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2 Table of Contents Abstract...Cover Introduction...Cover Background...3 Transducer Gain...3 Stability Analysis...4 Available Gain Design Procedure...5 Noise Figure Design Procedure b Amplifier Design Requirements...7 Transistor S-Parameters and Nonlinear Model...8 S-Parameter Data Validation...11 ATF54143 Stability...14 Amplifier EM/Circuit Co-Simulation and PCB Fabrication...29 Amplifier Nonlinear Analysis...48 Simulation Results Versus Specification Requirements...49 TRL Calibration Kit...49 Fabricated Amplifier and TRL Calibration Standards...53 Amplifier Linear S-Parameter Measurements Using TRL...53 Measured Versus Modeled...56 Conclusion References...61 Contact Agilent...Back cover 2

3 Background For low noise amplifier designs, the available gain design approach is typically utilized to facilitate a gain versus noise trade-off. Most applications do not allow or necessarily require a minimum noise design since gain is reduced to allow for the lower noise performance. Thus, a gain versus noise trade-off is appropriate. Knowledge about the system in which the amplifier is to be used is required to make the appropriate gain versus noise trade-off. If subsequent stages following the RF amplifier have a high cumulative noise figure, more gain is required to take-over the noise figure of those stages, thus providing the lowest possible system noise. An example system is shown in Figure 1. System noise factor is calculated using the Friis formula as follows: Equation 1. F F T = F 2 1 F F +... n 1 + g 1 g 1 g 2 g 1 g... 2 g n 1 where: FT is the total system noise factor, F1 is the noise factor of stage one, F2 is the noise factor of stage two, Fn is the noise factor of stage number n. g1 is the numeric gain factor of stage one, g2 is the numeric gain factor of stage two, gn-1 is the numeric gain factor of the second to the last stage. Based on Equation 1, earlier gain stages diminish the effect of cumulative noise added by stages farther back in the system. Thus, trading away too much gain for lower noise figure in the early stages of the system may degrade the overall system noise due to less noise take-over of the following stages. Equations 2 and 3, respectively, convert noise figure, NF in db, to numeric noise factor, F and gain, G in db to gain factor, g: Equation 2. F = 10NF 10 Equation 3. g = 10 G 10 Equations 4 and 5 respectively, convert noise factor, F to noise figure, NF in db, and gain factor, g to gain, G in db: Equation 4. NF = 10logF Equation 5. G = 10log(g) Use Equations 1 through 5 to determine amplifier gain and noise figure requirements for a given system. Transducer Gain A two-port network is terminated as shown in Figure 2. The generalized transducer numeric gain equation for the two-port s-parameter block terminated by Γ S and Γ L of Figure 2 is given by Equation 6: Equation 6. g T = S 21 2 (1 Γ S 2 )(1 Γ L 2 ) (1 S 11 Γ S )(1 S 22 Γ L ) S 21 S 12 Γ S Γ L 3

4 The s-parameters describe a device for a particular set of conditions, such as frequency, bias, and temperature as shown in Equation 6. Transducer gain, g T, is a function of the s-parameters, Γ S, and Γ L. Convert numeric transducer gain g T, to gain G T in db by use of Equation 5. When the device is terminated in the same impedance as when s-parameters were measured, Γ S and Γ L are zero and g T = S Γ S [S] Γ L Figure 2. Γ S Γ IN Γ OUT Γ L Stability Analysis The Figure 2 two-port network may be stable or potentially unstable. It is imperative that the amplifier does not oscillate in the product environment, since such behavior leads to product malfunction. If the two-port is potentially unstable, there are conditions where oscillations can occur. Certain source or load terminations that produce the oscillations provide the conditions necessary for the unstable behavior. This type of design is called a conditionally stable design. If the conditionally stable design method is utilized, extreme care must be observed to guarantee that a source or load termination that produces an oscillation is never presented to the amplifier. This applies to all frequencies in-band and out-of-band. This can be a difficult task at best in most applications. The unconditionally stable design approach allows any source or load terminations, which have reflection coefficient magnitudes between 0 and 1, inclusive, presented to the amplifier without the possibility of an oscillation. It is highly recommended that the two-port is made unconditionally stable at all frequencies. An unconditionally stable design guards against unexpected oscillations, which cause product malfunction. Two-port stability is analyzed using stability circles or equations. In this design example, stability equations are used to achieve an unconditionally stable design at all frequencies. The stability equations are a function of the Figure 2 two-port s-parameters. Equation 7 gives the value for stability factor K, which is made greater than or equal to unity for stability. Additionally, stability factors, B1, and B2 are shown by Equations 8, 9, and 10 respectively. To achieve unconditional stability, the two-port must satisfy Equation 7 and either Equation 8, 9, or 10. If Equation 8, 9, or 10 is satisfied, all three equations are, by definition, satisfied. Thus, if K 1, the two-port network may not be unconditionally stable. Having K 1 is a necessary, but not sufficient, condition for unconditional stability. Additionally, Equation 8, 9, or 10 is analyzed to determine if the two-port network stability is unconditional. Thus, < 1, or B1 > 0, or B2 > 0 must also be met along with K 1 to guarantee unconditional stability. Equation 7. Equation 8. K = 1 S 11 2 S S 12 S 21 = S 11 S 22 S 21 S 12 < 1 1 Equation 9. B 1 =1+ S 11 2 S > 0 Equation 10. B 2 =1+ S 22 2 S > 0 4

