitation signal and the second analog excitation signal; determining at least one performance characteristic of the circuit based on the functional relationship and the digital output signals.

11. The method of claim 10 wherein the mixed signal circuit is an analog-to-digital converter.

12. The method of claim 11 wherein the first functional relationship is defined by a nonlinear signal function having a slope.

13. The method of claim 11 wherein the at least one performance characteristic includes an integral non-linearity characteristic.

14. The method of claim 11 wherein the at least one performance characteristic is associated with the conversion mode of the analog-to-digital converter.

15. The method of claim 11 wherein the at least one performance characteristic is associated with the identification and calibration mode of the analog-to-digital converter.

16. The method of claim 15 wherein the at least one performance characteristic includes a transfer characteristic.

17. The method of claim 16 further comprising wherein correction codes are generated during the step of determining.

18. The method of claim 17 further comprising calibrating output of the analog-to-digital converter by adding one of the correction codes.

19. A method for testing a mixed signal circuit comprising: applying digital input signals to the circuit; measuring analog outputs from the circuit associated with applying the digtal input signals with a first measurement device; measuring analog outputs from the circuit associated with arriving the digtal input signals with a second measurement device, the first measurement device having a second functional relationship with the second measurement device; determining at least one performance characteristic of the circuit at least partialLy based on the functional relationship and the measurement results.

20. The method of claim 19 wherein the mixed signal circuit is a digital to analog converter.

21. The method of claim 19 wherein the method is a built-in self-test method.

22. An integrated circuit, comprising: an integrated circuit portion under test; an integrated circuit excitation signal portion for providing at least one pxcitatioft signal to the portion under test; an integrated circuit measurement portion for providing at least one measuremtrlt of at least one output from the portion under test; an integrated circuit performance characteristic determination portion for determining at least one performance characteristic of the portion under test at least partially based on the at least one excitation signal and the at least one measurement and at least one functional relationship.

23. The integrated circuit of claim 22 wherein the functional relationship is an input excitation signal function relating a plurality of excitation signals.

24. The integrated circuit of claim 23 wherein the excitation signal function is nonlinear.

25. The integrated circuit of claim 22 wherein the functional relationship relates a plurality of the at least one measurements.

26. The integrated circuit of claim 22 wherein the performance characteristic portion is operatively connected to the portion under test to provide feedback to the portion under test.
Description



BACKGROUND OF THE INVENTION

The present invention relates to the testing of analog and mixed-signal circuits. More particularly, although not exclusively, the present application relates to the testing of analog and/or mixed-signal circuits in both built in self test (BIST) and production environments.

The use of mixed-signal circuits continues to grow, as does their complexity. At the same time, there is a need for such devices to be of lower cost and to have decreased production time. One significant obstacle in trying to meet these constraints involves the resources required for testing. These resources can include the time it takes to test each device, the costs of testing and measurement equipment, and the availability of testing and measurement equipment. In addition, there is a problem in that the load of the tester may mask or alter the measurements of the device under test.

Therefore, it can be seen that problems with testing analog and/or mixed-signal circuits in both production test and BIST environments remains. Thus, it is a primary object of the invention to improve upon the state of the art.

A further object, feature, or advantage of the present invention is to provide for a method of testing that allows for the production of high performance mixed-signal integrated circuits using low cost components and subcircuits.

A still further object, feature, or advantage of the present invention is to provide for accurate and complete testing of high performance analog and mixed-signal circuits.

Another object, feature, or advantage of the present invention is to provide for accurate testing of analog and mixed-signal circuits suitable for application in a low cost production test environment.

Yet another object, feature, or advantage of the present invention is to provide for testing of analog and mixed-signal circuits suitable for use in built-in self test applications.

Yet another object, feature, or advantage of the present invention is to provide performance enhancement, yield enhancement and/or area reduction by using feedback from a BIST structure to adapt or calibrate the device under test (DUT).

These and/or other objects, features, and advantages of the present invention will become apparent from the subject matter disclosed herein.

SUMMARY OF THE INVENTION

According to one aspect of the invention, a method for testing analog and mixed-signal circuits is disclosed that does not require precise knowledge of the input and measurement system. Instead of requiring precise knowledge of the input and measurement system, functional relationships are exploited to determine performance characteristics of the circuits. Two or more functionally related excitations (FRE) serve as inputs to a device under test (DUT). Measurements are made with two or more functionally related measurement devices (FRM). From the observed outputs, the performance characteristics of interest of the DUT are determined by making appropriate calculations based upon, without limitation, information obtained from the outputs, knowledge about the relationships between the inputs and knowledge about the relationships between the measurements.

Where the circuit is a mixed-signal circuit with digital inputs, such as a digital-to-analog converter (DAC) then the two or more functionally related excitations are not used as the input signal is digital. Where the circuit is a mixed-signal circuit with digital outputs, such as an analog-to-digital converter (ADC), the two or more functionally related measurement devices are not used because the output is digital.

According to another aspect of the invention, an analog or mixed-signal circuit is provided having FRE and/or FRM structures for implementing a BIST. Because precise knowledge about the excitations and the measurement system is not needed, the die area for implementing the excitation and measurement systems can be made smaller with only modest performance requirements.

According to another aspect of the invention, a circuit having a BIST is used to evaluate and enhance the performance and/or yield of analog and mixed-signal circuits after fabrication. The performance of the chip is measured and a feedback loop is provided to adapt (tune) the circuit to meet target specifications.

According to another aspect of the invention, the FRE/FRM approach is used in the circuit design process for debugging designs and for designing new architectures with FRE/FRM capability in a feedback control loop for self adaptation.

