LMH6555 LMH6555 Low Distortion 1.2 GHz Differential Driver Literature Number: SNOSAJ1C LMH6555 Low Distortion 1.2 GHz Differential Driver General Description Features The LMH6555 is an ultra high speed differential line driver with 53 dB SFDR at 750 MHz. The LMH6555 features a fixed gain of 13.7 dB. An input to the device allows the output common mode voltage to be set independent of the input common mode voltage in order to simplify the interface to high speed differential input ADCs. A unique architecture allows the device to operate as a fully differential driver or as a singleended to differential converter. The outstanding linearity and drive capability (100 differential load) of this device are a perfect match for driving high speed analog-to-digital converters. When combined with the ADC081000/ ADC081500 (single or dual ADC), the LMH6555 forms an excellent 8-bit data acquisition system with analog bandwidths exceeding 750 MHz. The LMH6555 is offered in a space saving 16-pin LLP package. Typical values unless otherwise specified. -3 dB bandwidth (VOUT = 0.80 VPP) 0.5 dB gain flatness (VOUT = 0.80 VPP) Slew rate 2nd/3rd Harmonics (750 MHz) Fixed gain Supply current Single supply operation Adjustable common-mode output voltage 1.2 GHz 330 MHz 1300 V/s -53/-54 dBc 13.7 dB 120 mA 3.3V 10% Applications Differential ADC driver National Semiconductor ADC081500/ ADC081000 (single or dual) driver Single ended to differential converter Intermediate frequency (IF) amplifier Communication receivers Oscilloscope front end Typical Application 20127704 Single Ended to Differential Conversion (c) 2011 National Semiconductor Corporation 201277 www.national.com LMH6555 Low Distortion 1.2 GHz Differential Driver March 30, 2011 LMH6555 Maximum Junction Temperature Storage Temperature Range Soldering Information Infrared or Convection (20 sec.) Wave Soldering (10 sec.) Absolute Maximum Ratings (Note 1) If Military/Aerospace specified devices are required, please contact the National Semiconductor Sales Office/ Distributors for availability and specifications. ESD Tolerance (Note 5) Human Body Model Machine Model VS Output Short Circuit Duration (one pin to ground) Common Mode Input Voltage 2000V 200V 4.2V Operating Ratings 235C 260C (Note 1) Temperature Range (Note 4) Supply Voltage Range -40C to +85C +3.3V 10% Package Thermal Resistance (JA)(Note 4) 16-Pin LLP Infinite -0.4V to 3V 3.3V Electrical Characteristics +150C -65C to +150C 65C/W (Note 2) Unless otherwise specified, all limits are guaranteed for TA= 25C, VCM_REF = 1.2V, both inputs tied to 0.3V through 50 (RS1 & RS2) each (Note 11), VS = 3.3V, RL = 100 differential, VOUT = 0.8 VPP. See the Definition of Terms and Specification section for definition of terms used throughout the datasheet. Boldface limits apply at the temperature extremes. Symbol Parameter Conditions Min (Note 8) Typ (Note 7) Max (Note 8) Units AC/DC Performance SSBW -3 dB Bandwidth LSBW VOUT = 0.25 VPP 1200 VOUT = 0.8 VPP 1200 Peak Peaking VOUT = 0.8 VPP 1.4 GF_0.1 dB Gain Flatness 0.1 dB 180 0.5 dB 330 GF_0.5 dB Ph_Delta Phase Delta Output Differential Phase Difference MHz dB MHz < 0.8 deg < 30 deg 0.75 ns 1 VPP f 1.2 GHz Lin_Ph Linear Phase Deviation GD Group Delay Each Output f 2 GHz Each Output f 2 GHz P_1 dB 1 dB Compression 1 GHz TRS/TRL Rise/ Fall Time VOUT = 0.2 VPP Each Output 320 pS OS Overshoot VOUT = 0.2 VPP Each Output 14 % SR Slew Rate 0.8V Step, 10% to 90%,(Note 6) 1300 V/s ts Settling Time 1% 2.2 ns AV_DIFF Insertion Gain (|S21|) 13.2 13.1 13.7 14.0 14.1 TC AV_DIFF Temperature Coefficient of Insertion Gain -0.9 AV_DIFF1 Insertion Gain Variation with VCM_REF VCM_REF Input Varied from 0.95V to 1.45, VOUT = 0.8 VPP -0.04 0.50 0.58 AV_DIFF2 Insertion Gain Variation with VI_CM -0.3 VI_CM 2.0V 0.03 0.48 0.55 250 MHz (Note 12) -60 500 MHz (Note 12) -62 750 MHz (Note 12) -53 250 MHz (Note 12) -67 HD3_M 500 MHz (Note 12) -61 HD3_H 750 MHz (Note 12) -54 dB mdB/C dB dB Distortion And Noise Response HD2_L 2nd Harmonic Distortion HD2_M HD2_H HD3_L www.national.com 3rd Harmonic Distortion 2 dBc dBc Parameter Conditions Min (Note 8) Typ (Note 7) Max (Note 8) Units OIP3 Output 3rd Order Intermodulation f = 1 GHz Intercept POUT (Each Tone) -8.5 dBm (Note 12, Note 13) 27.5 dBm OIM3 3rd Order Intermodulation Distortion f = 1 GHz POUT (Each Tone) = -6 dBm (Note 12, Note 13) -67 dBc eno Output Referred Voltage Noise 1 MHz 19 NF Noise Figure Relative to a Differential Input nV/ 15.0 dB 10 MHz Input Characteristics RIN CM Input Resistance Each Input to Ground 45 RIN_DIFF Differential Input Resistance Differential 66 CIN Input Capacitance Each Input to GND CMRR Common Mode Rejection Ratio -0.3 CMVR 2.0V 40 36 50 55 78 100 0.3 pF 68 dB Output Characteristics VOOS Output Offset Voltage Differential Mode TCVOOS Output Offset Voltage Average Drift (Note 9) RO Output Resistance RT1 and RT2 BAL_Error_DC Output Gain Balance Error 15 50 55 V/C 100 43 BAL_Error_AC mV 50 53 -57 -38 dB -48 BAL_Error_AC_ Output Phase Balance Error Phase f = 750 MHz, VOUT+ - VOUT- Phase 0.6 deg |VO_CM/VI_CM| Output Common Mode Gain DC -26 -22 -21 dB VOS_CM = VO_CM - VCM_REF -4 60 85 mV VCM_REF Characteristics VOS_CM Output CM Offset Voltage TC_VOS_CM CM Offset Voltage Temp Coefficient IB_CM VCM_REF Bias Current RIN_CM VCM_REF Input Resistance Gain_VCM_REF VCM_REF Input Gain to Output VO_CM/VCM_REF IS Supply Current RS1 & RS2 Open (Note 3) PSRR Differential Power Supply Rejection Ratio DC, VS = 0.3V, VOUT/VS -27 -25 -44 PSRR_CM Common Mode PSRR DC, VS = 0.3V, VO_CM/VS -29 -27 -39 -0.2 0.95V VCM_REF 1.45V (Note 10) -25 mV/C 390 415 A 3.5 5.8 0.97 0.99 1.00 V/V 120 150 156 mA k Power Supply 3 dB dB www.national.com LMH6555 Symbol LMH6555 Note 1: Absolute Maximum Ratings indicate limits beyond which damage to the device may occur. Operating Ratings indicate conditions for which the device is intended to be functional, but specific performance is not guaranteed. For guaranteed specifications, see the Electrical Characteristics tables. Note 2: Electrical Table values apply only for factory testing conditions at the temperature indicated. Factory testing conditions result in very limited self-heating of the device such that TJ = TA. No guarantee of parametric performance is indicated in the electrical tables under conditions of internal self-heating where TJ > TA. Note 3: Total supply current is affected by the input voltages connected through RS1 and RS2. Supply current tested with input