5 Alternately, the single test stability factor μ Source or μ Load is calculated using Equation 11 or Equation 12. If μ Source 1 then μ Load 1 by definition and vice versa. If Equation 7 is satisfied and either of Equations 8, 9, or 10 are satisfied, then both Equations 11 and 12 are satisfied. And, of course, if Equations 11 or 12 are satisfied, then Equations 7 through 10 are satisfied. Equation 11. Equation S 11 2 μ Source = S 22 (S* 11 ) + S 21 S 12 1 μ 1 S 22 2 S 11 (S* 22 ) + S 21 S 12 1 Load = If the two-port network is not unconditionally stable, and unconditional stability is required, stabilizing networks are added. Methods of stabilizing the two-port include feedback. These methods typically degrade some parameter such as maximum gain or noise figure. If care is taken, minimal degradation is possible while achieving unconditional stability. Once the stability networks are added, they become part of the two-port network and new s-parameters that describe the new two-port network are calculated. These new s-parameters are used in the stability equations to verify stability. Once the two-port network is unconditionally stable, input and/or output matching networks are added to get the desired performance. Available Gain Design Procedure For low noise amplifier design, the available gain design approach is typically performed. When performing the available gain design procedure, the source termination is constrained to some arbitrary impedance (usually for better noise performance), and the resulting output reflection coefficient of the device is conjugately matched. Thus, a mismatch may exist at the input whereas the output is perfectly matched. If a mismatch exists at the device input, the amount of gain is less than the maximum possible gain as is the case when both input and output are conjugately matched. To determine the amount of available gain with the input mismatched, Equation 6 is modified. Since the output is conjugately matched for a given source termination, Γ OUT is expressed in terms of Γ S and the two-port s-parameters. By substitution and rearrangement, this also allows Equation 6 to be expressed in terms of ΓS and the two-port s-parameters. The available gain design procedure is applicable to both the conditionally stable and unconditionally stable cases. This amplifier design procedure examines the unconditionally stable case only. The transducer gain equation g T of Equation 6, is rearranged as shown in Equations 13 and 14: Equation Γ g S 2 1 Γ L 2 T = S 1 S 11 Γ S Γ OUT Γ L 2 where: Equation 14. Γ OUT = S 22 + S 21 S 12 Γ S 1 S 11 Γ S 5

