Application Note 132 February 2011 Fidelity Testing for A→D Converters Proving Purity Jim Williams and Guy Hoover Introduction The ability to faithfully digitize a sine wave is a sensitive test of high resolution A→D converter fidelity. This test requires a sine wave generator with residual distortion products approaching one part-per-million. Additionally, a computer-based A→D output monitor is necessary to read and display converter output spectral components. Performing this testing at reasonable cost and complexity requires construction of its elements and performance verification prior to use. Overview Figure 1 diagrams the system. A low distortion oscillator drives the A→D via an amplifier. The A→D output interface formats converter output and communicates with the computer which executes the spectral analysis software and displays the resulting data. Oscillator Circuitry The oscillator is the system’s most difficult circuit design aspect. To meaningfully test 18-bit A→Ds, the oscillator must have transcendentally low levels of impurity, and these characteristics must be verified by independent means. Figure 2 is basically an “all inverting” 2kHz Wien bridge design (A1-A2) adapted from work by Winfield Hill of Harvard University. The original designs J-FET gain control is replaced with a LED driven CdS photocell isolator, eliminating J-FET conductivity modulation introduced errors and the trim required to minimize them. Band limited A3 receives A2 output and DC offset bias, providing output via a 2.6 KHz filter which drives the A→D input amplifier. Automatic gain control (AGC) for the A1-A2 oscillator is taken from the circuit output (“AGC sense”) by AC-coupled A4 which feeds rectifier A5-A6. A6’s DC output represents the AC amplitude of the circuit output sine wave. This value is balanced against the LT®1029 reference by current summing resistors which terminate into AGC amplifier A7. A7, driving Q1, closes a gain control loop by setting LED current, and hence CdS cell resistance, to stabilize oscillator output amplitude. Deriving gain control feedback from the circuit’s output maintains output amplitude despite the attenuating band-limiting response of A3 and the output filter. It also places demands on A7 loop closure dynamics. Specifically, A3’s band limiting combines with the output filter, A6’s lag and ripple reduction components in Q1’s base to generate significant phase delay. A 1μF dominant pole at A7 along with an RC zero accommodates the L, LT, LTC, LTM, Linear Technology and the Linear logo are registered trademarks and PScope is a trademark of Linear Technology Corporation. All other trademarks are the property of their respective owners. SOFTWARE 2kHz OSCILLATOR AqD INPUT AMPLIFIER AqD DATA ACQUISITION/ INTERFACE COMPUTER AND DISPLAY AN132 F01 100MHz CLOCK Figure 1. Block Diagram of A→D Spectral Purity Test System. Assuming a Distortionless Oscillator, Computer Displays Fourier Components Due to Amplifier and A→D Infidelities an132f AN132-1 Application Note 132 OSCILLATOR 7.87k 0.01μF 0.1% 0.0068 0.01μF 5pF 7.87k 0.1% 40.2k 0.1% OUTPUT AMP AND FILTER 12k* – 19.1k 909Ω* 0.1% 249Ω A1 LT1468 + – 9.09k* + – 100Ω + A2 LT1468 + 36k 5% 100μF 0.5V 0V + A7 LT1006 100k 28k 4.3k 5% LT1029 5V 10μF + + 4V BIASED ON 0.5V + 470Ω 5% – Q1 2N3904 100Ω 5% ≈2kHz DC OFFSET 15μF 15V 15V 5V 4.5V 47μF 1μF 470Ω 5% ≈2kHz TO AqD AMPLIFIER INPUT 0.47 12k 12k TRIM 100Ω ADJ FOR ≈5V ACROSS HERE 130Ω A3 LT1468 –15V AGC 1μF 10k NO CERAMIC CAPACITORS ANYWHERE. USE MYLAR OR SILVER MICA 10k 5k – 1N4148 A6 LT1122 10k A5 LT1122 + = SILONEX NSL32SR3 10k 1N4148 – A4 LT1122 0.1 AGC SENSE + + 0.01μF = POLYSTYRENE PERFERRED. POLYPROPELENE, PPS ACCEPTABLE. OUTER FOIL TO AMPLIFIER OUTPUT – BYPASS EACH AMPLIFIER WITH 10μF OS-CON 1M AN132 F02 ALL = 1% METAL FILM UNLESS NOTED RECTIFIER * = IRC TYPE CAR-5, 1% 0.1% = IRC TYPE CAR-5 RESELECT 909Ω IN SERIES WITH 100Ω TRIM IF NECESSARY Figure 2. Wien Bridge Oscillator Uses Inverting Amplifiers in Signal Path, Achieves 3ppm Distortion. LED Photocell Replaces Usual J-FET as Gain Control, Eliminating Conductivity Modulation Induced Distortion. A3 Associated Filtering Attenuation is Compensated by Sensing AGC Feedback at Circuit Output. DC Offset Biases Output Into A→D Input Amplifier Range delay, achieving stable loop compensation. This approach replaces closely tuned high order output filters with simple RC roll-offs, minimizing distortion while maintaining output amplitude1. Eliminating oscillator related components from the LED bias is essential to maintaining low distortion. Any such residue will amplitude modulate the oscillator, introducing impure components. The band-limited AGC signal forward path is well filtered and the heavy RC time constant in Q1’s base provides a final, steep roll-off. Figure 3, Q1’s emitter current, shows about 1nA of oscillator related ripple out of a 10mA total, less than 0.1ppm. Note 1. This is loosely akin to forcing food through a meat grinder to produce purée. AN132-2 A = 2V/DIV ON 0.5V DC B = 10nA/DIV ON 10mA DC 30kHz BW HORIZ = 500μs/DIV AN132 F03 Figure 3. Oscillator (Trace A) Related Residue (Trace B), Just Discernible in Q1 Emitter Noise, ≈1nA, About 0.1ppm of LED Current. Characteristic, Deriving From Heavy AGC Signal Path Filtering, Prevents Modulation