removed. Note 4: The maximum power dissipation is a function of TJ(MAX), JA and TA. The maximum allowable power dissipation at any ambient temperature is PD= (TJ(MAX) -- TA)/ JA. All numbers apply for package soldered directly into a 2 layer PC board with zero air flow. Package should be soldered unto a 6.8 mm2 copper area as shown in the "recommended land pattern" shown in the package drawing. Note 5: Human Body Model, applicable std. MIL-STD-883, Method 3015.7. Machine Model, applicable std. JESD22-A115-A (ESD MM std. of JEDEC) Field-Induced Charge-Device Model, applicable std. JESD22-C101-C (ESD FICDM std. of JEDEC). Note 6: Slew Rate is the average of the rising and falling edges. Note 7: Typical values represent the most likely parametric norm as determined at the time of characterization. Actual typical values may vary over time and will also depend on the application and configuration. The typical values are not tested and are not guaranteed on shipped production material. Note 8: Limits are 100% production tested at 25C. Limits over the operating temperature range are guaranteed through correlation using Statistical Quality Control (SQC) methods. Note 9: Drift determined by dividing the change in parameter at temperature extremes by the total temperature change. Note 10: Positive current is current flowing into the device. Note 11: Quiescent device common mode input voltage is 0.3V. Note 12: Distortion data taken under single ended input condition. Note 13: 0 dBm = 894 mVPP across 100 differential load Ordering Information Package Part Number Package Marking Transport Media LMH6555SQ 16-Pin LLP LMH6555SQE L6555SQ 250 Units Tape and Reel LMH6555SQX 4.5k Units Tape and Reel Connection Diagram 16-Pin LLP 20127705 www.national.com NSC Drawing 1k Units Tape and Reel 4 SQA16A LMH6555 Definition of Terms and Specifications (Alphabetical Order) Unless otherwise specified, VCM_REF = 1.2V 1. AV_CM (dB) Change in the differential output voltage (VOUT ) with respect to the change in input common mode voltage (VI_CM) 2. AV_DIFF (dB) Insertion gain from a single ended 50 (or 100 differential) source to the differential output (VOUT) 3. AV_DIFF (dB) Variation in insertion gain (AV_DIFF) 4. BAL_ERR_DC & BAL_ERR_AC 5. CM Common Mode 6. CMRR (dB) Common Mode rejection defined as: AV_DIFF (dB) - AV_CM (dB) 7. CMVR (V) Range of input common mode voltage (VI_CM) 8. Gain_VCM_REF (V/V) Variation in output common mode voltage (VO_CM) with respect to change in VCM_REF input (VCM_REF) with maximum differential output 9. PSRR (dB) Differential output change (VOUT) with respect to the power supply voltage change (VS) with nominal differential output 10. PSRR_CM (dB) Output common mode voltage change (VO_CM) with respect to the change in the power supply voltage 11. RIN () Single ended input impedance to ground 12. RIN_DIFF () Differential input impedance 13. RL () Differential output load 14. RO () Device output impedance equivalent to RT1 & RT2 15. RS1, RS2 () Source impedance to VIN+ and VIN- respectively 16. RT1, RT2 () Output impedance looking into each output 17. VCM_REF (V) Device input pin which controls output common mode 18. VCM_REF (V) Change in the VCM_REF input 19. VI_CM (V) DC average of the inputs (VIN+, VIN-) or the common mode signal at those same input pins 20. VI_CM (V) Variation in input common mode voltage (VI_CM) 21. VIN+, VIN- (V) Device input pin voltages 22. VIN (V) Terminated (50 for single ended and 100 for differential) generator voltage 23. VO_CM (V) Output common mode voltage (DC average of VOUT+ and VOUT-) 24. VO_CM (V) Variation in output common mode voltage (VO_CM) (VS) 25. Balance Error. Measure of the output swing balance of VOUT+ and VOUT-, as reflected on the output common mode voltage (VO_CM), relative to the differential output swing (VOUT). Calculated as output common mode voltage change (VO_CM) divided into the output differential voltage change (VOUT which is nominally around 800 mVPP) 26. 27. VOOS (V) DC Offset Voltage. Differential output voltage measured with both inputs grounded through 50 28. VOS_CM (V) Difference between the output common mode voltage (VO_CM) and the voltage on the VCM_REF input, for the allowable VCM_REF range 29. VOUT (V) Differential Output Voltage (VOUT+ - VOUT-) (Corrected for DC offset (VOOS)) 30. VOUT (V) Change in the differential output voltage (Corrected for DC offset (VOOS)) 31. VOUT+, VOUT- (V) Device output pin voltages 32. VS (V) Supply Voltage (V+ - V-) 33. VS (V) Change in VCC supply voltage 5 www.national.com LMH6555 Typical Performance Characteristics Unless otherwise specified, RS1 = RS2 = 50, VS = 3.3V, RL = 100 differential, VOUT = 0.8 VPP. See the Definition of Terms and Conditions section for definition of terms used throughout the datasheet. Frequency Response 0.5 dB Gain Flatness 20127760 20127773 Linear Phase Deviation & Group Delay Bal_Error vs. Frequency 20127758 20127759 -1 dB Compression vs. Frequency Step Response (VOUT+) 20127772 20127757 www.national.com 6 LMH6555 Step Response Settling Time Harmonic Distortion vs. Frequency 20127742 20127771 3rd Order Intermodulation Distortion AV_DIFF & RIN_DIFF vs. VI_CM 20127770 20127761 Insertion Gain Distribution Insertion Gain Variation vs. Input Amplitude 20127768 20127774 7 www.national.com LMH6555 PSRR & PSRR_CM vs. Frequency CMRR vs. VI_CM 20127756 20127775 CMRR vs. Frequency Noise Density & Noise Figure 20127755 20127754 S_Parameters vs. Frequency Differential Output Offset Variation for 3 Representative Units 20127763 20127766 www.national.com 8 LMH6555 Common Mode Offset Voltage Variation vs. VCM_REF Supply Current vs. Temperature 20127769 20127767 9 www.national.com LMH6555 is forced by the built-in common mode amplifier with VCM_REF as its input. As shown, in Figure 1 below, the VCMO output of most differential high speed ADC's is tied to the VCM_REF input of the LMH6555 for direct output common mode control. In some cases, the output drive capability of the ADC VCMO output may need an external buffer, as shown, to increase its current capability in order to drive the VCM_REF pin. The LMH6555 Electrical Characteristics table shows the gain (Gain_VCM_REF) and the offset (VOS_CM) from the VCM_REF to the device output common mode. Application Information See the Definition of Terms and Conditions section for definition of terms used. GENERAL The LMH6555 consists of three individual amplifiers: The VOUT+ driver, VOUT- driver, and the common mode