6 When the device output is conjugately matched for a given source termination Γ S, then transducer gain, g T, is simplified in terms of the s-parameters and Γ S. Conjugately matching the output mathematically yields Γ L = Γ OUT * and Equation 15 yields available gain, g A : 1 Γ g S 2 1 Equation 15. A = S 1 S 11 Γ S Γ OUT 2 Substituting Equation 14 into Equation 15 yields the available gain equation, g A, as shown in Equation 16, which is a function of Γ S and the two-port s-parameters. Equation 16. S g 21 2 (1 Γ S 2 ) A = ( 2 S 22 Γ 1 S 1 S 1 S 11 Γ S 2 11 Γ S A family of circles known as available gain circles are constructed that provide a specific amount of mismatch at the device input. An infinite number of source terminations forming the circle allow selection of mismatch at the device input. To construct an available gain circle, locate the center of the circle on a Smith chart and draw the circumference from a calculated radius. Locate the center for a particular gain circle using Equation 20, which yields a magnitude and angle. The desired available gain in db is converted to numeric gain factor g A for Equation 17. Equation 17 is then used in Equations 19 and 20. ( Equation 17. Equation 18. g A g a = S 21 2 C 1 = S 11 S* 22 The radius of an available gain circle is calculated by equation 19: Equation 19. Equation 20. R a = [1 2K S 12 S 21 g a + S 12 S 21 2 g 2 a] ½ 1 + g a ( S ) C a = g a C 1 * 1 + g a ( S ) Plotting available gain circles in conjunction with noise contours allows an easy selection of gain versus noise figure for the amplifier. Noise Figure Design Procedure Equation 21 describes transistor noise factor performance. As shown in this equation, transistor noise performance is independent of load termination and is determined solely by its source termination and noise parameters. The noise parameters fully describe the noise performance of a device for a specific set of conditions such as frequency, bias, and temperature. Equation 21. 4r F = F Min + n Γ S Γ opt 2 (1 Γ S 2 ) 1 + Γ opt 2 Transistor noise factor F is a function of Γ S, F Min, r n, and Γ opt, where F Min, r n, and Γ opt are known as the transistor noise parameters. Γ S terminates the two-port input of Figure 2. As Γ S approaches Γ opt, the transistor noise factor approaches its minimum. As Γ S departs from Γ opt, the noise factor increases from its minimum value. The rate at which the noise factor increases depends on the noise resistance r n. Conversion of transistor noise factor to noise figure in db is obtained from Equation 4. Equation 22 obtains the noise resistance rn if F Min, Γ opt, and the noise factor with the input terminated in 50 Ω is known. (Γ S = 0) 6

7 Equation 22. r n = (F Γ s =0 F min ) 1+Γ opt 2 4 Γ opt 2 Since noise factor degrades as the source termination departs from Γ opt, contours may be constructed which yield a given noise performance for a particular source termination called noise circles. An infinite number of source terminations forming a circle provide a given noise figure. The noise circles are plotted by first locating the center of a particular circle using Equation 24. Equation 23. N i = F F i min 1+Γ 4r opt 2 n Equation 24. C F i = Γ opt 1+ N i Equation 25 calculates the radius of each noise circle. Equation 25. R F i = 1 1+ N i N 2 i +N i (1 Γ opt 2 ) For low noise amplifier design, a gain versus noise trade-off is typically made. Available gain circles are plotted with constant noise figure circles for a trade-off between gain and noise figure. The optimum noise performance seldom coincides with the maximum gain of the device. Since each gain or noise circle describes the device performance under a given set of conditions, a prediction of gain and noise figure is determined by a known source termination. Enhanced noise performance is obtained with a source termination closer to the optimum noise termination Γ opt, at the expense of gain. More gain results when the source termination is conjugately matched to the device input, Γ MS, at the expense of noise figure. A trade-off is made between noise and gain by selecting an intermediate source termination. Thus, neither optimum noise nor maximum gain is obtained b Amplifier Design Requirements A low noise amplifier (LNA) is required for a WCS (wireless communication system) receiver application. Using Equations 1 through 5 and system specifications, it is determined that the LNA requires the following performance: Frequency range: GHz to 2.48 GHz Gain:... > 12 db Noise figure:... < 2.5 db Input return loss... > 10 db Output return loss... > 10 db Third order input intercept point:... > 0 dbm Supply voltage: Volts Supply current:... < 100 ma Several manufacturers produce high performance transistors that are suitable for this particular design. Frequency range, maximum gain, minimum noise figure, and linearity are all considered during the active device selection process. One aspect that is often overlooked during the selection process is whether or not measured s-parameters, noise parameters, and a nonlinear model exist for the chosen transistor. Design cycle times are significantly reduced if nonlinear models and measured s-parameter and noise parameter data is available from the manufacturer. Having the data in electronic form speeds import into the chosen RF/μ Wave circuit simulator. It is highly recommended that supplied data is verified in a measurement lab if available to ensure its validity before too many design resources are committed to a particular device. 7