According to another aspect of the present invention, a method is provided to prevent noise associated with one excitation or measurement from corrupting and/or interfering with other excitation(s) and/or measurement(s) in the FRE/FRM approach.

According to another aspect of the present invention, a method of arranging multiple excitations or measurements in time or location is provided to reduce the sensitivity of the test procedure to nonstationarity of the test environment.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 provides an overview of one embodiment of the methodology of the present invention.

FIG. 2 provides a block diagram of one embodiment of an integrated circuit having BIST.

FIG. 3 is a block diagram illustrating one embodiment of imprecise stimuli and/or imprecise measurement provides for measurement of characteristics of a device under test according to one embodiment of the present invention.

FIG. 4 illustrates one embodiment of an ADC with digital calibration according to one embodiment of the present invention.

DETAILED DESCRIPTION OF EXEMPLARY EMBODIMENTS

The present invention includes a method of testing analog and mixed-signal circuits in which precise knowledge of the input and measurement system is not needed. With this approach, two or more functionally related excitations (FRE) serve as inputs to a device under test (DUT). Measurements are made with two or more functionally related measurement devices (FRM). From the observed outputs, the performance characteristics of interest of the DUT are determined by making appropriate calculations based upon, without limitation, information obtained from the outputs, knowledge about the relationships between the inputs, knowledge about the relationships between the measurements and information about the characteristics of the excitations and measurement systems. The FRE/FRM approach is applicable to either production test or built in self-test (BIST) implementations. Since precise knowledge about the excitations and the measurement system are not needed, the cost and complexity of the excitation and measurement systems can be reduced in a production test environment and the die area for implementing the excitation and measurements system can be made small with modest performance requirements in BIST environments. In a BIST implementation, the FRE/FRM approach can be used to evaluate and enhance the performance of analog and mixed-signal circuits after fabrication. In a design process, the FRE/FRM approach can be used for debugging designs and for designing new architectures with FRE/FRM capability in a feedback control loop for self adaptation.

FIG. 1 provides an overview of the methodology according to one embodiment of the present invention. In FIG. 1, a first excitation signal is applied to a DUT in step 100 and a second excitation signal is applied to a DUT in step 101. The present invention contemplates that the DUT is an integrated circuit or a portion of an integrated circuit. In steps 102 and 103, the outputs of the DUT from steps 100 and 101 are measured with the first measurement device. In steps 106 and 107, the outputs of the DUT from steps 104 and 105 are measured with the second measurement device. In step 108, performance characteristics of the DUT are determined at least partially based on one or more relationships between the excitation signals and/or one or more relationships between the measured outputs. Because the relationships are used, the precision associated with the excitation signals and/or measurement devices is of less importance.

FIG. 2 illustrates a block diagram of one embodiment of the present invention where an integrated circuit is adapted with FRE/FRM used for built-in self test. In FIG. 2, an integrated circuit 200 is shown. The integrated circuit includes a portion or subcircuit 202 that is to be tested. A FRE signal(s) portion 204 of the integrated circuit 200 is used to generate one or more excitation signals that are applied to the under test portion 202 of the integrated circuit 200. A FRM measurement portion 206 of the circuit is operatively connected to the under test portion 202 of the integrated circuit 200 for measuring the effect of an excitation signal generated by excitation signal(s) portion 204 on the under test portion 202. The measurement portion 206 can include one or more measurement devices. The performance determination portion 208 uses the relationships between excitation signals and/or relationships between measurement devices to determine information related to the performance characteristics of the device under test portion 202. The present invention allows for the information determined by the performance determination portion 208 to be output via a feedback connection 210 to the portion of the device under test 202 to adjust or tune the circuit. The test results can also be output to the device periphery. The FRE and/or FRM structures allow for performance determination without the need for precise knowledge about the excitations and the measurement system. Because precise knowledge about the excitations and the measurement system is not needed, the die area for implementing the excitation and measurement systems can be made small with only modest performance requirements.

Special cases of this approach are systems where the output is inherently digital in which case no measurement system is needed or where the input is inherently digital in which case no analog excitation is required. Analog to Digital Converters (ADCs) are an example of systems where the output is inherently digital and Digital to Analog Converters (DACs) are an example of a system where the input is inherently digital. Other special cases of this approach include those where precise inputs are available and functionally related measurements are made or where precise measurement systems are available and functionally related excitations are used.

In one embodiment of the present invention, the methodology of the present invention is used to test ADCs. This approach can be appropriately termed testing of ADCs with FRE. With the FRE approach to testing ADCs, two or more excitations are applied to the input of the ADC under test (DUT) and the corresponding outputs are observed. From the observed outputs, the performance characteristics of interest of the ADC are inferred by making appropriate calculations based upon information obtained from the outputs and knowledge about the relationships between the inputs. These calculations are based upon a mathematical formulation of the FRE test procedure and the sequence of calculations are termed FRE algorithms. In contrast to most existing approaches to testing of ADCs which depend upon making calculations based upon the observed output and precise knowledge of the input waveform or waveforms, the FRE approach does not require precisely knowing the input waveform or waveforms. The inherent advantage of this approach is that very imprecise excitations which can be readily and inexpensively generated can be used for ADC testing. The FRE approach offers potential for reducing the cost of production testing if FRE algorithms that provide good correlation between inferred ADC performance and actual ADC performance are used and if the costs of implementing these algorithms are sufficiently low. The FRE approach also offers potential for partially or fully built in self test (BIST) in which some or all of the FRE excitations and some or all of the FRE algorithms are implemented on a chip or in a system. With the FRE approach, the relationship between the excitations may be precisely known, or the relationship between the excitations may be only approximately known, or the relationship between the excitations may have a known form but with unknown parameters. Many different excitations can be used to implement the FRE and for a given pair or set of excitations, many different FRE algorithms can be used to infer how the DUT is performing.