amplifier. Being a differential amplifier, the LMH6555 will not respond to the common mode input (as long as it is within its input common mode range) and instead the output common mode 20127704 FIGURE 1. Single Ended to Differential Conversion The single ended input and output impedances of the LMH6555 I/O pins are close to 50 as specified in the Electrical Characteristics table (RIN and RO). With differential input drive, the differential input impedance (RIN_DIFF) is close to 78. The device nominal input common mode voltage (VI_CM) is close to 0.3V when RS1 and RS2 of Figure 1 are open. Thus, the input source will experience a DC current with 0V input. Because of this, the differential output offset voltage is influenced by the matching between RS1 and RS2. So, in a single ended input condition, if the signal source is AC coupled to one input, the undriven input needs to also be AC coupled in order to cancel the output offset voltage (VOOS). In applications where low output offset is required, it is possible to inject some current to the appropriate input www.national.com (VIN+ or VIN-) as an effective method of trimming the output offset voltage of the LMH6555. This is explained later in this document. The nominal value of RS1 and RS2 will also affect the insertion gain (AV_DIFF). The LMH6555 can also be used with the input AC coupled through equal valued DC blocking capacitors (C) in series with VIN+ and VIN-. In this case, the coupling capacitors need to be large enough to not block the low frequency content. The lower cutoff frequency will be 1/(REQC)Hz with REQ= RS1+ RS2 + RIN_DIFF where RIN_DIFF 78. The single ended output impedance of the LMH6555 is 50. The LMH6555 Electrical Characteristics shows the device performance with 100 differential output load, as would be the case if a device such as the ADC081000/ ADC081500 (single/ dual ADC) were being driven. 10 LMH6555 CIRCUIT ANALYSIS Figure 2 shows the block diagram of the LMH6555. 20127708 RG1 = RG2 = RG = 39 RE1 = RE2 = RE = 25 RF1 = RF2 = RF = 430 ICQ1 = ICQ2 = 12.6 mA FIGURE 2. Block Diagram The differential input stage consists of cross-coupled common base bipolar NPN stages, Q1 and Q2. These stages give the device its differential input characteristic. The internal loop gain from Vx and Vy internal nodes (Q1 and Q2 emitters) to the output is large, such that these nodes act as a virtual ground. The cross-coupling will ensure that these nodes are at the same voltage as long as the amplifier is operating within its normal range. Output common mode voltage is enforced through the action of "ACM" which servos the output common mode to the "VCM_REF" input voltage. The discussion that follows, provides the formulas needed to analyze single ended and differential input applications. For a more detailed explanation including derivations, please see the Appendix at the end of the datasheet. 11 www.national.com LMH6555 SINGLE-ENDED INPUT The following is the procedure for determining the device operating conditions for single ended input applications. This example will use the schematic shown in Figure 3. VIN_DIFF = IIN_DIFF * RIN_DIFF For Figure 3 VIN_DIFF = 1.685 mAPP * 78 = 131.4 mVPP 5. Calculate the undriven input's swing, based on VIN_DIFF determined in step 4 and VIN+ calculated in step 1: VIN- = VIN+ - VIN_DIFF For Figure 3 20127710 VIN- = 150 mVPP - 131.4 mVPP = 18.6 mVPP FIGURE 3. Single-Ended Input Drive 6. 1. Determine the driven input's (VIN+ or VIN-) swing knowing that each input common mode impedance to ground (RIN) is 50: VI_CM = 12.6 mA * RE * RS / (RS + RG + RE) where RE = 25 & RG = 39 (both internal VIN+ (or VIN-) = VIN * RIN/(RIN + RS) to the LMH6555) For Figure 3 For Figure 3 RS = 50 VI_CM = 15.75 / (RS + 64) VIN+ = 0.3 VPP * 50/(50+50) = 0.15 VPP 2. Determine the DC average of the two inputs (VI_CM) by using the following expression: VI_CM = 15.75/ (50+64) = 138.2 mV Calculate VOUT knowing the Insertion Gain (AV_DIFF): The values determined with the procedure outlined here are shown in Figure 4. VOUT = (VIN/2) * AV_DIFF AV_DIFF = 2 * RF/ (2RS + RIN_DIFF) where RF = 430 & RIN_DIFF = 78 For Figure 3 RS = 50 AV_DIFF = 4.83 V/V VOUT = (0.3 VPP/2) * 4.83 V/V= 724.5 mVPP 3. Determine the peak-to-peak differential current (IIN_DIFF) through the device's differential input impedance (RIN_DIFF) which would result in the VOUT calculated in step 2: IIN_DIFF = VOUT/ RF For Figure 3 20127764 IIN_DIFF = 724.5 mVPP/ 430 = 1.685 mAPP 4. FIGURE 4. Input Voltage for Figure 3 Schematic Determine the swing across the input terminals (VIN_DIFF) which would give rise to the IIN_DIFF calculated in step 3 above. www.national.com 12 20127720 Assuming transformer secondary, VIN, of 300 mVPP FIGURE 5. Differential Input Drive 1. Calculate the swing across the input terminals (VIN_DIFF) by considering the voltage division from the differential source (VIN) to the LMH6555 input terminals with differential input impedance RIN_DIFF: 20127765 FIGURE 6. Input Voltage for Figure 5 Schematic SOURCE IMPEDANCE(S) AND THEIR EFFECT ON GAIN AND OFFSET The source impedances RS1 and RS2, as shown in Figure 3 or Figure 5, affect gain and output offset. The datasheet tables and typical performance graphs are generated with equal valued source impedances RS1 and RS2, unless otherwise specified. Any mismatch between the values of these two impedances would alter the gain and offset voltage. VIN_DIFF = VIN * RIN_DIFF/ (2RS + RIN_DIFF) For Figure 5 VIN_DIFF = 300 mVPP * 78 / (100 + 78) = 131.5 mVPP 2. Calculate each input pin swing to be 1/2 the swing determined in step 1: OUTPUT OFFSET CONTROL AND ADJUSTMENT There are applications which require that the LMH6555 differential output voltage be set by the user. An example of such an application is a unipolar signal which is converted to a differential output by the LMH6555. In order to utilize the full scale range of the ADC input, it is beneficial to shift the LMH6555 outputs to the limits of the ADC analog input range under minimal signal condition. That is, one LMH6555 output is shifted close to the negative limit of the ADC analog input and the other close to the positive limit of the ADC analog input. Then, under maximum signal condition, with proper gain, the full scale range of the ADC input can be traversed and the ADC input dynamic range is properly utilized. If this forced offset were not imposed, the ADC output codes would be reduced to half of what the ADC is capable of