8 Transistor S-Parameters and Nonlinear Model Several transistors were selected as candidates for the WCS LNA by inspection of corresponding data sheets. Many devices were quickly eliminated since a nonlinear model and measured s-parameters were not available from the particular manufacturer in electronic form. The Avago ATF54143 has measured s-parameter and noise parameter data at various bias conditions and a nonlinear model available in electronic form and specifications that should yield a design with the desired performance. The ATF54143 nonlinear model available from Avago is shown in Figure 3. Latest ATF-54143curtice ADS MODEL Figure 3. ATF54143model.dsn Since both the nonlinear model and measured s-parameters are available, a quick validation is possible and recommended. Avago measured s-parameter data with a 3.0 Volt bias voltage at the drain and a drain-to-source current of 60 ma. Figure 4 shows an s-parameter simulation that plots the Avago measured s-parameter. An Amplifier Design Guide (from a schematic, select: DesignGuides > Amplifier > S-Parameter Simulations > S-Params., Noise Fig., Gain, Stability, Circles, and Group Delay) is used to quickly set up the simulation as shown in Figure 4. The ATF541433_3V60mA.s2p file has both s-parameters and noise data included. The simulation is performed from 100 MHz to 6 GHz, stepped every 10 MHz and stored in a dataset. These results are later compared to the nonlinear model s-parameter simulation. 8

9 S-Parameters, Noise Figure, Gain, Stability, Circles, and Group Delay versus Frequency Figure 4. ATF54143_Avago_S-parameters.dsn Now, the nonlinear model is biased at the same DC operating point as was the device for the measured s-parameter data provided by Avago as shown in Figure 5. The target product has a 3.3 V regulated supply voltage available for biasing the amplifier. The ATF54143 nonlinear model sub-circuit is shown as a symbol (sub-circuit) and labeled Latest_ATF The ATF54143 nonlinear model has the 3.3 V supply voltage connected to the drain through a 5 Ω resistor Rd. This resistor drops the supply voltage from 3.3 V to 3.0 V when 60 ma of bias current flows through the drain terminal. The transistor s-parameters are affected very little when the drain voltage is 3.3 V instead of 3.0 V. However, adding the resistor will make the application conditions more closely resemble conditions for the Avago measured device s-parameters. It could also slightly limit a short circuit condition at the transistor drain when the bias choke coil is at its self-resonant frequency. Figure 5 shows a DC choke coil, DC_Feed that is later replaced with an inductor in the built-up circuit. Note that the ATF54143 is an enhancement mode FET that requires a positive gate voltage with respect to its source to obtain the desired drain-to-source bias current of 60 ma. A voltage divider network is provided by Ra and Rb and is adjusted in the simulator to quickly obtain the required 60 ma drain-to-source current. Standard resistor values are used. Ra is arbitrarily set to 33 kω. Next, Rb is manually adjusted by entering standard resistor values to yield the desired bias current as shown in Figure 5. Note that Rg, the 10 kω resistor is not necessary for transistor DC bias, but acts as an all-frequency choke to effectively isolate the gate from the bias network RF-wise. This will be important when the RF aspects of the design are accomplished. Nearly any resistor value is acceptable from a DC bias standpoint since no DC current flows through this resistor. Larger resistor values provide better RF isolation than smaller ones. A smaller resistor can be used in this position if it is determined that the transistor is unstable and requires parallel loading at the input to achieve stability. Adding a bypass capacitor to ground at the Ra, Rb, and Rg junction effectively AC grounds Rg. For now, the 10 kω resistor is used for the DC simulations and preliminary RF simulations. 9

10 Figure 5. DCbias.dsn Figure 6 shows the DC simulation results with Ra set to 33 kω and Rb set to 6.8 kω. Note that the drain bias current is nearly 60 ma (61.38mA) and the drain voltage is nearly 3 Volt (2.993V). This is close enough to the target bias values. freq Idrain.i Vd Hz ma V Figure 6. DCbias.dds An s-parameter simulation is now possible on the biased nonlinear model. DC blocking capacitors and 50 Ω terminations are added to the circuit input and output of Figure 5 to obtain the circuit shown in Figure 7. S-parameter simulations are now obtained from 100 MHz to 6 GHz with a frequency step of 10MHz. (The Avago ATF54143 datasheet indicates that device s-parameters were measured on a 20 mil thick PCB and recommends connecting two vias in parallel with each other on each source to ground. This was added to the Figure 7 circuit and found to have a minimal effect. The nonlinear model simulated s-parameter data without the ground vias closely matches measured s-parameter data. Thus, the PCB ground vias are not added as indicated in the datasheet.) Figure 8 plots nonlinear model simulated s-parameters and the Avago measured s-parameter data. Note the close similarity between the two s-parameter data sets. Figure 7. S-parametersModel.dsn 10