According to one embodiment of the present invention, Slope Error Compensated Histogram (SECH) methods are used as the FRE algorithms. According to a second embodiment, Stimulus Error Identification and Removal (SEIR) methods are used as the FRE algorithms. Examples showing both types of algorithms are provided. In the SECH methods, an estimated slope of a nonlinear input signal function is required as a part of a histogram method and the error in this estimate is corrected if need be. The type of slope estimation selected can also be used to reduce errors.

In the SEIR methods, potential sources of error, such as the effect of additive noise, the effect of quantization error in transition time, the effect of the shift between two signals and others, or other sources of error are identified and analyzed so the proper adjustments can be made to reduce or remove error.

1. Example for ADC Testing with Low Accuracy Stimuli Using a Slope Error Compensated Histogram (SECH) Method

In this embodiment a method of testing ADCs is described that uses a SECH methodology for ADC testing with low accuracy stimuli and imprecise measurements. Familiarity with traditional ADC linearity testing is assumed. This embodiment illustrates the use of both FRE and FRM. A method and system for testing is shown in FIG. 3. In contrast to the standard test flow where a precise input stimulus is used and a precise measurement is taken, this alternative method and system for testing uses multiple imprecise excitations and correspondingly has multiple imprecise measurements.

As shown in FIG. 3, it is assumed that there are k imprecise stimuli presented to the DUT and there are h imprecise measurements. If all h imprecise measurements are made for each imprecise excitation, a set of input and output test vectors are obtained for each stimulus-measurement combination. Mathematically, the resultant family of test vectors can be expressed as X.sub.OUT(i,j)=M.sub.i(U(F.sub.j(X.sub.IN(i,j))))+N(X.sub.IN(i,j)) for 1.ltoreq.i.ltoreq.h, 1.ltoreq.j.ltoreq.k (1)

The immediate question that needs to be addressed is whether sufficient information exists in the resultant family of test vectors to uniquely determine U. The answer to this question depends strongly on the nature of the sequences of stimulus and measurement functions. According to this embodiment, sufficient information does exist for testing ADCs with one class of imprecise stimuli. There are many other classes of stimulus and measurement functions that will provide sufficient information to uniquely determine U as well. The present invention is in no way limited to the particular classes of stimulus and measurement functions described herein. Preferably, however, the classes of stimulus and measurement functions are selected such that a manageable number of measurements arithmetic manipulations are used.

This embodiment shows how imprecise stimuli can be used to test ADCs. A detailed mathematical explanation is provided. The performance of this embodiment is supported by computer simulations and measured results obtained from a production test environment. The ADC example shows that both the number of measurements and the number of arithmetic manipulations needed are manageable. The present invention is in no way limited to this particular embodiment as the present invention contemplates other approaches of characterization of analog or mixed signal circuits. Instead of generating a very precise ramp signal, the ADC is characterized with multiple imprecise inputs. In particular, two input signals V.sub.IN.sup.1 and V.sub.IN.sup.2 that can be imprecise are used. The two signals can be highly nonlinear; the algorithm exploits the relationship between the two signals while estimating the INL and DNL of an ADC without being affected by input-introduced errors.

Consider the testing of an ADC with imprecise stimulus signals. In this exemplary algorithm, two nonlinear ramp signals are used, with the second being a constant-shifted version of the first. The input signal is assumed to be a strictly increasing function of time and the speed at which the signal increase does not change dramatically. Furthermore, we assume that the signal generator is short-time stationary, meaning that if the same signal is regenerated within a short time period, the regenerated signal should be very close to the original signal, with the maximum difference much smaller than 1 LSB. Except for these reasonable and easy-to-satisfy conditions, the stimulus signals are allowed to be imprecise. The signal could have a significant error from what it is supposed to be, an ideal ramp in this case. Furthermore, the error is unknown to the design engineers or test engineers. It is uncertain in the sense that it is process and environment dependent. This significantly relaxes the requirement on the signal generator so that it can be easily implemented with low cost or on chip.

FIG. 4 is used to illustrate the basic idea of the algorithm used in this embodiment of the present invention. The vertical axis is marked with the actual and the end-point fit-line transition points of the ADC, respectively. The two nonlinear curves represent the two ramp-like signals. Mathematically, the two nonlinear signals can be described by V.sub.IN.sup.1=f(t) (2) V.sub.IN.sup.2=f(t)-.alpha. (3) where .alpha. is the constant shift between the two signals. The tallies of codes obtained when V.sub.IN.sup.1 and V.sub.IN.sup.2 are presented as the ADC input signals are C.sub.k.sup.1 and C.sub.k.sup.2, respectively. The amount of shift between the two signals is unknown and not measurable externally and need to be estimated as an additional variable. Assuming the signals are sampled uniformly with a sampling period T.sub.SAMP, the time index when the value of the signal V.sub.IN.sup.1(V.sub.IN.sup.2) crosses transition level T.sub.k (indicating that the value of the input signal equals the value of the particular transition voltage of the ADC), measured in units of sampling period T.sub.SAMP, is .SIGMA.C.sub.k.sup.2(.SIGMA.C.sub.k.sup.2). And this relationship is subject to time quantization errors. That is

.PSI..apprxeq..function..times..times..PSI..apprxeq..function..times..alph- a..times. ##EQU00001##

To simplify the analysis, we will consider the system to be noiseless. The effects of noise and errors will be discussed later. Subtracting the (k-1).sup.th equation in (5) from the k.sup.th equation in (4) yields:

.PSI..PSI..function..times..function..times..alpha..times..times. ##EQU00002##

Expressions in the equation above are given in LSB. The 1 in front of the equation means 1 LSB. On the left hand side of (6) is the code width T.sub.k-T.sub.k-1 corresponding to code D.sub.k. On the right hand side is the code width expressed as a function of the summation of tallies. The difference between the first two terms on the right hand side of (6) can be written as

.function..times..function..times.'.function..xi..times..times..times..tim- es..times. ##EQU00003## where f'(.xi..sub.k) is an unknown variable, because the exact function form of the input signal is unknown. Though we use the notation of derivative in the expression, its physical meaning is simply the slope of a section of the nonlinear function f(t) between f(t)=T.sub.k and f(t)=T.sub.k-1+.alpha..