producing, resulting in a significant reduction in ENOB. The choice of the direction of this shift is determined by the polarity of the expected signal. Another scenario where it may be necessary to shift the LMH6555 output offset voltage is in applications where it is necessary to improve the specified Output Offset Voltage (differential mode), "VOOS". Some ADC's, including the ADC081000/ ADC081500 (and their dual counterparts), have internal registers to correct for the driver's (LMH6555) VOOS. If the LMH6555 VOOS rating exceeds the maximum value allowed into this register, then shifting the output is required for maximum ADC performance. It is possible to affect output offset voltage by manipulating the value of one input resistance relative to the other (e.g. RS1 relative to RS2 or vice versa). However, this will also alter the gain. Assuming that the source is applied to the VIN+ side through RS1, Figure 7(A) shows the effect of varying RS1 on the overall gain and output offset voltage. Figure 7(B) shows the same effects but this time for when the undriven side impedance, RS2, is varied. VIN+ = VIN- = VIN_DIFF/ 2 For Figure 5 VIN+ = VIN- = 131.5 mVPP/ 2 = 65.7 mVPP 3. Determine the DC average of the two inputs (VI_CM) by using the following expression: VI_CM = 12.6 mA * RE * RS / (RS + RG + RE) where RE = 25 & RG = 39 (both internal to the LMH6555) For Figure 5 RS = 50 VI_CM = 15.75 / (RS+ 64) VI_CM = 15.75/ (50+64) = 138.2 mV 4. Calculate VOUT knowing the Insertion Gain (AV_DIFF): VOUT = (VIN * / 2) * AV_DIFF AV_DIFF = 2 * RF/ (2RS + RIN_DIFF) where RF= 430 & RIN_DIFF = 78 For Figure 5 RS = 50 AV_DIFF = 4.83 V/V VOUT = (0.3 VPP/2) * 4.83 V/V= 724.5 mVPP 13 www.national.com LMH6555 The values determined with the procedure outlined here are shown in Figure 6. DIFFERENTIAL INPUT The following is the procedure for determining the device operating conditions for differential input applications using the Figure 5 schematic as an example. LMH6555 20127730 20127732 FIGURE 8. Gain & Output Offset Voltage vs. Source Impedance Shift for Differential Input Drive It is possible to manipulate output offset with little or no effect on source resistance balance, gain, and, cable termination. 20127731 FIGURE 7. Gain & Output Offset Voltage vs. Source Impedance Shift for Single Ended Input Drive 20127733 (a) As can be seen in Figure 7, the source impedance of the input side being driven has a bigger effect on gain than the undriven source impedance. RS1 and RS2 affect the output offset in opposite directions. Manipulating the value of RS2 for offset control has another advantage over doing the same to RS1 and that is the signal input termination is not affected by it. This is especially important in applications where the signal is applied to the LMH6555 through a transmission line which needs to be terminated in its characteristic impedance for minimum reflection. For reference, Figure 8 shows the effect of source impedance misbalance on overall gain and output offset voltage with differential input drive. 20127752 (b) FIGURE 9. Differential Output Shift Circuits RX, shown in Figure 9(a) and Figure 9(b), injects current into the input to achieve the required output shift. For a positive shift, positive current would need to be injected into the VIN+ terminal (Figure 9(a)) and for a negative shift, to the VIN- terminal (Figure 9(b)). Figure 10 shows the effect of RX on the output with VX = 3.3V or 5V, and RS1 = RS2 = 50. www.national.com 14 (1) The expression derived for VOUT in Equation 1 can be set equal to zero to solve for RX resulting in RX = 4.95 k. If the differential output offset voltage, VOOS, is also known, VOUT could be set to a value equal to -VOOS. For example, if the VOOS for the particular LMH6555 is +30 mV, then the following nulls the differential output: 20127734 (2) FIGURE 10. LMH6555 Differential Output Shift Due to RX in Figure 9 RX >> RS2 confirming the assumption made in the derivation. Note that Equation 2, which is derived based on the configuration in Figure 9(b), will yield a real solution for RX if and only if: To shift the LMH6555 differential output negative by about 100 mV, referring to the plot in Figure 10, RX would be chosen to be around 3.9 k in the schematic of Figure 9(b) (using VX = VS = 3.3V). In applications where VIN has a built-in non-zero offset voltage, or when RS1 and RS2 are not 50, the Figure 10 plot cannot be used to estimate the required value for RX. Consider the case of a more general offset correction application, shown in Figure 11(a), where RS1 = RS2 = 75 and VIN has a built-in offset of -50 mV. It is necessary to shift the differential output offset voltage of the LMH6555 to 0 mV. Figure 11(b) is the Thevenin equivalent of the circuit in Figure 11(a) assuming RX >> RS2. (3) where VIN_OFFSET is the source offset shown as -50 mV in Figure 11(a). If Equation 3 were not satisfied, then Figure 9(a) offset correction, where RX is tied to the VIN+ side, should be employed instead. Alternatively, replace the VX and RX combination with a discrete current source or current sink. Because of a current source's high output impedance, there will be less gain imbalance. However, a current source might have a relatively large output capacitance which could degrade high frequency performance. INTERFACE DESIGN EXAMPLE As shown in Figure 12 below, the LMH6555 can be used to interface an open collector output device (U1) to a high speed ADC. In this application, the LMH6555 performs the task of amplifying and driving the 100 differential input impedance of the ADC. 20127735 (a) 20127706 20127753 VCM_REF buffer not shown (b) FIGURE 12. Differential Amplification and ADC Drive FIGURE 11. Offset Correction Example (RS = 75) 15 www.national.com LMH6555 From the gain expression in Equation 4 (see Appendix) (but with opposite polarity because VTH is applied to VIN- instead): LMH6555 For applications similar to the one shown in Figure 12, the following conditions should be maintained: 1. The LMH6555 differential output voltage has to comply with the ADC full scale voltage (800 mVPP in this case). 