11 Figure 8. ATF54143_MeasVsModel_S-parameters.dds S-Parameter Data Validation It is beneficial to validate data obtained from any vendor if a measurement lab is available. In this case, s-parameter data is measured with an Intercontinental Microwave (ICM) transistor test fixture. The ICM transistor test fixture is used with the appropriate midsection and ICM TOSL-3001 calibration kit. Before calibration is performed, all TOSL-3001 calibration coefficients are loaded into the network analyzer. Each calibration standard has a unique set of coefficients that describe it s RF response. The ICM calibration coefficients used to describe the TOSL-3001 calibration kit are shown in Tables 1 and 2. The upper frequency limit for the ICM calibration kit is 6 GHz. Once the ICM calibration coefficients are loaded into the network analyzer, the TOSL calibration for the transistor test fixture is possible. Figure 9 shows the measurement setup used to measure ATF54143 s-parameter data. The HP4142B DC Source/Monitor is connected to the E8364B network analyzer bias tees located on the back of that instrument. The HP4142B will supply 3.0 Volts to the Port 2 bias tee and will supply a voltage between 0 V and 1 V at the Port 1 bias tee. The current sourced from the HP4142B is limited to 100 ma to ensure that the 500 ma bias tee fuses are not accidentally blown. The HP4142B DC Source/Monitor should be disconnected or turned off during calibration to avoid blowing the port bias fuses in the network analyzer as an added safety precaution. The E8364B network analyzer source power is set to 25 dbm to ensure the measured device is not driven into compression during measurement. The network analyzer IF bandwidth is set to 300 Hz to limit noise and increase the dynamic range of the measurement system. The TOSL calibration is now performed using the ICM TOSL-3001 calibration kit. 11

12 Figure 9. Transistor s-parameter measurement setup Standard Class Assignments Calibration Kit: ICM TOSL-3001 CLASS A B C D E F G Standard Class Label S 11 A 2 S 11 B 1 S 11 C 3 S 11 A 2 S 11 B 1 S 11 C 3 Forward Transmission 4 Reverse Transmission 4 Forward Match 4 Reverse Match 4 Response Response & Isolation TRL Thru TRL Reflect TRL Line Adapter TRL Option Cal Z0: System Z0 Line Z0 Set Ref: Thru Reflect Table 1. Calibration kit: 1CM TOSL-3001 STANDARD # TYPE C F L H C F/Hz L H/Hz C F/Hz2 L H/Hz2 C F/Hz3 L H/Hz3 Fixed or Sliding Terminal Impedance Ω Delay psec Offset Z0 Ω Loss GΩ /s Frequency (GHz) MIN MAX Coax or Waveguide 1 SHORT COAX SHORT 2 OPEN COAX OPEN 3 LOAD FIXED COAX LOAD 4 THRU COAX THRU 5 Standard Label Table 2. 12

13 S-Parameters, Noise Figure, Gain, Stability, Circles, and Group Delay versus Frequency Figure 10. ATF54143_ICM_S-parameters.dsn Once calibration is completed and verified, the HP4142B DC Source/Monitor is reconnected or turned back on as shown in Figure 9. Using the HP4142B is a very accurate way of setting/monitoring voltages and currents. First, the 3 Volt DC bias is supplied to Port 2 on the network analyzer through the Port 2 bias tee to bias the transistor drain terminal. The HP4142B DC Source/Monitor compliance is set to 100 ma so as to limit current into the bias tees. The desired bias current into Port 2 is 60 ma, thus the compliance (current limit) is set to 100 ma. Essentially, no current is needed to bias the gate of the FET connected to Port 1, so the compliance is set to 10 ma. The bias voltage on Port 1, which is connected to the transistor gate through the bias tee, is set to 0.5 Volt. Drain current is now measured with the HP4142B DC Source/Monitor and found to be slightly below 60 ma. The Port 1 (gate) voltage is slowly increased until 60 ma is measured with the HP4142B DC Source/Monitor going into Port 2 the drain terminal. Once the drain-to-source current is set to 60 ma with the drain voltage at 3.0 V, the s-parameters are now measured and saved to a Touchstone file. Figure 10 uses an Amplifier Design Guide to plot the lab-measured s-parameters with the simulator. 13