There are different ways to approximate the slope and the present invention contemplates that where slope approximation is used, any of a numbers of different ways can be used. In one embodiment, a simple approximation for slope is provided by averaging the slopes of V.sub.IN.sup.1 and V.sub.IN.sup.2 over the interval between T.sub.k-1 and T.sub.k as shown in equation (8):

.function..xi..apprxeq..times..PSI..PSI..PSI..PSI..times..times. ##EQU00004##

If the nonlinearity in the input has a form of a second order polynomial, the approximation in equation (8) is actually exact. The effects of the slope approximation will be further discussed later. Substituting (7) and (8) into equation (6) and rearranging lead us to

.alpha..gamma..PSI..PSI..times..times. ##EQU00005## where

.gamma..times..times..times..times. ##EQU00006## Equation (9) is a set of linear equations with respect to unknown variables .alpha. and .PSI..sub.k, k=1,2, . . . , N-3. Many standard mathematical methods can solve this type of equation set. Some of them have a computational complexity proportional to (N-2).sup.3. For high resolution ADCs, N is very large and these methods will take a prohibitively long time to get the results. We propose a method with a computational complexity only proportional to N-2. Notice that by adding all equations in (9), the -.PSI..sub.k term of one equation will cancel the .PSI..sub.k term of the next equation and we have

.alpha..times..times..gamma..PSI..PSI. ##EQU00007## Using the fact .PSI..sub.0=.PSI..sub.N-2=0, we get an estimation of the shift between the two stimuli

.alpha..times..gamma. ##EQU00008##

Substituting the value of .alpha. into equation (9), we can estimate the integral nonlinearity of the ADC as

.PSI..times..gamma..times..alpha..times..times. ##EQU00009##

Based on the estimated value of integral nonlinearity, we can calculate the differential nonlinearity of the ADC as

.DELTA..alpha..gamma..times..times. ##EQU00010##

From the integral nonlinearity and the differential nonlinearity, both the INL and DNL parameters are calculated as:

.times..PSI..times..times..times..times..times..DELTA. ##EQU00011## 1.1 The ADC Identification Algorithm Using Low Accuracy Stimuli

The method discussed above can be summarized as an algorithm with the following steps. 1. Use a signal V.sub.IN.sup.1 to excite the ADC under test and collect the histogram {C.sub.k.sup.1, k=0,1, . . . , N-1} 2. Regenerate the signal V.sub.IN.sup.1 but shift it down by a constant voltage .alpha. to obtain V.sub.IN.sup.2. 3. Use the signal V.sub.IN.sup.2 to excite the ADC under test and collect the histogram {C.sub.k.sup.2, k=0,1, . . . , N-1} 4. Calculate

.gamma..times..times..times..times..times..times..times..times..times. ##EQU00012## 5. Calculate

.alpha..times..times..gamma. ##EQU00013## 6. Calculate

.PSI..times..times..gamma..times..alpha..times. ##EQU00014## 7. Calculate

.DELTA..times..alpha..gamma..times. ##EQU00015## 8.

.times..PSI..times..times..times..times..times..DELTA. ##EQU00016##

The input signals can be generated very fast. It is not necessary to wait until the stimulus settles because they are not required to be linear. So test time of an ADC can be dramatically reduced. The histogram data collection in step 1 and 3 is the same as that for the traditional ADC linearity test. The voltage shift in step 2 is simply an analog addition and can be realized in hardware. Steps 4, 5 and 6 can be done by either a computer or through on-chip DSP functionality. The performance of these steps does not add significant processing time to test.

1.2 Performance Analysis

This embodiment of an algorithm has the capability to test an ADC using low accuracy input signals and estimate the integral and differential nonlinearities of the ADC to higher accuracy than that of the stimuli, which is inherently not doable for the traditional histogram method. Therefore, this algorithm of the present invention has wider applications for low cost production test and mixed signal BIST, where high accuracy input signals are too expensive to build or too challenging to design.

Comparison of algorithm with traditional histogram method

The traditional histogram method will directly transform the nonlinear error in input signals into the error in estimation of integral and differential nonlinearities. To estimate the INL and DNL of an ADC to accuracy of 0.1 LSB, the input signal must be a decade more linear than the ADC so that the input nonlinearity is less than 0.1 LSB. This is the common knowledge that to test an n-bit ADC, the input signal should be more than (n+3)-bit linear. Furthermore, because of noise errors, even with an (n+3)-bit linear input, accuracy of 0.1 LSB is usually not achievable. Including the noise effect, a reasonable error bound for ADC production test in the industry is half LSB. This embodiment of an algorithm of the present invention can eliminate the effect of the huge input nonlinearity and estimate the INL to an error less than 0.8 LSB as further discussed herein. This embodiment of an algorithm of the present invention can do the INL and DNL test for an n-bit ADC by using only (n-7)-bit linear signals and has the performance comparable to that of the traditional histogram method which requires (n+3)-bit linear input signals.