2. The LMH6555 input Common Mode Voltage Range is observed. "CMVR", as specified in the Electrical Characteristics table, is to be between -0.3V and 2.0V for the specified CMRR. 3. U1 collector voltage swing must to be observed so that the U1 output transistors do not saturate. The expected operating range of these output transistors is defined by the specifications and operating conditions of U1. Consider a numerical example (RL refers to RL1 & RL2, RS refers to RS1 & RS2). Assume: VCC = 10V, U1 peak-to-peak collector current (IPP) = 15 mAPP with 10 mA quiescent (IcQ), and minimum operational U1 collector voltage = 6V. Here are the series of steps to take in order to carry out this design: a. IN (differential) * RF = 800 mVPP RS = (RL* IPP * RF/ 0.8) - RG - RL where RF = 430, RG = 39 (RF and RG are internal LMH6555 resistances). So, in this case: RS = (169 * 15 mAPP * 430/ 0.8) - 39 - 169 = 1154 Choose 1.15 k, 1% resistors for RS. c. The "Vx" node voltage within the LMH6555 (see Figure 13) would need to be calculated. Use the Common Mode component of the Norton equivalent source from above, and write the KCL at the Vx node as follows: Select the RL value which allows compliance with the U1 collector voltage (6V in this case) with 1V extra as margin because of LMH6555 loading. Vx / RE + Vx / RN = 12.6 mA + IN (common mode); with RE = 25. Vx / RE + Vx / RN = 12.6 mA + (VCC - IcQ RL )/ (RL + RS + RG) RL = [10 - (6+1)] V / (10+ 7.5) mA = 171 Choose 169, 1% resistors for RL b. With RL and RS defined, ensure that the U1 collector voltage(s) minimum is not violated due to the loading effect of the LMH6555 through RS. Also, it is important to ensure that the LMH6555's CMVR is also not violated. Vx = 0.4595V Find the value of RS to get the proper swing at the output (800 mVPP). To do so, convert the input stage into its Norton equivalent as shown in Figure 13. With Vx calculated, both the input voltage range (high and low) and the low end of the U1 collector voltage (VC) can be derived to be within the acceptable range. If necessary, steps "a" through "c" would have to be repeated to readjust these values. VC = VX RL / RN + IN (RS + RG) IN_High = 7.05 mA, IN_Low = 5.19 mA (based on the values derived) VC_High = 0.4595 * 169 / 1358 + 7.05 mA (1150 + 39) = 8.44V VC_Low = 0.4595 * 169 / 1358 + 5.19 mA (1150 + 39) = 6.22V VIN = VX (RN - RG) / RN + IN RG VIN_High = 0.4595 * (1358- 39) / 1358 + 7.05 mA * 39 20127748 = 0.721V FIGURE 13. Norton Equivalent of the Input Circuitry Tied to Q1 within the LMH6555 in Figure 12 VIN_Low = 0.4595 * (1358- 39) / 1358 + 5.19 mA * 39 = 0.649V IN = IN (common mode) + IN (differential) Figure 14 shows the complete solution using the values derived above, with the node voltages marked on the schematic for reference. IN (common mode) = (VCC - IcQ * RL) / (RL + RS + RG) IN (differential) = IPP * RL / (RL + RS + RG) The entirety of the Norton source differential component will flow through the feedback resistors within the LMH6555 and generate an output. Therefore: www.national.com 16 VIN = VX RG. IN (differential) /2 VIN_High = 0.3150 + 39 * 1.88 mA /2 = 0.3517V VIN_Low = 0.3150 - 39 * 1.88 mA /2 = 0.2783V Figure 16 shows the AC coupled implementation of the Figure 15 schematic along with the node voltages marked to demonstrate the reduced VI_CM of the LMH6555 and the increase in the U1 collector voltage minimum. 20127749 FIGURE 14. Implementation #1 of Figure 12 Design Example It is important to note that the matching of the resistors on either input side of the LMH6555 (RS1 to RS2 and RL1 to RL2) is very important for output offset voltage and gain balance. This is particularly true with values of RS higher than the nominal 50. Therefore, in this example, 1% or better resistor values are specified. If the U1 collector voltage turns out to be too low due to the loading of the LMH6555, lower RL. Lower values of RL result in lower RS which in turn increases the LMH6555's VI_CM because of increased pull up action towards VCC. The upper limit on VI_CM is 2V. Figure 15 shows the 2nd implementation of this same application with lowered values of RL and RS. Notice that the lower end of U1's collector voltage and the upper end of LMH6555's VI_CM have both increased compared to the 1st implementation. 20127751 FIGURE 16. AC Coupled Version of Figure 15 Note that the lower cut-off frequency is: f_cut-off = 1 / (ReqCS) where Req = RS1+ RS2 + RIN_DIFF where RIN_DIFF 78 So, for the component values shown (CS = 0.01 F and RS1 = RS2 = 523): f_cut-off = 28.2 kHz DATA ACQUISITION APPLICATIONS Figure 17 shows the LMH6555 used as the differential driver to the National Semiconductor ADC081500 running at 1.5G samples/second. 20127750 FIGURE 15. Implementation #2 of Figure 12 Design Example An alternative would be to AC couple the LMH6555 inputs. With this approach, the design steps would be very similar to the ones outlined except that there would be no common mode interaction between the LMH6555 and U1 and this results in fewer design constraints: Vx / RE = 12.6 mA Vx = 0.3150V 20127704 For the component values shown in Figure 15 use: FIGURE 17. Schematic of the LMH6555 Interfaced to the ADC081500 VC_High = VCC - RL (IcQ + IPP / 2 - IN (differential) /2) VC_Low = VCC - RL (IcQ - IPP / 2 + IN (differential) /2) IN (differential) = IPP * RL / (RL + RS + RG) = 1.88 mA (based on the values used.) 17 www.national.com LMH6555 VC_High = 10 - 80.6 (10 + 15 / 2 - 1.88 /2) mA = 8.67V VC_Low = 10 - 80.6 (10 - 15 / 2 + 1.88 /2) mA = 9.72V LMH6555 shows CO placed across the LMH6555 output terminals to reduce the frequency response gain peaking and thereby to increase the 0.5 dB gain flatness frequency. In the schematic of Figure 17, the LMH6555 converts a single ended input into a differential output for direct interface to the ADC's 100 differential input. An alternative approach to using the LMH6555 for this purpose, would have been to use a balun transformer, as shown in Figure 18. 