14 Figure 11. ATF54143_ALL3_S-parameters.dds A comparison is now made between the Avago measured s-parameters, the nonlinear model generated s-parameters, and the lab measured s-parameters. Figure 11 plots all s-parameter results and shows that all are in close agreement with each other. Since measured data and modeled data are consistent with each other, any of these can be used to proceed with the linear design. Of course, third order intermodulation distortion and gain compression require the nonlinear model for simulation purposes. Noise figure simulation requires linear noise parameters. Noise parameters are included in the s-parameter Touchstone file ATF541433_3V60mA.s2p provided by Avago. This s-parameter data file also has data up to 18GHz where as the ICM data is only measured to 6 GHz due to the calibration kit frequency limitation. Stability should be considered for all frequencies or at least with data covering as much frequency range as possible. Thus, the Avago measured data is used to simulate stability, available gain, and noise figure. ATF54143 Stability A preliminary stability analysis is performed using an Amplifier Design Guide and the Avago measured s-parameter data as shown in Figure 12. Note that the stability analysis is performed from 100 MHz to 18 GHz the entire range of the data file. 14

15 S-Parameters, Noise Figure, Gain, Stability, Circles, and Group Delay versus Frequency Figure 12. ATF54143_StabilityAnalysis.dsn It is highly recommended that the amplifier circuit is made unconditionally stable at all frequencies to ensure that it does not produce unwanted oscillations. If the amplifier should happen to oscillate while being used in it s product environment, it may cause product malfunction. It can be very difficult to determine the root cause of product malfunction due to oscillating amplifiers. To achieve unconditional stability, Equations 7 through 10, show that K 1 and { < 1 or B1 > 0 or B2 > 0}; or separately Equation 11 or Equation 12 geometric stability factors μ source 1 or μ load 1. The ADS Amplifier Design Guide calculates and displays Equations 7, 11, and 12. Note that satisfying K 1 does not indicate or guarantee unconditional stability. If either μ source 1 or μ load 1 then the amplifier circuit is guaranteed to be unconditionally stable. If the equations indicate unconditional stability, it means that the amplifier will not oscillate when its input and output are terminated with impedances having zero or positive resistances. In other words, as long as the input and output are terminated with reflection coefficient magnitudes between 0 and 1, inclusive, the circuit will not oscillate. If feedback through inductive coupling is introduced or modified, by putting the amplifier in a metal housing, the amplifier may still oscillate. Environmental conditions, such as temperature, can also produce unwanted oscillations. A change in temperature changes the active device s-parameters. To ensure unconditional stability, s-parameters should be taken under all extreme conditions and a stability analysis performed. One other way to ensure stability as far as environmental conditions are concerned is to provide significant margin to the stability conditions. In other words, make K >> 1 at all frequencies if possible. 15

18 Figure 15. ATF54143_StabilityOpt.dds Component and layout parasitics are not included in the design yet. Typically, if the preliminary analysis does not meet the design criteria, the final actual circuit with parasitics will not meet the objectives. In other words, parasitics typically degrade RF performance. In this case, the preliminary analysis indicates the transistor and amplifier topology chosen may indeed yield a design that meets all design objectives. Next, some of the component parasitics and preliminary layout parasitics are considered to determine what affects they may have on circuit performance. Component parasitics include loss and unexpected reactance. Inductors have losses and parasitic capacitance whereas capacitors have loss and parasitic inductance. For this design, an inductor is needed to feed DC bias into the FET drain terminal. Figures 5 and 7 show an ideal DC feed (choke) to inject bias current into the FET drain. A Coilcraft Midi series air-wound inductor replaces the ideal DC feed. The inductor is needed merely to feed DC bias current to the FET drain. Ideally, a very large inductance is needed for the DC feed coil. Inductor parasitic capacitance limits the allowable inductance value due to self-resonance. A 27 nh Coil Craft Midi series inductor has a minimum self-resonance frequency of 2.7 GHz. This gives the highest possible inductive reactance at the 2.5 GHz operating frequency while the inductor self-resonant frequency is still above the amplifier operating frequency. Figure 16. CC1812SMS.dsn 18

