The present invention relates to laser scanning systems. Specifically, it describes methods and techniques for inducing changes in electronic circuits with the scanning laser and then sensing the changes in the dynamic behavior of the circuits. This basic method and technique can be applied to scanning imaging systems that utilize both optical and non-optical sources, e.g. electron beam and acoustic sources.
Cole, et al. (U.S. Pat. Nos. 5,430,305 and 6,078,183) showed that laser beams can be used to induce electrical changes in electronic circuits, specifically integrated circuits. These changes can be induced through heating of circuit components by the laser and through photocarrier generation in the integrated circuit. Laser wavelength with respect to the semiconductor bandgap determines which of the two effects dominates.
The efforts of Cole, et al. focused on sensing the changes in the current draw of the electronic circuit while it was scanned by the laser. Basically, the laser modulates the impedance of the overall circuit, which can be sensed with appropriate impedance sensing means. These techniques, often referred to as LIVA and TIVA, are capable of locating static shorts and opens in circuits. Work in this area was also performed by Nikawa (U.S. Pat. No. 5,804,980) using the terminology OBRICH.
There are additional classes of circuit failures that do not reveal themselves as static failures. For example, time delays or slow rise times in digital circuits can cause timing failures as the operating frequency is increased. Methods for location of dynamic failures were first explored by Burns, et al. (Reliability/Design Assessment by Internal-Node Timing-Margin Analysis Using Laser Photocurrent-Injection, D. J. Burns, M. T. Pronobis, C. A. Eldering, and R. J. Hillman, Proceedings IEEE/IRPS, 76-82 [1984] and U.S. Pat. No. 4,498,587) and later by Bruce, et al. (U.S. Pat. No. 6,483,326). All of these methods are highly related, differences only occurring in choice of laser wavelength for photo carrier creating versus heating as an example. Further, the methods are specific to digital circuitry.
These dynamic techniques are characterized by two processes:
Therefore, there exists a need for techniques for measuring dynamic failures in both analog and digital circuits.
The present invention provides methods and system for sensing dynamic failures in an electronic circuit. An exemplary system includes a drive source, a radiant energy source, and a signal comparator. The drive source supplies a dynamic input signal to the electronic circuit, thereby causing the electronic circuit to output a signal. The radiant energy source generates and directs radiant energy at the electronic circuit and thus induces localized changes in the output signal of the electronic circuit. The signal comparator compares the output signal to an expected output signal, thereby producing a comparison signal proportional to the match between the input and output signals.
In one aspect of the invention, the system may also include a data processing device that generates an image based on the comparison signal and a display device that displays the generated image.
In another aspect of the invention, the system may also include a sensor that produces a reflection signal based on a reflection of the directed radiant energy. The data processing device generates an image based on the reflection signal and the display device displays the reflection signal image. The data processing device extracts one or more portions of the comparison signal image and superimposes the extracted one or more portions on the reflection signal image based on location information associated with the reflection signal image and the comparison signal image.
The comparison signal indicates a measure of quality of the electronic circuit.
The preferred and alternative embodiments of the present invention are described in detail below with reference to the following drawings.
The current invention will first be described as a general signal comparison instrument. Specific examples will follow.
A radiant energy source 4 is utilized to excite the test structure 2. There are many options for the radiant energy source 4, including but not limited to:
The radiant energy source 4 may produce an excitement in the test structure 2 via a number of means, including but not limited to:
A radiant energy beam 6 produced by the radiant energy source 4 is directed towards a scanning device 8. In the case where the beam 6 is an optical radiant energy beam, the scanner device 8 may include a scanning mirror assembly 102 and a lens 104 for focusing the radiant energy beam 6 onto the test structure 2. A control line 106 is also shown. The control line 106 is utilized to synchronize the position of the scanner device 8 with the other data acquisition processes described below. In the case where the beam 6 is an electron or ion beams, the scanning device may include equivalent electromagnetic beam deflectors and focusing elements. The scanning device 8 directs the radiant energy beam 6 on to the test structure 2 and scans the beam 6 across the test structure 2. Any assembly that produces this result is acceptable. Shown in
A drive source 12 supplies a drive signal 14 and a reference signal 15. The drive signal 14 is used as a dynamic operational input to the test structure 2. The drive signal 14 is any modulated signal such as a digital clock, a digital pattern, a sine wave, etc. that is needed to place the test object 2 into a desired dynamic mode and in turn induces the test object 2 to produce a test signal 16. The drive signal 14, the reference signal 15, and the test signal 16 can include single or multiple lines with any combination of digital and analog signals.