20127777 20127776 FIGURE 18. Single Ended to Differential Conversion (AC only) with a Balun Transformer FIGURE 19. Increasing 0.5 dB Gain Flatness using External Output Capacitance, CO In the circuit of Figure 18, the ADC will see a 100 differential driver which will swing the required 800 mVPP when VIN is 1.6 VPP. The source (VIN) will see an overall impedance of 200 for the frequency range that the transformer is specified to operate. Note that with this scheme, the signal to the ADC must be AC coupled, because of the transformer's minimum operating frequency which would prevent DC coupling. For the transformer specified, the lower operating frequency is around 4.5 MHz and the input high pass filter's -3 dB bandwidth is around 340 kHz for the values shown (or (1/REQC) Hz where REQ = 200). Table 1 compares the LMH6555 solution (Figure 17) vs. that of the balun transformer coupling (Figure 18) for various categories. Figures 20, 21 and Figure 22 show the FFT analysis results with the setup shown in Figure 17. TABLE 1. ADC Input Coupling Schemes Compared Preferred Solution Category LMH6555 Lower Power Consumption Lower Distortion Wider Dynamic Range DC Coupling & Broadband Applications Input/ Output Broadband Impedance Matching (Highest Return Loss) Additional Gain Highest SNR Ability to Control Gain Flatness 20127743 FIGURE 20. LMH6555 FFT Result When Used as the Differential Driver to ADC081500 Highest Gain & Phase Balance ADC Input Protection against Overdrive Balun Transformer (see below) 20127744 GAIN FLATNESS In applications where the full 1.2 GHz bandwidth of the LMH6555 is not necessary, it is possible to improve the gain flatness frequency at the expense of bandwidth. Figure 19 www.national.com FIGURE 21. LMH6555 FFT Result When Used as the Differential Driver to ADC081500 (Lower Fs/2 Region Magnified) 18 TABLE 2. Differential Input ADC's Compatible with the LMH6555 Driver ADC Part Number Resolution (bits) 20127745 FIGURE 22. LMH6555 FFT Result When Used as the Differential Driver to ADC081500 (Upper Fs/2 Region Magnified) Figures 20, 21, and Figure 22 information summary: * Fundamental Test Frequency * LMH6555 Output 744 MHz * Sampling Rate: * 2nd Harmonic 1.5G samples/ second * 3rd Harmonic -57 dBc @ 732 MHz or |1.5 GHz*1- 744 MHz *3| * 4th Harmonic -71 dBc @ 24 MHz or |1.5 GHz*2 - 744 MHz *4| * 5th Harmonic -68 dBc @ 720 MHz or |1.5 GHz*2- 744 MHz*5| * 6th Harmonic -68 dBc @ 36 MHz or |1.5 GHz*3- 744 MHz*6| -51.8 dBc 43.4 dB * THD * SNR * Spurious Free Dynamic Range (SFDR): * SINAD * ENOB 0.8 VPP ADC08D500 8 Single/ Dual Speed (MSPS) S 500 ADC081000 8 S 1000 ADC08D1000 8 D 1000 ADC08D1020 8 D 1000 ADC081500 8 S 1500 ADC08D1500 8 D 1500 ADC08D1520 8 D 1500 ADC083000 8 S 3000 ADC08B3000 8 S 3000 EXPOSED PAD LLP PACKAGE The LMH6555 is in a thermally enhanced package. The exposed pad (device bottom) is connected to the GND pins. It is recommended, but not necessary, that the exposed pad be connected to the supply ground plane. The thermal dissipation of the device is largely dependent on the connection of this pad. The exposed pad should be attached to as much copper on the circuit board as possible, preferably external copper. However, it is very important to maintain good high speed layout practices when designing a system board. Here is a link to more information on the National 16-pin LLP package: -59 dBc @ 12 MHz or |1.5 GHz*1- 744 MHz*2| http://www.national.com/packaging/folders/sqa16a.html EVALUATION BOARD National Semiconductor suggests the following evaluation board as a guide for high frequency layout and as an aid in device testing and characterization. 57 dB 42.8 dB 6.8 bits The LMH6555 is capable of driving a variety of National Semiconductor Analog to Digital Converters. This is shown in Table 2, which offers a complete list of possible signal path ADC+ Amplifier combinations. The use of the LMH6555 to Device Package LMH6555 16-Pin LLP Evaluation Board Ordering ID LMH6555EVAL The evaluation board can be ordered when a device sample request is placed with National Semiconductor. 19 www.national.com LMH6555 drive an ADC is determined by the application and the desired sampling process (Nyquist operation, sub-sampling or oversampling). See application note (AN-236) for more details on the sampling processes and application note (AN-1393) for details on "Using High Speed Differential Amplifiers to Drive ADCs". For more information regarding a particular ADC, refer to the particular ADC datasheet for details. LMH6555 The first task would be to derive the internal transistor emitter voltages based on the schematic of Figure 23 (assuming that there is no interaction between the stages.) Here is the derivation of VX and Vy: Appendix Here is a more detailed analysis of the LMH6555, including the derivation of the expressions used throughout the Application Information. INPUT STAGE Because of the input stage cross-coupling, if the instantaneous values of the input node voltages (VIN+ and VIN-) and current values are required, use the circuit of Figure 23 as the equivalent input stage for each input (VIN+ and VIN-). VX varies with VIN+ (0.213V with negative VIN swing and 0.279V with positive.) The values derived above assume that the two halves of the input circuit do not interact with each other. They do through the common mode amplifier and the input stage cross-coupling. Vx and Vy are equal to the average of Vy with either end of the swing of VX. This is calculated below along with the derivation of VIN+ and VIN- based on this new average emitter voltage (the average of VX and Vy.) 20127709 FIGURE 23. Equivalent Input Stage Using this simplified circuit, one can assume a constant collector current, to simplify the analysis. This is a valid approximation as the large open loop gain of the device will keep the two collector currents relatively constant. First derive Q1 and Q2 emitter voltages. From there, derive the voltages at VIN+ and VIN-. With the component values shown, it is possible to analyze the input circuits of Figure 23 in order to determine Q1 and Q2 emitter voltages. This will result in a first order estimate of Q1 and Q2 emitter voltages. Since Q1 and Q2 emitters are cross-coupled, the voltages derived would have to be equal. With the action of the common mode amplifier, "ACM", shown in Figure 2, these two emitters will be equalized. So, one other iteration can be performed whereby both emitters are set to be equal to the average of the 1st derived emitter voltages. Using this new emitter voltage, one could recalculate VIN+ and VIN- voltages. The values derived in this fashion will be within 10% of the measured values. With 0.3 VPP VIN, VIN+ experiences 150 mVPP (213 mV - 63.2 mV) of swing and VIN- will swing by about 18.6 mVPP in the process (147 mV - 129 mV). The input voltages are shown in Figure 25. Single Ended Input Analysis Here is an actual example to further clarify the procedure. Consider the case where the LMH6555 is used as a single ended to differential converter shown in Figure 24. 