20 Figure 18 shows an s-parameter plot from the Figure 17 analysis. Both S11 and S22 are inside the unit radius Smith chart, which is a necessary, but not sufficient condition for unconditional stability. The db(s21) plot shows the 50 Ω gain of db at 2.5 GHz which is slightly lower than the db of gain predicted by Figures 14 and 15. The lower gain is partly due to the resistor values being changed to standard value resistors and the additional loss added by the 27 nh bias tee choke inductor. A stability analysis could be performed on this circuit since the S11 and S22 are inside the unit radius Smith chart, but a study of ground inductance effects on circuit performance is now desirable. As mentioned earlier, the lumped inductor L1 in Figure 17 is added to represent parasitic ground inductance. An arbitrary value of 1nH is now used to get an indication on how sensitive the circuit is to parasitic ground inductance. The 1 nh inductance value is very small. Higher values of ground inductance are not uncommon in PCB layouts. Figure 19 shows the L1 parasitic ground inductor from Figure 17 is changed to 1nH. Everything else in the circuit remains unchanged. The simulation is now executed from 10 MHz to 10 GHz. Figure 18. ATF54143amp1_1pH.dds 20

22 Figure 20. ATF54143amp1_1nH.dds Figure 21. ATF54143amp1_1nH_Admittance 22

23 Figure 22. ATF54143amp1_1nH_Stabilize.dsn Figure 22 shows the input parallel load resistor set to 50 Ω. The parasitic ground inductance is still set to 1 nh. Figure 23 shows the analysis results. With the parallel input 50 Ω resistor R1, the input reflection coefficient magnitude remains less than unity at all frequencies from 10 MHz to 10 GHz. The 50 Ω gain is 7.47 db which is only 0.01 db less than the case with the 240 Ω input parallel resistive load. This shows that the input loading has little affect on the circuit at 2.5 GHz due to the 0.5 pf capacitor being used as the bypass, but has a huge affect at higher frequencies. Since both input and output reflection coefficient magnitudes remain less than unity when the circuit input and output is terminated with 50 Ω, a stability analysis is now performed. Note that because the input and output reflection coefficient magnitudes are less than unity, doesn t mean the circuit is unconditionally stable. There may still be source or load terminations other than 50 Ω that can cause unwanted oscillations. 23

24 Figure 23. ATF54143amp1_1nH_Stabilize.dds 24

25 S-Parameters, Noise Figure, Gain, Stability, Circles, and Group Delay versus Frequency Figure 24. ATF54143_StabilityAnalysis2.dsn Figure 24 is a stability analysis from 100 MHz to 18 GHz with the parasitic ground inductance set to 1 nh and the input parallel load resistor set to 50 Ω from Figure 22. The 50 Ω gain of 7.47 db plotted in Figure 23 is not adequate gain for the 12 db design goal. Stability is checked for the case of 1 nh ground inductance before investigating the next case of parasitic ground inductance. Figure 25 is the same ADS Amplifier Design Guide data display from before that plots Equations 7, 11, and 12 stability factors K, μ source, and μ load respectively. The circuit from Figure 24 data indicates potential instability between 6 GHz and 9.5 GHz as shown in the red box since μ source < 1 and μ load < 1. Before making any further adjustments to stabilizing networks, the parasitic ground inductance L1 is adjusted down to 0.5 nh. The 1nH value was arbitrarily chosen to begin with, so it is helpful to see how sensitive the circuit is when the parasitic ground inductance is cut in half. Figure 26 shows the new circuit set up with the 0.5 nh parasitic ground inductance L1 for the stability analysis. 25