Products From Influencing Photocell Response an132f Application Note 132 The oscillator achieves its performance using only a single trim. This adjustment, which centers AGC capture range, is set in accordance with the schematic note. Verifying Oscillator Distortion Verifying oscillator distortion necessitates sophisticated measurement techniques. Attempts to measure distortion with a conventional distortion analyzer, even a high grade type, encounter limitations. Figure 4 shows oscillator output (Trace A) and its indicated distortion residuals at the analyzer output (Trace B). Oscillator related activity is faintly outlined in the analyzer noise and uncertainty floor. The HP-339A employed specifies a minimum measurable distortion of 18ppm; this photograph was taken with the instrument indicating 9ppm. This is beyond specification, and highly suspect, because of the pronounced uncertainties introduced when measuring distortion at or near equipment limits2. Specialized analyzers with exquisitely low uncertainty floors are needed to meaningfully measure oscillator distortion. The Audio Precision 2722, specified at a 2.5ppm Total Harmonic Distortion + Noise (THD + N) limit (1.5ppm typical), supplied Figure 5’s data. This figure A = 2V/DIV B = 9ppm INDICATED DISTORTION HORIZ = 200μs/DIV AN132 F04 Figure 4. HP-339A Distortion Analyzer Operating Beyond Its Resolution Limit Provides Misleading Distortion Indication (Trace B). Analyzer Output Contains Uncertain Combination of Oscillator and Instrument Signatures and Cannot Be Relied Upon. Trace A Is Oscillator Output indicates a Total Harmonic Distortion (THD) of –110dB, or about 3ppm. Figure 6, taken with the same instrument, shows THD + N of 105dB, or about 5.8ppm. In Figure 7’s final test, the analyzer determines the oscillator’s spectral components with the third harmonic dominating at –112dB, or about 2.4ppm. These measurements provide confidence in applying the oscillator to A→D fidelity characterization. A→D Testing A→D testing routes oscillator output to the A→D via its input amplifier. The test measures distortion products produced by the input amplifier/A→D combination. A→D output is examined by the computer, which quantitatively indicates spectral error components in Figure 8’s display.3 The display includes time domain information showing the biased sine wave centered into the converter’s operating range, a Fourier transform indicating spectral error components and detailed tabulated readings. The LTC®2379 18-Bit A→D/LT6350 amplifier combination under test produces 2nd harmonic distortion of –111dB, about 2.8ppm, with higher frequency harmonics well below this level. This indicates the A→D and its input amplifier are operating properly and within specifications. Possible harmonic cancellation between the oscillator and amplifier/ A→D mandates testing several amplifier/A→D samples to enhance measurement confidence4. Note 2. Distortion measurements at or near equipment limits are full of unpleasant surprises. See LTC Application Note 43, “Bridge Circuits”, Appendix D, “Understanding Distortion Measurements” by Bruce Hofer of Audio Precision. Note 3. Input amplifier/A→D converter, computer data acquisition and clock boards, necessary for testing, are available from LTC. Software code may be downloaded at www.linear.com. See Appendix A “Tools for A→D Fidelity Testing” for details. Note 4. Review text section, “Verifying Oscillator Distortion” and footnote 2 for relevant commentary. an132f AN132-3 Application Note 132 AN132 F05 Figure 5. Audio Precision 2722 Analyzer Measures Oscillator THD at –110dB, About 3ppm an132f AN132-4 Application Note 132 AN132 F05 Figure 6. AP-2722 Analyzer Measures Oscillator THD + N at ≈ –105dB, About 5.8ppm an132f AN132-5 Application Note 132 AN132 F07 Figure 7. AP-2722 Spectral Output Indicates 3rd Harmonic Peak at –112.5dB, ≈2.4ppm Figure 8. Figure 1’s Test System Partial Display Includes Time Domain Information, Fourier Spectral Plot and Detailed Tabular Readings for LTC2379 18-Bit A→D Driven by LT6350 Amplifier AN132 F08 an132f AN132-6 Application Note 132 APPENDIX A Tools for A→D Fidelity Testing Circuit boards for implementing the text’s A→D testing are available. Table 1 lists the board functions and their part numbers. The computer software, PScope™, is also available from Linear Technology and may be downloaded at www.linear.com. Table 1 BOARD FUNCTION PART NUMBER LT6350/LTC1279 Amp/A→D DC-1783A-E Interface DC718 100MHz Clock* DC1216A-A Oscillator To Be Released *Any stable, low phase noise 3.3V clock capable of driving 50Ω may be used. an132f Information furnished by Linear Technology Corporation is believed to be accurate and reliable. However, no responsibility is assumed for its use. Linear Technology Corporation makes no representation that the interconnection of its circuits as described herein will not infringe on existing patent rights. AN132-7 Application Note 132 “Summon a vision and declare it pure.” –Theodore Roethke “Four for Sir John Davies” 1953 an132f AN132-8 Linear Technology Corporation LT 0211 • PRINTED IN USA 1630 McCarthy Blvd., Milpitas, CA 95035-7417 (408) 432-1900 ● FAX: (408) 434-0507 ● www.linear.com © LINEAR TECHNOLOGY CORPORATION 2011
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