20127764 FIGURE 25. Input Voltages for Figure 24 Schematic 20127710 FIGURE 24. Single Ended Input Drive www.national.com 20 Differential Input Analysis Assume that the LMH6555 is used as a differential amplifier with a transformer with its Center Tap at ground as shown in Figure 26: 20127765 20127720 FIGURE 27. Input Voltages for Figure 26 Schematic Assuming transformer secondary, VIN, of 300 mVPP FIGURE 26. Differential Input Drive Knowing the device input terminal voltages, one can estimate the differential input impedance as follows: The input voltages (VIN+ and VIN-) can be derived using the technique explained previously. Assuming no transformer output and referring to the schematic of Figure 23: This is comparable to RIN_DIFF found in the Electrical Characteristic table. OUTPUT STAGE AND GAIN ANALYSIS Differential gain is determined by the differential current flow through the feedback resistors RF1 and RF2 as shown in Figure 2. Current through RF1 (or RF2) sets the VOUT- (or VOUT+) swing. The nominal value of these resistors is close to 430. The LMH6555 output stage consists of two bipolar common emitter amplifiers with built in output resistances, RT1 and RT2, of 50, as shown in Figure 28. The peak VIN+ and VIN- voltages can be determined using the transformer output voltage. Assuming there is 0.3 VPP of signal across the transformer secondary, 1/2 of that, or 0.15 VPP (75 mV peak), would appear at each input side (V1 or V2 in Figure 26). Here is the derivation of the LMH6555 input terminal's peak voltages. When V1 swings positive, V2 will go negative by the same value, and vice versa. Therefore, the values derived above for Vx can be used to determine the average emitter voltage, as described earlier: 20127725 FIGURE 28. Output Stage Including External Load RL 21 www.national.com LMH6555 With the transformer voltage of 0.3 VPP, each input (VIN+ and VIN-) swings from 105.3 mV to 171.0 mV or about 65.7 mVPP. The input voltages are shown in Figure 27. Using the calculated swing on VIN+ with known VIN, one can estimate the input impedance, RIN as follows: LMH6555 The following is the expression for the Insertion Gain, AV_DIFF: With an output differential load, RL, of 100, half the differential swing between the output emitters appears at the LMH6555 output terminals as VOUT. With good matching between the input source impedances, RS1 and RS2 shown in Figure 24 and Figure 26, it is possible to infer the gain and output swing by inspection. The differential input impedance of the LMH6555, RIN_DIFF, is close to 78. In differential input drive applications, there is a balanced swing across the input terminals of the LMH6555, VIN+ and VIN-. So, by using the RIN_DIFF value, one determines the differential current flow through the input terminals and from that the output swing and gain. The expressions above apply equally to the single ended input drive case as well, as long as RS1 = RS2 = 50. For the case of the single ended input drive: (4) For the special case where RS1 = RS2 = RS = 50 we have: www.national.com This is comparable to AV_DIFF found in the Electrical Characteristic table. 22 LMH6555 Physical Dimensions inches (millimeters) unless otherwise noted 16-Pin LLP NS Package Number SQA16A 23 www.national.com LMH6555 Low Distortion 1.2 GHz Differential Driver Notes For more National Semiconductor product information and proven design tools, visit the following Web sites at: www.national.com Products Design Support Amplifiers www.national.com/amplifiers WEBENCH(R) Tools www.national.com/webench Audio www.national.com/audio App Notes www.national.com/appnotes Clock and Timing www.national.com/timing Reference Designs www.national.com/refdesigns Data Converters www.national.com/adc Samples www.national.com/samples Interface www.national.com/interface Eval Boards www.national.com/evalboards LVDS www.national.com/lvds Packaging www.national.com/packaging Power Management www.national.com/power Green Compliance www.national.com/quality/green Switching Regulators www.national.com/switchers Distributors www.national.com/contacts LDOs www.national.com/ldo Quality and Reliability www.national.com/quality LED Lighting www.national.com/led Feedback/Support www.national.com/feedback Voltage References www.national.com/vref Design Made Easy www.national.com/easy www.national.com/powerwise Applications & Markets www.national.com/solutions Mil/Aero www.national.com/milaero PowerWise(R) Solutions Serial Digital Interface (SDI) www.national.com/sdi Temperature Sensors www.national.com/tempsensors SolarMagicTM www.national.com/solarmagic PLL/VCO www.national.com/wireless www.national.com/training PowerWise(R) Design University THE CONTENTS OF THIS DOCUMENT ARE PROVIDED IN CONNECTION WITH NATIONAL SEMICONDUCTOR CORPORATION ("NATIONAL") PRODUCTS. NATIONAL MAKES NO REPRESENTATIONS OR WARRANTIES WITH RESPECT TO THE ACCURACY OR COMPLETENESS OF THE CONTENTS OF THIS PUBLICATION AND RESERVES THE RIGHT TO MAKE CHANGES TO SPECIFICATIONS AND PRODUCT DESCRIPTIONS AT ANY TIME WITHOUT NOTICE. NO LICENSE, WHETHER EXPRESS, IMPLIED, ARISING BY ESTOPPEL OR OTHERWISE, TO ANY INTELLECTUAL PROPERTY RIGHTS IS GRANTED BY THIS DOCUMENT. TESTING AND OTHER QUALITY CONTROLS ARE USED TO THE EXTENT NATIONAL DEEMS NECESSARY TO SUPPORT NATIONAL'S PRODUCT WARRANTY. EXCEPT WHERE MANDATED BY GOVERNMENT REQUIREMENTS, TESTING OF ALL PARAMETERS OF EACH PRODUCT IS NOT NECESSARILY PERFORMED. NATIONAL ASSUMES NO LIABILITY FOR APPLICATIONS ASSISTANCE OR BUYER PRODUCT DESIGN. BUYERS ARE RESPONSIBLE FOR THEIR PRODUCTS AND APPLICATIONS USING NATIONAL COMPONENTS. PRIOR TO USING OR DISTRIBUTING ANY PRODUCTS THAT INCLUDE NATIONAL COMPONENTS, BUYERS SHOULD PROVIDE ADEQUATE DESIGN, TESTING AND OPERATING SAFEGUARDS. EXCEPT AS PROVIDED IN NATIONAL'S TERMS AND CONDITIONS OF SALE FOR SUCH PRODUCTS, NATIONAL ASSUMES NO LIABILITY WHATSOEVER, AND NATIONAL DISCLAIMS ANY EXPRESS OR IMPLIED WARRANTY RELATING TO THE SALE AND/OR USE OF NATIONAL PRODUCTS INCLUDING LIABILITY OR WARRANTIES RELATING TO FITNESS FOR A PARTICULAR PURPOSE, MERCHANTABILITY, OR INFRINGEMENT OF ANY PATENT, COPYRIGHT OR OTHER INTELLECTUAL PROPERTY RIGHT. LIFE SUPPORT POLICY NATIONAL'S PRODUCTS ARE NOT AUTHORIZED FOR USE AS CRITICAL COMPONENTS IN LIFE SUPPORT DEVICES OR SYSTEMS WITHOUT THE EXPRESS PRIOR WRITTEN APPROVAL OF THE CHIEF EXECUTIVE OFFICER AND GENERAL COUNSEL OF NATIONAL SEMICONDUCTOR CORPORATION. As used herein: Life support devices or systems are devices which (a) are intended for surgical implant into the body, or (b) support or sustain life and whose failure to perform when properly used in accordance with instructions for use provided in the labeling can be reasonably expected to result in a significant injury to the user. A critical