1.2.1 Effects of Slope Approximation

Two major factors contribute to the error in the proposed algorithm. The first is the error of associated with the slope approximation using the average in equation (8). The second is the error in C.sub.k.sup.1 and C.sub.k.sup.2. We will talk about each of them as follows.

In the algorithm used in this embodiment of the present invention, we were required to estimate the slope of the nonlinear input function over the interval between .SIGMA.C.sub.k.sup.1 and .SIGMA.C.sub.k.sup.2. This slope strongly depends on the nature of the unknown nonlinear input signal function. There are many ways to do the estimation and without the knowledge of the input, no one method can be said to be more accurate than the other. Therefore we use the average of slopes at two end-points of the interval, .SIGMA.C.sub.k.sup.1 and .SIGMA.C.sub.k.sup.2, to approximate the required slope factor in equation (8). Although not very precise, this approximation gives us a simple calculation towards INL estimation. If the nonlinear function representing the input is a second order polynomial, then the above estimate gives the exact value of the slope. Let's assume that the input is of the general form given by f(t)=at.sup.2+bt (14) The slope of the input signal over the interval between t.sub.1 and t.sub.2 is given by

.function..function..times..function. ##EQU00017## On the other hand, if we derivatives t.sub.1 and t.sub.2 and obtain their average, we will have

'.function.'.function..times..times..function. ##EQU00018##

We can see that the slope and the average are exactly the same. This corroborates the fact that if the nonlinear input is mainly in the shape of a second order polynomial, our slope approximation will not introduce major errors in INL and DNL parameter estimation.

In reality, the input can have various shapes different from a second order polynomial. But our slope approximation is still accurate under most of the situations, such as that the slope of the nonlinear function changes slowly, or that the length of the interval is small, i.e., a small shift between two signals, etc. The effectiveness of the simple average slope approximation will be verified by both simulation and experimental results in the next section.

1.2.2 Error in Histogram Measurement

The histogram data, C.sub.k.sup.1 and Ck.sub.k.sup.2, are mainly affected by the additive noise at the input of the ADC. Let us assume that the additive noise is stationary with mean 0 and variance .sigma..sup.2. The noise may result in a different output code than the expected value and larger variance makes the code more likely to be different from its expected value. For instance, if we consider the accumulated histogram, .SIGMA.C.sub.k.sup.1, which is the number of codes less than or equal to code k. In the traditional histogram method, this number is the estimated value of the k.sup.th transition point except for a constant scaling factor. In the proposed algorithm also, this number gives the first order approximation of the k.sup.th transition point. But any error in this number will translate into an error in the integral nonlinearity estimation and finally into an error in INL and DNL estimation. However, since there are many samples for each code, an addition or subtraction of one or two samples will not have a significant effect on the total number of samples for a code. Intuitively, the variance of .SIGMA.C.sub.k.sup.1 may increase as the variance of the additive noise increases. With detailed statistic analysis, we can show that the following relationship is true.

.sigma..times..times..times..sigma. ##EQU00019## where N.sub.S is the average sample density. The subscript N signifies that the variance of .SIGMA.C.sub.k.sup.1 is due to additive noise. Equation (17) states that the variance of the accumulated histogram is proportional to the standard deviation of the additive noise, where B.sub.1 is a coefficient dependent on the distribution of the noise. When the noise becomes large, the uncertainty in the accumulated histogram data will also increase, but at a speed slower than that of the noise. This implies that the error in INL and DNL estimation will not increase as fast as the noise. The time domain quantization errors have effects on the accumulated histogram and the final INL and DNL estimation. The quantization effect is closely related to the average number of samples per code. With more samples, the quantization error will be small and the accumulated histogram can accurately characterize the transition points. Since the quantization error is distributed between 0 and 1/N.sub.S, we have

.sigma..times..times. ##EQU00020##

The subscript Q signifies that this part is due to the time domain quantization effect. B.sub.2 is a coefficient dependent on the distribution of the quantization error. From the expression above we can see that increasing the number of samples can significantly reduce the quantization error in accumulated histogram and give out better estimation for INL and DNL. The total estimation error will be due to the combined effect of the quantization errors and additive noise.

1.3 Simulation and Experimental Results

Simulations and experiments are done to verify the performance of the proposed algorithm. Simulation results show that the algorithm can estimate the integral and differential nonlinearities for a 12-bit ADC to 12-bit accuracy by using input signals of only 7-bit linearity and the performance of the algorithm is in agreement to theoretical analyses. In experiments, the integral and differential nonlinearities of 10-bit ADCs are estimated to more than 9-bit accuracy by using 2-bit linear signals.

1.3.1 Simulation Results

Simulations were run under different combinations of parameters such as noise variance, the resolution of ADCs, the number of samples per code, etc. The nonlinear input signal used in the simulation is given by f(t)=t+0.04.times.(t.sup.2-t).sub.--0.02.times.(t.sup.3-1.5t.sup.2+0.5t) (19)

It has second order and higher order polynomial nonlinear terms with linearity less than 7 bits. Although in reality we can easily generate much better input signals a highly nonlinear input was used in our simulations to confirm the rigidity of the algorithm. Simulation results were obtained for a 12-bit ADC. The average number of samples per bin was chosen to be 32 (N.sub.S=32) and .sigma.=0.8 in simulation. It was observed that the actual integral nonlinearity of the ADC is between +6 and -4 LSB. Stimulation confirmed the nonlinearity of the device as predicted using the proposed algorithm with a 7-bit linear input signal. The difference between the actual nonlinearity values and estimated nonlinearity values is between +1 and -0.8 LSB. It can be observed that using the newly proposed algorithm, a 12-bit device can be characterized to within +/-1 LSB with an input signal which is just 7-bit accurate. The traditional algorithm identifies the device to have 45 LSB INL. This magnitude of error is observed because the conventional histogram approach assumes that the input is a highly linear ramp, and any nonlinearity in input is wrongly interpreted as errors in the ADC. The proposed algorithm is not affected by this nonlinearity in the input. The performance of the proposed algorithm under different noise and samples/bin were also simulated on a 10-bit ADC. The results are summarized in Table 1. The actual integral nonlinearity of the software modeled 10-bit ADC is between +3 and -2 LSB. The proposed algorithm was then used to identify the device and for each combination of noise and samples/bin, the algorithm was run 32 times to compute the variance.