26 Figure 25. ATF54143_StabilityAnalysis2.dds Figure 27 displays the Figure 26 simulation results with ground parasitic inductance set to 0.5 nh. K, μ source, and μ load are plotted and highlighted in the red box. The plot indicates unconditional stability from 100 MHz to 18 GHz with more stability margin at higher frequencies as desired. At this stage of the design, it is not yet known how much parasitic ground inductance at the transistor source is contained in the PCB layout because the layout is not yet started. Special attention is given to the layout procedure to ensure that parasitic ground inductance at the transistor source is kept as low as possible. Once the layout is complete, EM simulations give an estimate on the amount of parasitic ground inductance. If estimated parasitic ground inductance is too high on the initial layout, the layout is revised in an attempt to lower the PCB ground inductance parasitic. Once electromagnetic (EM) simulations are performed on grounding and other layout features, a stability and gain analysis with PCB layout parasitics included are performed to ensure the amplifier meets all design objectives. 26

27 S-Parameters, Noise Figure, Gain, Stability, Circles, and Group Delay versus Frequency Figure 26. ATF54143_StabilityAnalysis3.dsn The gain, noise figure, and stability plots of Figure 25 show three spikes over the 100 MHz to 18 GHz frequency range. The transmission line used in the Coilcraft 27 nh inductor model causes these spikes in the frequency response plots. The actual Coilcraft inductor does not behave as suggested by the model above its self-resonance frequency. A one-port measurement of the inductor is made using an E8364B network analyzer up to 6GHz and saved to a touchstone file named Lp1812SMS_27NG. This one-port measured data file is now used in the amplifier circuit simulation to more accurately predict the behavior of the amplifier circuit above the self-resonant frequency of the inductor up to 6 GHz. It was noticed during the inductor measurement that the results above the self resonant frequency are sensitive to the position of the inductor in the fixture. These variations cause more variability in the model prediction results above the 2.7 GHz inductor self-resonant frequency. In other words, it is more difficult to get the circuit model data to agree with final circuit measured data especially above the inductor selfresonant frequency because of the measurement sensitivity. 27

28 Figure 27. ATF54143_StabilityAnalysis3.dds Figure 28 shows the amplifier circuit with the 27 nh inductor one-port s-parameter measurements included in place of the Coilcraft lumped equivalent model. Figure 29 presents the Figure 28 simulation results. The inductor primary self-resonant frequency response is still noticeable in the amplifier frequency response plots as expected, although it is not as pronounced. Figure 28. ATF54143_StabilityAnalysis4.dsn 28

29 Maximum Available Gain is displayed and highlighted with orange boxes in Figures 27 and 29. The predicted maximum possible gain is around 10.8 db in both figures. This is 1.2 db below the 12 db design goal. Note that this predicted gain value is obtained with an arbitrary estimated amount of transistor source terminal parasitic ground inductance 0.5 nh for Figures 27 and 29. Although the gain is below the target value in these simulations, the gain without parasitic inductance is well above the target value. A matching network is added at the amplifier input. In this case, a parallel inductor followed by a series capacitor is added. These values have not yet been calculated, but a preliminary match analysis indicates that the parallel inductor coming from the 50 Ω source followed by a series capacitor going into the transistor input provides a valid matching topology for the amplifier input. The matching design procedure is further explained later for the final input matching analysis. The approximate matching inductor value allows selection from a family of inductors that may be used. This allows a layout of the inductor footprint. In this case, a CoilCraft air core inductor from the Mini-Spring family of inductors provides a range of inductors suitable for the input matching network. Next, the amplifier circuit is laid out with special attention to grounding the FET source terminals. Once the layout is completed, an EM simulation predicts parasitic ground inductance at the transistor source terminal. With an estimate of parasitic inductance, new predictions of gain and stability are possible. Figure 29. ATF54143_StabilityAnalysis4.dds Amplifier EM/Circuit Co-Simulation and PCB Fabrication The amplifier is built on Arlon 25N, which is available in many standard laminate thicknesses. Arlon 25N has a dielectric constant of 3.38 and a loss tangent of about at 2.5 GHz. Double-sided laminate having 1 ounce copper on each side, with a 30 ±3 mil thickness is selected for the design. Arlon 25N has a very consistent dielectric constant over frequency and temperature and is easily processed by manufacturers that process standard FR4 PCBs. Since performance specifications are very consistent and repeatable, using the Arlon 25N material greatly enhances the possibility of completing a one-pass design. In other words, the 25N material properties are used in the EM and circuit simulations to get an accurate simulation of PCB and circuit performance before resources are committed to actually building a board. Circuit repeatability from lot-to-lot is also greatly increased due to the repeatability of the Arlon 25N material. 29

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