The test signal 16 is feed into a signal comparator 18. The reference signal 15 is also shown being feed into the signal comparator 18, however, it is not necessary in all implementations of the current invention. The signal comparator 18 compares the quality of the test signal 16 to a perfect test signal. A comparison signal 20 is the result of the comparison of the test signal 16 with this perfect test signal. The comparison signal 20 is thereby a measurement of the quality of the test signal 16.
Once produced, the comparison signal 20 is sent to a processing and display device 22. For example, the processing and display device 22 may be a general purpose computer and a monitor. The comparison signal 20 is collected as a function of position of the radiant energy beam 6 on the test structure 2 as determined by the control line 106 and then is displayed as an image or map as a function of the position.
In one embodiment, the device 1 is a laser scanning or confocal imaging system and the radiant energy source 4 is a laser. The beam from the laser propagates to the scanning device 8. The scanning device 8 includes a scanning mirror assembly 102 coupled with a focusing lens 104. The laser beam passes through the scanning mirror assembly 102, which deflects the laser beam at an angle versus time. The first lens 104 transforms the angular scan into a position scan on the test structure 2. The first lens 104 also focuses the laser beam onto the test structure 2.
A sufficiently high power laser beam can heat the test structure 2 by 10's to hundreds of degrees centigrade. This temperature rise induces changes in the impedance of components within the test structure 2. When the test structure 2 is a semiconductor device additional impedance changes can occur due to production of photocarriers, however, the laser wavelength must be short compared to the semiconductor band gap for photocarrier production to occur. It is via these impedance changes that the laser beam induces changes in the test signal 18.
An additional feature of the laser scanning embodiment is the ability to collect a reflected light image simultaneously with the thermal-acoustic image through use of a reflected light sensor 200. The radiant energy beam 6, when in the form of a laser beam, is reflected back from the test structure 2 and recollected by the focus lens 104. The reflected beam is redirected by a beam splitter 202 in the sensor 200 towards a detector lens 204, which focuses the reflected beam onto a detector 206. Note that the detector lens 204 is not strictly necessary in all laser-scanning configurations. The detector 206 produces a reflected light signal 208 that is proportional to the amount of the laser beam reflected back from the test structure. The reflected light signal is directed to the processing and display means 22 where an image of the test structure can be displayed. Thus, the reflected light sensor 200 produces a standard confocal image of the test structure 2 that is pixel-by-pixel correlated with the image/map of the comparison signal 20. This confocal image can be used in an overlay process to correlate the location of a specific comparison signal 20 to a physical location on the test structure 2.
The signal comparator 18 can take on a variety of forms, depending on the nature of the test signal 16.
A laser scanning, confocal imaging system as described above was used to supply the remaining components of this embodiment of the invention. As the laser is scanned over the defect that is causing the unwanted time delay, its impedance changes, which causes a change in the phase delay. The time delay is recorded at the laser is scanned, producing a time delay map of the device. An example image/map obtained using this technique is shown in
As can be seen, the basic form of the current invention can be implemented in a wide range of specific forms depending on the specific measures of the quality of the test signal 16 that are of importance to the tester. Examples of measures can be broken down into digital and analog measures as follows.
Digital measures of quality can include but are not limited to
Analog measures of signal quality can include but are not limited to
Each of these measures have a variety of means by which the drive source 12, the drive signal 14, the reference signal 15, the test signal 16, the signal comparator 18 and the comparison signal can be implemented. Procedures for measuring each of the above listed parameters is known by those of ordinary skill in the art.
While the preferred embodiment of the invention has been illustrated and described, as noted above, many changes can be made without departing from the spirit and scope of the invention. Accordingly, the scope of the invention is not limited by the disclosure of the preferred embodiment. Instead, the invention should be determined entirely by reference to the claims that follow.
This is application claims the benefit of U.S. Provisional Application Ser. No. 60/602,802 filed Aug. 18, 2004, which is hereby incorporated by reference.
| Number | Date | Country | |
|---|---|---|---|
| 60602802 | Aug 2004 | US |