TABLE-US-00001 TABLE 1 Variance of the error in INL estimation vs. .sigma. and N.sub.s N.sub.s .sigma. N.sub.s = 16 N.sub.s = 32 N.sub.s = 64 .sigma. = 0.2 0.2458 0.0773 0.0324 .sigma. = 0.4 0.7265 0.2036 0.0804 .sigma. = 0.8 1.5633 0.4806 0.1813 .sigma. = 1.6 2.4974 0.9912 0.3505

From the result we can see that the error in INL estimation is affected by both the noise effects and quantization effects as discussed in section IV. By choosing appropriate sample density, we can estimate the INL of an ADC to a reasonable accuracy, e.g., less than 0.5 LSB, even under large noise variance.

1.3.2. Experimental Results

Simulation shows that the proposed algorithm can test INL and DNL for high resolution, 12-bit or above, ADCs to accuracy that is better than 1 LSB. In experiment, 10-bit commercial pipelined ADCs were tested to prove the effectiveness of the algorithm. Though test for 10-bit ADCs is a known art, an input of 13 bit or higher linearity is always required. We are going to show the test result for a 10-bit ADC by using signals that are less than 3-bit linear. If the traditional method was used, it would be very unlikely to accurately identify the INL and DNL of a 10-bit ADC by using a 3-bit linear signal. There. might be errors of hundreds of LSBs. By using the proposed algorithm we will see that the INL and DNL of 10-bit ADCs can be estimated to accuracy of better than 0.3 LSB in experiment. This result is as good as the result for a traditional histogram method by using a 13-bit signal.

A commercially available ADC was tested to estimate the effectiveness of the algorithm. Different ADCs and raw data were obtained. The entire testing was performed in a production test environment. As a first attempt, a commercial tester used in production testing was used to generate the input signals and collect the output histograms. The tester was programmed to generate input signals with only 2 3 bit linearity (much more nonlinear than what was used in software simulations reported above). Although signals of much better linearity can be generated on-chip, to confirm the robustness of the algorithm and to consider the case of high resolution ADCs (14 bit and above) where 8 9 bit linear input signals are limiting factor, the input signals used in the test runs were intentionally limited to a low linearity. The second signal was obtained by subtracting a DC shift value of about 10 LSB from the first signal. This amount of shift and the exact nature of the input signal were unknown to the algorithm. These values were independently computed as part of the algorithm. Results of INL estimation using the proposed algorithm with the above described highly nonlinear input signals were then compared to the results calculated from using the traditional histogram algorithm with a highly linear ramp signal. The signals were sampled at 32 samples per code on average.

To start with, the results using the highly linear signal and the traditional histogram method were considered to be the true nonlinearity of the ADC. The difference between the results using the proposed algorithm and the traditional method is then the residual error of the new algorithm. The algorithm is able to identify the nonlinearity of the device to within 0.7 LSB using an input signals that is just 2 bit linear. The experiments were then repeated on 20 different ADCs. The same input signal with nearly 2 bit linearity was used to test all the devices. The amount by which the second nonlinear signal was shifted with respect to the first was nearly 10 LSB for all devices.

The parts can be identified to accuracy of 1 LSB using the new algorithm. Further, to see the effect of noise, one part was randomly picked again, and a highly linear ramp and traditional histogram test was performed on the same device twice; and the INL predicted using the two linear ramp data were compared. Ideally we would expect the INL prediction to be same, since they represent the same device. But a maximum error of 0.7 LSB was found between the two runs.

Thus even with a highly linear ramp and the traditional test approach, we get a marginal difference between repeated runs on the same device, indicating that noise in measurement is a major limiting factor in the identification of the device performance, and places a lower bound on the estimation accuracy. Given this effect of noise in measurement, due to factors like temperature and time related drift, the above errors in estimation using the proposed algorithm is very reasonable.

1.4 Conclusions Regarding SECH Embodiment

This embodiment illustrates one example of a new invention for analog and mixed-signal circuit test Unlike traditional approaches that require precise, linear and stationary input stimuli and measurement, the methodology of the present invention can work with imprecise and nonlinear stimuli and measurements. To identify the performance of a DUT, post-processing of data acquired from imprecise stimuli and measurements is required. This methodology includes an algorithm for ADC linearity test using nonlinear stimuli. As described in this embodiment, the ADC's INL and DNL parameters can be accurately estimated by using input signals with much lower linearity. Simulation and experimental results show that this algorithm can identify the INL of 10-bit or high resolution ADCs to sub LSB accuracy by using stimuli of less than 7-bit linearity, only 2 bit linearity in the experiment. This methodology can be used for built-in self-test and low cost production test.

2. Stimulus Error Identification and Removal (SEIR) Method

This embodiment of the present invention is demonstrated in the context of an ADC linearity test. The present invention is not limited to this embodiment, and contemplates numerous methods for using FRE and/or FRM. For purposes of this example, knowledge of conventional methodology of testing ADC linearity is assumed.