component is any component in a life support device or system whose failure to perform can be reasonably expected to cause the failure of the life support device or system or to affect its safety or effectiveness. National Semiconductor and the National Semiconductor logo are registered trademarks of National Semiconductor Corporation. All other brand or product names may be trademarks or registered trademarks of their respective holders. Copyright(c) 2011 National Semiconductor Corporation For the most current product information visit us at www.national.com National Semiconductor Americas Technical Support Center Email: support@nsc.com Tel: 1-800-272-9959 www.national.com National Semiconductor Europe Technical Support Center Email: europe.support@nsc.com National Semiconductor Asia Pacific Technical Support Center Email: ap.support@nsc.com National Semiconductor Japan Technical Support Center Email: jpn.feedback@nsc.com IMPORTANT NOTICE Texas Instruments Incorporated and its subsidiaries (TI) reserve the right to make corrections, modifications, enhancements, improvements, and other changes to its products and services at any time and to discontinue any product or service without notice. Customers should obtain the latest relevant information before placing orders and should verify that such information is current and complete. All products are sold subject to TI's terms and conditions of sale supplied at the time of order acknowledgment. TI warrants performance of its hardware products to the specifications applicable at the time of sale in accordance with TI's standard warranty. Testing and other quality control techniques are used to the extent TI deems necessary to support this warranty. Except where mandated by government requirements, testing of all parameters of each product is not necessarily performed. TI assumes no liability for applications assistance or customer product design. Customers are responsible for their products and applications using TI components. To minimize the risks associated with customer products and applications, customers should provide adequate design and operating safeguards. TI does not warrant or represent that any license, either express or implied, is granted under any TI patent right, copyright, mask work right, or other TI intellectual property right relating to any combination, machine, or process in which TI products or services are used. Information published by TI regarding third-party products or services does not constitute a license from TI to use such products or services or a warranty or endorsement thereof. Use of such information may require a license from a third party under the patents or other intellectual property of the third party, or a license from TI under the patents or other intellectual property of TI. Reproduction of TI information in TI data books or data sheets is permissible only if reproduction is without alteration and is accompanied by all associated warranties, conditions, limitations, and notices. Reproduction of this information with alteration is an unfair and deceptive business practice. TI is not responsible or liable for such altered documentation. Information of third parties may be subject to additional restrictions. Resale of TI products or services with statements different from or beyond the parameters stated by TI for that product or service voids all express and any implied warranties for the associated TI product or service and is an unfair and deceptive business practice. TI is not responsible or liable for any such statements. TI products are not authorized for use in safety-critical applications (such as life support) where a failure of the TI product would reasonably be expected to cause severe personal injury or death, unless officers of the parties have executed an agreement specifically governing such use. Buyers represent that they have all necessary expertise in the safety and regulatory ramifications of their applications, and acknowledge and agree that they are solely responsible for all legal, regulatory and safety-related requirements concerning their products and any use of TI products in such safety-critical applications, notwithstanding any applications-related information or support that may be provided by TI. Further, Buyers must fully indemnify TI and its representatives against any damages arising out of the use of TI products in such safety-critical applications. TI products are neither designed nor intended for use in military/aerospace applications or environments unless the TI products are specifically designated by TI as military-grade or "enhanced plastic." Only products designated by TI as military-grade meet military specifications. Buyers acknowledge and agree that any such use of TI products which TI has not designated as military-grade is solely at the Buyer's risk, and that they are solely responsible for compliance with all legal and regulatory requirements in connection with such use. TI products are neither designed nor intended for use in automotive applications or environments unless the specific TI products are designated by TI as compliant with ISO/TS 16949 requirements. Buyers acknowledge and agree that, if they use any non-designated products in automotive applications, TI will not be responsible for any failure to meet such requirements. Following are URLs where you can obtain information on other Texas Instruments products and application solutions: Products Applications Audio www.ti.com/audio Communications and Telecom www.ti.com/communications Amplifiers amplifier.ti.com Computers and Peripherals www.ti.com/computers Data Converters dataconverter.ti.com Consumer Electronics www.ti.com/consumer-apps DLP(R) Products www.dlp.com Energy and Lighting www.ti.com/energy DSP dsp.ti.com Industrial www.ti.com/industrial Clocks and Timers www.ti.com/clocks Medical www.ti.com/medical Interface interface.ti.com Security www.ti.com/security Logic logic.ti.com Space, Avionics and Defense www.ti.com/space-avionics-defense Power Mgmt power.ti.com Transportation and Automotive www.ti.com/automotive Microcontrollers microcontroller.ti.com Video and Imaging RFID www.ti-rfid.com OMAP Mobile Processors www.ti.com/omap Wireless Connectivity www.ti.com/wirelessconnectivity TI E2E Community Home Page www.ti.com/video e2e.ti.com Mailing Address: Texas Instruments, Post Office Box 655303, Dallas, Texas 75265 Copyright (c) 2011, Texas Instruments Incorporated