In conventional methodology, the input nonlinearity is calculated in a manner that includes nonlinearities from different sources coupled to each other which cannot be identified at the same time. In the algorithm of this embodiment of the present invention, two analog input signals will be used, and the nonlinearity in the input and INL of an ADC will be separated first and then identified. The second signal is simply a shifted replica of the first input signal with a shift voltage .alpha.. Such a shift could easily be obtained in hardware by an analog summing circuit. x.sub.1(t)=T.sub.0+(T.sub.N-2-T.sub.0)t+F(t) (20) x.sub.2(t)=T.sub.0+(T.sub.N-2-T.sub.0)t+F(t)-.alpha. (21) Transition time for the two signals is defined by following equations T.sub.i=x.sub.1(t.sub.i.sup.(1)) (22) T.sub.i=x.sub.2(t.sub.i.sup.(2)) (23) Equations 22 and 23 are key to understand the logic behind our new method. Any non-linear (or linear) input maps the transition points of the ADC onto the time axis represented by histogram counts. The same ADC transition points can be mapped onto time axis with different histogram counts, using a different input.

Notice that this allows the ADC nonlinearity to be left at one side of the equation. If {C.sub.i.sup.(1), i=0,1, . . . , N-1} and {C.sub.i.sup.(2), i=0,1, . . . , N -1} are histogram data collected by using x.sub.1 and x.sub.2, respectively, estimates of transition time can be expressed in following equation. Therefore, the non-uniform sampling pattern on the normalized time axis (corresponding to ADC transitions projected through each nonlinear input) is given by:

.times..times..times..times. ##EQU00021## where time is shifted and scaled with respect to the first signal, with origin at C.sub.0.sup.(1) and unit time at C.sub.N-2.sup.(1). We can now have the estimate of INL formulated using each input signal and corresponding histogram counts.

.times..times..times..times..times..function..times..times..times..times..- times..times..times..function..alpha..times..times..times..times..ltoreq. ##EQU00022## Notice that instead of the nonlinearity only being parameterized on the interval [0, 1,] as in the traditional method, in (25) some transition time of the second input will be larger than 1. For that part of transition time, parameters are not well defined by the traditional method, so those corresponding equations are excluded from (27). Roughly speaking the last .alpha. (in LSB) equations in (27) will have transition time larger than 1, so the total number of equations will be N-3-.alpha.. We will see for a reasonable shift value this reduction in number of equations will not affect the performance of the new method and discuss it effects later.

Equations (26) and (27) constitute the body of our method. The left hand side of the equations (ADC's trip points) will cancel when two equations are subtracted from each other and the input nonlinearity will be left alone in a parameterized form. Moreover, there will be more equations than parameters, so the system can be solved using a standard parameter estimation method. Regardless of the difference between two estimates of a same INL, we still have N+M-3 unknowns, N-3 INL and M a.sub.j parameters. But this time we have two input signals and a nearly doubled number of 2(N-3)-.alpha. equations with small shift. This makes the identification of the unknowns possible. Equating the right hand side of (26) and (27), we have

.times..times..times..function..times..times..times..function..alpha. ##EQU00023##

We can see that there is only the nonlinearity in the input signal and no INL of the ADC in the equation above. Move the linear terms of transition time to one side and nonlinear and shift terms to the other side, we have

.times..times..times..times..times..times..function..function..times..alph- a..times..times..times..ltoreq. ##EQU00024##

There are roughly N-3-.alpha. linear equations for M unknown parameters a.sub.j. If the number of codes is much larger than the number of basis functions and the shift, parameters are over constrained by (29) and can be estimated by using the least mean squares (LMS) method. The LMS method has a beneficial property that if there is any noise or errors in equation (29), their effects will be partially or totally averaged out by the LMS method. Naming estimated values of the parameters to be a.sub.j, j=1,2, . . . , M and substituting them into either equation (26) or (27) or their combination, we can estimate INL of the ADC. Using (26) for example, we will have

.times..times..times..times..times..function..times..times. ##EQU00025## 2.1 Error Analysis

There are several sources of errors that will affect the performance of the algorithm. Among them the additive noise in the signal, the non-parameterized error of the signal, and the quantization error of transition time as in equation may have the most significant effects on the INL test results obtained by our method. Using the first signal as an example, with noise and errors the relationship between transition points and the estimated transition time can be written as

.times..times..times..function..function..function..times..times..times. ##EQU00026## where e({circumflex over (t)}.sub.i.sup.(1)) is the non-parameterized error, n({circumflex over (t)}.sub.i.sup.(1)) is the effect of the additive noise, and d({circumflex over (t)}.sub.i.sup.(1)-t.sub.i.sup.(1)) is the quantization error. We further assume the noise and errors will not affect the LMS estimation of a.sub.j, j=1,2, . . . , M so that they can viewed the same as a.sub.j, j=1,2, . . . , M. This is a fair assumption based on the following reasons. First, the non-parameterized error is orthogonal to the first M sinusoidal functions by definition. Second, the additive noise and quantization error are usually changing very fast as a function of time so that they have little components correlated to low frequency basis functions. Third, the LMS method will also average out the effect of fast changing components in noise and errors. Therefore the difference between the INL calculated in equation (30) and the actual INL is INL.sub.i-I{circumflex over (N)}L.sub.i=e({circumflex over (t)}.sub.i.sup.(1))+n({circumflex over (t)}.sub.i.sup.(1))+d({circumflex over (t)}.sub.i.sup.(1)-t.sub.i.sup.(1)) (32) Each of these terms is discussed separately.

2.1.1 Effects of the Non-Parameterized Error in Input Signals

The magnitude of e({circumflex over (t)}.sub.i.sup.(1)) is dependent on the number of basis functions used in parameterization, M, and on the nonlinearity of the input signal itself. As mentioned earlier, e({circumflex over (t)}.sub.i.sup.(1)) can be reduced to arbitrarily small by increasing M. In reality, we can require the input signal to be stationary and changing slowly. The nonlinearity in the input can be large, but it doesn't change too fast so that we can parameterize it with reasonable number of basis functions to get a small residue error. Higher spatial-frequency nonlinearities can be handled by increasing the number of basis functions.

2.1.2 Effects of the Non-Parameterized Error in Input Signals

Assume the additive noise at the input to an ADC is stationary and Gaussian with variance .sigma..sup.2. The noise may make the output code different from its expected value so that bin counts are affected by it. Larger variance of the noise makes the code more likely to be different from its expectation. However, there are many samples for each code. Change of one or two samples' value will not have a significant effect on the total number of samples for a code. Intuitively, the variance n({circumflex over (t)}.sub.i.sup.(1) may be proportional to the variance of the additive noise and inversely proportionally to the average number of samples per code. With more detailed statistic analysis, we can show that the following general relationship is true.

.sigma..times..times..function..times..times..times..sigma..times..times. ##EQU00027## where N.sub.s is the average number of samples per code. A is a constant dependent on the distribution of the noise. For Gaussian noise, A=0.5642. This sensitivity to noise is also a fundamental problem in conventional histogram based ADC test algorithm.

2.1.3 Effects of the Quantization Error in Transition Time

The quantization error of transition time is bounded. A smaller clock period T.sub.c will produce more samples in total and a larger average number of samples per code N.sub.s. So the quantization error will become smaller. The standard deviation of the quantization error can be expressed in terms of N.sub.s as

.sigma..times..times..times..times..times..times..times..times..times. ##EQU00028##

In equation (34) we assume the quantization error is uniformly distributed. Typically, in an all codes production testing environment, N.sub.s is between 20 to 100 samples per code. The magnitude of the additive noise determines which term of (33) and (34) is more important to the test result. If the standard deviation of the additive noise is comparable to 1 LSB, the quantization error is much smaller than the effect of the noise.

For high resolution ADCs, up to 1 LSB rms noise is typical. That is why we state earlier that the quantization effect of transition time can be neglected. The same quantization error is also an issue in traditional histogram based testing.

2.1.4 Effects of the Shift Between Two Signals and Others

The value of voltage shift a between two input signals also affects the final INL estimation results. If the shift is too small, the difference between the nonlinearity of the two input signals at the same code level will be very small and noise in equation (31) will have significant effects on the LMS method. The assumption that estimated parameters a.sub.j, j=1,2, . . . , M are close to the actual value doesn't hold any more and the numerical behavior of the LMS method is no longer reliable under that situation. The shift can not be too large as well. As mentioned before, the last .alpha. equations in (29) will not be used to estimate the parameters, so the LMS result is only optimal for part of the input nonlinearity and not necessary to be optimal for the nonlinearity on the whole interval of [0, 1]. Analysis shows that 0.1 to 1% shift is appropriate for the proposed method. Both simulation and experimental results support this conclusion. The method estimates the amount of shift, so, no prior knowledge on the amount of shift is assumed.

We assume the two input signals are identical but with a constant shift. This is not true in reality. We always have time varying effects in the test, e.g. the drift of reference voltage. The signal source may change from the first to second run, which will introduce gain error and different nonlinearity between two signals. These non-stationary effects can be eliminated by well designed time interleaving measurement. Two signals are interleaved in time to excite the ADC and collect histogram data. By using "common-centroid" sequence to interchange between the two signals, most of the non-stationary effects are cancelled in experiment.

2.1.5 Simulation Results

Simulation has been done in Matlab, using different combinations of ADC resolution, the average number of samples per code, the nonlinearity of the input, the additive noise, and the voltage shift between two input signals. Simulation results show that the algorithm can accurately identify INL of an ADC of different resolution by using nonlinear excitations under various situations. Results for testing a 14-bit simulated ADC under different noise level and average number of samples are summarized as follows. The first nonlinear input signal is modeled as x.sub.1(t)=(N-2).left brkt-bot.t+0.004*(t.sup.2-t).right brkt-bot.+noise (35)

The maximum nonlinearity specified in (35) is 0.1% of the total input range. The shift between the first and second signals is assumed to be unknown but chosen to be 128 LSBs. 11 sinusoidal basis functions are used in parameterization of the nonlinear term in the input. If the additive noise has a standard deviation of 0.8 LSB and 16 samples are taken for each code on average, the error in INL estimation is less than 1 LSB.

Other results for different combination of the average number of samples per code and noise are summarized in Table 2 for the same ADC.

TABLE-US-00002 TABLE 2 Error in INL estimation for different N.sub.s and .sigma. Shift = 128 LSB, 11 sinusoidal basis functions INL error .sigma. INL error N.sub.s .SIGMA. (LSB) (LSB) N.sub.s (LSB) (LSB) 16 0.8 0.78 16 0.2 0.46 32 0.8 0.54 16 0.4 0.60 64 0.8 0.40 16 0.8 0.78 128 0.8 0.32 16 1.6 1.22

For each of the INL error data in Table 2, four tests are simulated for each set of the same N.sub.s and, and an average value of error are calculated and listed. This allows us to statistically analyze the performance of the proposed algorithm. From Table 2, we can see that if N.sub.s is increased by 4 times, the error in INL estimation is reduced by about 50%; if the standard deviation of the additive noise is increased by 4 times, the error in INL estimation is increased by 2 times. This is totally in agreement with equation (33).

2.2


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